Refrigeration cycle device for vehicle

Information

  • Patent Grant
  • 11920077
  • Patent Number
    11,920,077
  • Date Filed
    Tuesday, July 16, 2019
    4 years ago
  • Date Issued
    Tuesday, March 5, 2024
    2 months ago
Abstract
No studies have been made regarding what kinds of refrigerants should be used in a refrigeration cycle device for a vehicle. An air conditioner (1) for a vehicle includes a refrigerant circuit (10) and a refrigerant that is sealed in the refrigerant circuit (10). The refrigerant circuit (10) includes a compressor (80), a first heat exchanger (85), which serves as a heat dissipater in a dehumidifying heating mode, an outside-air heat exchanger (82), a cooling control valve (87), and a second heat exchanger (86), which serves as an evaporator in the dehumidifying heating mode. The refrigerant is a refrigerant having a low GWP.
Description
TECHNICAL FIELD

The present disclosure relates to a refrigeration cycle device for a vehicle that uses a refrigerant having a low global warming potential (GWP).


BACKGROUND ART

Hitherto, in a heat cycle system of a refrigeration device or a freezing device, R134a, which is a single refrigerant, has been frequently used as a refrigerant. In addition, R410A or R404 may be used. R410A is a two-component mixed refrigerant containing (CH2F2; HFC-32 or R32) and pentafluoroethane (C2HF5; HFC-125 or R125), and is a pseudo-azeotropic composition. R404 is a three-component mixed refrigerant containing R125, R134a, and R143a, and is a pseudo-azeotropic composition.


However, the global warming potential (GWP) of R134a is 1430, the global warming potential (GWP) of R410A is 2088, and the global warming potential (GWP) of R404A is 3920. In recent years, due to increasing concern about global warming, refrigerants having a lower GWP are more frequently being used.


For example, Japanese Literature 1 (International Publication No. 2005/105947) proposes various mixed refrigerants having a low GWP that can be used as alternatives for R134a; Japanese Literature 2 (International Publication No. 2015/141678) proposes various mixed refrigerants having a low GWP that can be used as alternatives for R410A; and Japanese Literature 3 (Japanese Unexamined Patent Application Publication No. 2018-184597) proposes various mixed refrigerants having a low GWP that can be used as alternatives for R404A.


SUMMARY OF INVENTION
Technical Problem

So far, no studies have been made regarding what kinds of refrigerants should be used among refrigerants having a low GWP in a refrigeration cycle device for a vehicle.


Solution to Problem

A refrigeration cycle device for a vehicle according to a first aspect includes a refrigerant circuit and a refrigerant that is sealed in the refrigerant circuit. The refrigerant circuit includes a compressor, a heat dissipater, a decompressor, and a heat absorber. The refrigerant contains at least 1,2-difluoroethylene.


A refrigeration cycle device for a vehicle according to a second aspect is the refrigeration cycle device for a vehicle according to the fast aspect, in which the refrigerant contains trans-1,2-difluoroethylene (HFO-1132(E)), trifluoroethylene (HFO1123), and 2,3,3,3-tetrafluoro-1-propene (R1234yf).


A refrigeration cycle device for a vehicle according to a third aspect is the refrigeration cycle device for a vehicle according to the second aspect, wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum in the refrigerant is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments OD, DG, GH, and HO that connect the following 4 points:


      point D (87.6, 0.0, 12A),


      point G (18.2, 55.1, 26.7),


      point H (56.7, 43.3, 0.0), and


      point O (100.0, 0.0, 0.0),


      or on the line segments OD, DG, and GH (excluding the points O and H);
    • the line segment DG is represented by coordinates (0.0047y2−1.5177y+87.598, y, −0.0047y2+0.5177y+12.402),
    • the line segment GH is represented by coordinates (−0.0134z2−1.0825z+56.692, 0.0134z2+0.0825z+43.308, z), and
    • the line segments HO and OD are straight lines.


A refrigeration cycle device for a vehicle according to a fourth aspect is the refrigeration cycle device for a vehicle according to the second aspect, wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum in the refrigerant is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments LG, GH, HI, and IL that connect the following 4 points:


      point L (72.5, 10.2, 17.3),


      point G (18.2, 55.1, 26.7),


      point H (56.7, 43.3, 0.0), and


      point I (72.5, 27.5, 0.0),


      or on the line segments LG, GH, and IL (excluding the points H and I);
    • the line segment LG is represented by coordinates (0.0047y2−1.5177y+87.598, y, −0.0047y2+0.5177y+12.402),
    • the line segment GH is represented by coordinates (−0.0134z2−1.0825z+56.692, 0.0134z2+0.0825z+43:308, z), and
    • the line segments HI and IL are straight lines.


A refrigeration cycle device for a vehicle according to a fifth aspect is the refrigeration cycle device for a vehicle according to any one of the second aspect to the fourth aspect, further comprising difluoromethane (R32).


A refrigeration cycle device for a vehicle according to a sixth aspect is the refrigeration cycle device for a vehicle according to the fifth aspect, wherein

    • when the mass % of HFO-1132(E), HFO-1123, R1234yf, and R32 based on their sum in the refrigerant is respectively represented by x, y, z, and a,
    • if 0<a≤10.0, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure surrounded by straight lines that connect the following 4 points:


      point A (0.02a2−2.46a+93.4, 0, −0.02a2+2.46a+6.6),


      point B′ (−0.008a2−1.38a+56.0.018a2−0.53a+26.3, −0.01a2+1.91a+17.7),


      point C (−0.016a2+1.02a+77.6, 0.016a2−1.02a+22.4, 0), and


      point O (100.0, 0.0, 0.0),


      or on the straight lines OA, AB′, and B′C (excluding point O and point C);
    • if 10.0<a≤16.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines that connect the following 4 points:


      point A (0.0244a2−2.5695a+94.056, 0, −0.0244a2+2.5695a+5.944),


      point B′ (0.1161a2−1.9959a+59.749, 0.014a2−0.3399a+24.8, −0.1301a2+2.3358a+15.451),


      point C (0.0161a2+1.02a+77.6, 0.0161a2−1.02a+22.4, 0), and


      point O (100.0, 0.0, 0.0),


      or on the straight lines OA, AB′, and B′C (excluding point C and point C); or
    • if 16.5<a≤71.8, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines that connect the following 4 points:


      point A (0.0161a2−2.3535a+92.742, 0, −0.0161a2+2.3535a+7.258),


      point B′ (−0.0435a2−0.0435a+50.406, −0.0304a2+1.8991a−0.0661, 0.0739a2−1.8556a+49.6601),


      point C (−0.0161a2+0.9959a+77.851, 0.0161a2−0.9959a+22.149, 0), and


      point O (100.0, 0.0, 0.0),


      or on the straight lines OA, AB′, and B′C (excluding point O and point C).


A refrigeration cycle device for a vehicle according to a seventh aspect is the refrigeration cycle device for a vehicle according to the second aspect, wherein

    • the refrigerant comprising HFO-1132(E) and HFO-1123 in a total amount of 99.5 mass % or more based on the entire refrigerant, and
    • the refrigerant comprising 62.5 mass % to 72.5 mass % of HFO-1132(E) based on the entire refrigerant.


A refrigeration cycle device for a vehicle according to a eighth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein.

    • the refrigerant comprising HFO-1132(E), R32, and R1234yf,


      wherein
    • when the mass % of HFO-1132(E), R32, and R1234yf based on their sum in the refrigerant is respectively represented by x, y, and z; coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments AC, CF, FD, and DA that connect the following 4 points:


      point A (71.1, 0.0, 28.9),


      point C (36.5, 18.2, 45.3),


      point F (47.6, 18.3, 34.1), and


      point D (72.0, 0.0, 28.0),


      or on these line segments;
    • the line segment AC is represented by coordinates (0.0181y2−2.2288y+71.096, y, 0.0181y2+1.2288y+28.904),
    • the line segment FD is represented by coordinates (0.02y2−1.7y+72, y, 0.02y2+0.7y+28), and
    • the line segments CF and DA are straight lines.


A refrigeration cycle device for a vehicle according to a ninth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein

    • the refrigerant comprising HFO-1132(E), R32, and R1234yf, wherein
    • when the mass % of HFO-1132(E), R32, and R1234yf based on their sum in the refrigerant is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments AB, BE, ED, and DA that connect the following 4 points:


      point A (711, 0.0, 28.9),


      point B (42.6, 14.5, 42.9),


      point E (51.4, 14.6, 34.0), and


      point D (72.0, 0.0, 28.0),


      or on these line segments;
    • the line segment AB is represented by coordinates (0.0181y2−2.2288y+71.096, y, −0.0181y2+1.2288y+28.904),
    • the line segment ED is represented by coordinates (0.02y2−1.7y+72, y, −0.02y2+0.7y+28), and
    • the line segments BE and DA are straight lines.


A refrigeration cycle device for a vehicle according to a tenth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein

    • the refrigerant comprising HFO-1132(E), R32, and R1234yf,


      wherein
    • when the mass % of HFO-1132(E), R32, and R1234yf based on their sum in the refrigerant is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments GI, IJ, and JG that connect the following 3 points:


      point G (77.5, 6.9, 15.6),


      point I (55.1, 18.3, 26.6), and


      point J (77.5, 18.4, 4.1),


      or on these line segments;
    • the line segment GI is represented by coordinates (0.02y2−2.4583y+93.396, y, −0.02y2+1.4583y+6.604), and
    • the line segments IJ and JO are straight lines.


A refrigeration cycle device for a vehicle according to a eleventh aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein

    • the refrigerant comprising HFO-1132(E), R32, and R1234yf,


      wherein.
    • when the mass % of HFO-1132(E), R32, and R1234yf based on their sum in the refrigerant is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments GH, HK, and KG that connect the following 3 points:


      point G (77.5, 6.9, 15.6),


      point H (61.8, 14.6, 23.6), and


      point K (77.5, 14.6, 7.9),


      or on these line segments;
    • the line segment GH is represented by coordinates (0.02y2−2.4583y+93.396, y, 0.02y2+1.4583y+6.604), and
    • the line segments HK and KG are straight lines.


A refrigeration cycle device for a vehicle according to a twelfth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein

    • the refrigerant comprising HFO-1132(E), HFO-1123, and R32,


      wherein
    • when the mass % of HFO-1132(E), HFO-1123, and R32 based on their sum in the refrigerant is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass % are within the range of a figure surrounded by line segments OC′, C′D′, D′E′, E′A′, and A′O that connect the following 5 points:


      point O (100.0, 0.0, 0.0),


      point C′ (56.7, 43.3, 0.0),


      point D′ (52.2, 38.3, 9.5),


      point E′ (41.8, 39.8, 18.4), and


      point A′ (81.6, 0.0, 18.4),


      or on the line segments C′D′, D′E′, and E′A′ (excluding the points C′ and A′);
    • the line segment C′D′ is represented by coordinates (−0.0297z2−0.1915z+56.7, 0.0297z2+1.1915z+43.3, z),
    • the line segment D′E′ is represented by coordinates (−0.0535z2+0.3229z+53.957, 0.0535z2+0.6771z+46.043, z), and
    • the line segments OC′, E′A′, and A′O are straight lines.


A refrigeration cycle device for a vehicle according to a thirteenth aspect is the refrigeration cycle device for a vehicle according to the fast aspect, wherein

    • the refrigerant comprising HFO-1132(E), HFO-1123, and R32,


      wherein
    • when the mass % of HFO-1132(E), HFO-1123, and R32 based on their sum in the refrigerant is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum off-MO-1132(E), HFO-1123, and R32 is 100 mass % are within the range of a figure surrounded by line segments OC, CD, DE, EA′, and A′O that connect the following 5 points:


      point O (100.0, 0.0, 0.0),


      point C (77.7, 22.3, 0.0),


      point D (76.3, 14.2, 9.5),


      point E (72.2, 9.4, 18.4), and


      point A′ (81.6, 0.0, 18.4),


      or on the line segments CD, DE, and EA′ (excluding the points C and A′);
    • the line segment CDE is represented by coordinates (−0.017z2+0.0148z+77.684, 0.017z2+0.9852z+22316, z), and
    • the line segments OC, EA′, and A′O are straight lines.


A refrigeration cycle device for a vehicle according to a fourteenth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein

    • the refrigerant comprising HFO-1132(E), HFO-1123, and R32,


      wherein
    • when the mass % of HFO-1132(E), HFO-1123, and R32 based on their sum in the refrigerant is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass % are within the range of a figure surrounded by line segments OC′, C′D′, D′A, and AO that connect the following 4 points:


      point O (100.0, 0.0, 0.0),


      point C′ (56.7, 43.3, 0.0),


      point D′ (52.2, 38.3, 9.5), and


      point A (90.5, 0.0, 9.5),


      or on the line segments C′D′ and D′A (excluding the points C′ and A);
    • the line segment C′D′ is represented by coordinates (−0.0297z2−0.1915z+56.7, 0.0297z2+1.1915z+43.3, z), and
    • the line segments OC′, D′A, and AO are straight lines.


A refrigeration cycle device for a vehicle according to a fifteenth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein

    • the refrigerant comprising HFO-1132(E), HFO-1123, and R32,


      wherein
    • when the mass % of HFO-1132(E), HFO-1123, and R32 based on their sum in the refrigerant is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass % are within the range of a figure surrounded by line segments OC, CD, DA, and AO that connect the following 4 points:


      point O (100.0, 0.0, 0.0),


      point C (77.7, 22.3, 0.0),


      point D (76.3, 14.2, 9.5), and


      point (90.5, 0.0, 9.5),


      or on the line segments CD and DA (excluding the points C and A);
    • the line segment CD is represented by coordinates (−0.017z2+0.0148z+77.684, 0.017z2+0.9852z+22.316, z), and
    • the line segments OC, DA, and AO are straight lines.


A refrigeration cycle device for a vehicle according to a sixteenth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein


the refrigerant contains CO2, trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (R1234yf);


wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,






    • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B″D and straight line CI):


      point I (0.0, 72.0, 28.0−w)


      point J (18.3, 48.5, 33.2−w)


      point K (36.8, 35.6, 27.6−w)


      point L (51.7, 28.9, 19.4−w)


      point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2−3.75w+49.5)


      point D (−2.9167w+40.317, 0.0, 1.9167w+59.683)


      point C (0.0, −4.9167w+58.317, 3.9167w+41.683);

    • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding the points on straight line B″D and straight line CI):


      point I (0.0, 72.0, 28.0−w)


      point J (18.3, 48.5, 33.2−w)


      point K (36.8, 35.6, 27.6−w)


      point L (51.7, 28.9, 19.4−w)


      point B″ (51.6, 0.0, 48.4−w)


      point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)


      point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and

    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B′D and straight line CI):


      point I (0.0, 72.0, 28.0−w)


      point J (18.3, 48.5, 33.2−w)


      point K (36.8, 35.6, 27.6−w)


      point L (51.7, 28.9, 19.4−w)


      point B″ (51.6, 0.0, 48.4−w)


      point D (−2.8w+40.1, 0.0, 0.1.8w+59.9)


      point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and

    • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28−w),

    • curve JK is represented by coordinates (x, 0.0095x2−1.2222x+67.676, −0.0095x2+0.2222x+32.324−w), and

    • curve KL is represented by coordinates (x, 0.0049x2−0.8842x+61.488, −0.0049x2−0.1158x+38.512).





A refrigeration cycle device for a vehicle according to a seventeenth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein the refrigerant contains CO2, trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (R1234yf);


wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,






    • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):


      point I (0.0, 72.0, 28.0−w)


      point 0.1 (18.3, 48.5, 33.2−w)


      point K (36.8, 35.6, 27.6−w)


      point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997)


      point C (0.0, −4.9167w+58.317, 3.9167w+41.683);

    • if 1.2<w≤1.3, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):


      point I (0.0, 72.0, 28.0−w)


      point J (18.3, 48.5, 33.2−w)


      point K (36.8, 35.6, 27.6−w)


      point F (36.6, −3w+3.9, 2w+59.5)


      point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553);

    • if 1.3<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line CI):


      point I (0.0, 72.0, 28.0−w)


      point J (18.3, 48.5, 33.2−w)


      point K (36.8, 35.6, 27.6−w)


      point B′(36.6, 0.0, −w+63.4)


      point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)


      point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and

    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line. CI):


      point I (0.0, 72.0, 28.0−w)


      point J (18.3, 48.5, 33.2−w)


      point K (36.8, 35.6, 27.6−w)


      point B′ (36.6, 0.0, −w+63.4)


      point D (−2.8w+40.1, 0.0, 1.8w+59.9)


      point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and

    • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28−w), and

    • curve JK is represented by coordinates (x, 0.0095x2 0.1.2222x+67.676, −0.0095x2+0.2222x+32.324−w).





A refrigeration cycle device for a vehicle according to a eighteenth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein


the refrigerant contains CO2, R32, HFO-1132(E), and R1234yf;


wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,






    • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 4 points or on these line segments (excluding points on straight line CI):


      point I (0.0, 72.0, 28.0−w)


      point J (18.3, 48.5, 33.2−w)


      point E (18.2, −1.1111w2−3.1667w+31.9, 1.1111w2+2.1667w+49.9)


      point C (0.0, −4.9167w+58.317, 3.9167w+41.683);

    • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 4 points or on these line segments (excluding points on straight line CI):


      point I (0.0, 72.0, 28.0−w)


      point J (18.3, 48.5, 33.2−w)


      point E (−0.0365w+18.26, 0.0623w2−4.5381w+31.856, −0.0623w2+3.5746w+49.884)


      point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and

    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 4 points or on these line segments (excluding points on straight line CI):


      point I (0.0, 72.0, 28.0−w)


      point J (18.3, 48.5, 33.2−w)


      point E (18.1, 0.0/111w2−4.3556w+31.411, −0.0444w2+3.3556w+50.489)


      point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and

    • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28−w).





A refrigeration cycle device for a vehicle according to a nineteenth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein


the refrigerant contains CO2, R32, HFO-1132(E), and R1234yf;


wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,






    • if 0<w≤0.6, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve GO, curve OP, straight line PB″, straight line B″D, and straight line DG that connect the following 5 points or on these line segments (excluding points on straight line B′D):


      point G (−5.8333w2−3.1667w+22.2, 7.0833w2+1.4167w+26.2, −1.25w2+0.75w+51.6)


      point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)


      point P (51.7, 1.1111w2+20.5, −1.1111w2−w+27.8)


      point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2−3.75w+49.5)


      point D (−2.9167w+40.317, 0.0, 1.9167w+59.683);


      and

    • if 0.6<w≤0.1.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve GN, curve NO, curve OP, straight line PB″, straight line B″D, and straight line DG that connect the following 6 points or on these line segments (excluding the


      points on straight line B″D):


      point G (5.8333w2−3.1667w+22.2, 7.0833w2+1.4167w+26.2, −1.25w2+0.75w+51.6)


      point N (18.2, 0.2778w2+3w+27.7, −0.2778w2−4w+54.1)


      point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)


      point P (51.7, 1.1111w2+20.5, 1.1111w2+20.5, −1.1111w2−w+27.8)


      point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2−3.75w+49.5)


      point D (−2.9167w+40.317, 0.0, 1.9167w+59.683); and

    • when 0<w≤0.6, curve GO is represented by coordinates (x, (0.00487w2−0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100−w−x−y);

    • when 0.6<w≤1.2, curve GN is represented by coordinates (x, (0.0122w2 0.0113w+0.0313)x2+(−0.3582w2+0.1624w−1.4551)x+2.7889w2+3.7417w+43.824, 100−w−x−y);

    • when 0.6<w≤1.2, curve NO is represented by coordinates (x, (0.00487w2−0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100−w−x−y); and

    • when 0<w≤1.2, curve OP is represented by coordinates (x, (0.0074w2 0.0133w+0.0064)x2+(−0.5839w2+1.0268w−0.7103)x+11.472w2−17.455w+40.07, 100−w−x−y);

    • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, curve OP, straight line PB″, straight line B″D, straight line DC, and straight line CM that connect the following 8 points or on these line segments (excluding points on straight line B′D and straight line CM):


      point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)


      point W (10.0, −0.3645w2+3.5024w+44.422, 0.3645w2−4.5024w+55.578)


      point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)


      point O (36.8, −0.1392w2+1.4381w+24.475, 0.1392w2−2.4381w+38.725)


      point P (51.7, −0.2381w2+1.881w+20.186, 0.2381w2−2.881w+28.114)


      point B″ (51.6, 0.0, −w+48.4)


      point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)


      point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553),


      and

    • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w 3.6193)x−0.3004w2+2.419w+55.53, 100−w−x−y),

    • curve WN is represented by coordinates (x, (0.0055w2−0.0326w+0.0665)x2+(−0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100−w−x−y),

    • curve NO is represented by coordinates (x, (−0.00062w2+0.0036w+0.0037)x2+(0.0375w2−0.239w−0.4977)x−0.8575w2+6.4941w+36.078, 100−w−x−y), and

    • curve OP is represented by coordinates (x, (−0.000463w2+0.0024w−0.0011)x2+(0.0457w2−0.2581w−0.075)x−1.355w2+8.749w+27.096, 100−w−x−y); and

    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, curve OP, straight line PB″, straight line B″D, straight line DC, and straight line CM that connect the following 8 points or on these line segments (excluding points on straight line BID and straight line CM):


      point M (0.0, −0.0667w2+0.8333w+58.133, 0.0667w2−1.8333w+41.867)


      point W (10.0, 0.0667w2+1.1w+39.267, 0.0667w2−2.1w+50.733)


      point N (18.2, −0.0889w2+1.3778w+31.411, 0.0889w2−2.3778w+50.389)


      point O (36.8, −0.0441w2+0.6889w+25.956, 0.0444w2−1.6889w+37.244)


      point P (51.7, −0.0667w2+0.8333w+21.633, 0.0667w2−1.8333w+26.667)


      point B (51.6, 0.0, −w+48.4)


      point D (−2.8w+40.1, 0.0, 1.8w+59.9)


      point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and

    • curve MW is represented by coordinates (x, (0.00357w2−0.0391w+0.1756)x2+(−0.0356w2+0.4178w−3.6422)x−0.0667w2+0.8333w+58.103, 100−w−x−y),

    • curve WN is represented by coordinates (x, (−0.002061w2+0.0218w−0.0301)x2+(0.0556w2−0.5821w−0.1108)x−0.4158w2+4.7352w+43.383, 100−w−x−y),

    • curve NO is represented by coordinates (x, 0.0082x2+(0.0022w2−0.0345w−0.7521)x−0.1307x2+2.0247w+42.327, 100−w−x−y), and

    • curve OP is represented by coordinates (x, (−0.0006258w2+0.0066w 0.0153)x2+(0.0516w2−0.5478w+0.9894)x−1.074w2+11.651 w+10.992, 100−w−x−y).





A refrigeration cycle device for a vehicle according to a twentieth aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein


the refrigerant contains CO2, R32, HFO-1132(E), and R1234yf;


wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,






    • if 0<w≤0.6, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve GO, straight line OF, and straight line FG that connect the following 3 points or on these line segments:


      point G (−58333w2−3.1667w+22.2, 7.0833w2−1.4167w+26.2, −1.25w2+3.5834w+51.6)


      point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)


      point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997), and

    • curve GO is represented by coordinates (x, (0.00487w2−0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100−w−x−y);
      • if 0.6<w≤1.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve GN, curve NO, straight line OF, and straight line FG that connect the following 4 points or on these line segments:


        point G (−5.8333w2−3.1667w+22.2, 7.0833w2−1.4167w+26.2, −1.25w2+3.5834w+51.6)


        point N (18.2, 0.2778w2+3.0w+27.7, −0.2.778w2−4.0w+54.1)


        point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)


        point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997), and

    • when 0.6<w≤1.2, curve GN is represented by coordinates (x, (0.0122w2−0.0113w+0.0313)x2+(−0.3582w2+0.1624w−1.4551)x+2.7889wz+3.7417w+43.824, 100−w−x−y), and

    • when 0.6<w≤1.2, curve NO is represented by coordinates (x, (0.00487w2−0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100−w−x−y); and
      • if 1.2<w≤1.3, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, straight line OF, straight line FC, and straight line CM that connect the following 6 points or on these line segments (excluding points on straight line CM):


        point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)


        point W (10.0, −0.3645w2+3.5024w−34.422, 0.3645w2−4.5024w+55.578)


        point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)


        point O (36.8, −0.1392w2+1.4381w+24.475, 0.1392w2−2.4381w+38.725)


        point F (36.6, −3w+3.9, 2w+59.5)


        point C (0.1081w2−5.169w+58.447, 0.0, −0.1081w2+4:169w+41.553),


        and

    • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100−w−x−y),

    • curve WN is represented by coordinates (x, (0.0055w2−0.0326w+0.0665)x2+(0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100−w−x−y), and

    • curve NO is represented by coordinates (x, (−0.00062w2+0.0036w+0.0037)x2+(0.0375w2−0.239w−0.4977)x−0.8575w2+6.4941w+36.078, 100−w−x−y);

    • if 1.3<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, straight line OB′, straight line B′D, straight line DC, and straight line CM that connect the following 7 points or on these line segments (excluding points on straight line CM):


      point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)


      point W (10.0, −0.3645w2+3.5024w+34.422, 03645w2−4.5024w+55.578)


      point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)


      point O (36.8, −0.1392w2+1.4381w+24.475, 0.1392w2−2.4381w+38.725)


      point B′(36.6, 0.0, −w+63.4)


      point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)


      point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553),


      and

    • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100−w−x−y),

    • curve WN is represented by coordinates (x, (0.0055w2−0.0326w+0.0665)x2+(−0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100−w−x−y), and

    • curve NO is represented by coordinates (x, (−0.00062w2+0.0036w+0.0037)x2+(0.0457w2−0.2581w−0.075)x−1.355w2+8.749w+27.096, 100−w−x−y); and

    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, straight line OB′, straight line B′D, straight line DC, and straight line CM that connect the following 7 points or on these line segments (excluding points on straight line CM):


      point M (0.0, −0.0667w2+0.8333w−58.133, 0.0667w2−1.8333w+41.867)


      point W (10.0, −0.0667w2+1.1w+39.267, 0.0667w2−2.1w+50.733)


      point N (18.2, −0.0889w2+1.3778w+31.411, 0.0889w2−2.3778w+50.389)


      point O (36.8, −0.0444w2+0.6889w+25.956, 0.0/141w2−1.6889w+37.244)


      point B′ (36.6, 0.0, −w+63.4)


      point D (−2.8w+40.1, 0.0, 1.8w+59.9)


      point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and

    • curve MW is represented by coordinates (x, (0.00357w2−0.0391w+0.1756)x2+(−0.0356w2+0.4178w−3.6422)x−0.0667w2+0.8333w+58.103, 100−w−x−y),

    • curve WN is represented by coordinates (x, (0.002061w2+0.0218w−0.0301)x2+(0.0556w2−0.5821w−0.1108)x−0.4158w2+4.7352w+43.383, 100−w−x−y), and

    • curve NO is represented by coordinates (x, (0.0082x2+(0.0022w2−0.0345w−0.7521)x−0.1307w2+2.0247w+42.327, 100−w−x−y).





A refrigeration cycle device for a vehicle according to a twenty-first aspect is the refrigeration cycle device for a vehicle according to the first aspect, wherein the refrigerant contains CO2, R32, HFO-1132(E), and R1234yf;


wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,






    • if 1.2<w≤4.0, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve MW, curve WN, straight line NE, straight line EC, and straight line CM that connect the following 5 points or on these line segments (excluding points on straight line CM):


      point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)


      point W (10.0, −0.3645w2+3.5024w+34.422, 0.3645w2−4.5024w+55.578)


      point (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)


      point E (0.0365w+18.26, 0.0623w2−4.5381w+31.856, −0.0623w2+3.5746w+49.884)


      point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553),


      and

    • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100−w−x−y), and

    • curve WN is represented by coordinates (x, (0.0055w2−0.0326w+0.0665)x2+(−0.1571w2+0.8981 w−2.6274)x+0.6555w2−2.2153w+54.044, 100−w−x−y); and

    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, straight line NE, straight line EC, and straight line CM that connect the following 5 points or on these line segments (excluding points on straight line CM):


      point M (0.0, −0.0667w2+0.8333w+58.133, 0.0667w2−1.8333w+41.867)


      point W (10.0, −0.0667w2+1.1w+39.267, 0.0667w2−2.1w+50.733)


      point N (18.2, −0.0889w2+1.3778w+31.411, 0.0889w2−2.3778w+50.389)


      point E (18.1, 0.0/1/14w2−4.3556w+31.411, −0.0444w2+3.3556w+50.489)


      point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and

    • curve MW is represented by coordinates (x, (0.00357w2−0.0391w+0.1756)x2+(−0.0356w2+0.4178w−3.6422)x−0.0667w2+0.8333w+58.103, 100−w−x−y), and

    • curve WN is represented by coordinates (x, (−0.002061w2+0.0218w 0.0301)x2+(0.0556w2−0.5821w−0.1108)x−0.4158w2+4.7352w+43.383, 100−w−x−y).





A refrigeration cycle device for a vehicle according to a twenty-second aspect includes a refrigerant circuit and a refrigerant that is sealed in the refrigerant circuit. The refrigerant circuit includes a compressor, a heat dissipater, a decompressor, and a heat absorber. The refrigerant contains at least trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (HFC-32), and 2,3,3,3-tetrafluoropropene (HFO-1234yf).


A refrigeration cycle device for a vehicle according to a twenty-third aspect is the refrigeration cycle device for a vehicle according to the twenty-second aspect, wherein

    • the refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (HFC-32) and 2,3,3,3-tetrafluoropropene (HFO-1234yf), and a total concentration of the three components is 99.5 mass % or more based on the entire refrigerant, and
    • a mass ratio of the three components is within a range of a region surrounded by a figure passing through four points:


      point A (HFO-1132(E)/HFC-32/HFO-1234yf=51.8/1.0/47.2 mass %),


      point B (HFO-1132(E)/HFC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


      point C (HFO-1132(E)/HFC-32/HFO-1234yf=10.1/18.0/71.9 mass %) and


      point D (HFO-1132(E)/HFC-32/HFO-1234yf=27.8/18.0/54.2 mass %);


      in a ternary composition diagram with the three components as respective apexes.


A refrigeration cycle device for a vehicle according to a twenty-fourth aspect is the refrigeration cycle device for a vehicle according to the twenty-second aspect, wherein

    • the refrigerant comprises HFO-1132(E), HFC-32 and HFO-1234yf, and a total concentration of the three components is 99.5 mass % or more based on the entire refrigerant, and
    • a mass ratio of the three components is within a range of a region surrounded by a figure passing through four points:


      point A (HFO-1132(E)/HFC-32/HFO-1234yf=51.8/1.0/47.2 mass %),


      point B (HFO-1132(E)/HFC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


      point E (HFO-1132(E)/HFC-32/HFO-1234yf=15.2/14.3/70.5 mass %) and


      point F (HFO-1132(E)/HFC-32/HFO-1234yf=31.1/14.3/54.6 mass %);


      in a ternary composition diagram with the three components as respective apexes.


A refrigeration cycle device for vehicle according to a twenty-fifth aspect is the refrigeration cycle device for a vehicle according to the twenty-second aspect, wherein

    • the refrigerant comprises WO-1132(E), HFC-32 and HFO-1234yf, and a total concentration of the three components is 99.5 mass % or more based on the entire refrigerant, and
    • a mass ratio of the three components is within a range of a region surrounded by a figure passing through five points:


      point P (HFO-1132(E)/HFC-32/HFO-1234y=45.6/1.0/53.4 mass %),


      point B (HFO-1132(E)/HFC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


      point Q (HFO-1132(E)/HFC-32/HFO-1234y=1.0/24.8/74.2 mass %),


      point R (HFO-1132(E)/HFC-32/HFO-1234yf=1.0/29.2/69.8 mass %) and


      point S (HFO-1132(E)/HFC-32/HFO-1234y=6.5/29.2/64.3 mass %);


      in a ternary composition diagram with the three components as respective apexes.


A refrigeration cycle device for a vehicle according to any one of the twenty-third aspect to the twenty-fifth aspect is the refrigeration cycle device for a vehicle according to the twenty-second aspect, wherein


the refrigerant consists only of HFO-1132(E), HFC-32 and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a twenty-seventh aspect includes a refrigerant circuit and a refrigerant that is sealed in the refrigerant circuit. The refrigerant circuit includes a compressor, a heat dissipater, a decompressor, and a heat absorber. The refrigerant contains at least HFO-1132(E), HFO-1123, and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a twenty-eighth aspect is the refrigeration cycle device for a vehicle according to the twenty-seventh aspect, wherein

    • the refrigerant comprises HFO-1132(E), HFO-1123 and HFO-1234yf, and a total concentration of the three components is 99.5 mass % or more based on the entire refrigerant, and
    • a mass ratio of the three components is within a range of a region surrounded by a figure passing through five points:


      point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


      point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


      point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


      point D (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/57.0/42.0 mass %) and


      point E (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/24.1/33.4 mass %);


      in a ternary composition diagram with the three components as respective apexes.


A refrigeration cycle device for a vehicle according to a twenty-ninth aspect is the refrigeration cycle device for a vehicle according to the twenty-seventh aspect, wherein

    • the refrigerant comprises HFO-1132(E), HFO-1123 and HFO-1234yf, and a total concentration of the three components is 99.5 mass % or more based on the entire refrigerant, and
    • a mass ratio of the three components is within a range of a region surrounded by a figure passing through five points:


      point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


      point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


      point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


      point F (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/52.2/46.8 mass %) and


      point G (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/18.9/38.6 mass %);


      in a ternary composition diagram with the three components as respective apexes.


A refrigeration cycle device for a vehicle according to a thirtieth aspect is the refrigeration cycle device for a vehicle according to the twenty-eighth or twenty-ninth aspect, wherein the refrigerant comprises HFO-1132(E), HFO-1123 and HFO-1234yf, and a total concentration of the three components is 99.5 mass % or more based on the entire refrigerant, and

    • a mass ratio of the three components is within a range of a region surrounded by a figure passing through six points:


      point A (ISO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


      point B (ISO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


      point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


      point H (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/35.2/63.8 mass %),


      point I (HFO-1132(E)/HFO-1123/HFO-1234yf=27.4/29.8/42.8 mass %) and


      point G (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/18.9/38.6 mass %);


      in a ternary composition diagram with the three components as respective apexes.


A refrigeration cycle device for a vehicle according to a thirty-first aspect is the refrigeration cycle device for a vehicle according to any one of the twenty-eighth aspect to the thirtieth aspect, wherein the refrigerant consists only of HFO-1132(E), HFO-1123 and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a thirty-second aspect includes a refrigerant circuit and a refrigerant that is sealed in the refrigerant circuit. The refrigerant circuit includes a compressor, a heat dissipater, a decompressor, and a heat absorber. The refrigerant contains at least HFO-1132(E) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a thirty-third aspect is the refrigeration cycle device for a vehicle according to the thirty-second aspect, wherein

    • the refrigerant comprises HFO-1132(E) and HFO-1234yf,
    • a content rate of HFO-1132(E) is 35.0 to 65.0 mass % and a content rate of HFO-1234yf is 65.0 to 35.0 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf, and
    • an evaporating temperature is −75 to −5° C.


A refrigeration cycle device for a vehicle according to a thirty-fourth aspect is the refrigeration cycle device for a vehicle according to the thirty-second aspect, wherein a content rate of HFO-1132(E) is 41.3 to 53.5 mass % and a content rate of HFO-1234yf is 58.7 to 46.5 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a thirty-fifth aspect is the refrigeration cycle device for a vehicle according to the thirty-third or thirty-fourth aspect, wherein the refrigerant consists only of HFO-1132(E) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a thirty-sixth aspect is the refrigeration cycle device for a vehicle according to the thirty-second aspect, wherein

    • the refrigerant comprises HFO-1132(E) and HFO-1234yf, and
    • a content rate of HFO-1132(E) is 40.5 to 49.2 mass % and a content rate of HFO-1234yf is 59.5 to 50.8 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf


A refrigeration cycle device for a vehicle according to a thirty-seventh aspect is the refrigeration cycle device for a vehicle according to the thirty-sixth aspect, wherein the refrigerant consists only of HFO-1132(E) and HFO-1234yf


A refrigeration cycle device for a vehicle according to a thirty-eighth aspect is the refrigeration cycle device for a vehicle according to the thirty-second aspect, wherein

    • the refrigerant comprises HFO-1132(E) and HFO-1234yf, and
    • a content rate of HFO-1132(E) is 31.1 to 39.8 mass % and a content rate of HFO-1234yf is 68.9 to 60.2 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a thirty-ninth aspect is the refrigeration cycle device for a vehicle according to the thirty-second aspect, wherein


a content rate of HFO-1132(E) is 31.1 to 37.9 mass % and a content rate of HFO-1234yf is 68.9 to 62.1 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a fortieth aspect is the refrigeration cycle device for a vehicle according to the thirty-eight or thirty-ninth aspect, wherein the refrigerant consists only of HFO-1132(E) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a forty-first aspect is the refrigeration cycle device for a vehicle according to the thirty-second aspect, wherein

    • the refrigerant comprises HFO-1132(E) and HFO-1234yf, and
    • a content rate of HFO-1132(E) is 21.0 to 28.4 mass % and a content rate of HFO-1234yf is 79.0 to 71.6 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a forty-second aspect is the refrigeration cycle device for a vehicle according to the forty-first aspect, wherein


the refrigerant consists only of HFO-1132(E) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a forty-third aspect is the refrigeration cycle device for a vehicle according to the thirty-second aspect, wherein


the refrigerant comprises HFO-1132(E) and HFO-1234yf,






    • a content rate of HFO-1132(E) is 12.1 to 72.0 mass % and a content rate of HFO-1234yf is 87.9 to 28.0 mass %, based on a total mass of HFO-1132(E) and WO-1234yf, and

    • the apparatus is in-car air conditioning equipment





A refrigeration cycle device for a vehicle according to a forty-fourth aspect includes a refrigerant circuit and a refrigerant that is sealed in the refrigerant circuit. The refrigerant circuit includes a compressor, a heat dissipater; a decompressor, and a heat absorber. The refrigerant contains at least HFC-32 and HFO-1234yf and at least one type selected from 1,1-difluoroethylene (HFO-1132a) and tetrafluoroethylene (FO-1114).


A refrigeration cycle device for a vehicle according to a forty-fifth aspect is the refrigeration cycle device for a vehicle according to the forty-fourth aspect, wherein


the refrigerant comprises HFO-1132a.


A refrigeration cycle device for a vehicle according to a forty-sixth aspect is the refrigeration cycle device for a vehicle according to the forty-fourth aspect, wherein


the refrigerant comprises 15.0 to 24.0 mass % of HFC-32 and 1.0 to 7.0 mass % of HFO-1132a when a total amount of HFC-32, HFO-1234yf and HFO-1132a is 100 mass %.


A refrigeration cycle device for a vehicle according to a forty-seventh aspect is the refrigeration cycle device for a vehicle according to the forty-fourth aspect, wherein

    • the refrigerant comprises 19.5 to 23.5 mass % of HFC-32 and 3.1 to 3.7 mass % of HFO-1132a when a total amount of HFC-32, HFO-1234yf and HFO-1132a is 100 mass %.


A refrigeration cycle device for a vehicle according to a forty-eighth aspect is the refrigeration cycle device for a vehicle according to the forty-fourth aspect, wherein

    • the refrigerant comprises HFC-32, HFO-1234yf and HFO-1132a, and when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which a sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within a range of a triangle surrounded by line segments RS, ST and TR that connect three points:
    • point R (21.80, 3.95, 74.25),
    • point S (21.80, 3.05, 75.15), and
    • point T (20.95, 75.30, 3.75);


      or are on the line segments.


A refrigeration cycle device for a vehicle according to a forty-ninth aspect is the refrigeration cycle device for a vehicle according to the forty-fourth aspect, wherein

    • the refrigerant comprises HFC-32, HFO-1234yf and HFO-1132a, and when HFC-32, HFO 1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which a sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within a range of a figure surrounded by line segments LF, FG, GO, OB and BL that connect five points:
    • point L (74.0, 19.9, 6.1),
    • point F (49.1, 25.9, 25.0),
    • point G (0.0, 48.6, 51.4),
    • point O (0.0, 0.0, 100), and
    • point B (73.9, 0.0, 26.1);


      or are on the line segments (but not on the line segments GO and OB),
    • the line segment LF is represented by
    • coordinate (y=0.0021x2−0.4975x+45.264),
    • the line segment FG is represented by
    • coordinate (y=0.0031x2−0.6144x+48.6), and
    • the line segments GO, OB and BL are straight lines.


A refrigeration cycle device for a vehicle according to a fifty aspect is the refrigeration cycle device for a vehicle according to the forty-fourth aspect, wherein

    • the refrigerant comprises HFC-32, HFO-1234yf and HFO-1132a, and when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which a sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within a range of a figure surrounded by line segments PF, FG, GO, OB′ and B′P that connect five points:
    • point P (59.1, 23.2, 17.7),
    • point F (49.1, 25.9, 25.0),
    • point G (0.0, 48.6, 51.4),
    • point O (0.0, 0.0, 100), and
    • point B′ (59.0, 0.0, 40.2);


      or are on the line segments (but not on the line segments GO and OH),
    • the line segment PF is represented by
    • coordinate (y=0.0021x2−0.4975x+45.264),
    • the line segment FG is represented by
    • coordinate (y=0.0031x2−0.6144x+48.6), and
    • the line segments GO, OB′ and B′P are straight lines.


A refrigeration cycle device for a vehicle according to a fifty-first aspect is the refrigeration cycle device for a vehicle according to the forty-fourth aspect, wherein

    • the refrigerant comprises HFC-32, HFO-1234yf and HFO-1132a, and when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which a sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within a range of a figure surrounded by segments MI, IJ, JB and BM that connect four points:
    • point M (74.0, 19.5, 6.5),
    • point I (62.9, 15.5, 21.6),
    • point J (33.5, 0.0, 66.5), and
    • point B (73.9, 0.0, 26.1),


      or are on the line segments (but not on the line segment JB),
    • the line segment MI is represented by
    • coordinate (y=0.006x2+1.1837x−35.264),
    • the line segment IJ is represented by
    • coordinate (y=0.0083x2−0.2719x−0.1953), and
    • the line segments JB and BM are straight lines.


A refrigeration cycle device for a vehicle according to a fifty-second aspect is the refrigeration cycle device for a vehicle according to the forty-fourth aspect, wherein

    • the refrigerant comprises HFC-32, HFO-1234yf and HFO-1132a, and when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which a sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within a range of a figure surrounded by line segments QJ, JB′ and B′Q that connect three points:
    • point Q (59.1, 12.7, 28.2),
    • point J (33.5, 0.0, 66.5), and
    • point B′ (59.0, 0.0, 40.2),


      or are on the line segments (but not on the line segment JB′),
    • the line segment QJ is represented by
    • coordinate (y=0.0083x2−0.2719x−0.1953), and
    • the line segments JB′ and B′Q are straight lines.


A refrigeration cycle device for a vehicle according to a fifty-third aspect is the refrigeration cycle device for a vehicle according to the forty-fourth aspect, wherein

    • the refrigerant comprises HFC-32, HFO-1234yf and HFO-1132a, and when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which a sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within a range of a figure surrounded by line segments QU, UV and VQ that connect three points:
    • point Q (59.1, 12.7, 28.2),
    • point U (59.0, 5.5, 35.5), and
    • point V (52.5, 8.4, 39.1),


      or are on the line segments,
    • the line segment VQ is represented by
    • coordinate (y=0.0083x2−0.2719x−0.1953),
    • the line segment UV is represented by
    • coordinate (y=0.0026x2−0.7385x+39.946), and
    • the line segment QU is a straight line.


A refrigeration cycle device for a vehicle according to a fifty-fourth aspect includes a refrigerant circuit and a refrigerant that is sealed in the refrigerant circuit. The refrigerant circuit includes a compressor, a heat dissipater, a decompressor, and a heat absorber. The refrigerant contains at least difluoromethane (R32), carbon dioxide (CO2), pentafluoroethane (R125), 1,1,1,2-tetrafluoroethane (R134a), and 2,3,3,3-tetrafluoropropene (R1234yf).


A refrigeration cycle device for a vehicle according to a fifty-fifth aspect is the refrigeration cycle device for a vehicle according to the fifty-fourth aspect, wherein

    • the refrigerant comprises difluoromethane (R32), carbon dioxide (CO2), pentafluoroethane (R125), 1,1,1,2-tetrafluoroethane (R134a), and 2,3,3,3-tetrafluoropropene (R1234yf), and
    • in a case where a mass % of R32 is defined as a, a mass % of CO2 is defined as b, a mass % of R125 is defined as c1, a mass % of R134a is defined as c2, a mass % of a total of R125 and R134a is defined as c and a mass % of R1234yf is defined as x, and c1/(c1+c2) is defined as r based on a sum of R32, CO2, R125, R134a and R1234yf in the refrigerant,
    • coordinates (a,b,c) in a three-component composition diagram with, as respective apexes, a point where R32 occupies (100−x) mass %, a point where CO2 occupies (100−x) mass % and a point where the total of R125 and R134a occupies (100−x) mass % are 1-1-1) with 43.8≥x≥41 and 0.5≥r≥0.25,


      within a range of a quadrangle surrounded by line segments that connect:
    • point A (−0.6902x+43.307, 100−a−x, 0.0),
    • point Or=0.25 to 0.5((−2.2857x+87.314)r2+(1.7143x−55.886)r+(−0.9643x+55.336), (2.2857x−112.91)r2+(−1.7143x+104.69)r+(−0.25x+11.05), 100−a−b−x),
    • point Dr=0.25 to 0.5 (0.0, −28.8r2+54.0r+(−x+49.9), 100−b−x) and
    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.25 to 0.5Q and QA is excluded), or


      1-1-2) with 43.8≥x≥41 and 1.0≥r≥0.5,


      within a range of a quadrangle surrounded by line segments that connect:
    • point A (0.6902x+43.307, 100−a−c, 0.0),
    • point Or=0.5 to 1.0((−0.2857x+8.5143)r2+(0.5x−10.9)+(−0.8571x+52.543), (−0.2857x+4.5143)r2+(0.5x+0.9)r+(−0.7143x+33.586), 100−a−b−x),
    • point Dr=0.5 to 1.0(0.0, (−0.5714x+12.229)r2+(0.8571x−0.3429)r+(−1, 2857x+66.814), 100−b−x) and
    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point online segments Dr=0.5 to 1.0Q and QA is excluded), or 1-2-1) with 46.5≥x≥43.8 and 0.5≥r≥0.25,


      within a range of a quadrangle surrounded by line segments that connect:
    • point A (−0.6902x+43.307, 100−a−x, 0.0),
    • point Or=0.25 to 0.5 ((1.1852x−64.711)r2+(−0.7407x+51.644)r+(−0.5556x+37.433), (−2.3704x+91.022)r2+(2.0741 x−61.244)r+(−0.963x+42.278), 100−a−b−x),
    • point Dr=0.25 to 0.5(0.0, 28.8r2+54.0r+(−x+49.9), 100−b−x) and
    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.25 to 0.5Q and QA is excluded), or 1-2-2) with 46.5≥x≥43 and 1.0≥r≥0.5,


      within a range of a quadrangle surrounded by line segments that connect:
    • point A (−0.6902x+43.307, 100−a−x, 0.0),
    • point Or=0.5 to 1.0((0.2963x−16.978)r2+(−0.3704x+27.222)r+(−0.5185x+37.711), −8.0r2+22.8r+(−0.5185x+25.011), 100−a−b−x),
    • point Dr=0.5 to 1.0(0.0; 12.8r2+37.2r+(−x+54.3), 100−b) and
    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.5 to 1.0Q and QA is excluded), or 1-3-1) with 50≥x≥46.5 and 0.5≥r≥0.25,


      within a range of a quadrangle surrounded by line segments that connect:
    • point A (−0.6902x+43.307, 100−a−x, 0.0),
    • point Or=0.25 to 0.5(−9.6r2+17.2r+(−0.6571x+42.157); 19.2r2+(0.2286x+24.571)r+(−0.6286x+26.729), 100−a−b−x),
    • point Dr=0.25 to 0.5(0.0, (0.9143x−71.314)r2+(−0.5714x+80.571)+(−0.9143x+45.914), 100−b−x) and
    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.25 to 0.5Q and QA is excluded), or 1-3-2) with 50≥x≥46.5 and 1.0≥r≥0.5,


      within a range of a quadrangle surrounded by line segments that connect:
    • point A (−0.6902x+43.307, 100−a−x, 0.0),
    • point Or=0.5 to 1.0((0.2286x+7.4286)r2+(0.4x−8.6)r+(−0.8x+50.8), (0.2286x−18.629)r2+(=0.2857x+36.086)r+(−0.4286x+20.829), 100−a−b−x),
    • point Dr=0.5 to 1.0(0.0, (0.2286x−23.429)r2+(−0.4x+55.8)r+(−0.8286x+46.329), 100−b−x) and
    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.5 to 1.0Q and QA is excluded).


A refrigeration cycle device for a vehicle according to a fifty-sixth aspect is the refrigeration cycle device for a vehicle according to the fifty-fourth aspect, wherein

    • the refrigerant comprises R32, CO2, R125, R134a and R1234yf, and
    • in a case where a mass % of R32 is defined as a, a mass % of CO2 is defined as b, a mass % of R125 is defined as et, a mass % of R134a is defined as c2, a mass % of a total of R125 and R134a is defined as c and a mass % of R1234yf is defined as x, and c1/(c1+c2) is defined as r based on a sum of R32, CO2, R125, R134a and R1234yf in the refrigerant,
    • coordinates (a,b,c) in a three-component composition diagram with, as respective apexes, a point where R32 occupies (100−x) mass %, a point where CO2 occupies (100−x) mass % and a point where the total of R125 and R134a occupies (100−x) mass % are 2-1-1) with 43.8≥x≥41 and 0.5≥r≥0.25,


      within a range of a triangle surrounded by line segments that connect:
    • point Fr=0.25 to 0.5 (0.0, (−1.1429x+37.257)r2+(1.2857x−38.714)r−(−1.7143x+106.89), 100−b−x),
    • point Pr=0.25 to 0.5 ((−1.1429x+34.057)r2+(1.0x−21.0)r+(−0.4643x+27.636), (2.2857x−119.31)r2+(−2.0x+122.0)r+(−0.3929x+19.907), 100−a−b−x) and
    • point Dr=0.25 to 0.5(0.0, 28.8x2+54.0r+(−x+49.9), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.25 to 0.5Fr=0.25 to 0.5 is excluded), or 2-1-2) with 43.8≥x≥41 and 1.0≥r≥0.5,


      within a range of a triangle surrounded by line segments that connect:
    • point Fr=0.5 to 1.0(0.0, (3.7143x−159.49)r2+(−5.0714x+222.53)r+(0.25x+25.45), 100−b−x),
    • point Pr=0.5 to 1.0((3.4286x−138.17)r2+(−5.4286x+203.57)+(1.6071x−41.593), (−2.8571x+106.74)r2+(4.5714x−143.63)r+(−2.3929x+96.027), 100−a−b−x) and
    • point Dr=0.5 to 1.0(0.0, (−0.5714x+12.229)x2+(0.8571x−0.3429)r+(−1.2857x+66.814), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.5 to 1.0Fr=0.5 to 1.0 is excluded), or 2-2-1) with 46.5≥x≥43 and 0.5≥r≥0.25,


      within a range of a triangle surrounded by line segments that connect:
    • point Fr=0.25 to 0.5 (0.0, (9.4815x−428.09)r2+(−7.1111 x+329.07)r+(−0.2593x+43.156), 100−b−x),
    • point Pr=0.25 to 0.5 ((−8.2963x+347.38)x2+(4.8889x−191.33)r+(−0.963 x+49.478), (7.1111 x−330.67)r2+(−4.1481x+216.09)r+(−0.2593x+14.056), 100−a−b−x) and
    • point Dr=0.25 to 0.5 (0.0, 28.8x2+54.0r+(−x+49.9), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.25 to 0.5Fr=0.25 to 0.5 is excluded), or 2-2-2) with 46.5≥x≥43 and 1.0≥r≥0.5,


      within a range of a triangle surrounded by line segments that connect:
    • point Fr=0.5 to 1.0(0.0, (−4.7407x+210.84)r2+(6.963x−304.58)r+(−3.7407x+200.24), 100−b−x),
    • point Pr=0.5 to 1.0((0.2963x−0.9778)r2+(0.2222x−43.933)r+(−0.7778x+62.867), (0.2963x−5.4222)r2+(−0.0741x+59.844)r+(−0.4′111x+10.867), 100−a−b−x) and
    • point Dr=0.5 to 1.0(0.0, 12.8x2+37.2r+(−x+54.3), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.5 to 1.0Fr=0.5 to 1.0 is excluded), or 2-3-1) with 50≥x≥46.5 and 0.37≥r≥0.25,


      within a range of a triangle surrounded by line segments that connect:
    • point Fr=0.25 to 0.37 (0.0, (−35.714x+1744.0)x2+(23.333x−1128.3)r+(−5.144x+276.32), 100−b−x),
    • point Pr=0.25 to 0.37 ((11.905x−595.24)r2+(−7.6189x+392.61)r+(0.9322x−39.027), (−27.778x+1305.6)r2+(17.46x−796.35)r+(−3.5147x+166.48), 100−a−b−x) and
    • point Dr=0.25 to 0.37 (0.0, (0.9143x−71.314)r2+(−0.5714x+80.571)+(−0.9143x+45.914), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.25 to 0.37Fr=0.25 to 0.37 is excluded), or 2-3-2) with 50≥x≥46.5 and 1.0≥r≥0.5,


      within a range of a triangle surrounded by line segments that connect:
    • point Fr=0.5 to 1.0(0.0, (2.2857x−115.89)r2+(−3.0857x+162.69)r+(−0.3714x+43.571), 100−b−x),
    • point Pr=0.5 to 1.0((−3.2x+161.6)r2+(4.4571x−240.86)r+(−2.0857x+123.69), (2.5143x−136.11)r2+(−3.3714x+213.17)r+(0.5429x−35.043), 100−a−b−x) and
    • point Dr=0.5 to 1.0(0.0, (0.2286x−23.429)r2+(−0.4x+55.8)r+(−0.8286x+46.329), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.25 to 0.5Fr=0.25 to 0.5 is excluded).


A refrigeration cycle device for a vehicle according to a fifty-seventh aspect is the refrigeration cycle device for a vehicle according to the fifty-fifth or the fifty-sixth aspect, wherein the refrigerant comprises 99.5 mass % or more in total of R32, CO2, R125, R134a and R1234yf based on the entire refrigerant.


A refrigeration cycle device for a vehicle according to a fifty-eighth aspect includes a refrigerant circuit and a refrigerant that is sealed in the refrigerant circuit. The refrigerant circuit includes a compressor, a heat dissipater, a decompressor, and a heat absorber. The refrigerant contains at least cis-1,2-difluoroethylene (HFO-1132(Z)) and 2,3,3,3-tetrafluoropropene (HFO-1234yf).


A refrigeration cycle device for a vehicle according to a fifty-ninth aspect is the refrigeration cycle device for a vehicle according to the fifty-eighth aspect, wherein


a content of HFO-1132(Z) is 53.0 to 59.5% by mass, and


a content of HFO-1234yf is 47.0 to 40.5% by mass,


based on a total mass of HFO-1132(Z) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a sixty aspect is the refrigeration cycle device for a vehicle according to the fifty-ninth aspect, wherein the refrigerant consists only of HFO-11320 and HFO-1234yf


A refrigeration cycle device for a vehicle according to a sixty-first aspect is the refrigeration cycle device for a vehicle according to the fifty-eighth aspect, wherein


a content of HFO-1132(Z) is 41.0 to 49.2% by mass, and


a content of HFO-1234yf is 59.0 to 50.8% by mass,


based on a total mass of HFO-1132(Z) and HFO-12343f.


A refrigeration cycle device for a vehicle according to a sixty-second aspect is the refrigeration cycle device for a vehicle according to the sixty first aspect, wherein


the refrigerant consists only of HFO-1132(Z) and HFO-1234yf.


A refrigeration cycle device for a vehicle according to a sixty-third aspect is the refrigeration cycle device for a vehicle according to the fifty-ninth or the sixty-second aspect, wherein wherein used as an alternative refrigerant to R134a, R22, R12, R404A, R407A, R407C, R407F, R407H, R410A, R413A, R417A, R422A, R422B, R422C, R422D, R423A, R424A, R426A, R427A, R428A, R430A, R434A, R437A, R438A, R448A, R449A, R449B, R449C, R450A, R452A, R452B, R454A, R452B, R454C, R455A, R465A, R502, R507, R513A, R513B, R515A, or R515B.


A refrigeration cycle device for a vehicle according to a sixty-fourth aspect is the refrigeration cycle device for a vehicle according to any one of the fifty-eighth aspect to the sixty-third aspect, wherein the refrigerant containing at least one substance selected from the group consisting of water, a tracer, an ultraviolet fluorescent dye, a stabilizer, and a polymerization inhibitor.


A refrigeration cycle device for a vehicle according to a sixty-fifth aspect is the refrigeration cycle device for a vehicle according to any one of the fifty-eighth aspect or the sixty-fourth aspect, wherein the refrigerant further containing a refrigerator oil and used as a working fluid for a refrigeration apparatus.


A refrigeration cycle device for a vehicle according to a sixty-sixth aspect is the refrigeration cycle device for a vehicle according to the sixty-fifth aspect, wherein the refrigerator oil contains at least one polymer selected from the group consisting of a polyalkylene glycol (PAG), a polyol ester (POE), and a polyvinyl ether (PVE).





BRIEF DESCRIPTION OF DRAWINGS


FIG. 1A is a schematic view of an apparatus used in a flammability test.



FIG. 1B is a diagram showing points A to M and O, and line segments that connect these points to each, other in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass %.



FIG. 1C is a diagram showing points A to C, B′ and O, and line segments that connect these points to each other in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass %.



FIG. 1D is a diagram showing points A to C, B′ and O, and line segments that connect these points to each other in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 95 mass % (R32 content is 5 mass %).



FIG. 1E is a diagram showing points A to C, B′ and O, and line segments that connect these points to each other in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 90 mass % (R32 content is 10 mass %).



FIG. 1F is a diagram showing points A to C, B′ and O, and line segments that connect these points to each other in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 85.7 mass % (R32 content is 14.3 mass %).



FIG. 1G is a diagram showing points A to C, B′ and O, and line segments that connect these points to each other in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 83.5 mass % (R32 content is 16.5 mass %).



FIG. 1H is a diagram showing points A to C, B′ and O, and line segments that connect these points to each other in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 80.8 mass % (R32 content is 19.2 mass %).



FIG. 1I is a diagram showing points A to C, B′ and O, and line segments that connect these points to each other in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 78.2 mass % (R32 content is 21.8 mass %).



FIG. 1J is a diagram showing points A to K and O to R, and line segments that connect these points to each other in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass %.



FIG. 1K is a diagram showing points A to D, A′ to D′, and O, and line segments that connect these points to each other in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass %.



FIG. 1L is a ternary composition diagram in which the sum of the concentrations of R32, HFO-1132(E), and R1234yf is 100 mass %, the diagram showing points and line segments defining the refrigerant according to the present disclosure.



FIG. 1M is a ternary composition diagram in which the sum of the concentrations of R32, HFO-1132(E), and R1234yf is 99.4 mass % (CO2 content is 0.6 mass %), the diagram showing points and line segments defining the refrigerant according to the present disclosure.



FIG. 1N is a ternary composition diagram in which the sum of the concentrations of R32, HFO-1132(E), and R1234yf is 98.8 mass % (CO2 content is 12 mass %), the diagram showing points and line segments defining the refrigerant according to the present disclosure.



FIG. 1O is a ternary composition diagram in which the sum of the concentrations of R32, HFO-1132(E), and R1234yf is 98.7 mass % (CO2 content is 1.3 mass %), the diagram showing points and line segments defining the refrigerant according to the present disclosure.



FIG. 1P is a ternary composition diagram in which the sum of the concentrations of R32, HFO-1132(E), and R1234yf is 97.5 mass % (CO2 content is 2.5 mass %), the diagram showing points and line segments defining the refrigerant according to the present disclosure.



FIG. 1Q is a ternary composition diagram in which the sum of the concentrations of R32, HFO-1132(E), and R1234yf is 96 mass % (CO2 content is 4 mass %), the diagram showing points and line segments defining the refrigerant according to the present disclosure.



FIG. 1R is a ternary composition diagram in which the sum of the concentrations of R32, HFO-1132(E), and R1234yf is 94.5 mass % (CO2 content is 5.5 mass %), the diagram showing points and line segments defining the refrigerant according to the present disclosure.



FIG. 1S is a ternary composition diagram in which the sum of the concentrations of R32, HFO-1132(E), and R1234yf is 93 mass % (CO2 content is 7 mass %), the diagram showing points and line segments defining the refrigerant according to the present disclosure.



FIG. 1T is a schematic view of an experimental apparatus for determining flammability (flammability or non-flammability).



FIG. 2A is a diagram representing the mass ratio (a region surrounded by a figure passing through four points of points A, B, C and D, and a region surrounded by a figure passing through four points of points A, B, E and F) of trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (HFC-32) and 2,3,3,3-tetrafluoropropene (HFO-1234yf) contained in a refrigerant A1, in a ternary composition diagram with HFO-1132(E), HFC-32 and HFO-1234yf.



FIG. 2B is a diagram representing the mass ratio (a region surrounded by a figure passing through five points of points P, B, Q, R and S) of HFO-1132(E), HFC-32 and HFO-1234yf contained in a refrigerant A2, in a ternary composition diagram with HFO-1132(E), HFC-32 and HFO-1234yf.



FIG. 2C is a diagram representing the mass ratio (a region surrounded by a figure passing through five points of points A, B, C, D and E, a region surrounded by a figure passing through five points of points A, B, C, F and G, and a region surrounded by figure passing through six points of points A, B, C, H, I and G) of HFO-1132(E), HFO-1123 and HFO-1234yf contained in a refrigerant 1B, in a ternary composition diagram with HFO-1132(E), HFO-1123 and HFO-1234yf.



FIG. 2Da is a three-component composition diagram for explaining the composition of any refrigerant 2D according to a first aspect and a second aspect of the present disclosure. In an enlarged view of FIG. 1A, the maximum composition of the refrigerant 2D according to the fast aspect is within the range of a quadrangle indicated by X or is on line segments of the quadrangle. In the enlarged view of FIG. 2A, a preferable composition of the refrigerant of the first aspect is within the range of a quadrangle indicated by Y or is on line segments of the quadrangle. In the enlarged view of FIG. 2A, the composition of the refrigerant 2D of the second aspect is within the range of a triangle surrounded by line segments RS, ST and TR or is on the line segments.



FIG. 2Db is a three-component composition diagram for explaining the composition of any refrigerant 2D according to a third aspect to a seventh aspect of the present disclosure.



FIG. 2E is a schematic view of an apparatus for use in a flammability test.



FIG. 2F is a schematic view illustrating one example of a countercurrent heat exchanger.



FIG. 2G are schematic views each illustrating one example of a countercurrent heat exchanger, and (a) is a plan view and (b) is a perspective view.



FIG. 2H is a schematic view illustrating one aspect of a refrigerant circuit in a refrigerator of the present disclosure.



FIG. 2I is a schematic view illustrating a variant of the refrigerant circuit in FIG. 2H.



FIG. 2J is a schematic view illustrating a variant of the refrigerant circuit in FIG. 2H.



FIG. 2K is a schematic view illustrating a variant of the refrigerant circuit in FIG. 2H.



FIG. 2L is a schematic view for explaining an off-cycle defrost.



FIG. 2M is a schematic view for explaining a heating defrost.



FIG. 2N is a schematic view for explaining a reverse cycle hot gas defrost.



FIG. 2O is a schematic view for explaining a normal cycle hot gas defrost.



FIG. 2P is a diagram representing a straight line Fr=0.25Pr=0.25 that connects any non-flammability limit point in ASHRAE represented in Tables 206 to 209, the point Fr=0.25 and the point Pr=0.25 in a three-component composition diagram with, as respective apexes, a point where R32 occupies (100−x) mass %, a point where CO2 occupies (100−x) mass % and a point where the total of R125 and R134a occupies (100−x) mass %, with respect to a refrigerant 2E.



FIG. 2Q is a diagram representing a straight line Fr=0.375Pr=0.375 that connects any non-flammability limit point in ASHRAE represented in Tables 206 to 209, the point Fr=0.375 and the point Pr=0.375 in a three-component composition diagram with, as respective apexes, a point where R32 occupies (100−x) mass %, a point where CO2 occupies (100−x) mass % and a point where the total of R125 and R134a occupies (100−x) mass %, with respect to a refrigerant 2E.



FIG. 2R is a diagram representing a straight line Fr=0.5Pr=0.5 that connects any non-flammability limit point in ASHRAE represented in Tables 206 to 209, the point Fr=0.5 and the point Pr=0.5 in a three-component composition diagram with, as respective apexes, a point where R32 occupies (100−x) mass %, a point where CO2 occupies (100−x) mass % and a point where the total of R125 and R134a occupies (100−x) mass %, with respect to a refrigerant 2E.



FIG. 2S is a diagram representing a straight line Fr=0.75Pr=0.75 that connects any non-flammability limit point in ASHRAE represented in Tables 206 to 209, the point Fr=0.75 and the point Pr=0.75 in a three-component composition diagram with, as respective apexes, a point where R32 occupies (100−x) mass %, a point where CO2 occupies (100−x) mass % and a point where the total of R125 and R134a occupies (100−x) mass %, with respect to a refrigerant 2E.



FIG. 2T is a diagram representing a straight line Fr=1.0Pr=1.0 that connects any non-flammability limit point in ASHRAE represented in Tables 206 to 209, the point Fr=1.0 and the point Pr=1.0 in a three-component composition diagram with, as respective apexes, a point where R32 occupies (100−x) mass %, a point where CO2 occupies (100−x) mass % and a point where the total of R125 and R134a occupies (100−x) mass %, with respect to a refrigerant 2E.



FIG. 2U is a ternary diagram representing points A, Or=0.25 to 1, Dr=0.25 to 1, Cr=0.25 to 1, Fr=0.25 to 1, Pr=0.25 to 1 and Q at a concentration of R1234yf of 41 mass % in a refrigerant 2E.



FIG. 2V is a ternary diagram representing points A, Or=0.25 to 1, Dr=0.25 to 1, Cr=0.25 to 1, Fr=0.25 to 1, Pr=0.25 to 1 and Q at a concentration of R1234yf of 43.8 mass % in a refrigerant 2E.



FIG. 2W is a ternary diagram representing points A, Or=0.25 to 1, Dr=0.25 to 1, Cr=0.25 to 1, Fr=0.25 to 1, Pr=0.25 to 1 and Q at a concentration of R1234yf of 46.5 mass % in a refrigerant 2E.



FIG. 2X is a ternary diagram representing points A, Or=0.25 to 1, Dr=0.25 to 1, Cr=0.25 to 1, Pr=0.25 to 1 and Q at a concentration of R1234yf of 50.0 mass % in a refrigerant 2E.



FIG. 2Y is a ternary diagram representing points Dr=0.25 to 1, Cr=0.25 to 1, Fr=0.25 to 0.37, Fr=0.5 to 1, Pr=0.25 to 0.37, Pr=0.50 to 1 and Q at a concentration of R1234yf of 46.5 mass % in a refrigerant 2E.



FIG. 2Z is a ternary diagram representing points Dr=0.25 to 1, Cr=0.25 to 1, Fr=0.25 to 0.37, Fr=0.37 to 1, Pr=0.25 to 0.37, Pr=0.37 to 1 and Q at a concentration of R1234yf of 50.0 mass % in a refrigerant 2E.



FIG. 3 is a schematic view of a configuration of an air conditioner for a vehicle according to a first embodiment of the present disclosure.



FIG. 4 is a schematic view of the configuration of the air conditioner for a vehicle, and illustrates a circulation path of a refrigerant in a heating mode.



FIG. 5 is a schematic view of the configuration of the air conditioner for a vehicle, and illustrates a circulation path of a refrigerant in a cooling mode.



FIG. 6 is a block diagram of a controlling device.



FIG. 7 is a schematic view of a configuration of an air conditioner for a vehicle according to a modification of the first embodiment.



FIG. 8 is a schematic view of a configuration of an air conditioner for a vehicle according to a second embodiment of the present disclosure.



FIG. 9 is a schematic view of the configuration of the air conditioner for a vehicle, and illustrates a circulation path of a refrigerant in a cooling mode.



FIG. 10 is a schematic view of the configuration of the air conditioner for a vehicle, and illustrates a circulation path of a refrigerant in a heating mode.



FIG. 11 is a block diagram of a controlling device.



FIG. 12 is a schematic view of a configuration of an air conditioner for a vehicle according to a modification of the second embodiment.





DESCRIPTION OF EMBODIMENTS

(1)


(1-1) Definition of Terms


In the present specification, the term “refrigerant” includes at least compounds that are specified in ISO 817 (International Organization for Standardization), and that are given a refrigerant number (ASHRAE number) representing the type of refrigerant with “R” at the beginning; and further includes refrigerants that have properties equivalent to those of such refrigerants, even though a refrigerant number is not yet given. Refrigerants are broadly divided into fluorocarbon compounds and non-fluorocarbon compounds in terms of the structure of the compounds. Fluorocarbon compounds include chlorofluorocarbons (CFC), hydrochlorofluorocarbons (HCFC), and hydrofluorocarbons (HFC). Non-fluorocarbon compounds include propane (R290), propylene (R1270), butane (R600), isobutane (R600a), carbon dioxide (R744), ammonia (R717), and the like.


In the present specification, the phrase “composition comprising a refrigerant” at least includes (1) a refrigerant itself (including a mixture of refrigerants), (2) a composition that further comprises other components and that can be mixed with at least a refrigeration oil to obtain a working fluid for a refrigerating machine, and (3) a working fluid for a refrigerating machine containing a refrigeration oil. In the present specification, of these three embodiments, the composition (2) is referred to as a “refrigerant composition” so as to distinguish it from a refrigerant itself (including a mixture of refrigerants). Further, the working fluid for a refrigerating machine (3) is referred to as a “refrigeration oil-containing working fluid” so as to distinguish it from the “refrigerant composition.”


In the present specification, when the term “alternative” is used in a context in which the first refrigerant is replaced with the second refrigerant, the first type of “alternative” means that equipment designed for operation using the first refrigerant can be operated using the second refrigerant under optimum conditions, optionally with changes of only a few parts (at least one of the following: refrigeration oil, gasket, packing, expansion valve, dryer, and other parts) and equipment adjustment. In other words, this type of alternative means that the same equipment is operated with an alternative refrigerant 2 Embodiments of this type of “alternative” include “drop-in alternative,” “nearly drop-in alternative,” and “retrofit,” in the order in which the extent of changes and adjustment necessary for replacing the first refrigerant with the second refrigerant is smaller.


The term “alternative” also includes a second type of “alternative,” which means that equipment designed for operation using the second refrigerant is operated for the same, use as the existing use with the first refrigerant by using the second refrigerant. This type of alternative means that the same use is achieved with an alternative refrigerant.


In the present specification, the term “refrigerating machine” refers to machines in general that draw heat from an object or space to make its temperature lower than the temperature of ambient air, and maintain a low temperature. In other words, refrigerating machines refer to conversion machines that gain energy from the outside to do work, and that perform energy conversion, in order to transfer heat from where the temperature is lower to where the temperature is higher.


Any refrigerant having “non-flammability” in the present disclosure means that the WCF composition (Worst case of formulation for flammability), as a composition exhibiting most flammability, among acceptable concentrations of the refrigerant is rated as “Class 1” in US ANSI/ASHRAE Standard 34-2013.


Any refrigerant having “low flammability” herein means that the WCF composition is rated as “Class 2” in US ANSI/ASHRAE Standard 34-2013.


Any refrigerant having “ASHRAE non-flammability” in the present disclosure means that the WCF composition or WCFF composition can be specified as exhibiting non-flammability according to a test based on the measurement apparatus and the measurement method according to ASTM E681-2009 [Standard Test Method for Concentration Limits of Flammability of Chemicals (Vapors and Gases)], and is classified to “Class 1 ASHRAE non-flammability (WCF non-flammability” or “Class 1 ASHRAE non-flammability (WCFF non-flammability)”. The WCFF composition (Worst case of fractionation for flammability: mixed composition causing most flammability) is specified by performing a leak test in storage, transport and use based on ANSI/ASHRAE 34-2013.


Any refrigerant having “lower flammability” herein means that the WCF composition is rated as “Class 2L” in US ANSI/ASHRAE Standard 34-2013.


The “temperature glide” can be herein restated as the absolute value of the difference between the start temperature and the end temperature in the course of phase transition of the composition including a refrigerant of the present disclosure, in any constituent element in a heat cycle system.


The “in-car air conditioning equipment” herein means one refrigerating apparatus for use in cars such as a gasoline-fueled car, a hybrid car, an electric car and a hydrogen-fueled car. The in-car air conditioning equipment refers to a refrigerating apparatus including a refrigeration cycle that allows a liquid refrigerant to perform heat exchange in an evaporator, allows a compressor to suction a refrigerant gas evaporated, allows a refrigerant gas adiabatically compressed to be cooled and liquefied by a condenser, furthermore allows the resultant to pass through an expansion valve and to be adiabatically expanded, and then anew feeds the resultant as a liquid refrigerant to an evaporating machine.


The “turbo refrigerator” herein means one large-sized refrigerator. The turbo refrigerator refers to a, refrigerating apparatus including a refrigeration cycle that allows a liquid refrigerant to perform heat exchange in an evaporator, allows a centrifugal compressor to suction a refrigerant gas evaporated, allows a refrigerant gas adiabatically compressed to be cooled and liquefied by a condenser, furthermore allows the resultant to pass through an expansion valve and to be adiabatically expanded, and then anew feeds the resultant as a liquid refrigerant to an evaporating machine. The “large-sized refrigerator” refers to a large-sized air conditioner for air conditioning in building units.


The “saturation pressure” herein means the pressure of saturated vapor.


The “discharge temperature” herein means the temperature of a mixed refrigerant at a discharge port in a compressor.


The “evaporating pressure” herein means the saturation pressure at an evaporating temperature.


The “critical temperature” herein means the temperature at a critical point, and means a boundary temperature where gas cannot turn to any liquid at a temperature more than such a boundary temperature even if compressed.


The GWP herein means the value based on the fourth report of IPCC (Intergovernmental Panel on Climate Change).


The description “mass ratio” herein has the same meaning as the description “composition ratio”.


(1-2) Refrigerant


Although the details thereof are described later, any one of the refrigerants 1A, 1B, 1C, 1D, 1E, 2A, 2B, 2C, 2D and 2E according to the present disclosure (sometimes referred to as “the refrigerant according to the present disclosure”) can be used as a refrigerant.


(1-3) Refrigerant Composition


The refrigerant composition according to the present disclosure comprises at least the refrigerant according to the present disclosure, and can be used for the same use as the refrigerant according to the present disclosure. Moreover, the refrigerant composition according to the present disclosure can be further mixed with at least a refrigeration oil to thereby obtain a working fluid for a refrigerating machine.


The refrigerant composition according to the present disclosure further comprises at least one other component in addition to the refrigerant according to the present disclosure. The refrigerant composition according to the present disclosure may comprise at least one of the following other components, if necessary. As described above, when the refrigerant composition according to the present disclosure is used as a working fluid in a refrigerating machine, it is generally used as a mixture with at least a refrigeration oil. Therefore, it is preferable that the refrigerant composition according to the present disclosure does not substantially comprise a refrigeration oil. Specifically, in the refrigerant composition according to the present disclosure, the content of the refrigeration oil based on the entire refrigerant composition is preferably 0 to 1 mass %, and more preferably 0 to 0.1 mass %.


(1-3-1) Water


The refrigerant composition according to the present disclosure may contain a small amount of water. The water content of the refrigerant composition is preferably 0.1 mass % or less based on the entire refrigerant 1A small amount of water contained in the refrigerant composition stabilizes double bonds in the molecules of unsaturated fluorocarbon compounds that can be present in the refrigerant, and makes it less likely that the unsaturated fluorocarbon compounds will be oxidized, thus increasing the stability of the refrigerant composition.


(1-3-2) Tracer


A tracer is added to the refrigerant composition according to the present disclosure at a detectable concentration such that when the refrigerant composition has been diluted, contaminated, or undergone other changes, the tracer can trace the changes.


The refrigerant composition according to the present disclosure may comprise a single tracer, or two or more tracers.


The tracer is not limited, and can be suitably selected from commonly used tracers.


Examples of tracers include hydrofluorocarbons, hydrochlorofluorocarbons, chlorofluorocarbons, hydrochlorocarbons, fluorocarbons, deuterated hydrocarbons, deuterated hydrofluorocarbons, perfluorocarbons, fluoroethers, brominated compounds, iodinated compounds, alcohols, aldehydes, ketones, and nitrous oxide (N2O). The tracer is particularly preferably a hydrofluorocarbon, a hydrochlorofluorocarbon, a chlorofluorocarbon, a hydrochlorocarbon, a fluorocarbon, or a fluoroether.


The following compounds are preferable as the tracer.


FC-14 (tetrafluoromethane, CF4)


HCC-40 (chloromethane, CH3Cl)


HFC-23 (trifluoromethane, CHF3)


HFC-41 (fluoromethane, CH3Cl)


HFC-125 (pentafluoroethane, CF3CHF2)


HFC-134a (1,1,1,2-tetrafluoroethane, CF3CH2F)


HFC-134 (1,1,2,2-tetrafluoroethane, CHF2CHF2)


HFC-143a (1,1,1-trifluoroethane, CF3CH3)


HFC-143 (1,1,2-trifluoroethane, CHF2CH2F)


HFC-152a (1,1-difluoroethane, CHF2CH3)


HFC-152 (1,2-difluoroethane, CH2FCH2F)


HFC-161 (fluoroethane, CH3CH2F)


HFC-245fa (1,1,1,3,3-pentafluoropropane, CF3CH2CHF2)


HFC-236fa (1,1,1,3,3,3-hexafluoropropane, CF3CH2CF3)


HFC-236ea (1,1,1,2,3,3-hexafluoropropane, CF3CHFCHF2)


HFC-227ea (1,1,1,2,3,3,3-heptafluoropropane, CF3CHFCF3)


HCFC-22 (chlorodifluoromethane, CHClF2)


HCFC-31 (chlorofluoromethane, CH2ClF)


CFC-1113 (chlorotrifluoroethylene, CF2═CClF)


HFE-125 (trifluoromethyl-difluoromethyl ether, CF3OCHF2)


HFE-134a (trifluoromethyl-fluoromethyl ether, CF3OCH2F)


HFE-143a (trifluoromethyl-methyl ether, CF3OCH3)


HFE-227ea (trifluoromethyl-tetrafluoroethyl ether; CF3OCHFCF3)


FIFE-236fa (trifluoromethyl-trifluoroethyl ether, CF3OCH2CF3)


The refrigerant composition according to the present disclosure may contain one or more tracers at a total concentration of about 10 parts per million by weight (ppm) to about 1000 ppm, based on the entire refrigerant composition. The refrigerant composition according to the present disclosure may preferably contain one or more tracers at a total concentration of about 30 ppm to about 500 ppm, and more preferably about 50 ppm to about 300 ppm, based on the entire refrigerant composition.


(1-3-3) Ultraviolet Fluorescent Dye


The refrigerant composition according to the present disclosure may comprise a single ultraviolet fluorescent dye, or two or more ultraviolet fluorescent dyes.


The ultraviolet fluorescent dye is not limited, and can be suitably selected from commonly used ultraviolet fluorescent dyes.


Examples of ultraviolet fluorescent dyes include naphthalimide, coumarin, anthracene, phenanthrene, xanthene, thioxanthene, naphthoxanthene, fluorescein, and derivatives thereof. The ultraviolet fluorescent dye is particularly preferably either naphthalimide or coumarin, or both.


(1-3-4) Stabilizer


The refrigerant composition according to the present disclosure may comprise a single stabilizer, or two or more stabilizers.


The stabilizer is not limited, and can be suitably selected from commonly used stabilizers.


Examples of stabilizers include nitro compounds, ethers, and amines.


Examples of nitro compounds include aliphatic nitro compounds, such as nitromethane and nitroethane; and aromatic nitro compounds, such as nitro benzene and nitro styrene.


Examples of ethers include 1,4-dioxane.


Examples of amines include 2,2,3,3,3-pentafluoropropylamine and diphenylamine.


Examples of stabilizers also include butylhydroxyxylene and benzotriazole.


The content of the stabilizer is not limited. Generally, the content of the stabilizer is preferably 0.01 to 5 mass %, and more preferably 0.05 to 2 mass %, based on the entire refrigerant.


(1-3-5) Polymerization Inhibitor


The refrigerant composition according to the present disclosure may comprise a single polymerization inhibitor, or two or more polymerization inhibitors.


The polymerization inhibitor is not limited, and can be suitably selected from commonly used polymerization inhibitors.


Examples of polymerization inhibitors include 4-methoxy-1-naphthol, hydroquinone, hydroquinone methyl ether, dimethyl-t-butylphenol, 2,6-di-tert-butyl-p-cresol, and benzotriazole.


The content of the polymerization inhibitor is not limited. Generally, the content of the polymerization inhibitor is preferably 0.01 to 5 mass %, and more preferably 0.05 to 2 mass %, based on the entire refrigerant


(1-4) Refrigeration Oil-Containing Working Fluid


The refrigeration oil-containing working fluid according to the present disclosure comprises at least the refrigerant or refrigerant composition according to the present disclosure and a refrigeration oil, for use as a working fluid in a refrigerating machine. Specifically, the refrigeration oil-containing working fluid according to the present disclosure is obtained by mixing a refrigeration oil used in a compressor of a refrigerating machine with the refrigerant or the refrigerant composition. The refrigeration oil-containing working fluid generally comprises 10 to 50 mass % of refrigeration oil.


(1-4-1) Refrigerating Oil


The composition according to the present disclosure may comprise a single refrigeration oil, or two or more refrigeration oils.


The refrigeration oil is not limited, and can be suitably selected from commonly used refrigeration oils. In this case, refrigeration oils that are superior in the action of increasing the miscibility with the mixture and the stability of the mixture, for example, are suitably selected as necessary.


The base oil of the refrigeration oil is preferably, for example, at least one member selected from the group consisting of polyalkylene glycols (PAG), polyol esters (POE), and polyvinyl ethers (PVE).


The refrigeration oil may further contain additives in addition to the base oil. The additive may be at least one member selected from the group consisting of antioxidants, extreme-pressure agents, acid scavengers, oxygen scavengers, copper deactivators, rust inhibitors, oil agents, and antifoaming agents.


A refrigeration oil with a kinematic viscosity of 5 to 400 cSt at 40° C. is preferable from the standpoint of lubrication.


The refrigeration oil-containing working fluid according to the present disclosure may further optionally contain at least one additive. Examples of additives include compatibilizing agents described below.


(1-4-2) Compatibilizer


The refrigeration oil-containing working fluid according to the present disclosure may comprise a single compatibilizing agent, or two or more compatibilizing agents.


The compatibilizing agent is not limited, and can be suitably selected from commonly used compatibilizing agents.


Examples of compatibilizing agents include polyoxyalkylene glycol ethers, amides, nitriles, ketones, chlorocarbons, esters, lactones, aryl ethers, fluoroethers, and 1,1,1-trifluoroalkanes. The compatibilizing agent is particularly preferably a polyoxyalkylene glycol ether.


(1-5) Various Refrigerants 1


Refrigerants 1A to 1E used in the present disclosure are described below in detail. The disclosures of the refrigerant 1A, the refrigerant 1B, the refrigerant 1C, the refrigerant 1D and the refrigerant 1E are independent from each other. Thus, the alphabetical letters used for points and line segments, as well as the numbers used for Examples and Comparative Examples, are all independent in each of the refrigerant 1A, the refrigerant 1B, the refrigerant 1C, the refrigerant 1D and the refrigerant 1E. For example, Example 1 of the refrigerant 1A and Example 1 of the refrigerant 1B each represent an example according to a different embodiment.


(1-5-1) Refrigerant 1A


Refrigerant 1A according to the present disclosure is a mixed refrigerant comprising trans-1,2-difluoroethylene (HFO-1132(E)), trifluoroethylene (HFO-1123), and 2,3,3,3-tetrafluoro-1-propene (R1234yf).


The refrigerant 1A according to the present disclosure has various properties that are desirable as an R410A-alternative refrigerant, i.e., a refrigerating capacity and a coefficient of performance that are equivalent to those of R410A, and a sufficiently low GWP.


The refrigerant 1A according to the present disclosure is a composition comprising HFO-1132(E) and R1234yf, and optionally further comprising HFO-1123, and may further satisfy the following requirements. This refrigerant 1A also has various properties desirable as an alternative refrigerant for R410A; i.e., it has a refrigerating capacity and a coefficient of performance that are equivalent to those of R410A, and a sufficiently low GWP.


Requirements


When the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum is respectively represented by x, y, and z,

    • coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments OD, DG, GH, and HO that connect the following 4 points:


      point D (87.6, 0.0, 12.4),


      point G (18.2, 55.1, 26.7),


      point H (56.7, 43.3, 0.0), and


      point O (100.0, 0.0, 0.0),


      or on the line segments OD, DG, and GH (excluding the points O and H);
    • the line segment DG is represented by coordinates (0.0047y2−1.5177y+87.598, y, −0.0047y2+0.5177y+12.402),
    • the line segment GH is represented by coordinates (−0.0134z2−1.0825z+56.692, 0.0134z2+0.0825z+43:308, z), and
    • the lines HO and OD are straight lines.


      When the requirements above are satisfied, the refrigerant 1A according to the present disclosure has a refrigerating capacity ratio of 92.5% or more relative to that of R410A, and a COP ratio of 92.5% or more relative to that of R410A.


The refrigerant 1A according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments LG, GH, HI, and IL that connect the following 4 points:


      point L (72.5, 10.2, 17.3),


      point G (18.2, 55.1, 26.7),


      point H (56.7, 43.3, 0.0), and


      point I (72.5, 27.5, 0.0),


      or on the line segments LG, GH, and IL (excluding the points H and I);
    • the line segment LG is represented by coordinates (0.0047y2−1.5177y+87.598, y, −0.0047y2+0.5177y+12.402),
    • the line segment GH is represented by coordinates (−0.0134z2−1.0825z+56.692, 0.0134z2+0.0825z+43.308, z), and
    • the line segments HI and IL are straight lines.


      When the requirements above are satisfied, the refrigerant 1A according to the present disclosure has a refrigerating capacity ratio of 92.5% or more relative to that of R410A, and a COP ratio of 92.5% or more relative to that of R410A; furthermore, the refrigerant has a lower flammability (Class 2L) according to the ASHRAE standard.


The refrigerant 1A according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments OD, DE, EF, and FO that connect the following 4 points:


      point D (87.6, 0.0, 12.4),


      point E (31.1, 42.9, 26.0),


      point F (65.5, 34.5, 0.0), and


      point O (100.0, 0.0, 0.0).


      or on the line segments OD, DE, and EF (excluding the points O and F);
    • the line segment DE is represented by coordinates (0.0047y2−1.5177y+87.598, y, −0.0047y2+0.5177y+12.402),
    • the line segment EF is represented by coordinates (−0.0064z2−1.1565z+65.501, 0.0064z2+0.1565z+34.499, z), and
    • the line segments FO and OD are straight lines.


When the requirements above are satisfied, the refrigerant 1A according to the present disclosure has a refrigerating capacity ratio of 93.5% or more relative to that of R410A, and a COP ratio of 93.5% or more relative to that of R410A.


The refrigerant 1A according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum is respectively represented by x, y, and z,
    • coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments LE, EF, FI, and IL that connect the following 4 points:


      point L (72.5, 10.2, 17.3),


      point E (31.1, 42.9, 26.0),


      point F (65.5, 34.5, 0.0), and


      point I (72.5, 27.5, 0.0),


      or on the line segments LE, EF, and IL (excluding the points F and I);
    • the line segment LE is represented by coordinates (0.0047y2−1.5177y+87.598, y, −0.0047y2+0.5177y+12.402),
    • the line segment EF is represented by coordinates (−0.0134z2−1.0825z+56.692, 0.0134z2+0.0825z+43.308, z), and
    • the line segments FI and IL are straight lines.


      When the requirements above are satisfied, the refrigerant 1A according to the present disclosure has a refrigerating capacity ratio of 93.5% or more relative to that of R410A, and a COP ratio of 93.5% or more relative to that of R410A; furthermore, the refrigerant has a lower flammability (Class 2L) according to the ASHRAE standard.


The refrigerant 1A according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum is respectively represented by x, y, and z,
    • coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within a figure surrounded by line segments OA, AB, BC, and CO that connect the following 4 points:


      point A (93.4, 0.0, 6.6),


      point B (55.6, 26.6, 17.8),


      point C (77.6, 22.4, 0.0), and


      point O (100.0, 0.0, 0.0),


      or on the line segments OA, AB, and BC (excluding the points O and C);
    • the line segment AB is represented by coordinates (0.0052y2−1.5588y+93.385, y, −0.0052y2+0.5588y+6.615),
    • the line segment BC is represented by coordinates (−0.0032z2−1.1791z+77.593, 0.0032z2+0.1791z+22.407, z), and
    • the line segments CO and OA are straight lines.


      When the requirements above are satisfied, the refrigerant 1A according to the present disclosure has a refrigerating capacity ratio of 95% or, more relative to that of R410A, and a COP ratio of 95% or more relative to that of R410A.


The refrigerant 1A according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum is respectively represented by x, y, and z,
    • coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within a figure surrounded by line segments KB, BJ, and JK that connect the following 3 points:


      point K (72.5, 14.1, 13.4),


      point B (55.6, 26.6, 17.8), and


      point J (72.5, 23.2, 4.3),


      or on the line segments KB, BJ, and JK;
    • the line segment KB is represented by coordinates (0.0052y2−1.5588y+93.385, y, and −0.0052y2+0.5588y+6.615),
    • the line segment BJ is represented by coordinates (−0.0032z2−1.1791z+77.593, 0.0032z2+0.1791 z+22.407, z), and
    • the line segment JK is a straight line.


      When the requirements above are satisfied, the refrigerant 1A according to the present disclosure has a refrigerating capacity ratio of 95% or more relative to that of R410A, and a COP ratio of 95% or more relative to that of R410A; furthermore, the refrigerant has a lower flammability (Class 2L) according to the ASHRAE standard.


The refrigerant 1A according to the present disclosure may further comprise difluoromethane (R32) in addition to HFO-1132(E), HFO-1123, and R1234yf as long as the above properties and effects are not impaired. The content of R32 based on the entire refrigerant 1A according to the present disclosure is not limited and can be selected from a wide range. For example, when the R32 content of the refrigerant 1A according to the present disclosure is 21.8 mass %, the mixed refrigerant has a GWP of 150. Therefore, the R32 content can be 21.8 mass % or less. The R32 content of the refrigerant 1A according to the present disclosure may be, for example, 5 mass % or more, based on the entire refrigerant.


When the refrigerant 1A according to the present disclosure further contains R32 in addition to HFO-1132(E), HFO-1123, and R1234yf, the refrigerant may be a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, R1234yf, and R32 based on their sum is respectively represented by x, y, z, and a,
    • if 0<a≤10.0, coordinates (x,y,z) in a ternary composition diagram (FIGS. 1C to 1I) in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure surrounded by straight lines that connect the following 4 points:


      point A (0.02a2−2.46a+93.4, 0, −0.02a2+2.46a+6.6),


      point B′(−0.008a2−1.38a+56, 0.018a2−0.53a+26.3, −0.01a2+1.91a+17.7),


      point C (−0.016a2+1.02a+77.6, 0.016a2−1.02a+22.4, 0), and


      point O (100.0, 0.0, 0.0),


      or on the straight lines OA, AB′, and B′C (excluding the points O and C);
    • if 10.0<a≤16.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines that connect the following 4 points:


      point A (0.0244a2−2.5695a+94.056, 0, −0.0244a2+2.5695a+5.944), point B′ (0.1161a2−1.9959a+59.749, 0.014a2−0.3399a+24.8, −0.1301a2+2.3358a+15.451),


      point C (−0.0161a2+1.02a+77.6, 0.0161a2−1.02a+22.4, 0), and


      point O (100.0, 0.0, 0.0),


      or on the straight lines OA, AB′, and B′C (excluding the points O and C); or
    • if 16.5<a≤1.8, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines that connect the following 4 points:


      point A (0.0161a2−2.3535a+92.742, 0, −0.0161a2+2.3535a+7.258), point B′(−0.0435a2−0.0435a+50.406, −0.0304a2+1.8991a−0.0661, 0.0739a2−1.8556a+49.6601),


      point C (−0.0161a2+0.9959a+77.851, 0.0161a2−0.9959a+22.149, 0), and


      point O (100.0, 0.0, 0.0),


      or on the straight lines OA, AB′, and B′C (excluding the points O and C).


      Note that when point B in the ternary composition diagram is defined as a point where a refrigerating capacity ratio of 95% relative to that of R410A and a COP ratio of 95% relative to that of R410A are both achieved, point B′ is the intersection of straight line AB and an approximate line formed by connecting the points where the COP ratio relative to that of R410A is 95%. When the requirements above are satisfied, the refrigerant 1A according to the present disclosure has a refrigerating capacity ratio of 95% or more relative to that of R410A, and a COP ratio of 95% or more relative to that of R410A.


The refrigerant 1A according to the present disclosure may further comprise other additional refrigerants in addition to HFO-1132(E), HFO-1123, R1234yf, and R32 as long as the above properties and effects are not impaired. In this respect, the refrigerant 1A according to the present disclosure preferably comprises HFO-1132(E), HFO-1123, R1234yf, and R32 in a total amount of 99.5 mass % or more, more preferably 99.75 mass % or more, and still more preferably 99.9 mass % or more, based on the entire refrigerant 1A.


The refrigerant 1A according to the present disclosure may comprise HFO-1132(E), HFO-1123, and R1234yf in a total amount of 99.5 mass % or more, 99.75 mass % or more, or 99.9 mass % or more, based on the entire refrigerant 1A.


The refrigerant 1A according to the present disclosure may comprise HFO-1132(E), HFO1123, R1234yf, and R32 in a total amount of 99.5 mass % or more, 99.75 mass % or more, or 99.9 mass % or more, based on the entire refrigerant 1A.


The additional refrigerants are not limited, and can be selected from a wide range of refrigerants. The mixed refrigerant may comprise a single additional refrigerant, or two or more additional refrigerants.


The refrigerant 1A according to the present disclosure is suitable for use as an alternative refrigerant for R410A.


Examples of Refrigerant 1A

The refrigerant 1A is described in more detail below with reference to Examples. However, the refrigerant 1A according to the present disclosure is not limited to the Examples.


Mixed refrigerants were prepared by mixing HFO-1132(E), HFO-1123, and R1234yf at mass % based on their sum shown in Tables 1 to 5.


The COP ratio and the refrigerating capacity ratio of the mixed refrigerants relative to those of R410 were determined. The conditions for calculation were as described below.


Evaporating temperature: 5° C.


Condensation temperature: 45° C.


Degree of superheating: 1 K


Degree of subcooling: 5 K


Ecomp (compressive modulus): 0.7 kWh


Tables 1 to 5 show these values together with the GWP of each mixed refrigerant.

















TABLE 1







Comp.
Example




Example




Ex.
1
Example
Example
Example
Example
6


Item
Unit
1
A
2
3
4
5
B























HFO-1132(E)
mass %
R410A
93.4
85.7
78.3
71.2
64.3
55.6


HFO-1123
mass %

0.0
5.0
10.0
15.0
20.0
26.6


R1234yf
mass %

6.6
9.3
11.7
13.8
15.7
17.8


GWP

2088
1
1
1
1
1
2


COP ratio
% (relative
100
98.0
97.5
96.9
96.3
95.8
95.0



to R410A)









Refrigerating
% (relative
100
95.0
95.0
95.0
95.0
95.0
95.0


capacity ratio
to R410A)





















TABLE 2







Comp.







Ex. 2
Example
Example
Example


Item
Unit
C
7
8
9




















HTO-1132(E)
mass %
77.6
71..6
65.5
59.2


HFO-1123
mass %
22.4
23.4
24.5
25.8


R1234yf
mass %
0.0
5.0
10.0
15.0


GWP

1
1
1
1


COP ratio
%
95.0
95.0
95.0
95.0



(relative







to R410A)






Refrigerating
%
102.5
100.5
98.4
96.3


capacity
(relative






ratio
to R410A)
























TABLE 3







Example





Example




10
Example
Example
Example
Example
Example
16


Item
Unit
D
11
12
13
14
15
G























HFO-1132(E)
mass %
87.6
72.9
59.1
46.3
34.4
23.5
18.2


HFO-1123
mass %
0.0
10.0
20.0
30.0
40.0
50.0
55.1


R1234yf
mass %
12.4
17.1
20.9
23.7
25.6
26.5
26.7


GWP

1
2
2
2
2
2
2


COP ratio
% (relative
98.2
97.1
95.9
94.8
93.8
92.9
92.5



to R410A)









Refrigerating
% (relative
92.5
92.5
92.5
92.5
92.5
92.5
92.5


capacity ratio
to R410A)
























TABLE 4







Comp.


Comp.


Example




Ex. 3
Example
Example
Ex. 4
Example
Example
21


Item
Unit
H
17
18
F
19
20
E























HFO-1132(E)
mass %
56.7
44.5
29.7
65.5
53.3
39.8
31.1


HFO-1123
mass %
43.3
45.5
50.3
34.5
36.7
40.2
42.9


R1234yf
mass %
0.0
10.0
20.0
0.0
10.0
20.0
26.0


GWP

1
1
2
1
1
2
2


COP ratio
% (relative
92.5
92.5
92.5
93.5
93.5
93.5
93.5



to R410A)









Refrigerating
% (relative
105.8
101.2
96.2
104.5
100.2
95.5
92.5


capacity ratio
to R410A)






















TABLE 5







Comp.
Example
Example
Example
Comp.




Ex. 5
22
23
24
Ex. 6


Item
Unit
I
J
K
L
M





















HFO-1132(E)
mass %
72.5
72.5
72.5
72.5
72.5


HFO-1123
mass %
27.5
23.2
14.1
10.2
0.0


R1234yf
mass %
0.0
4.3
13.4
17.3
27.5


GWP

1
1
1
2
2


COP ratio
% (relative
94.4
95.0
96.4
97.1
98.8



to R410A)







Refrigerating
% (relative
103.5
100.8
95.0
92.5
85.7


capacity ratio
to R410A)









These results indicate that under the condition that the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum is respectively represented by x, y, and z, when coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure (FIG. 1B) surrounded by line segments OD, DG, GH, and HO that connect the following 4 points:


point D (87.6, 0.0, 12.4),


point G (18.2, 55.1, 26.7),


point H (56.7, 43.3, 0.0), and


point O (100.0, 0.0, 0.0),


or on the line segments OD, DG, and GH (excluding the points O and H), the refrigerant has a refrigerating capacity ratio of 92.5% or more relative to that of R410A, and a COP ratio of 92.5% or more relative to that of R410A.


Likewise, the results indicate that when coordinates (x,y,z) are within the range of a figure (FIG. 1B) surrounded by line segments OD, DE, EF, and FO that connect the following 4 points:


point D (87.6, 0.0, 12.4),


point E (31.1, 42.9, 26.0),


point F (65.5, 34.5, 0.0), and


point O (100.0, 0.0, 0.0),


or on the line segments OD, DE, and EF (excluding the points O and F), the refrigerant has a refrigerating capacity ratio of 93.5% or more relative to that of R410A, and a COP ratio of 93.5% or more relative to that of R410A.


Likewise, the results indicate that when coordinates (x,y,z) are within the range of a figure (FIG. 1B) surrounded by line segments OA, AB, BC, and CO that connect the following 4 points:


point (93.4, 0.0, 6.6),


point B (55.6, 26.6, 17.8),


point C (77.6, 22.4, 0.0), and


point O (100.0, 0.0, 0.0),


or on the line segments OA, AB, and BC (excluding the points O and C), the refrigerant has a refrigerating capacity ratio of 95% or more relative to that of R410A, and a COP ratio of 95% or more relative to that of R410A.


R1234yf contributes to reduction of flammability and reduction of deterioration of polymerization etc. in these compositions. Therefore, the composition according to the present disclosure preferably contains R1234yf.


Further, the burning velocity of these mixed refrigerants was measured according to the ANSI/ASHRAE Standard 34-2013. Compositions that showed a burning velocity of 10 cm/s or less were determined to be Class 2L (lower flammability). These results clearly indicate that when the content of HFO-1132(E) in a mixed refrigerant of HFO-1132(E), HFO-1123, and R1234yf is 72.5 mass % or less based on their sum, the refrigerant can be determined to be Class 2L (lower flammability).


A burning velocity test was performed using the apparatus shown in FIG. 1A in the following manner. First, the mixed refrigerants used had a purity of 99.5% or more, and were degassed by repeating a cycle of freezing, pumping, and thawing until no traces of air were observed on the vacuum gauge. The burning velocity was measured by the closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between the electrodes in the center of a sample cell. The duration of the discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of the flame was visualized using schlieren photographs. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light transmission acrylic windows was used as the sample cell, and a xenon lamp was used as the light source. Schlieren images of the flame were recorded by a high-speed digital video camera at a frame rate of 600 fps and stored on a PC.


Mixed refrigerants were prepared by mixing HFO-1132(E), HFO-1123, R1234yf, and R32 in amounts shown in Tables 6 to 12, in terms of mass %, based on their sum.


The COP ratio and the refrigerating capacity ratio of these mixed refrigerants relative to those of R410A were determined. The calculation conditions were the same as described above. Tables 6 to 12 show these values together with the GWP of each mixed refrigerant.



















TABLE 6








Comp.


Example
Comp.


Comp.




Comp.
Ex. 7
Comp.
Comp.
25
Ex. 10
Example
Example
Ex. 11


Item
Unit
Ex. 1
A
Ex. 8
Ex. 9
B′
B
26
27
C

























HFO-
mass %
R410A
93.4
78.3
64.3
56.0
55.6
60.0
70.0
77.6


1132(E)












HFO-1123
mass %

0.0
10.0
20.0
26.3
26.6
25.6
23.7
22.4


R1234yf
mass %

6.6
11.7
15.7
17.7
17.8
14.4
6.3
0.0


R32
mass %

0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

2088
1
1.4
1.5
1.5
1.5
1.4
1.2
1.0


COP ratio
% (relative
100
98.0
96.9
95.8
95.0
95.0
95.0
95.0
95.0



to R410A)











Refrigerating
% (relative
100
95.0
95.0
95.0
95.0
95.0
96.5
100.0
102.5


capacity ratio
to R410A)

























TABLE 7







Comp.


Example
Comp.


Comp.




Ex. 12
Comp.
Comp.
28
Ex. 15
Example
Example
Ex. 16


Item
Unit
A
Ex. 13
Ex. 14
B′
B
29
30
C
























HFO-1132(E)
mass %
81.6
67.3
53.9
48.9
47.2
60.0
70.0
77.3


HFO-1123
mass %
0.0
10.0
20.0
24.1
25.3
21.6
19.2
17.7


R1234yf
mass %
13.4
17.7
21.1
22.0
22.5
13.4
5.8
0.0


R32
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

35
35
35
35
35
35
35
35


COP ratio
% (relative
97.6
96.6
95.5
95.0
95.0
95.0
95.0
95.0



to R410A)










Refrigerating
% (relative
95.0
95.0
95.0
104.4
95.0
99.0
102.1
104.4


capacity ratio
to R410A)

























TABLE 8







Comp.
Comp.
Comp.
Example
Comp.


Comp.




Ex. 17
Ex.
Ex.
31
Ex. 20
Example
Example
Ex. 21


Item
Unit
A
18
19
B′
B
32
33
C
























HFO-1132(E)
mass %
70.8
57.2
44.5
41.4
36.4
60.0
70.0
76.2


HFO-1123
mass %
0.0
10.0
20.0
22.8
26.7
18.0
15.3
13.8


R1234yf
mass %
19.2
22.8
25.5
25.8
26.9
12.0
4.7
0.0


R32
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


GWP

69
69
69
69
69
69
69
68


COP ratio
% (relative
97.4
96.5
95.6
95.0
95.0
95.0
95.0
95.0



to R410A)










Refrigerating
% (relative
95.0
95.0
95.0
106.2
95.0
101.5
104.4
106.2


capacity ratio
to R410A)

























TABLE 9







Comp.


Example
Comp.


Comp.




Ex. 22
Comp.
Comp.
34
Ex. 25
Example
Example
Ex. 26


Item
Unit
A
Ex. 23
Ex. 24
B′
B
35
36
C
























HFO-1132(E)
mass %
62.3
49.3
37.1
34.5
24.9
60.0
70.0
74.5


HFO-1123
mass %
0.0
10.0
20.0
22.8
30.7
15.4
12.4
11.2


R1234yf
mass %
23.4
26.4
28.6
28.4
30.1
10.3
3.3
0.0


R32
mass %
14.3
14.3
14.3
14.3
14.3
14.3
14.3
14.3


GWP

98
98
98
98
98
98
97
97


COP ratio
% (relative
97.3
96.5
95.7
95.5
95.0
95.0
95.0
95.0



to R410A)










Refrigerating
% (relative
95.0
95.0
95.0
95.4
95.0
103.7
106.5
107.7


capacity ratio
to R410A)

























TABLE 10







Comp.


Example
Comp.


Comp.




Ex. 27
Comp.
Comp.
37
Ex. 30
Example
Example
Ex. 31


Item
Unit
A
Ex. 28
Ex. 29
B′
B
38
39
C
























HFO-1132(E)
mass %
58.3
45.5
33.5
31.2
16.5
60.0
70.0
73.4


HFO-1123
mass %
0.0
10.0
20.0
23.0
35.5
14.2
11.1
10.1


R1234yf
mass %
25.2
28.0
30.0
29.3
31.5
9.3
2.4
0.0


R32
mass %
16.5
16.5
16.5
16.5
16.5
16.5
16.5
16.5


GWP

113.0
113.1
113.1
113.1
113.2
112.5
112.3
112.2


COP ratio
% (relative
97.4
96.6
95.9
95.6
95.0
95.0
95.0
95.0



to R410A)










Refrigerating
% (relative
95.0
95.0
95.0
95.7
95.0
104.9
107.6
108.5


capacity ratio
to R410A)

























TABLE 11







Comp.


Example
Comp.


Comp.




Ex. 32
Comp.
Comp.
40
Ex. 35
Example
Example
Ex. 36


Item
Unit
A
Ex. 33
Ex. 34
B′
B
41
42
C
























HFO-1132(E)
mass %
53.5
41.0
29.3
25.8
0.0
50.0
60.0
71.7


HFO-1123
mass %
0.0
10.0
20.0
25.2
48.8
16.8
12.9
9.1


R1234yf
mass %
27.3
29.8
31.5
29.8
32.0
14.0
7.9
0.0


R32
mass %
19.2
19.2
19.2
19.2
19.2
19.2
19.2
19.2


GWP

131.2
131.3
131.4
131.3
131.4
130.8
130.6
130.4


COP ratio
% (relative
97.4
96.7
96.1
97.8
95.0
95.0
95.0
95.0



to R410A)










Refrigerating
% (relative
95.0
95.0
95.0
96.3
95.0
104.0
106.4
109.4


capacity ratio
to R410A)

























TABLE 12







Comp.


Example
Comp.


Comp. Ex.




Ex. 37
Comp.
Comp.
43
Ex. 40
Example
Example
41


Item
Unit
A
Ex. 38
Ex. 39
B′
B
44
45
C
























HFO-1132(E)
mass %
49.1
36.9
25.5
20.0
0.0
50.0
60.0
69.7


HFO-1123
mass %
0.0
10.0
20.0
26.9
45.3
15.8
11.9
8.5


R1234yf
mass %
29.1
31.3
20.0
31.3
32.9
12.4
6.3
0.0


R32
mass %
21.8
21.8
21.8
21.8
21.8
21.8
21.8
21.8


GWP

148.8
148.9
148.9
148.9
148.9
148.3
148.1
147.9


COP ratio
% (relative
97.6
96.9
96.4
95.9
95.5
95.0
95.0
95.0



to R410A)










Refrigerating
% (relative
95.0
95.0
95.0
98.4
95.0
105.6
108.0
110.3


capacity ratio
to R410A)









These results indicate that the refrigerants according to the present disclosure that satisfy the following conditions have a refrigerating capacity ratio of 95% or more relative to that of R410A, and a COP ratio of 95% or more relative to that of R410A:

    • when the mass % of HFO-1132(E), HFO-1123, R1234yf, and R32 based on their sum is respectively represented by x, y, z, and a,
    • if 0<a≤10.0, coordinates (x,y,z) in a ternary composition diagram (FIGS. 1C to 1I) in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass % are within the range of a figure surrounded by straight lines that connect the following 4 points:


      point A (0.02a2−2.46a+93.4, 0, −0.02a2+2.46a+6.6),


      point B′(−0.008a2−1.38a+56, 0.018a2−0.53a+26.3, −0.01a2+1.91a+17.7),


      point C (−0.016a2+1.02a+77.6, 0.016a2−1.02a+22.4, 0), and


      point O (100.0, 0.0, 0.0),


      or on the straight lines OA, AB′, and B′C (excluding the points O and C);
    • if 10.0<a≤16.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines that connect the following 4 points:


      point A (0.0244a2−2.5695a+94.056, 0, −0.0244a2+2.5695a+5.944), point B′(0.1161a2−1.9959a+59.749, 0.014a2−0.3399a+24.8, −0.1301a2+2.3358a+15.451),


      point C (−0.0161a2+1.02a+77.6, 0.0161a2−1.02a+22.4, 0), and


      point O (100.0, 0.0, 0.0), or on the straight lines OA, AB′, and B′C (excluding the points O and C); or if 16.5<a≤21.8, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines that connect the following 4 points:


      point A (0.0161a2−2.3535a+92.742, 0, −0.0161a2+2.3535a+7.258), point B′(−0.0435a2−0.0435a+50.406, −0.0304a2+1.8991a−0.0661, 0.0739a2−1.8556a+49.6601),


      point C (−0.0161a2+0.9959a+77.851, 0.0161a2−0.9959a+22.149, 0), and


      point O (100.0, 0.0, 0.0),


      or on the straight lines OA, AB′, and B′C (excluding the points O and C).



FIGS. 1C to 1I show compositions whose R32 content a (mass %) is 0 mass %, 5 mass %, 10 mass %, 14.3 mass %, 16.5 mass %, 19.2 mass %, and 21.8 mass %, respectively.


Note that when point B in the ternary composition diagram is defined as a point where a refrigerating capacity ratio of 95% relative to that of R410A and a COP ratio of 95% relative to that of R410A are both achieved, point B′ is the intersection of straight line AB and an approximate line formed by connecting three points, including point C, where the COP ratio relative to that of R410A is 95%.


Points A, B′, and C were individually obtained by approximate calculation in the following manner.


Point A is a point where the HFO-1123 content is 0 mass % and a refrigerating capacity ratio of 95% relative to that of R410A is achieved. Three points corresponding to point A were obtained in each of the following three ranges by calculation, and their approximate expressions were obtained.












TABLE 13





Item
10.0 ≥ R32 ≥ 0
16.5 ≥ R32 ≥10.0
21.8 ≥ R32 ≥ 16.5
























R32
0.0
5.0
10.0
10.0
14.3
16.5
16.5
19.2
21.8


HFO-1132(E)
93.4
81.6
70.8
70.8
62.3
58.3
58.3
53.5
49.1


HFO-1123
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R1234yf
6.6
13.4
19.2
19.2
23.4
25.2
25.2
27.3
29.1










R32
x
x
x


HFO-1132(E)
0.02x2 − 2.46x + 93.4
0.0244x2 − 2.5695x + 94.056
0.0161x2 − 2.3535x + 92.742


approximate





expression





HFO-1123
0
0
0


approximate





expression





R1234yf
100-R32-HFO-1132(E)
100-R32-HFO-1132(E)
100-R32-HFO-1132(E)


approximate





expression









Point C is a point where the R1234yf content is 0 mass % and a COP ratio of 95% relative to that of R410A is achieved. Three points corresponding to point C were obtained in each of the following three ranges by calculation, and their approximate expressions were obtained.












TABLE 14





Item
10.0 ≥ R32 ≥ 0
16.5 ≥ R32 ≥10.0
21.8 ≥ R32 ≥ 16.5
























R32
0
5
10
10
14.3
16.5
16.5
19.2
21.8


HFO-1132(E)
77.6
77.3
76.2
76.2
74.5
73.4
73.4
71.7
69.7


HFO-1123
22.4
17.7
13.8
13.8
11.2
10.1
10.1
9.1
8.5


R1234yf
0
0
0
0
0
0
0
0
0










R32
x
x
x


HFO-1132(E)
100-R32HFO-1123
100-R32HFO-1123
100-R32HFO-1123


approximate





expression





HFO-1123
0.016x2 − 1.02x + 22.4
0.0161x2 − 0.9959x + 22.149
0.0161*2 − 0.9959* + 22.149


approximate





expression





R1234yf
100-R32-HFO-1132(E)
100-R32-HFO-1132(E)
100-R32-HFO-1132(E)


approximate





expression









Three points corresponding to point B′ were obtained in each of the following three ranges by calculation, and their approximate expressions were obtained.












TABLE 15





Item
10.0 ≥ R32 ≥ 0
16.5 ≥ R32 ≥10.0
21.8 ≥ R32 ≥ 16.5
























R32
0
5
10
10
14.3
16.5
16.5
19.2
21.8


HFO-1132(E)
56
48.9
41.4
41.4
34.5
31.2
31.2
25.8
20


HFO-1123
26.3
24.1
22.8
22.8
22.8
23
23
25.2
26.9


R1234yf
17.7
22
25.8
25.8
28.4
29.3
29.3
29.8
31.3










R32
x
x
x


HFO-1132(E)
−0.008*2 − 1.38*56
0.0161x2 − 1.9959x + 59.749
−0.0435x2 − 0.4456x + 50.406


approximate





expression





HFO-1123
0.018x2 − 0.53x + 26.3
0.014x2 − 0.3399x + 24.8
−0.0304*2 + 1.8991* − 0.0661


approximate





expression





R1234yf
100-R32-HFO-1132(E)
100-R32-HFO-1132(E)
100-R32-HFO-1132(E)


approximate





expression










(1-5-2) Refrigerant 1B


Refrigerant 1B according to the present disclosure is a mixed refrigerant comprising HFO-1132(E) and HFO-1123 in a total amount of 99.5 mass % or more based on the entire refrigerant 1B, and the refrigerant 1B comprising 62.5 mass % to 72.5 mass % of HFO-1132(E) based on the entire refrigerant 1B.


The refrigerant 1B according to the present disclosure has various properties that are desirable as an R410A-alternative refrigerant, i.e., (1) a coefficient of performance equivalent to that of R410A, (2) a refrigerating capacity equivalent to that of R410A, (3) a sufficiently low GWP, and (4) a lower flammability (Class 2L) according to the ASHRAE standard.


The refrigerant 1B according to the present disclosure is particularly preferably a mixed refrigerant comprising 72.5 mass % or less of HFO-1132(E), because it has a lower flammability (Class 2L) according to the ASHRAE standard.


The refrigerant 1B according to the present disclosure is more preferably a mixed refrigerant comprising 62.5 mass % or more of HFO-1132(E). In this case, the refrigerant 1B according to the present disclosure has a superior coefficient of performance relative to that of R410A, the polymerization reaction of HFO-1132(E) and/or HFO-1123 is further suppressed, and the stability is further improved.


The refrigerant 1B according to the present disclosure may further comprise other additional refrigerants in addition to HFO-1132(E) and HFO-1123, as long as the above properties and effects are not impaired. In this respect, the refrigerant 1B according to the present disclosure preferably comprises HFO-1132(E) and HFO-1.123 in a total amount of 99.75 mass % or more, and more preferably 99.9 mass % or more, based on the entire refrigerant 1B.


Such additional refrigerants are not limited, and can be selected from a wide range of refrigerants. The mixed refrigerant may comprise a single additional refrigerant, or two or more additional refrigerants.


The refrigerant 1B according to the present disclosure is suitable for use as an alternative refrigerant for HFC refrigerants, such as R410A, R407C, and R404A, as well as for HCFC refrigerants, such as R22.


Examples of Refrigerant 1B

The refrigerant 1B is described in more detail below with reference to Examples. However, the refrigerant 1B according to the present disclosure is not limited to the Examples.


Mixed refrigerants were prepared by mixing HFO-1132(E) and HFO-1123 at mass % based on their sum shown in Tables 16 and 17.


The GWP of compositions each comprising a mixture of R410A (R32=50%/R125=50%) was evaluated based on the values stated in the Intergovernmental Panel on Climate Change (IPCC), fourth report. The GWP of HFO-1132(E), which was not stated therein, was assumed to be 1 from HFO-1132a (GWP=1 or less) and HFO-1123 (GWP=0.3, described in PTL 1). The refrigerating capacity of compositions each comprising R410A and a mixture of HFO-1132(E) and HFO-1123 was determined by performing theoretical refrigeration cycle calculations for the mixed refrigerants using the National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0) under the following conditions.


Evaporating temperature: 5° C.


Condensation temperature: 45° C.


Superheating temperature: 1 K


Subcooling temperature: 5 K.


Compressor efficiency: 70%


Tables 1 and 2 show GWP, COP, and refrigerating capacity, which were calculated based on these results. The COP and refrigerating capacity are ratios relative to R410A.


The coefficient of performance (COP) was determined by the following formula.

COP=(refrigerating capacity or heating capacity)/power consumption


For the flammability, the burning velocity was measured according to the ANSI/ASHRAE Standard 34-2013. Compositions having a burning velocity of 10 cm/s or less were determined to be “Class 2L (lower flammability).”


A burning velocity test was performed using the apparatus shown in FIG. 1A in the following manner. First, the mixed refrigerants used had a purity of 99.5% or more, and were degassed by repeating a cycle of freezing, pumping, and thawing until no traces of air were observed on the vacuum gauge. The burning velocity was measured by the closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between the electrodes in the center of a sample cell. The duration of the discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of the flame was visualized using schlieren photographs. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light transmission acrylic windows was used as the sample cell, and a xenon lamp was used as the light source. Schlieren images of the flame were recorded by a high-speed digital video camera at a frame rate of 600 fps and stored on a PC.
















TABLE 16







Comp. Ex. 1
Comp. Ex. 2






Item
Unit
R410A
HFO-1132E
Comp. Ex. 3
Example 1
Example 2
Example 3






















HFO-1132E
mass %
0
100
80
72.5
70
67.5


HFO-1123
mass %
0
0
20
27.5
30
32.5


GWP

2088
1
1
1
1
1


COP ratio
% (relative
100
98
95.3
94.4
94.1
93.8



to R410A)








Refrigerating
% (relative
100
98
102.1
103.5
103.9
104.3


capacity ratio
to R410A)








Discharge
MPa
2.7
2.7
2.9
3.0
3.0
3.1


pressure









Burning
cm/sec
Non-
20
13
10
9
9 or less


velocity

flammable























TABLE 17












Comp. Ex. 7


Item
Unit
Example 4
Example 5
Comp. Ex. 4
Comp. Ex. 5
Comp. Ex. 6
HFO-1123






















HFO-1132E
mass %
65
62.5
60
50
25
0


HFO-1123
mass %
35
37.5
40
50
75
100


GWP

1
1
1
1
1
1


COP ratio
% (relative
93.5
93.2
92.9
91.8
89.9
89.9



to R410A)








Refrigerating
% (relative
104.7
105.0
105.4
106.6
108.1
107.0


capacity ratio
to R410A)








Discharge
MPa
3.1
3.1
3.1
3.2
3.4
3.4


pressure









Burning
cm/sec
9 or less
9 or less
9 or less
9 or less
9 or less
5


velocity









The compositions each comprising 62.5 mass % to 72.5 mass % of HFO-1132(E) based on the entire composition are stable while having a low GWP (GWP=1), and they ensure ASHRAE 2L flammability. Further, surprisingly, they can ensure performance equivalent to that of R410A.


(1-5-3) Refrigerant 1C


(5-3) Refrigerant 1C


Refrigerant 1C according to the present disclosure is a mixed refrigerant comprising HFO-1132(E), R32, and 2,3,3,3-tetrafluoro-1-propene (R1234yf).


The refrigerant 1C according to the present disclosure has various properties that are desirable as an R410A-alternative refrigerant; i.e., a refrigerating capacity equivalent to that of R410A, a sufficiently low GWP, and a lower flammability (Class 2L) according to the ASHRAE standard.


The refrigerant 1C according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), R32, and R1234yf based on their sum is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments AC, CF, FD, and DA that connect the following 4 points:


      point A (71.1, 0.0, 28.9),


      point C (36.5, 18.2, 45.3),


      point F (47.6, 18.3, 34.1), and


      point D (72.0, 0.0, 28.0),


      or on these line segments;
    • the line segment AC is represented by coordinates (0.0181y2−2.2288y+71.096, y, −0.0181y2+1.2288y+28.904),
    • the line segment FD is represented by coordinates (0.02y2−1.7y+72, y, −0.02y2+0.7y+28), and
    • the line segments CF and DA are straight lines. When the requirements above are satisfied, the refrigerant 1C according to the present disclosure has a refrigerating capacity ratio of 85% or more relative to that of R410A, a GWP of 125 or less, and a lower flammability (Class 2L) according to the ASHRAE standard.


The refrigerant 1C according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), R32, and R1234yf based on their sum is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments AB, BE, ED, and DA that connect the following 4 points:


      point A (71.1, 0.0, 28.9),


      point B (42.6, 14.5, 42.9),


      point E (51.4, 14.6, 34.0), and


      point D (72.0, 0.0, 28.0),


      or on these line segments;
    • the line segment AB is represented by coordinates (0.0181y2−2.2288y+71.096, y, −0.0181y2+1.2288y+28.904),
    • the line segment ED is represented by coordinates (0.02y2−1.7y+72, y, −0.02y2+0.7y+28), and
    • the line segments BE and DA are straight lines. When the requirements above are satisfied, the refrigerant 1C according to the present disclosure has a refrigerating capacity ratio of 85% or more relative to that of R410A, a GWP of 100 or less, and a lower flammability (Class 2L) according to the ASHRAE standard.


The refrigerant 1C according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), R32, and R1234yf based on their sum is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of WO-1132(E), R32, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments GI, IJ, and JG that connect the following 3 points:


      point G (77.5, 6.9, 15.6),


      point I (55.1, 18.3, 26.6), and


      point J (77.5, 18.4, 4.1),


      or on these line segments;
    • the line segment GI is represented by coordinates (0.02y2−2.4583y+93.396, y, −0.02y2+1.4583y+6.604), and
    • the line segments IJ and JG are straight lines. When the requirements above are satisfied, the refrigerant 1C according to the present disclosure has a refrigerating capacity ratio of 95% or more relative to that of R410A and a GWP of 100 or less, undergoes fewer or no changes such as polymerization or decomposition, and also has excellent stability.


The refrigerant 1C according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), R32, and R1234yf based on their sum is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are within the range of a figure surrounded by line segments GH, HK, and KG that connect the following 3 points:


      point G (77.5, 6.9, 15.6),


      point H (61.8, 14.6, 23.6), and


      point K (77.5, 14.6, 7.9),


      or on these line segments;
    • the line segment GH is represented by coordinates (0.02y2−2.4583y+93.396, y, −0.02y2+1.4583y+6.604), and
    • the line segments HK and KG are straight lines. When the requirements above are satisfied, the refrigerant 1C according to the present disclosure has a refrigerating capacity ratio of 95% or more relative to that of R410A and a GWP of 100 or less, undergoes fewer or no changes such as polymerization or decomposition, and also has excellent stability.


The refrigerant 1C according to the present disclosure may further comprise other additional refrigerants in addition to HFO-1132(E), R32, and R1234yf, as long as the above properties and effects are not impaired. In this respect, the refrigerant 1C according to the present disclosure preferably comprises HFO-1132(E), R32, and R1234yf in a total amount of 99.5 mass % or more, more preferably 99.75 mass % or more, and still more preferably 99.9 mass % or more based on the entire refrigerant 1C.


Such additional refrigerants are not limited, and can be selected from a wide range of refrigerants. The mixed refrigerant may comprise a single additional refrigerant, or two or more additional refrigerants.


The refrigerant 1C according to the present disclosure is suitable for use as an alternative refrigerant for R410A.


Examples of Refrigerant 1C

The refrigerant 1C is described in more detail below with reference to Examples. However, the refrigerant 1C according to the present disclosure is not limited to the Examples.


The burning velocity of individual mixed refrigerants of HFO-1132(E), R32, and R1234yf was measured in accordance with the ANSI/ASHRAE Standard 34-2013. A formulation that shows a burning velocity of 10 cm/s was found by changing the concentration of R32 by 5 mass %. Table 18 shows the formulations found.


A burning velocity test was performed using the apparatus shown in FIG. 1A in the following manner. First, the mixed refrigerants used had a purity of 99.5% or more, and were degassed by repeating a cycle of freezing, pumping, and thawing until no traces of air were observed on the vacuum gauge. The burning velocity was measured by the closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between the electrodes in the center of a sample cell. The duration of the discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of the flame was visualized using schlieren photographs. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light transmission acrylic windows was used as the sample cell, and a xenon lamp was used as the light source. Schlieren images of the flame were recorded by a high-speed digital video camera at a frame rate of 600 fps and stored on a PC.















TABLE 18








R32 = 5
R32 = 10
R32 = 15
R32 = 20


Item
Unit
Point D
mass %
mass %
mass %
mass %





















HFO-
Mass %
72
64
57
51
46


1132E








R32
Mass %
0
5
10
15
20


R1234yf
Mass %
28
31
33
34
34


Burning
cm/s
10
10
10
10
10


Velocity









The results indicate that under the condition that the mass % of HFO-1132(E), R32, and R1234yf based on their sum is respectively represented by x, y, and z, when coordinates (x,y,z) in the ternary composition diagram shown in FIG. 1J in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are on the line segments that connect the 5 points shown in Table 18 or on the right side of the line segments, the refrigerant has a lower flammability (Class 2L) according to the ASHRAE standard.


This is because R1234yf is known to have a lower burning velocity than HFO-1132(E) and R32.


Mixed refrigerants were prepared by mixing HFO-1132(E), R32, and R1234yf in amounts (mass %) shown in. Tables 19 to 23 based on the sum of HFO-1132(E), R32, and R1234yf. The coefficient of performance (COP) ratio and the refrigerating capacity ratio relative to those of R410A of the mixed refrigerants shown in Tables 19 to 23 were determined. The conditions for calculation were as described below.


Evaporating temperature: 5° C.


Condensation temperature: 45° C.


Degree of superheating: 1 K


Degree of subcooling: 5 K


Ecomp (compressive modulus): 0.7 kWh


Tables 19 to 23 show these values together with the GWP of each mixed refrigerant.
















TABLE 19











Example
Example





Comp. Ex. 2

Example
3
4


Item
Unit
Comp. Ex. 1
A
Example 1
2
B
C






















HFO-1132E
Mass %
R410A
71.1
60.4
50.6
42.6
36.5


R32
Mass %

0.0
5.0
10.0
14.5
18.2


R1234yf
Mass %

28.9
34.6
39.4
42.9
45.3


GWP

2088
2
36
70
100
125


COP Ratio
% (relative
100
98.9
98.7
98.7
98.9
99.1



to R410A)








Refrigerating
% (relative
100
85.0
85.0
85.0
85.0
85.0


Capacity Ratio
to R410A)





















TABLE 20







Comp.
Comp.
Comp.
Comp.




Ex. 3
Ex. 4
Ex. 5
Ex. 6


Item
Unit
O
P
Q
R




















HFO-1132E
Mass %
85.3
0.0
81.6
0.0


R32
Mass %
14.7
14.3
18.4
18.1


R1234yf
Mass %
0
85.7
0.0
81.9


GWP

100
100
125
125


COP Ratio
%
96.2
103.4
95.9
103.4



(relative







to R410A)






Refrigerating
%
105.7
57.3
107.4
60.9


Capacity
(relative






Ratio
to R410A)
























TABLE 21







Comp. Ex. 7


Example 7

Example 9



Item
Unit
D
Example 5
Example 6
E
Example 8
F
Comp. Ex. 8























HFO-1132E
Mass %
72.0
64.0
57.0
51.4
51.0
47.6
46.0


R32
Mass %
0.0
5.0
10.0
14.6
15.0
18.3
20.0


R1234yf
Mass %
28.0
31.0
33.0
34.0
34.0
34.1
34.0


GWP

1.84
36
69
100
103
125
137


COP Ratio
%
98.8
98.5
98.2
98.1
98.1
98.0
98.0



(relative










to










R410A)









Refrigerating
%
85.4
86.8
88.3
89.8
90.0
91.2
91.8


Capacity Ratio
(relative










to










R410A)






















TABLE 22










Example 11
Example 12


Item
Unit
Comp. Ex. 9
Comp. Ex. 10
Example 10
H
I





















HFO-1132E
Mass %
93.4
81.6
70.8
61.8
55.1


R32
Mass %
0.0
5.0
10.0
14.6
18.3


R1234yf
Mass %
6.6
13.4
19.2
23.6
26.6


GWP

1
35
69
100
125


COP Ratio
% (relative
98.0
97.6
97.4
97.3
97.4



to R410A)







Refrigerating
% (relative
95.0
95.0
95.0
95.0
95.0


Capacity Ratio
to R410A)






















TABLE 23








Example 13
Example 14
Example 15



Item
Unit
Comp. Ex. 11
J
K
G
Comp. Ex. 12





















HFO-1132E
Mass %
77.5
77.5
77.5
77.5
77.5


R32
Mass %
22.5
18.4
14.6
6.9
0.0


R1234yf
Mass %
0.0
4.1
7.9
15.6
22.5


GWP

153
125
100
48.0
2


COP Ratio
% (relative
95.8
96.1
96.5
97.5
98.6



to R410A)







Refrigerating
% (relative
109.1
105.6
102.3
95.0
88.0


Capacity Ratio
to R410A)









The results indicate that under the condition that the mass % of HFO-1132(E), R32, and R1234yf based on their sum is respectively represented by x, y, and z, when coordinates (x,y,z) in the ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are within the range of a figure (FIG. 1J) surrounded by line segments AC, CF, FD, and DA that connect the following 4 points:


point A (71.1, 0.0, 28.9),


point C (36.5, 18.2, 45.3),


point F (47.6, 18.3, 34.1), and


point D (72.0, 0.0, 28.0),


or on these line segments,


the refrigerant has a refrigerating capacity ratio of 85% or more relative to that of R410A, a GWP of 125 or less, and a lower flammability (Class 2L) according to the ASHRAE standard.


Likewise, the results indicate that when coordinates (x,y,z) are within the range of a figure (FIG. 1J) surrounded by line segments AB, BE, ED, and DA that connect the following 4 points:


point A (71.1, 0.0, 28.9),


point B (42.6, 14.5, 42.9),


point E (51.4, 14.6, 34.0), and


point D (72.0, 0.0, 28.0),


or on these line segments,


the refrigerant has a refrigerating capacity ratio of 85% or more relative to that of R410A, a GWP of 100 or less, and a lower flammability (Class 2L) according to the ASHRAE standard.


Likewise, the results indicate that when coordinates (x,y,z) are within the range of a figure (FIG. 1J) surrounded by line segments GI, IJ, and JG that connect the following 3 points:


point G (77.5, 6.9, 15.6),


point I (55.1, 18.3, 26.6), and


point J (77.5, 18.4, 4.1),


or on these line segments,


the refrigerant has a refrigerating capacity ratio of 95% or more relative to that of R410A and a GWP of 125 or less, undergoes fewer or no changes such as polymerization or decomposition, and also has excellent stability.


Likewise, the results indicate that when coordinates (x,y,z) are within the range of a figure (FIG. 1J) surrounded by line segments GH, HK, and KG that connect the following 3 points:


point G (77.5, 6.9, 15.6),


point H (61.8, 14.6, 23.6), and


point K (77.5, 14.6, 7.9),


or on these line segments,


the refrigerant has a refrigerating capacity ratio of 95% or more relative to that of R410A and a GWP of 100 or less, undergoes fewer or no changes such as polymerization or decomposition, and also has excellent stability.


(1-5-4) Refrigerant 1D


(5-4) Refrigerant 1D


Refrigerant 1D according to the present disclosure is a mixed refrigerant comprising HFO-1132(E), HFO-1123, and R32.


The refrigerant 1D according to the present disclosure has various properties that are desirable as an R410A-alternative refrigerant, i.e., a coefficient of performance equivalent to that of R410A and a sufficiently low GWP.


The refrigerant 1D according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R32 based on their sum is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass % are within the range of a figure surrounded by line segments OC′, C′D′, D′E′, E′A′, and A′O that connect the following 5 points:


      point O (100.0, 0.0, 0.0),


      point C′ (56.7, 43.3, 0.0),


      point D′ (52.2, 38.3, 9.5),


      point E′ (41.8, 39.8, 18.4), and


      point A′ (81.6, 0.0, 18.4),


      or on the line segments C′D′, D′E′, and E′A′ (excluding the points C′ and A′);
    • the line segment C′D′ is represented by coordinates (−0.0297z2−0.1915z+56.7, 0.0297z2−1.1915z+43.3, z),
    • the line segment D′E′ is represented by coordinates (−0.0535z2+0.3229z+53.957, 0.0535z2−0.6771z+46.043, z), and
    • the line segments OC′, E′A′, and A′O are straight lines. When the requirements above are satisfied, the refrigerant 1D according to the present disclosure has a COP ratio of 92.5% or more relative to that of R410A, and a GWP of 125 or less.


The refrigerant 1D according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R32 based on their sum is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass % are within the range of a figure surrounded by line segments OC, CD, DE, EA′, and A′O that connect the following 5 points:


      point O (100.0, 0.0, 0.0),


      point C (77.7, 22.3, 0.0),


      point D (76.3, 14.2, 9.5),


      point E (72.2, 9.4, 18.4), and


      point A′ (81.6, 0.0, 18.4),


      or on the line segments CD, DE, and EA′ (excluding the points C and A′);
    • the line segment CDE is represented by coordinates (−0.017z2+0.0148z+77.684, 0.017z2+0.9852z+22.316, z), and
    • the line segments OC, EA′, and A′O are straight lines. When the requirements above are satisfied, the refrigerant 1D according to the present disclosure has a COP ratio of 95% or more relative to that of R410A, and a GWP of 125 or less.


The refrigerant 1D according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R32 based on their sum is respectively represented by x; y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass % are within the range of a figure surrounded by line segments OC′, C′D′, D′A, and AO that connect the following 4 points:


      point O (100.0, 0.0, 0.0),


      point C′ (56.7, 43.3, 0.0),


      point D′ (52.2, 38.3, 9.5), and


      point A (90.5, 0.0, 9.5),


      or on the line segments C′D′ and D′A (excluding the points C′ and A);
    • the line segment C′D′ is represented by coordinates (−0.0297z2−0.1915z+56.7, 0.0297z2+1.1915z+43.3, z), and
    • the line segments OC′, D′A, and AO are straight lines. When the requirements above are satisfied, the refrigerant 1D according to the present disclosure has a COP ratio of 93.5% or more relative to that of R410A, and a GWP of 65 or less.


The refrigerant 1D according to the present disclosure is preferably a refrigerant wherein

    • when the mass % of HFO-1132(E), HFO-1123, and R32 based on their sum is respectively represented by x, y, and z, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass % are within the range of a figure surrounded by line segments OC, CD, DA, and AO that connect the following 4 points:


      point O (100.0, 0.0, 0.0),


      point C (77.7, 22.3, 0.0),


      point D (76.3, 14.2, 9.5), and


      point (90.5, 0.0, 9.5),


      or on the line segments CD and DA (excluding the points C and A);
    • the line segment CD is represented by coordinates (−0.017z2+0.0148z+77.684, 0.017z2+0.9852z+22:316, z), and
    • the line segments OC, DA, and AO are straight lines. When the requirements above are satisfied, the refrigerant 1D according to the present disclosure has a COP ratio of 95% or more relative to that of R410A, and a GWP of 65 or less.


The refrigerant 1D according to the present disclosure may further comprise other additional refrigerants in addition to HFO-1132(E), HFO-1123, and R32, as long as the above properties and effects are not impaired. In this respect; the refrigerant 1D according to the present disclosure preferably comprises HFO-1132(E), HFO-1123, and R32 in a total amount of 99.5 mass % or more, more preferably 99.75 mass % or more, and even more preferably 99.9 mass % or more, based on the entire refrigerant 1D.


Such additional refrigerants are not limited, and can be selected from a wide range of refrigerants. The mixed refrigerant may comprise a single additional refrigerant, or two or more additional refrigerants.


The refrigerant 1D according to the present disclosure is suitable for use as an alternative refrigerant for R410A.


Examples of Refrigerant 1D

The refrigerant 1D is described in more detail below with reference to Examples. However, the refrigerant 1D according to the present disclosure is not limited to the Examples.


Mixed refrigerants were prepared by mixing HFO-1132(E), HFO-1123, and R32 at mass % based on their sum shown in Tables 24 to 26.


The COP ratio and the refrigerating capacity (which may be referred to as “cooling capacity” or “capacity”) ratio relative to those of R410 of the mixed refrigerants were determined.


The conditions for calculation were as described below.


Evaporating temperature: 5° C.


Condensation temperature: 45° C.


Degree of superheating: 1K


Degree of subcooling: 5K


Ecomp(compressive modulus): 0.7 kWh.


Tables 24 to 26 show these values together with the GWP of each mixed refrigerant.

















TABLE 24








Comp.

Example

Example
Comp.




Comp.
Ex. 2
Example
2
Example
4
Ex. 3


Item
Unit
Ex. 1
C
1
D
3
E
O























HFO-1132(E)
mass %
R410A
77.7
77.3
76.3
74.6
72.2
100.0


HFO-1123
mass %

22.3
17.7
14.2
11.4
9.4
0.0


R32
mass %

0.0
5.0
9.5
14.0
18.4
0.0


GWP

2088
1
35
65
95
125
1


COP ratio
% (relative to
100.0
95.0
95.0
95.0
95.0
95.0
97.8



R410A)









Refrigerating capacity
% (relative to
100.0
102.5
104.4
106.0
107.6
109.1
97.8


ratio
R410A)
























TABLE 25







Comp. Ex.

Example

Example
Comp.
Comp. Ex.




4
Example
6

8
Ex. 5
6


Item
Unit
C′
5
D′
Example 7
E′
A
B























HFO-1132(E)
mass %
56.7
55.0
52.2
48.0
41.8
90.5
0.0


HFO-1123
mass %
43.3
40.0
38.3
38.0
39.8
0.0
90.5


R32
mass %
0.0
5.0
9.5
14.0
18.4
9.5
9.5


GWP

1
35
65
95
125
65
65


COP ratio
% (relative
92.5
92.5
92.5
92.5
92.5
96.6
90.8



to R410A)









Refrigerating
% (relative
105.8
107.9
109.7
111.5
113.2
103.2
111.0


capacity ratio
to R410A)
























TABLE 26







Comp. Ex.
Comp.









7
Ex. 8
Example
Example
Example
Comp.
Comp. Ex.


Item
Unit
A′
B′
9
10
11
Ex. 9
10























HFO-1132(E)
mass %
81.6
0.0
85.0
65.0
70.0
50.0
20.0


HFO-1123
mass %
0.0
81.6
10.0
30.0
15.0
20.0
20.0


R32
mass %
18.4
18.4
5.0
5.0
15.0
30.0
60.0


GWP

125
125
35
35
102
203
405


COP ratio
% (relative
95.9
91.9
95.9
93.6
94.6
94.3
97.6



to R410A)









Refrigerating
% (relative
107.4
113.8
102.9
106.5
108.7
114.6
117.6


capacity ratio
to R410A)









The results indicate that under the condition that the mass % of HFO-1132(E), HFO-1123, and R32 based on their sum is respectively represented by x, y, and z, when coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass % are within the range of a figure (FIG. 1K) surrounded by line segments OC′, C′D′, D′E′, E′A′, and A′O that connect the following 5 points:


point O (100.0, 0.0, 0.0),


point C′ (56.7, 43.3, 0.0),


point D′ (52.2, 38.3, 9.5),


point E′ (41.8, 39.8, 18.4), and


point A′ (81.6, 0.0, 18.4),


or on the line segments C′D′, D′E′, and E′A′ (excluding the points C′ and A′),


the refrigerant has a COP ratio of 92.5% or more relative to that of R410A, and a GWP of 125 or less.


The results also indicate that when coordinates (x,y,z) are within the range of a figure (FIG. 1K) surrounded byline segments OC, CD, DE, EA′, and A′O that connect the following 5 points:


point O (100.0, 0.0, 0.0),


point C (77.7, 22.3, 0.0),


point D (76.3, 14.2, 9.5),


point E (72.2, 9.4, 18.4), and


point A′ (81.6, 0.0, 18.4),


or on the line segments CD, DE, and EA′ (excluding the points C and A′),


the refrigerant has a COP ratio of 95% or more relative to that of R410A, and a GWP of 125 or less.


The results also indicate that when coordinates (x,y,z) are within the range of a figure (FIG. 1K) surrounded by line segments OC′, C′D′, D′A, and AO that connect the following 4 points:


point O (100.0, 0.0, 0.0),


point C′ (56.7, 43.3, 0.0),


point D′ (52.2, 38.3, 9.5), and


point A (90.5, 0.0, 9.5),


or on the line segments C′D′ and D′A (excluding the points C′ and A),


the refrigerant has a COP ratio of 92.5% or more relative to that of R410A, and a GWP of 65 or less.


The results also indicate that when coordinates (x,y,z) are within the range of a figure (FIG. 1K) surrounded by line segments OC, CD, DA, and AO that connect the following 4 points:


point O (100.0, 0.0, 0.0),


point C (77.7, 22.3, 0.0),


point D (76.3, 14.2, 9.5), and


point (90.5, 0.0, 9.5),


or on the line segments CD and DA (excluding the points C and A),


the refrigerant has a COP ratio of 95% or more relative to that of R410A, and a GWP of 65 or less.


In contrast, as shown in Comparative Examples 2, 3, and 4, when R32 is not contained, the concentrations of HFO-1132(E) and HFO-1123, which have a double bond, become relatively high; this undesirably leads to deterioration, such as decomposition, or polymerization in the refrigerant compound.


Moreover, as shown in Comparative Examples 3, 5, and 7, when HFO-1123 is not contained, the combustion-inhibiting effect thereof cannot be obtained; thus, undesirably, a composition having lower flammability cannot be obtained.


(1-5-5) Refrigerant 1E


(5-5) Refrigerant 1E


Refrigerant 1E according to the present disclosure is a mixed refrigerant containing CO2 and R32, HFO-1132(E), and R1234yf.


Refrigerant 1E according to the present disclosure has various properties that are desirable as an R410A-alternative refrigerant, i.e., a refrigerating capacity equivalent to that of R410A, a sufficiently low GWP, and lower flammability. Refrigerant 1E according to the present disclosure is a refrigerant wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,

    • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line BM, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B″D and straight line CI):
    • point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)
    • point K (36.8, 35.6, 27.6−w)
    • point L (51.7, 28.9, 19.4−w)
    • point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w−2.3.75w+49.5)
    • point D (−2.9167w+40.317, 0.0, 1.9167w+59.683)


      point C (0.0, −4.9167w+58.317, 3.9167w+41.683);
    • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding the points on straight line B′D and straight line CI):
    • point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)
    • point K (36.8, 35.6, 27.6−w)
    • point L (51.7, 28.9, 19.4−w)
    • point B″ (51.6, 0.0, 48.4−w)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and
    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B″D and straight line CI):
    • point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)
    • point K (36.8, 35.6, 27.6−w)
    • point L (51.7, 28.9, 19.4−w)
    • point B″ (51.6, 0.0, 48.4−w)
    • point D (−2.8w+40.1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7),


      and
    • curve IJ is represented by coordinates (x, 0.0236x2 1.716x+72, −0.0236x2+0.716x+28−w),
    • curve JK is represented by coordinates (x, 0.0095x2−1.2222x+67.676, −0.0095x2+0.2222x+32.324−w), and
    • curve KL is represented by coordinates (x, 0.0049x2−0.8842x+61.488, −0.0049x2−0.1158x+38.512).


Refrigerant 1E according to the present disclosure has a refrigerating capacity ratio of 80% or more relative to R410A, a GWP of 350 or less, and a lower WCF flammability.


Refrigerant 1E according to the present disclosure is preferably a refrigerant wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,

    • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)
    • point K (36.8, 35.6, 27.6−w)
    • point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997)
    • point C (0.0, −4.9167w+58.317, 3.9167w+41.683);
    • if 1.2<w≤1.3, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)
    • point K (36.8, 35.6, 27.6−w)
    • point F (36.6, −3w+3.9, 2w+59.5)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553);
    • if 1.3<w≤_4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)
    • point K (36.8, 35.6, 27.6−w)
    • point B′(36.6, 0.0, −w+63.4)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and
    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)
    • point K (36.8, 35.6, 27.6−w)
    • point B′ (36.6, 0.0, −w+63.4)
    • point D (−2.8w+40.1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7),


      and
    • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28−w), and
    • curve JK is represented by coordinates (x, 0.0095x2−1.2222x+67.676, −0.0095x2+0.2222x+32.324−w).


      When the requirements above are satisfied, refrigerant 1E according to the present disclosure has a refrigerating capacity ratio of 80% or more relative to R410A, a GWP of 250 or less, and a lower WCF flammability.


Refrigerant 1E according to the present disclosure is preferably a refrigerant wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,

    • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 4 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)
    • point E (18.2, −1.1111w2−3.1667w+31.9, 1.1111w2+2.1667w+49.9)
    • point C (0.0, −4.9167w+58.317, 3.9167w+41.683);
    • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 4 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)


      point E (−0.0365w+18.26, 0.0623w2−4.5381w+31.856, −0.0623w2+3.5746w+49.884)
    • point C (0.0, 0.1081w2−5.169w+58.447, 0.1081w2+4.169w+41.553); and
    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 4 points or on these line segments (excluding points on straight line CI):


      point I (0.0, 72.0, 28.0−w)
    • point J (18.3, 48.5, 33.2−w)
    • point E (18.1, 0.0444w2−4.3556w+31.411, −0.0444w2+3.3556w+50.489)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7),


      and
    • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.023 6x2+0.716x+28−w).


      When the requirements above are satisfied, refrigerant 1E according to the present disclosure has a refrigerating capacity ratio of 80% or more relative to R410A, a GWP of 125 or less, and a lower WCF flammability.


Refrigerant 1E according to the present disclosure is preferably a refrigerant wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,

    • if 0<w≤0.6, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve GO, curve OP, straight line PB″, straight line B″D, and straight line DG that connect the following 5 points or on these line segments (excluding points on straight line B″D):
    • point G (−5.8333w2−3.1667w+22.2, 7.0833w2+1.4167w+26.2, −1.25w2+0.75w+51.6)
    • point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)
    • point P (51.7, 1.1111w2+20.5, −1.1111w2−w+27.8)
    • point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2−3.75w+49.5)
    • point D (−2.9167w+40.317, 0.0, 1.9167w+59.683); and
    • if 0.6<w≤1.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve GN, curve NO, curve OP, straight line PB″, straight line B″D, and straight line DG that connect the following 6 points or on these line segments (excluding the points on straight line B″D):
    • point G (−5.8333w2−3.1667w+22.2, 7.0833w2+1.4167w+26.2, −1.25w2+0.75w+51.6)
    • point N (18.2, 0.2778w2+3w+27.7, −0.2778w2−4w+54.1)
    • point O (36.8, 0.8333w2+1.8333w+22.6, 0.8333w2−2.8333w+40.6)
    • point P (51.7, 1.1111w2+20.5, −1.1111w2−w+27.8)
    • point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2−3.75w+49.5)
    • point D (−2.9167w+40.317, 0.0, 1.9167w+59.683); and
    • when 0<w≤0.6, curve GO is represented by coordinates (x, (0.00487w2 0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100−w−x−y);
    • when 0.6<w≤1.2, curve GN is represented by coordinates (x, (0.0122w2−0.0113w+0.0313)x2+(−0.3582w2+0.1624w−1.4551)x+2.7889w2+3.7417w+43.824, 100−w−x 100−w−x−y);
    • when 0.6<w≤<1.2, curve NO is represented by coordinates (x, (0.00487w2 0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100−w−x−y); and
    • when 0<w≤1.2, curve OP is represented by coordinates (x, (0.0074w2−0.0133w+0.0064)x2+(−0.5839w2+1.0268w−0.7103)x+11.472w2−17.455w+40.07, 100−w−x−y);
    • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, curve OP, straight line PB″, straight line B″D, straight line DC, and straight line CM that connect the following 8 points or on these line segments (excluding points on straight line B′D and straight line CM):
    • point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)
    • point W (10.0, −0.3645w2+3.5024w+44.422, 0.3645w2−4.5024w+55.57)
    • point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)
    • point O (36.8, −0.1392w2+1.4381w+24.475, 0.1392w2−2.4381w+38.725)
    • point P (51.7, −0.2381w2+1.881w+20.186, 0.2381w2−2.881w+28.114)
    • point B″ (51.6, 0.0, −w+48.4)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553),


      and
    • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100−w−x−y),
    • curve WN is represented by coordinates (x, (0.0055w2−0.0326w+0.0665)x2+(−0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100−w−x−y),
    • curve NO is represented by coordinates (x, (−0.00062w2+0.0036w+0.0037)x2+(0.0375w2−0.239w−0.4977)x−0.8575w2+6.4941w+36.078, 100−w−x−y), and
    • curve OP is represented by coordinates (x, (−0.000463w2+0.0024w−0.0011)x2+(0.0457w2−0.2581w−0.075)x−1.355w2+8.749w+27.096, 100−w−x−y); and
    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, curve OP, straight line PB″, straight line B″D, straight line DC, and straight line CM that connect the following 8 points or on these line segments (excluding points on straight line B′D and straight line CM):
    • point M (0.0, −0.0667w2+0.8333w+58.133, 0.0667w2−1.8333w+41.867)
    • point W (10.0, −0.0667w2+1.1w+39.267, 0.0667w2−2.1w+50.733)
    • point N (18.2, −0.0889w2+1.3778w+31.411, 0.0889w2−2.3778w+50.389)
    • point O (36.8, −0.0444w2+0.6889w+25.956, 0.0444w2−1.6889w+37.244)
    • point P (51.7, −0.0667w2+0.8333w+21.633, 0.0667w2−1.8333w+26.667)
    • point B″ (51.6, 0.0, −w+48.4)
    • point D (−2.8w+40.1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and
    • curve MW is represented by coordinates (x, (0.00357w2−0.0391w+0.1756)x2+(−0.0356w2+0.4178w−3.6422)x−0.0667w2+0.8333w+58.103, 100−w−x−y),
    • curve WN is represented by coordinates (x, (−0.002061w2+0.0218w−0.0301)x2+(0.0556w2−0.5821w−0.1108)x−0.4158w2+4.7352w+43.383, 100−w−x−y),
    • curve NO is represented by coordinates (x, 0.0082x2+(0.0022w2−0.0345w−0.7521)x−0.1307w2+2.0247w+42.327, 100−w−x−y), and
    • curve OP is represented by coordinates (x, (−0.0006258w2+0.0066w−0.0153)x2+(0.0516w2−0.5478w+0.9894)x−1.074w2+11.651w+10.992, 100−w−x−y).


When the requirements above are satisfied, refrigerant 1E according to the present disclosure has a refrigerating capacity ratio of 80% or more relative to R410A, a GWP of 350 or less, and a lower ASHRAE flammability.


Refrigerant 1E according to the present disclosure is preferably a refrigerant wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,

    • if 0<w≤0.6, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve GO, straight line OF, and straight line FG that connect the following 3 points or on these line segments:
    • point G (−5.8333w2−3.1667w+22.2, 7.0833w2−1.4167w+26.2, −1.25w2+3.5834w+51.6)
    • point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)
    • point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997), and
    • curve GO is represented by coordinates (x, (0.00487w2−0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100−w−x−y);
    • if 0.6<w≤1.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve GN, curve NO, straight line OF, and straight line FG that connect the following 4 points or on these line segments:
    • point G (−5.8333w2−3.1667w+22.2, 7.0833w2−1.4167w+26.2, −1.25w2+3.5834w+51.6)
    • point N (18.2, 0.2778w2+3.0w+27.7, −0.2.778w2−4.0w+54.1)
    • point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)
    • point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997), and
    • when 0.6<w≤1.2, curve GN is represented by coordinates (x, (0.0122w2−0.0113w+0.0313)x2+(−0.3582w2+0.1624w−1.4551)x+2.7889w2+30.7417w+43.824, 100−w−x−y), and
    • when 0.6<w≤1.2, curve NO is represented by coordinates (x, (0.00487w2−0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100−w−x−y); and
    • if 1.2<w≤1.3, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW curve WN, curve NO, straight line OF, straight line FC, and straight line CM that connect the following 6 points or on these line segments (excluding points on straight line CM):
    • point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)
    • point W (10.0, −0.3645w2+3.5024w−34.422, 0.3645w2−4.5024w+55.578)
    • point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)
    • point O (36.8, −0.1392w2+1.4381w+24.475, 0.1392w2−2.4381w+38.725)
    • point F (36.6, −3w+3.9, 2w+59.5)
    • point C (0.1081w2−5.169w+58.447, 0.0, −0.1081w2+4.169w+41.553),


      and
    • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100−w−x−y),
    • curve WN is represented by coordinates (x, (0.0055w2−0.0326w+0.0665)x2+(−0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100−w−x−y), and
    • curve NO is represented by coordinates (x, (−0.00062w2+0.0036w+0.0037)x2+(0.0375w2 0.239w−0.4977)x−0.8575w2+6.4941w+36.078, 100−w−x−y);
    • if 1.3<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, straight line OB′, straight line B′D, straight line. DC, and straight line CM that connect the following 7 points or on these line segments (excluding points on straight line CM):


      point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)
    • point W (10.0, −0.3645w2+3.5024w+34.422, 0.3645w2−4.5024w+55.578)
    • point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)
    • point O (36.8, −0.1392w2+1.4381w+24.475, 0.1392w2−2.4381w+38.725)
    • point B′(36.6, 0.0, −w+63.4)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553),


      and
    • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100−w−x−y),
    • curve WN is represented by coordinates (x, (0.0055w2−0.0326w+0.0665)x2+(0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100−w−x−y), and
    • curve NO is represented by coordinates (x, (−0.00062w2+0.0036w+0.0037)x2+(0.0457w2−0.2581w−0.075)x−1.355w2+8.749w+27.096, 100−w−x−y); and
    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, straight line OB′, straight line B′D, straight line DC, and straight line CM that connect the following 7 points or on these line segments (excluding points on straight line CM):


      point M (0.0, −0.0667w2+0.8333w−58.133, 0.0667w2−1.8333w+41.867)
    • point W (10.0, −0.0667w2+1.1w+39.267, 0.0667w2−2.1w+50.733)
    • point N (18.2, −0.0889w2+1.3778w+31.411, 0.0889w2−2.3778w+50.389)
    • point O (36.8, −0.0444w2+0.6889w+25.956, 0.0444w2−1.6889w+37.244)
    • point B′ (36.6, 0.0, −w+63.4)
    • point D (−2.8w+40.1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and
    • curve MW is represented by coordinates (x, (0.00357w2−0.0391w+0.1756)x2+(−0.0356w2+0.4178w−3.6422)x−0.0667w2+0.8333w+58.103, 100−w−x−y),
    • curve WN is represented by coordinates (x, (−0.002061w2+0.0218w−0.0301)x2+(0.0556w2−0.5821w−0.1108)x−0.4158w2+4.7352w+43.383, 100−w−x−y), and
    • curve NO is represented by coordinates (x, (0.0082x2+(0.0022w2−0.0345w 0.7521)x−0.1307w2+2.0247w+42.327, 100−w−x−y).


When the requirements above are satisfied, refrigerant 1E according to the present disclosure has a refrigerating capacity ratio of 80% or more relative to R410A, a GWP of 250 or less, and a lower ASHRAE flammability.


Refrigerant 1E according to the present disclosure is preferably a refrigerant wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,

    • if 1.2<w≤4.0, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve MW, curve WN, straight line NE, straight line EC, and straight line CM that connect the following 5 points or on these line segments (excluding points on straight line CM):
    • point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)
    • point W (10.0, −0.3645w2+3.5024w+34.422, 0.3645w2−4.5024w+55.578)
    • point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)
    • point E (−0.0365w+18.26, 0.0623w2−4.5381w+31.856, −0.0623w2+3.5746w+49.884)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553),


      and
    • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100−w−x−y), and
    • curve WN is represented by coordinates (x, (0.0055w2−0.0326w+0.0665)x2+(−0.1571w2+0.8981w 2.6274)x+0.6555w2−2.2153w+54.044, 1100−w−x−y); and
    • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, straight line NE, straight line EC, and straight line CM that connect the following 5 points or on these line segments (excluding points on straight line CM):
    • point M (0.0, −0.0667w2+0.8333w+58.133, 0.0667w2−1.8333w+41.867)
    • point W (10.0, −0.0667w2+1.1w+39.267, 0.0667w2−2.1w+50.733)
    • point N (18.2, −0.0889w2+1.3778w+31.411, 0.0889w2−2.3778w+50.389)
    • point E (18.1, 0.01′14w2−4.3556w+31.411, −0.0444w2+3.3556w+50.489)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and
    • curve MW is represented by coordinates (x; (0.00357w2−0.0391w+0.1756)x2+(−0.0356w2+0.4178w 3.6422)x−0.0667w2+0.8333w+58.103, 100−w−x−y), and
    • curve WN is represented by coordinates (x, (−0.002061w2+0.0218w−0.0301)x2+(0.0556w2−0.5821w−0.1108)x−0.4158w2+4.7352w+43.383, 100−w−x−y).


      When the requirements above are satisfied, refrigerant 1E according to the present disclosure has a refrigerating capacity ratio of 80% or more relative to R410A, a GWP of 125 or less, and a lower ASH RAE flammability.


Refrigerant 1E may further comprise an additional refrigerant in addition to CO2, R32, HFO-1132(E), and R1234yf, as long as the above characteristics and effects of the refrigerant are not impaired. From this viewpoint, refrigerant 1E according to the present disclosure preferably comprises R32, HFO-1132(E), and R1234yf in a total amount of 99.5 mass % or more, more preferably 99.75 mass % or more, and even more preferably 99.9 mass % or more, of the entire refrigerant.


The additional refrigerant is not limited, and can be selected from a wide range of refrigerants. The mixed refrigerant may comprise a single additional refrigerant, or two or more additional refrigerants.


Refrigerant 1E according to the present disclosure can be preferably used as a working fluid in a refrigerating machine.


The composition according to the present disclosure is suitable for use as an alternative refrigerant for R410A.


Examples of Refrigerant 1E

The present disclosure is described in more detail below with reference to Examples. However, refrigerant 1E according to the present disclosure is not limited to the Examples.


The burning velocity of each of the mixed refrigerants of CO2, R32, HFO-1132(E), and R1234yf was measured in accordance with the ANSI/ASHRAE Standard 34-2013. While changing the concentration of CO2, a formulation that shows a burning velocity of 10 cm/s was found. Tables 27 to 29 show the formulations found.


A burning velocity test was performed using the apparatus shown in FIG. 1A in the following manner. First, the mixed refrigerants used had a purity of 99.5% or more and were degassed by repeating a cycle of freezing, pumping, and thawing until no traces of air were observed on the vacuum gauge. The burning velocity was measured by using a closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between the electrodes in the center of a sample cell. The duration of the discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of the flame was visualized using schlieren photographs. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two acrylic light transmission windows was used as the sample cell, and a xenon lamp was used as the light source. Schlieren images of the flame were recorded with a high-speed digital video camera at a frame rate of 600 fps and stored on a PC.


The WCFF concentration was obtained by using the WCF concentration as the initial concentration and performing leak simulation using NIST Standard Reference Database REFLEAK Version 4.0.









TABLE 27







0% CO2

















Comp.

Comp.

Comp.

Comp.




Ex. 13
Comp.
Ex.15
Comp.
Ex. 17
Comp.
Ex. 19


Item
Unit
I
Ex. 14
J
Ex. 16
K
Ex. 18
L





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
28.0
32.8
33.2
31.2
27.6
23.8
19.4


CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Burning velocity
cm/s
10
10
10
10
10
10
10


(WCF)










0.6% CO2

















Example

Example

Example






3
Example
5
Example
7
Example
Example 9


Item
Unit
I
4
J
6
K
8
L





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
27.4
32.6
32.6
30.6
27.0
23.3
10.8


CO2
mass %
0.6
0.6
0.6
0.6
0.6
0.6
0.6


Burning velocity
cm/s
10
10
10
10
10
10
10


(WCF)










1.2% CO2

















Comp.

Example

Example

Example




Ex. 48
Example
18
Example
20
Example
22


Item
Unit
I
17
J
19
K
21
L





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
26.8
31.6
32.0
30.0
26.4
22.7
18.2


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2


Burning velocity
cm/s
10
10
10
10
10
10



(WCF)










1.3% CO2

















Comp.

Example

Example

Example




Ex. 59
Example
30
Example
32
Example
34


Item
Unit
I
29
J
31
K
33
L





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
26.7
31.5
31.9
29.9
26.3
22.6
18.1


CO2
mass %
1.3
1.3
1.3
1.3
1.3
1.3
1.3


Burning velocity
cm/s
10
10
10
10
10
10
10


(WCF)










2.5% CO2

















Comp

Example

Example

Example




Ex. 69
Example
45
Example
47
Example
49


Item
Unit
I
44
J
46
K
48
L





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
25.5
30.3
30.7
28.7
25.1
21.3
16.9


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5


Burning velocity
cm/s
10
10
10
10
10
10
10


(WCF)










4.0 CO2

















Comp.

Example

Example

Example




Ex. 79
Example
60
Example
62
Example
64


Item
Unit
I
59
J
61
K
63
L





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
24.0
28.8
29.2
27.2
23.6
19.8
15.4


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0


Burning velocity
cm/s
10
10
10
10
10
10
10


(WCF)










5.5 CO2

















Comp

Example

Example

Example




Ex. 89
Example
75
Example
77
Example
79


Item
Unit
I
74
J
76
K
78
L





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
22.5
27.3
27.7
25.7
22.1
18.3
13.9


CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5


Burning velocity
cm/s
10
10
10
10
10
10
10


(WCF)










7.0 CO2

















Comp.

Example

Example

Example




Ex. 99
Example
90
Example
92
Example
94


Item
Unit
I
89
J
91
K
93
L





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
21.0
25.8
26.2
24.2
20.6
16.8
12.4


CO2
mass %
7.0
7.0
7.0
7.0
7.0
7.0
7.0


Burning velocity
cm/s
10
10
10
10
10
10
10


(WCF)
















TABLE 28







0% CO2





















Comp.

Comp.

Comp.

Comp.

Comp.





Ex. 20
Comp.
Ex. 22
Comp.
Ex. 24
Comp.
Ex. 26
Comp.
Ex. 28
















Item
M
Ex. 21
W
Ex. 23
N
Ex. 25
O
Ex. 27
P





















WCF
HFO-1132(E)
mass %
52.6
39.2
32.4
29.3
27.7
24.5
22.6
21.2
20.5



R32
mass %
0.0
5.0
10.0
14.5
18.2
27.6
36.8
44.2
51.7



R1234yf
mass %
47.4
55.8
57.6
56.2
54.1
47.9
40.6
34.6
27.8



CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
















Leak conditions to make WCFF
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,





















−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,





at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas





phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side


WCFF
HFO-1132(E)
mass %
72.0
57.8
48.7
43.6
40.6
34.9
31.4
29,2
27.1



R32
mass %
0.0
9.5
17.9
24.2
28.7
38.1
45.7
51.1
56.4



R1234yf
mass %
28.0
32.7
33.4
32.2
30.7
27.0
23.0
19.7
16.5



CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0

















Burning velocity (WCF)
cm/s
58
8
58
58
58
58
58
8
58


Buming velocity (WCFF)
cm/s
10
10
10
10
10
10
10
10
10










0.6% CO2





















Comp.

Comp.























Ex. 35
Comp.
Ex. 38
Comp.
Example 1

Example 11

Example 13


Item
C═M
Ex. 37
W
Ex. 39
N(═E═G)
Example 10
O
Example 12
P





















WCF
HFO-1132(E)
mass %
55.4
42.4
35.1
31.6
29.6
26.3
24.0
22.4
20.9



R32 mass %

0.0
5.0
10.0
14.5
18.2
27.6
36.8
44.0
51.7



R1234yf
mass %
44.0
52.0
54.3
53.3
51.6
45.5
38.6
33.0
26.8



CO2 mass %

0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6
















Leak conditions to make WCFF
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,





















−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,
−40° C., 0%,





at release, gas
at release, gas
at release,
at release,
at release, gas
at release, gas
at release,
at release,
at release,





phase side
phase side
liquid phase
liquid phase
phase side
phase side
liquid phase
liquid phase
liquid phase







side
side


side
side
side


WCFF
HFO-1132(E)
mass %
72.0
58.6
49.7
44.5
41.3
35.8
32.1
29.8
27.8



R32
mass %
0.0
8.9
16.9
23.0
27.4
36.6
44.1
49.4
54.7



R1234yf
mass %
2.7
29.1
30.2
29.4
28.3
24.8
21.1
18.2
14.9



CO2
mass %
3.3
3.4
3.2
3.1
3.0
2.8
2.7
2.6
2.6

















Buming velocity (WCF)
cm/s
58
58
58
58
58
58
58
58
58


Burning velocity (WCFF)
cm/s
10
10
10
10
10
10
10
10
10










1.2% CO2





















Comp.













Ex.49
Comp.
Example 16

Example 24

Example 26

Example 28
















Item
M
Ex.50
G═W
Example 23
N
Example 25
O
Example 27
P





















WCF
HFO-1132(E)
mass %
58.0
45.2
38.1
34.0
31.7
27.9
25.4
23.7
22.1



R32
mass %
0.0
5.0
10.0
14.4
18.2
27.6
36.8
44.0
51.7



R1234yf
mass %
40.8
48.6
50.7
48.9
48.9
43.3
36.0
31.1
25.0



CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2
















Leak conditions to make WCFF
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,





















−40° C., 0%,
−40° C., 6%,
−40° C., 6%,
−40° C., 4%,
−40° C., 4%,
−40° C., 4%,
−40° C., 4%,
−40° C., 4%,
−40° C., 4%,





release, gas
at release, gas
at release, liquid
at release, liquid
at release, liquid
at release, liquid
at release, liquid
at release, liquid
at release, liquid





phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side


WCFF
HFO-1132(E)
mass %
72.0
59.3
50.9
45.6
42.2
36.4
32.7
30.3
28.3



R32
mass %
0.0
8.3
15.8
21.7
26.2
35.3
42.8
48.1
53.4



R1234yf
mass %
24.8
28.0
28.5
27.7
26.7
23.6
20.0
17.1
13.9



CO2
mass %
3.2
4.4
4.8
5.0
4.9
4.7
4.5
4.5
4.4

















Burning velocity (WCF)
cm/s
58
58
58
<8
58
58
58
58
58


Buming velocity (WCFF)
cm/s
10
10
10
10
10
10
10
10
10










1.3% CO2





















Comp.













Ex.60

Example 36

Example 38

Example 40

Example 42
















Item
M
Example 35
W
Example 37
N
Example 39
O
Example 41
P





















WCF
HFO-1132(E)
mass %
58.2
45.5
38.4
34.3
31.9
28.1
25.6
23.9
22.3



R32
mass %
0.0
5.0
10.0
14.4
18.2
27.6
36.8
44.0
51.7



R1234yf
mass %
40.5
48.2
50.3
50.0
48.6
43.0
36.3
30.8
24.7



CO2
mass %
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3
















Leak conditions to make WCFF
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,





















−40° C., 0%,
−40° C., 8%,
−40° C., 6%,
−40° C.,6%,
−40° C., 6%,
−40° C., 4%,
−40° C., 4%,
−40° C., 4%,
−40° C., 4%,





release, gas
release, gas
at release, liquid
at release, liquid
at release, liquid
at release, liquid
at release, liquid
at release, liquid
at release, liquid





phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side


WCFF
HFO-1132(E)
mass %
72.0
59.4
51.0
45.7
42.2
36.5
32.8
30.4
28.4



R32
mass %
0.0
8.2
15.8
21.5
26.0
35.1
42.6
47.9
53.2



R1234yf
mass %
25.0
27.6
28.1
27.8
26.9
26.3
19.7
16.9
13.6



CO2
mass %
3.0
4.8
5.1
5.0
4.9
5.1
4.9
4.8
4.8

















Burning velocity (WCF)
cm/s
58
58
58
58
58
58
58
58
58


Buming velocity (WCFF)
cm/s
10
10
10
10
10
10
10
10
10
















TABLE 29







2.5% CO2





















Comp.













Ex. 70

Example 51

Example 53

Example 55

Example 57
















Item
M
Example 50
W
Example 52
N
Example 54
O
Example 56
P





















WCF
HFO-1132(E)
mass %
59.7
48.1
40.9
36.9
34.2
29.9
27.2
25.2
23.4



R32
mass %
0.0
5.0
10.0
14.4
18.2
27.6
36.8
44.0
51.7



R1234yf
mass %
37.8
44.4
46.6
46.2
45.1
40.0
33.5
28.1
22.4



CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5
















Leak conditions to make WCFF
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,





















−40° C., 26%, at
−40° C., 20%, at
−40° C., 20%, at
−40° C., 20%, at
−40° C., 18%
−40° C., 18%
−40° C., 18%
−40° C., 20%, at
−40° C., 22%, at





release, gas
release, gas
release, gas
release, gas
at release, liquid
at release, liquid
at release, liquid
release, gas
release, gas





phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side


WCFF
HFO-1132(E)
mass %
72.0
60.3
52.1
46.9
43.2
37.1
33.2
30.6
28.3



R32
mass %
0.0
7.5
14.6
20.2
24.7
34.1
41.8
47.6
53.4



R1234yf
mass %
24.9
27.4
28.4
28.0
26.7
23.4
19.7
16.9
13.8



CO2
mass %
3.1
4.8
4.9
4.9
5.4
5.4
5.4
4.9
4.5

















Buming velocity (WCF)
cm/s
8
≤8
58
58
58
58
58
58
58


Buming velocity (WCFF)
cm/s
10
10
10
10
10
10
10
10
10










4.0% CO2





















Comp.




Example 69
Example 70
Example 71
Example 72





Ex. 80

Example 66

Example 68




















Item
M
Example 65
W
Example 67
N

O

P





















WCF
HFO-1132 (E)
mass %
60.4
49.6
42.6
38.3
35.5
31.0
28.0
25.9
23.9



R32
mass %
0.0
5.0
10.0
14.4
18.2
27.6
36.8
44.0
51.7



R1234yf
mass %
35.6
41.4
43.4
43.3
42.3
37.4
31.2
26.1
20.4



CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0
















Leak conditions to make WCFF
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,





















−40° C., 32%,
−40° C., 28%,
−40° C., 28%,
−40° C., 28%
−40° C., 28%,
−40° C., 28%,
−40° C., 32%,
-40° C., 32%,
−40° C., 32%





at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas





phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side


WCFF
HFO-1132 (E)
mass %
72.0
60.9
52.9
47.5
43.8
37.4
33.1
30.5
28.1



R32
mass %
0.0
7.1
13.9
19.4
23.9
33.5
41.7
47.6
53.6



R1234yf
mass %
24.5
27.0
28.0
27.8
26.9
23.6
20.5
17.2
13.5



CO2
mass %
3.5
5.0
5.2
5.3
5.4
5.5
4.7
4.7
4.8

















Burning velocity (WCF)
cm/s
58
58
58
8
58
58
58
58
58


Buming velocity (WCFF)
cm/s
10
10
10
10
10
10
10
10
10










5.5% CO2





















Comp.













Ex. 90

Example 81

Example 83

Example 85

Example 87
















Item
M
Example 80
W
Example 82
N
Example 84
O
Example 86
P





















WCF
HFO-1132 (E)
mass %
60.7
50.3
43.3
39.0
36.3
31.6
28.4
26.2
24.2



R32
mass %
0.0
5.0
10.0
14.4
18.2
27.6
36.8
44.0
51.7



R1234yf
mass %
33.8
39.2
41.2
41.1
40.0
35.3
29.3
24.3
18.6



CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5
















Leak conditions to make WCFF
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,





















−40° C., 36%,
-40° C., 34%,
−40° C., 34%,
−40° C., 32%,
−40° C., 34%,
−40° C., 36%,
−40° C., 38%
-40° C., 40%,
40°° C., 40%,





at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas





phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side


WCFF
HFO-1132 (E)
mass %
72.0
61.2
53.2
47.8
44.2
37.6
33.2
30.3
27.9



R32
mass %
0.0
6.8
13.5
19.0
23.4
33.2
41.7
47.9
54.2



R1234yf
mass %
24.5
27.0
28.1
27.7
26.8
23.9
20.2
17.3
13.3



CO2
mass %
3.5
5.0
5.2
5.5
5.6
5.3
4.9
4.5
4.6

















Burning velocity (WCF)
cm/s
58
58
≤8
58
58
58
58
58
58


Burning velocity (WCFF)
cm/s
10
10
10
10
10
10
10
10
10










7.0% CO2





















Comp. Ex.













100

Example 96

Example 98

Example 100

Example 102
















Item
M
Example 95
W
Example 97
N
Example 99
O
Example 101
P





















WCF
HFO-1132(E)
mass %
60.7
50.3
43.7
39.5
36.7
31.9
28.6
26.4
24.2



R32
mass %
0.0
5.0
10.0
14.4
18,2
27.6
36.8
44.0
51.7



R1234yf
mass %
32.3
37.7
39.3
39.1
38.1
33.5
27.6
22.6
17.1



CO2
mass %
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0
















Leak conditions to make WCFF
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,
Storage/transport,





















−40° C., 42%,
−40° C., 34%,
−40° C., 38%,
−40° C., 40%,
-40° C., 40%,
−40° C., 42%,
−40° C., 42%,
−40° C., 42%,
-40° C., 44%,





at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas
at release, gas





phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side
phase side


WCFF
HFO-1132(E)
mass %
72.0
61.2
53.4
48.1
44.4
37.7
33.2
30.4
27.8



R32
mass %
0.0
6.8
13.3
18.7
23.2
33.1
41.7
47.9
54.6



R1234yf
mass %
24.4
27.0
27.8
28.1
27.1
24.1
19.8
16.3
12.7



CO2
mass %
3.6
5.0
5.5
5.1
5.3
5.1
5.3
5.4
4.9

















Burning velocity (WCF)
cm/s
58
8
58
58
58
58
58
58
58


Burning velocity (WCFF)
cm/s
10
10
10
10
10
10
10
10
10









These results indicate that when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum is respectively represented by w, x, y, and z, the mixed refrigerant has a lower WCF flammability when coordinates (x,y,z) in the ternary composition diagram shown in FIGS. 1B to 1I, in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass %, are on the line segments that connect point I, point J, point K, and point L, or below these line segments.


The results further indicate that the refrigerant has a lower ASHRAE flammability when coordinates (x,y,z) in the ternary composition diagram shown in FIG. 1B are on the line segments that connect point M, point N, point, 0, and point P, or below these line segments.


Mixed refrigerants were prepared by mixing R32, HFO-1132(E), and R1234yf in amounts in terms of mass % shown in Tables 30 to 40, based on their sum. The coefficient of performance (COP) ratio and the refrigerating capacity ratio of the mixed refrigerants shown in Tables 30 to 37 relative to those of R410 were determined.


The GWP of compositions comprising a mixture of R410A (R32=50%/R125=50%) and R1234yf was evaluated based on the value stated in the Intergovernmental Panel on Climate Change (IPCC), fourth report. The GWP of HFO-1132(E), which is not stated in the report; was assumed to be 1 from HFO-1132a (GWP=1 or less) and HFO-1123 (GWP=03, described in PTL 1). The refrigerating capacity of R4 t 0A and that of compositions comprising a mixture of HFO-1132(E), HFO-1123, and R1234yf were determined by performing theoretical refrigeration cycle calculations for mixed refrigerants using the National Institute of Science and Technology (NIST) Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0) under the following conditions.

    • Evaporating temperature: 5° C.
    • Condensation temperature: 45° C.
    • Superheating temperature: 1 K
    • Supercooling temperature: 5 K
    • Ecomp (compressive modulus): 0.7 kWh


Tables 30 to 37 show these values together with the GWP of each mixed refrigerant. Tables 30 to 37 show cases at a CO2 concentration of 0 mass %, 0.6 mass %, 1.2 mass %, 1.3 mass %, 2.5 mass %, 4 mass %, 5.5 mass %, and 7 mass %, respectively.









TABLE 30





0% CO2




























Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.




Comp.
Ex. 2
Ex. 3
Ex. 4
Ex. 5
Ex. 6
Ex. 7
Ex. 8
Ex. 9


Item
Unit
Ex. 1
A
B
A’
B’
A”
B”
C
D





HFO-1132(E)
mass %
R410A
81.6
0.0
63.1
0.0
48.2
0.0
58.3
0.0


R32
mass %

18.4
18.1
36.9
36.7
51.8
51.5
0.0
40.3


R1234yf
mass %

0.0
81.9
0.0
63.3
0.0
49.5
41.7
59.7


CO2
mass %

0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

2088
125
125
250
250
350
350
2
274


COP ratio
% (relative
100
98.7
103.6
98.7
102.3
99.2
102.1
100.3
102.2



to R410A)











Refrigerating
% (relative
100
105.3
62.5
109.9
77.5
112.1
87.0
80.0
80.0


capacity ratio
to R410A)











Condensation glide
° C.
0.1
0.3
6.8
0.1
4.5
0.0
2.7
2.9
4.0







Comp.
Comp.
Comp.
Comp.

Comp.

Comp.





Ex. 10
Ex. 11
Ex. 12
Ex. 13
Comp.
Ex. 15
Comp.
Ex. 17
Comp.


Item
Unit
E
F
G
I
Ex. 14
J
Ex. 16
K
Ex. 18





HFO-1132(E)
mass %
31.9
5.2
26.2
72.0
57.2
48.5
41.2
35.6
32.0


R32
mass %
18.2
36.7
22.2
0.0
10.0
18.3
27.6
36.8
44.2


R1234yf
mass %
49.9
58.1
51.6
28.0
32.8
33.2
31.2
27.6
23.8


CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

125
250
152
2
69
125
188
250
300


COP ratio
% (relative
100.3
101.8
100.5
99.9
99.5
99.4
99.5
99.6
99.8



to R410A)











Refrigerating
% (relative
82.3
80.8
82.4
86.6
88.4
90.9
94.2
97.7
100.5


capacity ratio
to R410A)











Condensation glide
° C.
4.4
4.3
4.5
1.7
2.6
2.7
2.4
1.9
1.6























Comp.
Comp.

Comp.

Comp.

Comp.






Ex. 19
Ex. 20
Comp.
Ex. 22
Comp.
Ex. 24
Comp.
Ex. 26
Comp.
Ex. 28


Item
Unit
L
M
Ex. 21
W
Ex. 23
N
Ex. 25
O
Ex. 27
P





HFO-1132(E)
mass %
28.9
52.6
39.2
32.4
29.3
27.7
24.5
22.6
21.2
20.5


R32
mass %
51.7
0.0
5.0
10.0
14.5
18.2
27.6
36.8
44.2
51.7


R1234yf
mass %
19.4
47.4
55.8
57.6
56.2
54.1
47.9
40.6
34.6
27.8


CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

350
2
36
70
100
125
188
250
300
350


COP ratio
% (relative
100.1
100.5
100.9
100.9
100.8
100.7
100.4
100.4
100.5
100.6



to R410A)












Refrigerating
% (relative
103.3
77.1
74.8
75.6
77.8
80.0
85.5
91.0
95.0
99.1


capacity ratio
to R410A)












Condensation glide
° C.
1.2
3.4
4.7
5.2
5.1
4.9
4.0
3.0
2.3
1.7
















TABLE 31





0.6% CO2



























Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.





Ex. 29
Ex. 30
Ex. 31
Ex. 32
Ex. 33
Ex. 34
Ex. 35
Ex. 36
Example 1


Item
Unit
A
B
A’
B’
A”
B”
C═M
D
E═G═N





HFO-1132(E)
mass %
81.0
0.0
62.5
0.0
47.6
0.0
55.4
0.0
29.6


R32
mass %
18.4
18.1
36.9
36.7
51.8
51.6
0.0
38.6
18.2


R1234yf
mass %
0.0
81.3
0.0
62.7
0.0
47.8
44.0
60.8
51.6


CO2
mass %
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6


GWP

125
125
250
250
350
350
2
263
125


COP ratio
% (relative
98.4
103.4
98.4
102.1
99.0
102.0
100.1
102.1
100.2



to R410A)











Refrigerating
% (relative
106.5
63.7
111.1
78.7
113.1
88.6
80.0
80.0
82.4


capacity ratio
to R410A)











Condensation glide
° C.
0.7
7.5
0.4
4.9
0.3
3.0
3.9
4.7
5.2







Example 2
Example 3
Example
Example 5
Example
Example 7
Example
Example 9
Comp.


Item
Unit
F
I
4
J
6
K
8
L
Ex. 37





HFO-1132(E)
mass %
2.7
72.0
57.2
48.5
41.2
35.6
32.0
28.9
42.4


R32
mass %
36.7
0.0
10.0
18.3
27.6
36.8
44.2
51.7
5.0


R1234yf
mass %
60.0
27.4
32.6
32.6
30.6
27.0
23.3
10.8
52.0


CO2
mass %
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6


GWP

250
2
69
125
188
250
300
350
36


COP ratio
% (relative
101.8
99.5
99.2
99.1
99.2
99.4
99.6
99.7
100.3



to R410A)











Refrigerating
% (relative
80.4
88.1
89.7
92.3
95.5
99.0
101.7
108.2
77.9


capacity ratio
to R410A)











Condensation glide
° C.
4.8
5.2
2.4
3.2
3.1
2.8
2.3
1.9
3.9



















Comp. Ex. 38
Comp.
Example
Example 11
Example
Example 13


Item
Unit
W
Ex. 39
10
O
12
P





HFO-1132(E)
mass %
35.1
31.6
26.3
24.0
22.4
20.9


R32
mass %
10.0
14.5
27.6
36.8
44.0
51.7


R1234yf
mass %
54.3
53.3
45.5
38.6
33.0
26.8


CO2
mass %
0.6
0.6
0.6
0.6
0.6
0.6


GWP

70
100
188
250
299
350


COP ratio
% (relative
100.4
100.3
100.1
100.1
100.2
100.4



to R410A)








Refrigerating
% (relative
78.5
80.4
87.8
93.0
96.8
100.5


capacity ratio
to R410A)








Condensation glide
° C.
5.1
5.5
5.4
5.1
4.2
3.2
















TABLE 32





1.2% CO2



























Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.





Ex. 40
Ex. 41
Ex. 42
Ex. 43
Ex. 44
Ex. 45
Ex. 46
Ex. 47
Example 14


Item
Unit
A
B
A’
B’
A”
B”
C
D
E





HFO-1132(E)
mass %
80.4
0.0
61.9
0.0
47.0
0.0
52.4
0.0
26.5


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
36.8
18.2


R1234yf
mass %
0.0
80.7
0.0
62.2
0.0
46.9
46.4
62.0
54.1


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

125
125
250
250
350
350
2
251
125


COP ratio
% (relative
98.1
103.2
98.2
101.9
98.7
101.7
99.9
101.9
100.2



to R410A)











Refrigerating
% (relative
107.7
65.0
112.2
79.8
114.2
89.9
80.0
80.0
82.0


capacity ratio
to R410A)











Condensation glide
° C.
1.2
8.1
0.8
5.4
0.6
3.4
4.9
5.3
6.0







Example
Example
Comp.

Example

Example

Example




15
16
Ex. 48
Example
18
Example
20
Example
22


Item
Unit
F
G═W
I
17
J
19
K
21
L





HFO-1132(E)
mass %
0.3
38.1
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
36.6
10.0
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
61.9
50.7
26.8
31.6
32.0
30.0
26.4
22.7
18.2


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

250
70
2
69
125
188
250
300
350


COP ratio
% (relative
101.9
99.9
99.2
98.9
98.8
98.9
99.1
99.4
99.6



to R410A)











Refrigerating
% (relative
80.0
81.6
89.7
91.3
93.7
96.9
100.3
103.0
105.8


capacity ratio
to R410A)











Condensation glide
° C.
5.4
5.7
3.1
3.6
3.6
3.2
2.6
2.2
1.8





















Comp.











Ex. 49
Comp.

Example 24

Example 26

Example 28


Item
Unit
M
Ex. 50
Example 23
N
Example 25
O
Example 27
P





HFO-1132(E)
mass %
58.0
45.2
34.0
31.7
27.9
25.4
23.7
22.1


R32
mass %
0.0
5.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
40.8
48.6
48.9
48.9
43.3
36.0
31.1
25.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

2
36
100
125
188
250
298
350


COP ratio
% (relative
99.6
99.8
99.8
99.8
99.7
99.7
99.9
100.0



to R410A)










Refrigerating
% (relative
82.9
80.9
83.6
84.9
90.0
95.3
98.7
102.4


capacity ratio
to R410A)










Condensation glide
° C.
4.3
5.4
5.6
5.4
4.4
3.4
2.8
2.2
















TABLE 33





1.3% CO2



























Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.




Ex. 51
Ex. 52
Ex. 53
Ex. 54
Ex. 55
Ex. 56
Ex. 57
Ex. 58
Ex. 59


Item
Unit
A
B
A’
B’═D═F
A”
B”
C
E
I





HFO-1132(E)
mass %
80.3
0.0
61.8
0.0
46.9
0.0
51.9
26.1
72.0


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
18.2
0.0


R1234yf
mass %
0.0
80.6
0.0
62.1
0.0
47.1
46.8
54.4
26.7


CO2
mass %
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3


GWP

125
125
250
250
350
350
2
125
2


COP ratio
% (relative
98.0
103.2
98.1
101.9
98.7
101.7
99.8
100.2
99.1



to R410A)











Refrigerating
% (relative
107.9
65.2
112.3
80.0
114.3
90.0
80.0
82.0
89.9


capacity ratio
to R410A)











Condensation glide
° C.
1.2
8.2
0.8
5.4
0.7
3.4
5.1
6.1
3.2








Example

Example

Example
Comp.

Example




Example
30
Example
32
Example
34
Ex. 60
Example
36


Item
Unit
29
J
31
K
33
L
M
35
W





HFO-1132 (E)
mass %
57.2
48.5
41.2
35.6
32.0
28.9
58.2
45.5
38.4


R32
mass %
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0
10.0


R1234yf
mass %
31.5
31.9
29.9
26.3
22.6
18.1
40.5
48.2
50.3


CO2
mass %
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3


GWP

69
125
188
250
300
350
2
36
70


COP ratio
% (relative
98.9
98.8
98.9
99.1
99.3
99.6
99.5
99.8
99.8



to R410A)











Refrigerating
% (relative
91.5
93.9
97.1
100.5
103.2
106.0
83.3
81.3
82.0


capacity ratio
to R410A)











Condensation glide
° C.
3.7
3.6
3.2
2.7
2.3
1.8
4.4
5.4
5.8




















Example 38

Example 40

Example 42


Item
Unit
Example 37
N
Example 39
O
Example 41
P





HFO-1132(E)
mass %
34.3
31.9
28.1
25.6
23.9
22.3


R32
mass %
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
50.0
48.6
43.0
36.3
30.8
24.7


CO2
mass %
1.3
1.3
1.3
1.3
1.3
1.3


GWP

100
125
188
250
298
350


COP ratio
% (relative
99.8
99.8
99.6
99.7
99.8
100.0



to R410A)








Refrigerating
% (relative
83.5
85.2
90.3
95.4
99.0
102.7


capacity ratio
to R410A)








Condensation glide
° C.
6
5.4
4.5
3.5
2.9
2.3
















TABLE 34





2.5% CO2



























Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Example




Ex. 61
Ex. 62
Ex. 63
Ex. 64
Ex. 65
Ex. 66
Ex. 67
Ex. 68
43


Item
Unit
A
B
A’
B’
A”
B”
C
D
E





HFO-1132(E)
mass %
79.1
0.0
60.6
0.0
45.7
0.0
46.2
0.0
20.9


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
33.2
18.2


R1234yf
mass %
0.0
79.4
0.0
60.9
0.0
45.9
51.3
64.3
58.4


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

125
125
250
250
350
350
3
227
125


COP ratio
% (relative
97.4
102.7
97.6
101.5
98.3
101.3
99.6
101.6
100.2



to R410A)











Refrigerating
% (relative
110.3
67.8
114.5
82.5
116.4
92.5
80.0
80.0
81.7


capacity ratio
to R410A)











Condensation glide
° C.
2.0
9.5
1.5
6.3
1.3
4.1
7.1
6.9
7.6







Comp.

Example

Example

Example
Comp.





Ex. 69
Example
45
Example
47
Example
49
Ex. 70
Example


Item
Unit
I
44
J
46
K
48
L
M
50





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9
59.7
48.1


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0


R1234yf
mass %
25.5
30.3
30.7
28.7
25.1
21.3
16.9
37.8
44.4


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

2
69
125
188
250
300
350
2
36


COP ratio
% (relative
98.4
98.2
98.2
98.4
98.6
98.9
99.1
98.8
99.0



to R410A)











Refrigerating
% (relative
93.1
94.5
96.7
99.8
103.1
105.9
108.6
87.1
85.7


capacity ratio
to R410A)











Condensation glide
° C.
4.4
4.7
4.5
3.9
3.3
2.8
2.4
5.6
6.3




















Example 51
Example
Example 53
Example
Example 55
Example
Example 57


Item
Unit
W
52
N
54
O
56
P





HFO-1132(E)
mass %
40.9
36.9
34.2
29.9
27.2
25.2
23.4


R32
mass %
10.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
46.6
46.2
45.
40.0
33.5
28.1
22.4


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

70
99
125
188
250
298
350


COP ratio
% (relative
99.1
99.1
99.1
99.0
99.1
99.3
99.5



to R410A)









Refrigerating
% (relative
86.2
87.7
89.2
94.0
98.8
102.4
105.8


capacity ratio
to R410A)









Condensation glide
° C.
6
6.3
6.0
5.0
4.0
3.4
2.8
















TABLE 35





4% CO2



























Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Example




Ex. 71
Ex. 72
Ex. 73
Ex. 74
Ex. 75
Ex. 76
Ex. 77
Ex. 78
58


Item
Unit
A
B
A’
B’
A”
B”
C
D
E





HFO-1132(E)
mass %
77.6
0.0
59.1
0.0
44.2
0.0
39.5
0.0
14.7


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
28.9
18.1


R1234yf
mass %
0.0
77.9
0.0
59.4
0.0
44.4
56.5
67.1
63.2


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

125
125
250
249
350
350
3
198
125


COP ratio
% (relative
96.7
102.2
97.0
101.0
97.7
100.8
99.4
101.3
100.4



to R410A)











Refrigerating
% (relative
113.3
71.2
117.3
85.7
118.9
95.6
80.0
80.0
81.2


capacity ratio
to R410A)











Condensation glide
° C.
3.0
10.9
2.2
7.2
2.0
5.0
9.6
8.7
9.6







Comp.





Example
Comp.





Ex. 79
Example
Example 60
Example
Example 62
Example
64
Ex. 80
Example


Item
Unit
I
59
J
61
K
63
L
M
65





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9
60.4
49.6


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0


R1234yf
mass %
24.0
28.8
29.2
27.2
23.6
19.8
15.4
35.6
41.4


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

2
69
125
188
250
300
350
2
36


COP ratio
% (relative
97.6
97.5
97.5
97.7
98.0
98.3
98.6
98.0
98.2



to R410A)











Refrigerating
% (relative
97.0
98.1
100.2
103.2
106.5
109.1
111.8
91.3
90.2


capacity ratio
to R410A)











Condensation glide
° C.
5.8
5.8
5.4
4.7
4.0
3.5
3.1
6.9
7.4










Example 66
Example
Example 68
Example
Example 70
Example
Example 72


Item
Unit
W
67
N
69
O
71
P





HFO-1132(E)
mass %
42.6
38.3
35.5
31.0
28.0
25.9
23.9


R32
mass %
10.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
43.4
43.3
42.3
37.4
31.2
26.1
20.4


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

70
99
125
188
250
298
350


COP ratio
% (relative
98.3
98.3
98.3
98.3
98.5
98.7
98.9



to R410A)









Refrigerating
% (relative
90.7
92.0
93.4
97.9
102.5
105.9
109.3


capacity ratio
toR410A)









Condensation glide
° C.
7
7.2
6.9
5.8
4.7
4.0
3.4
















TABLE 36





5.5% CO2



























Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Example




Ex. 81
Ex. 82
Ex. 83
Ex. 84
Ex. 85
Ex. 86
Ex. 87
Ex. 88
73


Item
Unit
A
B
A’
B’
A”
B”
C
D
E





HFO-1132(E)
mass %
76.1
0.0
57.6
0.0
42.7
0.0
33.0
0.0
8.8


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
24.7
18.1


R1234yf
mass %
0.0
76.4
0.0
57.9
0.0
42.9
61.5
69.8
67.6


CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

125
125
250
249
350
350
3
170
125


COP ratio
% (relative
96.0
101.8
96.4
100.5
97.2
100.3
99.4
101.2
100.6



to R410A)











Refrigerating
% (relative
116.2
74.6
119.9
88.9
121.5
98.7
80.0
80.0
80.8


capacity ratio
to R410A)











Condensation glide
° C.
3.7
12.3
2.9
8.2
2.6
5.8
12.1
10.8
11.5







Comp.

Example

Example

Example
Comp.





Ex. 89
Example
75
Example
77
Example
79
Ex. 90
Example


Item
Unit
I
74
J
76
K
78
L
M
80





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9
60.7
50.3


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0


R1234yf
mass %
22.5
27.3
27.7
25.7
22.1
18.3
13.9
33.8
39.2


CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

2
69
125
188
250
299
350
2
36


COP ratio
% (relative
96.8
96.8
96.9
97.1
97.4
97.7
98.0
97.2
97.4



to R410A)











Refrigerating
% (relative
100.9
101.8
103.8
106.6
109.8
112.4
115.0
95.4
94.3


capacity ratio
to R410A)











Condensation glide
° C.
6.9
6.7
6.2
5.4
4.7
4.1
3.7
8.1
8.5




















Example

Example








81
Example
83

Example 85

Example 87


Item
Unit
W
82
N
Example 84
O
Example 86
P





HFO-1132(E)
mass %
43.3
39.0
36.3
31.6
28.4
26.2
24.2


R32
mass %
10.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
41.2
41.1
40.0
35.3
29.3
24.3
18.6


CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

70
99
125
188
250
298
350


COP ratio
% (relative
97.5
97.6
97.6
97.7
97.9
98.1
98.3



to R410A)









Refrigerating
% (relative
94.7
95.9
97.4
101.6
106.1
109.3
112.6


capacity ratio
to R410A)









Condensation glide
° C.
8
8.1
7.6
6.5
5.4
4.7
4.0
















TABLE 37





7% CO2



























Comp. Ex.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp. Ex.
Comp.





91
Ex. 92
Ex. 93
Ex. 94
Ex. 95
Ex. 96
97
Ex. 98
Example 88


Item
Unit
A
B
A’
B’
A”
B”
C
D
E





HFO-1132(E)
mass %
74.6
0.0
56.1
0.0
41.2
0.0
26.8
0.0
3.1


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
20.5
18.1


R1234yf
mass %
0.0
74.9
0.0
56.4
0.0
41.4
66.2
72.5
71.8


CO2
mass %
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0


GWP

125
125
250
249
350
350
3
141
125


COP ratio
% (relative
95.3
101.3
95.8
100.0
96.7
99.8
99.5
101.1
100.9



to R410A)











Refrigerating
% (relative
119.0
78.0
122.6
92.2
124.0
101.9
80.0
80.0
80.3


capacity ratio
to R410A)











Condensation
° C.
4.4
13.6
3.4
9.0
3.1
6.5
14.6
13.0
13.3


glide







Comp.

Example

Example

Example
Comp.





Ex. 99
Example
90
Example
92
Example
94
Ex. 100
Example


Item
Unit
I
89
J
91
K
93
L
M
95





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9
60.7
50.3


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0


R1234yf
mass %
21.0
25.8
26.2
24.2
20.6
16.8
12.4
32.3
37.7


CO2
mass %
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0


GWP

2
69
125
188
250
299
350
2
36


COP ratio
% (relative
96.0
96.1
96.2
96.5
96.8
97.1
97.5
96.5
96.7



to R410A)











Refrigerating
% (relative
104.7
105.5
107.3
110.0
113.1
115.6
118.2
99.2
98.0


capacity ratio
to R410A)











Condensation
° C.
7.9
7.5
6.9
6.0
5.3
4.7
4.2
9.2
9.4


glide




















Example

Example

Example

Example




96

98

100

102


Item
Unit
W
Example 97
N
Example 99
O
Example 101
P





HFO-1132(E)
mass %
43.7
39.5
36.7
31.9
28.6
26.4
24.2


R32
mass %
10.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
39.3
39.1
38.1
33.5
27.6
22.6
17.1


CO2
mass %
7.0
7.0
7.0
7.0
7.0
7.0
7.0


GWP

70
99
125
188
250
298
350


COP ratio
% (relative
96.9
96.9
97.0
97.1
97.3
97.5
97.8



to R410A)









Refrigerating
% (relative
98.6
99.7
101.1
105.2
109.5
112.7
115.8


capacity ratio
to R410A)









Condensation
° C.
9
8.8
8.4
7.1
6.0
5.2
4.6


glide

























TABLE 38









Comp.
Comp.
Comp.
Example
Example
Comp.
Comp.
Comp.


Item
Unit
Ex. 101
Ex. 102
Ex. 103
103
104
Ex. 104
Ex. 105
Ex. 106





HFO-1132(E)
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
mass %
78.8
68.8
58.8
48.8
38.8
28.8
18.8
8.8


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

532
465
398
331
264
197
130
63


COP ratio
% (relative
101.3
101.2
101.1
101.0
101.0
101.3
102.0
102.8



to R410A)










Refrigerating
% (relative
108.5
104.1
99.2
93.6
87.2
80.1
72.2
63.1


capacity ratio
to R410A)










Condensation glide
° C.
1.1
1.6
2.2
3.1
4.3
5.8
7.4
8.4







Comp.
Comp.
Example
Example
Example
Comp.
Comp.
Comp.


Item
Unit
Ex. 107
Ex. 108
105
106
107
Ex. 109
Ex. 110
Ex. 111





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
30.0


R32
mass %
68.8
58.8
48.8
38.8
28.8
18.8
8.8
58.8


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
10.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

465
398
331
264
197
130
62
398


COP ratio
% (relative
100.6
100.5
100.4
100.3
100.4
100.9
101.8
100.0



to R410A)










Refrigerating
% (relative
108.6
103.9
98.6
92.6
85.8
78.2
69.6
108.3


capacity ratio
to R410A)










Condensation glide
° C.
1.1
1.7
2.5
3.5
4.8
6.4
7.7
1.2







Example
Example
Example
Example
Comp.
Comp.
Comp.
Example


Item
Unit
108
109
110
111
Ex. 112
Ex. 113
Ex. 114
112





HFO-1132(E)
mass %
30.0
30.0
30.0
30.0
30.0
40.0
40.0
40.0


R32
mass %
48.8
38.8
28.8
18.8
8.8
48.8
38.8
28.8


R1234yf
mass %
20.0
30.0
40.0
50.0
60.0
10.0
20.0
30.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

331
263
196
129
62
330
263
196


COP ratio
% (relative
99.9
99.8
99.8
100.1
100.8
99.4
99.3
99.3



to R410A)










Refrigerating
% (relative
103.2
97.5
91.0
83.7
75.6
107.5
102.0
95.8


capacity ratio
to R410A)










Condensation glide
° C.
1.8
2.7
3.8
5.2
6.6
1.3
2.0
2.9







Example
Example
Comp.
Comp.
Comp.
Example
Comp.
Comp.


Item
Unit
113
114
Ex. 115
Ex. 116
Ex. 117
115
Ex. 118
Ex. 119





HFO-1132(E)
mass %
40.0
40.0
50.0
50.0
50.0
50.0
60.0
60.0


R32
mass %
18.8
8.8
38.8
28.8
18.8
8.8
28.8
18.8


R1234yf
mass %
40.0
50.0
10.0
20.0
30.0
40.0
10.0
20.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

129
62
263
196
129
62
195
128


COP ratio
% (relative
99.5
100.0
99.0
98.9
99.0
99.4
98.7
98.7



to R410A)










Refrigerating
% (relative
88.9
81.1
106.2
100.3
93.7
86.2
104.5
98.2


capacity ratio
to R410A)










Condensation glide
° C.
4.1
5.4
1.4
2.2
3.2
4.3
1.5
2.4







Comp.
Comp.
Comp.
Comp.
Example
Example
Example
Example


Item
Unit
Ex. 120
Ex. 121
Ex. 122
Ex. 123
116
117
118
119





HFO-1132(E)
mass %
60.0
70.0
70.0
80.0
15.0
15.0
15.0
15.0


R32
mass %
8.8
18.8
8.8
8.8
48.8
46.3
43.8
41.3


R1234yf
mass %
30.0
10.0
20.0
10.0
35.0
37.5
40.0
42.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

61
128
61
61
331
314
297
281


COP ratio
% (relative
99.0
98.5
98.8
98.6
100.7
100.7
100.6
100.6



to R410A)










Refrigerating
% (relative
91.0
102.4
95.5
99.7
96.1
94.7
93.1
91.6


capacity ratio
to R410A)










Condensation glide
° C.
3.3
1.7
2.5
1.9
2.8
3.0
3.3
3.6







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
120
121
122
123
124
125
126
127





HFO-1132(E)
mass %
15.0
15.0
15.0
15.0
15.0
17.5
17.5
17.5


R32
mass %
38.8
36.3
33.8
31.3
28.8
48.8
46.3
43.8


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
32.5
35.0
37.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

264
247
230
214
197
331
314
297


COP ratio
% (relative
100.6
100.7
100.7
100.7
100.8
100.5
100.5
100.5



to R410A)










Refrigerating
% (relative
89.9
88.3
86.6
84.8
83.0
97.4
95.9
94.4


capacity ratio
to R410A)










Condensation glide
° C.
3.9
4.2
4.6
4.9
5.3
2.6
2.9
3.1

























TABLE 39









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
128
129
130
131
132
133
134
135





HFO-1132(E)
mass %
17.5
17.5
17.5
17.5
17.5
17.5
17.5
20.0


R32
mass %
41.3
38.8
36.3
33.8
31.3
28.8
26.3
46.3


R1234yf
mass %
40.0
42.5
45.0
47.5
50.0
52.5
55.0
32.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

281
264
247
230
213
197
180
314


COP ratio
% (relative
100.5
100.5
100.5
100.5
100.6
100.6
100.7
100.4



to R410A)










Refrigerating
% (relative
92.9
91.3
89.6
87.9
86.2
84.4
82.6
97.1


capacity ratio
to R410A)










Condensation glide
° C.
3.4
3.7
4.0
4.3
4.7
5.1
5.4
2.7







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
136
137
138
139
140
141
142
143





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
22.5
22.5


R32
mass %
43.8
41.3
36.3
33.8
31.3
26.3
46.3
43.8


R1234yf
mass %
35.0
37.5
42.5
45.0
47.5
52.5
30.0
32.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

297
280
247
230
213
180
314
297


COP ratio
% (relative
100.3
100.3
100.3
100.3
100.4
100.5
100.2
100.2



to R410A)










Refrigerating
% (relative
95.7
94.1
90.9
89.3
87.5
84.0
98.4
96.9


capacity ratio
to R410A)










Condensation glide
° C.
2.9
3.2
3.8
4.1
4.4
5.2
2.5
2.7







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
144
145
146
147
148
149
150
151





HFO-1132(E)
mass %
22.5
22.5
22.5
22.5
22.5
22.5
22.5
22.5


R32
mass %
41.3
38.8
36.3
33.8
31.3
28.8
26.3
23.8


R1234yf
mass %
35.0
37.5
40.0
42.5
45.0
47.5
50.0
52.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

280
264
247
230
213
197
180
163


COP ratio
% (relative
100.2
100.2
100.2
100.2
100.2
100.3
100.3
100.4



to R410A)










Refrigerating
% (relative
95.4
93.8
92.2
90.6
88.9
87.1
85.3
83.5


capacity ratio
to R410A)










Condensation glide
° C.
3.0
3.3
3.6
3.9
4.2
4.5
4.9
5.3







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
152
153
154
155
156
157
158
159





HFO-1132(E)
mass %
25.0
25.0
25.0
25.0
25.0
25.0
27.5
27.5


R32
mass %
33.8
31.3
28.8
26.3
23.8
21.3
21.9
21.9


R1234yf
mass %
40.0
42.5
45.0
47.5
50.0
52.5
45.0
47.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

230
213
196
180
163
146
150
150


COP ratio
% (relative
100.0
100.0
100.1
100.1
100.2
100.3
100.0
100.1



to 410A)










Refrigerating
% (relative
91.8
90.2
88.4
86.7
84.8
83.0
86.3
85.4


capacity ratio
to 410A)










Condensation glide
° C.
3.6
4.0
4.3
4.7
5.0
5.4
4.8
4.9


















Example
Example
Example
Example
Example


Item
Unit
160
161
162
163
164





HFO-1132(E)
mass %
27.5
27.5
30.0
32.0
34.0


R32
mass %
21.9
21.9
21.9
21.9
13.8


R1234yf
mass %
50.0
52.5
52.5
51.0
51.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2


GWP

150
150
150
150
96


COP ratio
% (relative
100.1
100.2
100.1
100.0
100.1



to R410A)







Refrigerating
% (relative
84.5
83.7
84.2
85.1
82.0


capacity ratio
to R410A)







Condensation glide
° C.
5.1
5.2
5.0
4.9
5.5

























TABLE 40









Comp.
Comp.
Comp.
Example
Example
Example
Comp.
Comp.


Item
Unit
Ex. 125
Ex. 126
Ex. 127
166
167
168
Ex. 128
Ex. 129





HFO-1132(E)
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
mass %
77.5
67.5
57.5
47.5
37.5
27.5
17.5
7.5


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

524
457
389
322
255
188
121
54


COP ratio
% (relative
100.9
100.8
100.6
100.5
100.5
100.9
101.6
102.4



to R410A)










Refrigerating
% (relative
110.6
106.2
101.2
95.5
89.1
81.9
74.0
64.8


capacity ratio
to R410A)










Condensation glide
° C.
1.8
2.3
3.0
4.0
5.3
7.0
8.8
10.1







Comp.
Comp.
Example
Example
Example
Comp.
Comp.
Comp.


Item
Unit
Ex. 130
Ex. 131
169
170
171
Ex. 132
Ex. 133
Ex. 134





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
30.0


R32
mass %
67.5
57.5
47.5
37.5
27.5
17.5
7.5
57.5


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
10.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

456
389
322
255
188
121
54
389


COP ratio
% (relative
100.1
100.0
99.9
99.8
100.0
100.5
101.3
99.5



to R410A)










Refrigerating
% (relative
110.7
106.0
100.6
94.5
87.7
80.1
71.5
110.4


capacity ratio
to R410A)










Condensation glide
° C.
1.8
2.5
3.3
4.4
5.9
7.7
9.3
1.9







Example
Example
Example
Example
Comp.
Comp.
Comp.
Example


Item
Unit
172
173
174
175
Ex. 135
Ex. 136
Ex. 137
176





HFO-1132(E)
mass %
30.0
30.0
30.0
30.0
30.0
40.0
40.0
40.0


R32
mass %
47.5
37.5
27.5
17.5
7.5
47.5
37.5
27.5


R1234yf
mass %
20.0
30.0
40.0
50.0
60.0
10.0
20.0
30.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

322
255
188
120
53
321
254
187


COP ratio
% (relative
99.3
99.2
99.3
99.6
100.3
98.9
98.8
98.7



to R410A)










Refrigerating
% (relative
105.3
99.5
93.0
85.7
77.5
109.6
104.1
97.9


capacity ratio
to R410A)










Condensation glide
° C.
2.6
3.6
4.8
6.4
8.1
2.0
2.8
3.9







Example
Example
Comp.
Comp.
Comp.
Example
Comp.
Comp.


Item
Unit
177
178
Ex. 138
Ex. 139
Ex. 140
179
Ex. 141
Ex. 142





HFO-1132(E)
mass %
40.0
40.0
50.0
50.0
50.0
50.0
60.0
60.0


R32
mass %
17.5
7.5
37.5
27.5
17.5
7.5
27.5
17.5


R1234yf
mass %
40.0
50.0
10.0
20.0
30.0
40.0
10.0
20.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

120
53
254
187
120
53
187
120


COP ratio
% (relative
98.9
99.4
98.4
98.3
98.4
98.8
98.0
98.1



to R410A)










Refrigerating
% (relative
91.0
83.1
108.4
102.5
95.9
88.4
106.8
100.4


capacity ratio
to R410A)










Condensation glide
° C.
5.3
6.8
2.2
3.1
4.3
5.6
2.4
3.4







Example
Comp.
Comp.
Comp.
Example
Example
Example
Example


Item
Unit
180
Ex. 143
Ex. 144
Ex. 145
181
182
183
184





HFO-1132 (E)
mass %
60.0
70.0
70.0
80.0
15.0
15.0
15.0
15.0


R32
mass %
7.5
17.5
7.5
7.5
50.0
47.5
45.0
42.5


R1234yf
mass %
30.0
10.0
20.0
10.0
32.5
35.0
37.5
40.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

52
119
52
52
339
322
305
289


COP ratio
% (relative
98.4
97.9
98.1
98.0
100.2
100.2
100.2
100.2



to R410A)










Refrigerating
% (relative
93.3
104.7
97.8
102.1
99.6
98.1
96.6
95.1


capacity ratio
to R410A)










Condensation glide
° C.
4.6
2.7
3.8
3.0
3.4
3.6
3.9
4.2







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
185
186
187
188
189
190
191
192





HFO-1132(E)
mass %
15.0
15.0
15.0
15.0
15.0
15.0
15.0
17.5


R32
mass %
40.0
37.5
35.0
32.5
30.0
27.5
25.0
50.0


R1234yf
mass %
42.5
45.0
47.5
50.0
52.5
55.0
57.5
30.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

272
255
238
222
205
188
171
339


COP ratio
% (relative
100.2
100.2
100.2
100.2
100.3
100.4
100.5
100.1



to R410A)










Refrigerating
% (relative
93.5
91.9
90.2
88.5
86.7
84.9
83.0
100.8


capacity ratio
to R410A)










Condensation glide
° C.
4.5
4.8
5.2
5.6
6.0
6.4
6.9
3.2

























TABLE 41









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
193
194
195
196
197
198
199
200





HFO-1132(E)
mass %
17.5
17.5
17.5
17.5
17.5
17.5
17.5
17.5


R32
mass %
47.5
45.0
42.5
40.0
37.5
35.0
32.5
30.0


R1234yf
mass %
32.5
35.0
37.5
40.0
42.5
45.0
47.5
50.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

322
305
289
272
255
238
221
205


COP ratio
% (relative
100.0
100.0
100.0
100.0
100.0
100.0
100.0
100.1



to R410A)










Refrigerating
% (relative
99.4
97.9
96.4
94.8
93.2
91.5
89.8
88.1


capacity ratio
to R410A)










Condensation glide
° C.
3.5
3.7
4.0
4.3
4.6
5.0
5.3
5.7







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
201
202
203
204
205
206
207
208





HFO-1132(E)
mass %
17.5
17.5
17.5
20.0
20.0
20.0
20.0
20.0


R32
mass %
27.5
25.0
22.5
50.0
45.0
42.5
40.0
35.0


R1234yf
mass %
52.5
55.0
57.5
27.5
32.5
35.0
37.5
42.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

188
171
154
339
305
289
272
238


COP ratio
% (relative
100.2
100.3
100.4
99.9
99.9
99.8
99.8
99.8



to R410A)










Refrigerating
% (relative
86.3
84.4
82.6
102.0
99.2
97.7
96.1
92.9


capacity ratio
to R410A)










Condensation glide
° C.
6.2
6.6
7.0
3.1
3.5
3.8
4.1
4.7







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
209
210
211
212
213
214
215
216





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
22.5
22.5
22.5


R32
mass %
32.5
30.0
25.0
22.5
20.0
50.0
47.5
45.0


R1234yf
mass %
45.0
47.5
52.5
55.0
57.5
25.0
27.5
30.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

221
205
171
154
138
339
322
305


COP ratio
% (relative
99.8
99.9
100.0
100.2
100.3
99.8
99.7
99.7



to R410A)










Refrigerating
% (relative
91.2
89.5
85.9
84.0
82.1
103.2
101.8
100.4


capacity ratio
to R410A)










Condensation glide
° C.
5.1
5.5
6.3
6.7
7.2
2.9
3.1
3.4







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
217
218
219
220
221
222
223
224





HFO-1132(E)
mass %
22.5
22.5
22.5
22.5
22.5
22.5
22.5
22.5


R32
mass %
42.5
40.0
37.5
35.0
32.5
30.0
27.5
25.0


R1234yf
mass %
32.5
35.0
37.5
40.0
42.5
45.0
47.5
50.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

288
272
255
238
221
205
188
171


COP ratio
% (relative
99.7
99.7
99.7
99.7
99.7
99.7
99.8
99.8



to R410A)










Refrigerating
% (relative
98.9
97.4
95.8
94.2
92.5
90.8
89.0
87.2


capacity ratio
to R410A)










Condensation glide
° C.
3.6
3.9
4.2
4.5
4.9
5.2
5.6
6.0







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
225
226
227
228
229
230
231
232





HFO-1132(E)
mass %
22.5
22.5
22.5
25.0
25.0
25.0
25.0
25.0


R32
mass %
22.5
20.0
17.5
40.0
37.5
35.0
32.5
30.0


R1234yf
mass %
52.5
55.0
57.5
32.5
35.0
37.5
40.0
42.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

154
137
121
272
255
238
221
204


COP ratio
% (relative
99.9
100.1
100.2
99.5
99.5
99.5
99.5
99.5



to R410A)










Refrigerating
% (relative
85.4
83.5
81.5
98.6
97.1
95.5
93.8
92.1


capacity ratio
to R410A)










Condensation glide
° C.
6.5
6.9
7.3
3.7
4.0
4.3
4.6
5.0







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
233
234
235
236
237
238
239
240





HFO-1132(E)
mass %
25.0
25.0
25.0
25.0
25.0
27.5
27.5
27.5


R32
mass %
27.5
25.0
22.5
20.0
17.5
32.5
30.0
27.5


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
37.5
40.0
42.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

188
171
154
137
121
221
204
188


COP ratio
% (relative
99.6
99.6
99.7
99.9
100.0
99.4
99.4
99.4



to R410A)










Refrigerating
% (relative
90.4
88.6
86.8
84.9
83.0
95.1
93.4
91.7


capacity ratio
to R410A)










Condensation glide
° C.
5.4
5.7
6.2
6.6
7.0
4.4
4.7
5.1

























TABLE 42









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
241
242
243
244
245
246
247
248





HFO-1132(E)
mass %
27.5
27.5
27.5
27.5
27.5
30.0
30.0
30.0


R32
mass %
25.0
22.5
20.0
17.5
15.0
25.0
22.5
20.0


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
42.5
45.0
47.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

171
154
137
121
104
171
154
137


COP ratio
%
99.5
99.5
99.6
99.8
99.9
99.3
99.4
99.5



(relative to











R410A)










Refrigerating
%
89.9
88.1
86.3
84.3
82.4
91.3
89.5
87.6


capacity ratio
(relative to











R410A)










Condensation
° C.
5.5
5.9
6.3
6.7
7.2
5.2
5.6
6.0


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
249
250
251
252
253
254
255
256





HFO-1132(E)
mass %
30.0
30.0
32.5
32.5
32.5
32.5
35.0
35.0


R32
mass %
15.0
12.5
20.0
17.5
15.0
12.5
15.0
12.5


R1234yf
mass %
52.5
55.0
45.0
47.5
50.0
52.5
47.5
50.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

104
87
137
120
104
87
104
87


COP ratio
%
99.7
99.9
99.3
99.4
99.5
99.7
99.3
99.5



(relative to











R410A)










Refrigerating
%
83.8
81.8
88.9
87.1
85.1
83.1
86.5
84.5


capacity ratio
(relative to











R410A)










Condensation
° C.
6.8
7.3
5.7
6.1
6.5
7.0
6.2
6.6


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
257
258
259
260
261
262
263
264





HFO-1132(E)
mass %
35.0
37.5
37.5
37.5
40.0
40.0
42.5
42.5


R32
mass %
10.0
12.5
10.0
7.5
10.0
5.0
7.5
5.0


R1234yf
mass %
52.5
47.5
50.0
52.5
47.5
52.5
47.5
50.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

70
87
70
53
70
36
53
36


COP ratio
%
99.6
99.3
99.4
99.6
99.3
99.6
99.3
99.4



(relative to











R410A)










Refrigerating
%
82.5
85.8
83.8
81.8
85.2
81.0
845
82.4


capacity ratio
(relative to











R410A)










Condensation
° C.
7.1
6.3
6.7
7.1
6.4
7.2
6.5
6.9


glide




















Example
Example
Example
Example
Example
Example
Example


Item
Unit
265
266
267
268
269
270
271





HFO-1132(E)
mass %
45.0
45.0
47.5
47.5
50.0
52.5
55.0


R32
mass %
5.0
2.5
4.0
1.5
2.5
1.5
1.0


R1234yf
mass %
47.5
50.0
46.0
48.5
45.0
43.5
41.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

36
19
29
13
19
12
9


COP ratio
%
99.3
99.4
99.2
99.3
99.1
99.1
99.0



(relative to










R410A)









Refrigerating
%
83.7
81.6
84.2
82.0
84.2
84.7
85.6


capacity ratio
(relative to










R410A)









Condensation
° C.
6.6
6.9
6.4
6.7
6.3
6.2
5.9


glide

























TABLE 43









Comp. Ex.
Comp. Ex.
Comp. Ex.
Example
Example
Example
Comp. Ex.
Comp. Ex.


Item
Unit
146
147
148
272
273
274
149
150





HFO-1132(E)
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
mass %
76.0
66.0
56.0
46.0
36.0
26.0
16.0
6.0


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

514
446
379
312
245
178
111
44


COP ratio
%
100.3
100.2
100.1
100.0
100.0
100.4
101.2
102.0



(relative to











R410A)










Refrigerating
%
113.0
108.6
103.5
97.8
91.3
84.1
76.1
66.8


capacity ratio
(relative to











R410A)










Condensation
° C.
2.5
3.1
3.9
5.0
6.4
8.3
10.4
12.2


glide







Comp. Ex.
Comp. Ex.
Example
Example
Example
Example
Comp. Ex.
Comp. Ex.


Item
Unit
146
147
275
276
277
278
153
154





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
30.0


R32
mass %
66.0
56.0
46.0
36.0
26.0
16.0
6.0
56.0


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
10.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

446
379
312
245
178
111
44
379


COP ratio
%
99.6
99.5
99.3
99.2
99.4
100.0
100.9
98.9



(relative to











R410A)










Refrigerating
%
113.1
108.4
103.0
96.8
89.9
82.3
73.7
112.9


capacity ratio
(relative to











R410A)










Condensation
° C.
2.6
3.3
4.2
5.5
7.1
9.2
11.2
2.7


glide







Example
Example
Example
Example
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example


Item
Unit
279
280
281
282
155
156
157
283





HFO-1132(E)
mass %
30.0
30.0
30.0
30.0
30.0
40.0
40.0
40.0


R32
mass %
46.0
36.0
26.0
16.0
6.0
46.0
36.0
26.0


R1234yf
mass %
20.0
30.0
40.0
50.0
60.0
10.0
20.0
30.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

312
245
177
110
43
311
244
177


COP ratio
%
98.7
98.6
98.7
99.0
99.8
98.3
98.1
98.1



(relative to











R410A)










Refrigerating
%
107.7
101.9
95.4
88.0
79.9
112.1
106.6
100.4


capacity ratio
(relative to











R410A)










Condensation
° C.
3.5
4.6
6.0
7.8
9.8
2.8
3.8
5.0


glide







Example
Example
Comp. Ex.
Comp. Ex.
Example
Example
Comp. Ex.
Comp. Ex.


Item
Unit
284
285
158
159
286
287
160
161





HFO-1132(E)
mass %
40.0
40.0
50.0
50.0
50.0
50.0
60.0
60.0


R32
mass %
16.0
6.0
36.0
26.0
16.0
6.0
26.0
16.0


R1234yf
mass %
40.0
50.0
10.0
20.0
30.0
40.0
10.0
20.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

110
43
244
177
110
43
177
109


COP ratio
%
98.3
98.8
97.7
97.7
97.8
98.2
97.3
97.4



(relative to











R410A)










Refrigerating
%
93.4
85.6
110.9
105.0
98.4
90.9
109.3
103.0


capacity ratio
(relative to











R410A)










Condensation
° C.
6.6
8.4
3.1
4.1
5.5
7.1
3.4
4.6


glide







Example
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example
Example
Example
Example


Item
Unit
288
162
163
164
289
290
291
292





HFO-1132(E)
mass %
60.0
70.0
70.0
80.0
15.0
15.0
15.0
15.0


R32
mass %
6.0
16.0
6.0
6.0
48.5
46.0
43.5
41.0


R1234yf
mass %
30.0
10.0
20.0
10.0
32.5
35.0
37.5
40.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

42
109
42
42
329
312
295
279


COP ratio
%
97.7
97.2
97.4
97.2
99.7
99.6
99.6
99.6



(relative to











R410A)










Refrigerating
%
95.9
107.3
100.5
104.9
101.9
100.4
98.9
97.4


capacity ratio
(relative to











R410A)










Condensation
° C.
6.0
3.8
5.1
4.3
4.3
4.6
4.9
5.2


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
293
294
295
296
297
298
299
300





HFO-1132(E)
mass %
15.0
15.0
15.0
15.0
15.0
15.0
15.0
15.0


R32
mass %
38.5
36.0
33.5
31.0
28.5
26.0
23.5
21.0


R1234yf
mass %
42.5
45.0
47.5
50.0
52.5
55.0
57.5
60.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

262
245
228
211
195
178
161
144


COP ratio
%
99.6
99.6
99.6
99.7
99.8
99.9
100.0
100.2



(relative to











R410A)










Refrigerating
%
95.8
94.1
92.4
90.7
88.9
87.1
85.2
83.3


capacity ratio
(relative to











R410A)










Condensation
° C.
5.6
5.9
6.3
6.8
7.2
7.7
8.2
8.7


glide

























TABLE 44









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
301
302
303
304
305
306
307
308





HFO-1132(E)
mass %
15.0
17.5
17.5
17.5
17.5
17.5
17.5
17.5


R32
mass %
18.5
48.5
46.0
43.5
41.0
38.5
36.0
33.5


R1234yf
mass %
62.5
30.0
32.5
35.0
37.5
40.0
42.5
45.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

128
329
312
295
278
262
245
228


COP ratio
%
100.4
99.5
99.5
99.4
99.4
99.4
99.4
99.4



(relative to











R410A)










Refrigerating
%
81.3
103.1
101.7
100.2
98.7
97.1
95.5
93.8


capacity ratio
(relative to











R410A)










Condensation
° C.
9.3
4.1
4.4
4.7
5.0
5.3
5.7
6.1


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
309
310
311
312
313
314
315
316





HFO-1132(E)
mass %
17.5
17.5
17.5
17.5
17.5
17.5
20.0
20.0


R32
mass %
31.0
28.5
26.0
23.5
21.0
18.5
48.5
43.5


R1234yf
mass %
47.5
50.0
52.5
55.0
57.5
60.0
27.5
32.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

211
195
178
161
144
127
329
295


COP ratio
%
99.5
99.5
99.6
99.8
99.9
100.1
99.3
99.3



(relative to











R410A)










Refrigerating
%
92.1
90.3
88.5
86.7
84.8
82.8
104.4
101.5


capacity ratio
(relative to











R410A)










Condensation
° C.
6.5
7.0
7.4
7.9
8.4
9.0
4.0
4.5


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
317
318
319
320
321
322
323
324





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
20.0


R32
mass %
41.0
38.5
33.5
31.0
28.5
23.5
21.0
18.5


R1234yf
mass %
35.0
37.5
42.5
45.0
47.5
52.5
55.0
57.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

278
262
228
211
195
161
144
127


COP ratio
%
99.3
99.2
99.3
99.3
99.3
99.5
99.6
99.8



(relative to











R410A)










Refrigerating
%
100.0
98.4
95.2
93.5
91.7
88.1
86.2
84.3


capacity ratio
(relative to











R410A)










Condensation
° C.
4.8
5.1
5.8
6.2
6.7
7.6
8.1
8.6


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
325
326
327
328
329
330
331
332





HFO-1132(E)
mass %
22.5
22.5
22.5
22.5
22.5
22.5
22.5
22.5


R32
mass %
48.5
46.0
43.5
41.0
38.5
36.0
33.5
31.0


R1234yf
mass %
25.0
27.5
30.0
32.5
35.0
37.5
40.0
42.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

329
312
295
278
262
245
228
211


COP ratio
%
99.2
99.2
99.1
99.1
99.1
99.1
99.1
99.1



(relative to











R410A)










Refrigerating
%
105.6
104.2
102.7
101.3
99.7
98.1
96.5
94.8


capacity ratio
(relative to











R410A)










Condensation
° C.
3.8
4.0
4.3
4.6
4.3
5.2
5.6
6.0


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
333
334
335
336
337
338
339
340





HFO-1132(E)
mass %
22.5
22.5
22.5
22.5
22.5
22.5
22.5
25.0


R32
mass %
28.5
26.0
23.5
21.0
18.5
16.0
13.5
43.5


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
57.5
60.0
27.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

194
178
161
144
127
111
94
295


COP ratio
%
99.1
99.2
99.3
99.4
99.5
99.7
99.9
99.0



(relative to











R410A)










Refrigerating
%
93.1
91.3
89.5
87.7
85.8
83.8
81.8
104.0


capacity ratio
(relative to











R410A)










Condensation
° C.
6.4
6.8
7.3
7.8
8.3
8.8
9.3
4.1


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
341
342
343
344
345
346
347
348





HFO-1132(E)
mass %
25.0
25.0
25.0
25.0
25.0
25.0
25.0
25.0


R32
mass %
41.0
38.5
36.0
33.5
31.0
28.5
26.0
23.5


R1234yf
mass %
30.0
32.5
35.0
37.5
40.0
42.5
45.0
47.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

278
261
245
228
211
194
178
161


COP ratio
%
98.9
98.9
98.9
98.9
98.9
99.0
99.0
99.1



(relative to











R410A)










Refrigerating
%
102.5
101.0
99.4
97.8
96.1
94.4
92.7
90.9


capacity ratio
(relative to











R410A)










Condensation
° C.
4.4
4.7
5.0
5.4
5.7
6.1
6.5
7.0


glide

























TABLE 45









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
349
350
351
352
353
354
355
356





HFO-1132(E)
mass %
25.0
25.0
25.0
25.0
27.5
27.5
27.5
27.5


R32
mass %
21.0
18.5
16.0
13.5
35.0
31.0
28.5
26.0


R1234yf
mass %
50.0
52.5
55.0
57.5
35.0
37.5
40.0
42.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

144
127
110
94
238
211
194
178


COP ratio
%
99.2
99.3
99.5
99.7
98.8
98.8
98.3
98.8



(relative to











R410A)










Refrigerating
%
89.1
87.2
85.2
83.2
99.4
97.4
95.8
94.0


capacity ratio
(relative to











R410A)










Condensation
° C.
7.5
8.0
8.5
9.0
5.0
5.5
5.9
6.3


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
357
358
359
360
361
362
363
364





HFO-1132(E)
mass %
27.5
27.5
27.5
27.5
27.5
27.5
30.0
30.0


R32
mass %
23.5
21.0
18.5
16.0
13.5
11.0
23.5
21.0


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
57.5
42.5
45.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

161
144
127
110
94
77
161
144


COP ratio
%
98.9
99.0
99.1
99.2
99.4
99.6
98.7
98.8



(relative to











R410A)










Refrigerating
%
92.3
90.4
88.6
86.7
84.7
82.6
93.6
91.8


capacity ratio
(relative to











R410A)










Condensation
° C.
6.7
7.2
7.6
8.1
8.7
9.2
6.4
6.9


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
365
366
367
368
369
400
401
402





HFO-1132(E)
mass %
30.0
30.0
30.0
30.0
32.5
32.5
32.5
32.5


R32
mass %
18.5
13.5
11.0
8.5
21.0
18.5
16.0
35.0


R1234yf
mass %
47.5
52.5
55.0
57.5
42.5
45.0
47.5
50.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

127
94
77
60
144
127
110
239


COP ratio
%
98.9
99.2
99.3
99.5
98.6
98.7
98.8
99.1



(relative to











R410A)










Refrigerating
%
89.9
86.1
84.1
82.0
93.1
91.3
89.4
94.0


capacity ratio
(relative to











R410A)










Condensation
° C.
7.3
8.3
8.8
9.3
6.6
7.0
7.5
5.5


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
403
404
405
406
407
408
409
410





HFO-1132(E)
mass %
32.5
32.5
32.5
35.0
35.0
35.0
35.0
35.0


R32
mass %
11.0
8.5
6.0
16.0
13.5
11.0
8.5
6.0


R1234yf
mass %
52.5
55.0
57.5
45.0
47.5
50.0
52.5
55.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

77
60
43
110
93
77
60
43


COP ratio
%
99.1
99.3
99.5
98.6
98.7
98.9
99.1
99.3



(relative to











R410A)










Refrigerating
%
85.5
83.4
81.3
90.8
88.8
86.9
84.8
82.8


capacity ratio
(relative to











R410A)










Condensation
° C.
8.5
9.0
9.5
7.2
7.6
8.1
8.6
9.1


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
411
412
413
414
415
416
417
418





HFO-1132(E)
mass %
37.5
37.5
37.5
37.5
37.5
40.0
40.0
40.0


R32
mass %
13.5
11.0
8.5
6.0
3.5
11.0
8.5
3.5


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
45.0
47.5
52.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

93
77
60
43
26
76
60
26


COP ratio
%
98.6
98.7
98.9
99.0
99.2
98.5
98.7
99.0



(relative to











R410A)










Refrigerating
%
90.2
88.2
86.2
84.2
82.0
89.6
87.6
83.4


capacity ratio
(relative to











R410A)










Condensation
° C.
7.3
7.8
8.3
8.8
9.2
7.5
7.9
8.9


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
419
420
421
422
423
424
425
426





HFO-1132(E)
mass %
40.0
42.5
42.5
42.5
42.5
45.0
45.0
45.0


R32
mass %
1.0
8.5
35.0
3.5
1.0
6.0
3.5
1.0


R1234yf
mass %
55.0
45.0
47.5
50.0
52.5
45.0
47.5
50.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

9
60
239
26
9
43
26
9


COP ratio
%
99.2
98.5
98.8
98.8
99.0
98.5
98.6
98.8



(relative to











R410A)










Refrigerating
%
81.2
88.9
95.6
84.8
82.6
88.3
86.2
84.0


capacity ratio
(relative to











R410A)










Condensation
° C.
9.3
7.6
5.0
8.5
9.0
7.8
8.2
8.7


glide























TABLE 46







Example
Example
Example
Example
Example
Example


Item
Unit
427
428
429
430
431
432






















HFO-1132(E)
mass %
47.5
47.5
50.0
50.0
52.5
55.0


R32
mass %
4.5
2.0
3.5
1.0
2.0
1.0


R1234yf
mass %
44.0
46.5
42.5
45.0
41.5
40.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0


GWP

33
16
26
9
16
9


COP ratio
%
98.4
98.6
98.3
98.5
98.3
98.2



(relative









to R410A)








Refrigerating
%
88.4
86.3
88.9
86.8
88.9
89.4


capacity ratio
(relative









to R410A)








Condensation
° C.
7.7
8.1
7.6
8.0
7.5
7.4


glide









These results indicate that when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum is respectively represented by w, x, y, and z, the mixed refrigerant has a GWP of 350 when coordinates (x,y,z) are on straight line A″B″ in the ternary composition diagrams shown in FIGS. 1B to 1I, in which the sum of R32, and R1234yf, and HFO-1132(E) is (100−w) mass %, and the mixed refrigerant has a GWP of less than 350 when coordinates (x,y,z) in the ternary composition diagrams are located to the right of straight line A″B″. The results further indicate that the mixed refrigerant has a GWP of 250 when coordinates (x,y,z) are on straight line A′B′ in the ternary composition diagrams shown in FIGS. 1B to 1I, and the mixed refrigerant has a GWP of less than 125 when coordinates (x,y,z) in the ternary composition diagrams are located to the right of straight line A′B′. The results further show that the mixed refrigerant has a GWP of 125 when coordinates (x,y,z) are on straight line segment AB in the ternary composition diagrams shown in FIGS. 1B to 1I, and the mixed refrigerant has a GWP of less than 125 when coordinates (x,y,z) in the ternary composition diagrams are located to the right of straight line segment AB.


The straight line that connects point D and point C is found to be roughly located slightly to the left of the curve that connect points where the mixed refrigerant has a refrigerating capacity ratio of 80% relative to R410A. Accordingly, the results show that when coordinates (x, y, z) are located on the left side of the straight line that connects point D and point C, the mixed refrigerant has a refrigerating capacity ratio of 80% or more relative to R410A.


The coordinates of point A and point B, point A′ and point B′, and point A″ and point B″ were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, the calculation was performed as shown in Table 47 (point A and point B), Table 48 (point A′ and point B′), and Table 49 (point A″ and point B″).












TABLE 47





Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0















Point A
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
81.6
81.0
80.4
80.4
79.1
77.6
77.6
76.1
74.6


R32
18.4
18.4
18.4
18.4
18.4
18.4
18.4
18.4
18.4


R1234yf
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0










CO2
W
w
w


Approximate
−w + 81.6
−w + 81.6
−w + 81.6


formula of





HFO-1132 (E)





Approximate
18.4
18.4
18.4


formula of





R32





Approximate
 0.0
 0.0
 0.0


formula of





R1234yf










Point B
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
18.1
18.1
18.1
18.1
18.1
18.1
18.1
18.1
18.1


R1234yf
81.9
81.3
80.7
80.7
79.4
77.9
77.9
76.4
74.9










CO2
w
w
W


Approximate
 0.0
 0.0
 0.0


formula of





HFO-1132 (E)





Approximate
18.1
18.1
18.1


formula of





R32





Approximate
−w + 81.9
−w + 81.9
−w + 81.9


formula of





R1234yf



















TABLE 48





Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0















Point A′
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
63.1
62.5
61.9
61.9
60.6
59.1
59.1
57.6
56.1


R32
36.9
36.9
36.9
36.9
36.9
36.9
36.9
36.9
36.9


R1234yf
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0










CO2
w
w
w


Approximate
−w + 63.1
−w + 63.1
−w + 63.1


formula of





HFO-1132 (E)





Approximate
36.9
36.9
36.9


formula of





R32





Approximate
 0.0
 0.0
 0.0


formula of





R1234yf










Point B′
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
36.7
36.7
36.6
36.6
36.6
36.6
36.6
36.6
36.6


R1234yf
63.3
62.7
62.2
62.2
60.9
59.4
59.4
57.9
56.4










CO2
w
w
w


Approximate
0 
 0.0
 0.0


formula of





HFO-1132 (E)





Approximate
100-R1234yf-CO2
36.6
36.6


formula of





R32





Approximate
−0.9167w + 63.283
−w + 63.4
−w + 63.4


formula of





R1234yf



















TABLE 49





Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0















Point A″
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
48.2
47.6
47.0
47.0
45.7
44.2
44.2
42.7
41.2


R32
51.8
51.8
51.θ
51.8
51.8
51.8
51.8
51.8
51.8


R1234yf
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0










CO2
W
w
w


Approximate
−w + 48.2
−w + 48.2
−w + 48.2


formula of





HFO-1132 (E)





Approximate
51.8 
51.8
51.8


formula of





R32





Approximate
0.0
 0.0
 0.0


formula of





R1234yf










Point B″
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
51.5
51.6
51.6
51.6
51.6
51.6
51.6
51.6
51.6


R1234yf
49.5
47.8
47.2
47.2
45.9
44.4
44.4
42.9
41.4










CO2
W
w
w


Approximate
0.0
 0.0
 0.0


formula of





HFO-1132 (E)





Approximate
100-R1234yf-CO2
51.6
51.6


formula of





R32





Approximate
1.5278W2 − 3.75w + 49.5
−w + 48.4
−w + 48.4


formula of





R1234yf









The coordinates of points C to G were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, the calculation was performed as shown in Tables 50 and 51.












TABLE 50







Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0










Point C
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
58.3
55.4
52.4
52.4
46.2
39.5
39.5
33.0
26.8


R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R1234yf
41.7
44.0
46.4
46.4
51.3
56.5
56.5
61.5
66.2










CO2
w
w
w


Approximate
−4.9167w + 58.317
0.1081w2
0.0667w2


formula of

5.169w + 58.447
4.9667w + 58.3


HFO-1132 (E)





Approximate
0.0
0.0
0.0


formula of





R32





Approximate
100-E-HFO-1132-CO2
100-E-HFO-1132-CO2
100-E-HFO-1132-CO2


formula of





R1234yf










Point D
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
40.3
38.6
36.8
36.8
33.2
28.9
28.9
24.7
20.5


R1234yf
59.7
60.8
62.0
62.0
64.3
67.1
67.1
69.8
72.5










CO2
w
W
w


Approximate
0.0
0.0
0.0


formula of





HFO-1132 (E)





Approximate
−2.9167w + 40.317
−2.8226w + 40.211
−2.8w + 40.1


formula of





R32





Approximate
100-R32-CO2
100-R32-CO2
100-R32-CO2


formula of





R1234yf










Point E
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
31.9
29.6
26.5
26.5
20.9
14.7
14.7
8.8
3.1


R32
18.2
18.2
18.2
18.2
18.2
18.1
18.1
18.1
18.1


R1234yf
49.9
51.6
54.1
54.1
58.4
63.2
63.2
67.6
71.8










CO2
w
W
W


Approximate
−1.1111w2
0.0623w2
0.0444w2


formula of
3.1667w + 31.9
4.5381w + 31.856
4.3556w + 31.411


HFO-1132 (E)





Approximate
18.2 
−0.0365w + 18.26
18.1 


formula of





R32





Approximate
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2


formula of





R1234yf












Item
1.2 ≥ CO2 > 0
1.3 ≥ CO2 > 1.2







Point F















CO2
0.0
0.6
1.2
1.2
1.3


E-HFO-1132
5.2
2.7
0.3
0.3
0


R32
36.7
36.7
36.6
36.6
36.6


R1234yf
58.1
60.0
61.9
61.9
62.1









CO2
W
w


Approximate
−4.0833w + 5.1833
−3w + 3.9


formula of




HFO-1132 (E)




Approximate
−0.0833w + 36.717
36.6


formula of




R32




Approximate
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2


formula of




R1234yf













Item
1.2 ≥ CO2 ≥ 0







Point G















CO2
0.0
0.6
1.2



E-HFO-1132
26.2
29.6
38.1



R32
22.2
18.2
10.0



R1234yf
51.6
51.6
50.7










CO2
w



Approximate
7.0833w2 + l.4167w + 26.2



formula of




HFO-1132 (E)




Approximate
−5.8333w2



formula of R32
3.1667w + 22.2



Approximate
100-E-HFO-1132-R32-CO2



formula of




R1234yf



















TABLE 51





Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0















Point M
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
52.6
55.4
58.0
58.0
59.7
60.4
0.0
33.0
26.8


R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R1234yf
47.4
44.0
40.8
40.8
37.8
35.6
56.5
61.5
66.2










CO2
w
w
w


Approximate
100-E-HFO-1132-R1234yf-CO2
100-E-HFO-1132-R1234yf-CO2
100-E-HFO-1132-R1234yf-CO2


formula of





HFO-1132 (E)





Approximate
 0.0
 0.0
 0.0


formula of





R32





Approximate
0.2778w2
0.3004w2
0.0667w2


formula of
5.8333w + 47.4
3.419w + 44.47
1.8333w + 41.867


R1234yf










Point W
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
32.4
35.1
38.1
38.1
40.9
42.6
42.6
43.3
43.7


R32
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R1234yf
57.6
54.3
50.7
50.7
46.6
43.4
43.4
41.2
39.3










CO2
W
w
w


Approximate
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2


formula of





HFO-1132 (E)





Approximate
10.0
10.0
10.0


formula of





R32





Approximate
−0.4167w2
0.3645w2
0.0667w2


formula of
5.25w + 57.6
4.5024w + 55.578
2.1w + 50.733


R1234yf










Point N
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
27.7
29.6
31.7
31.7
34.2
35.5
35.5
36.3
36.7


R32
18.2
18.2
18.2
18.2
18.2
18.2
18.2
18.2
18.2


R1234yf
54.1
51.6
48.9
48.9
45.1
42.3
42.3
40.0
38.1










CO2
w
w
w


Approximate
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2


formula of





HFO-1132 (E)





Approximate
18.2
18.2
18.2


formula of





R32





Approximate
−0.2778w2
0.3773w2
0.0889w2


formula of
4w + 54.1
4.319w + 53.54
2.3778w + 50.389


R1234yf










Point O
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
22.6
24.0
25.4
25.4
27.2
28.0
28.0
28.4
28.6


R32
36.8
36.8
36.8
36.8
36.8
36.8
36.8
36.8
36.8


R1234yf
40.6
38.6
36.0
36.0
33.5
31.2
31.2
29.3
27.6










CO2
w
w
w


Approximate
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2


formula of





HFO-1132 (E)





Approximate
36.8
36.8
36.8


formula of





R32





Approximate
−0.8333w2
0.1392w2
0.0444w2


formula of
2.8333w + 40.6
2.4381w + 38.725
1.6889w + 37.244


R1234yf










Point P
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
20.5
20.9
22.1
22.1
23.4
23.9
23.9
24.2
24.2


R32
51.7
51.7
51.7
51.7
51.7
51.7
51.7
51.7
51.7


R1234yf
27.8
26.8
25.0
25.0
22.4
20.4
20.4
18.6
17.1










CO2
W
w
w


Approximate
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2


formula of





HFO-1132 (E)





Approximate
51.7
51.7
51.7


formula of





R32





Approximate
−1.1111w2
0.2381w2
0.0667w2


formula of
w + 27.8
2.881w + 28.114
1.8333w + 26.667


R1234yf









The coordinates of points on curve IJ, curve JK, and curve KL were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, the calculation was performed as shown in Table 52.


















TABLE 52





Refrigerant type
I
Example
J
J
Example
K
K
Example
L

























CO2
R32
0.0
10.0
18.3
18.3
27.6
36.8
36.8
44.2
51.7


0.0
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
28.0
32.8
33.2
33.2
31.2
27.6
27.6
23.8
19.4


0.6
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
27.4
32.2
32.6
32.6
30.6
27.0
27.0
23.2
18.8


1.2
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
26.8
31.6
32.0
32.0
30.0
26.4
26.4
22.6
18.2


2.5
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
25.5
30.3
30.7
30.7
28.7
25.1
25.1
21.3
16.9


4.0
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
24.0
28.8
29.2
29.2
27.2
23.6
23.6
19.8
15.4


5.5
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
22.5
27.3
27.7
27.7
25.7
22.1
22..1
18.3
13.9


7.0
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
21.0
25.8
26.2
26.2
24.2
20.6
20.6
16.8
12.4











w =
Approximate
0.0236x2
0.0095x2
0.0049x2


CO2
formula of
1.716x + 72
1.2222x + 67.676
0.8842x + 61.488



E-HFO-1132






when x = R32






R1234yf
100-E-HFO-1132-x-w
100-E-HFO-1132-x-w
100-E-HFO-1132-x-w









The coordinates of points on curve MW and curve WM were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, calculation was performed as shown in Table 53 (when 0 mass %<CO2 concentration≤1.2 mass %), Table 54 (when 1.2 mass %<CO2 concentration≤4.0 mass %), and Table 55 (4.0 mass %<CO2 concentration≤7.0 mass %).









TABLE 53







1.2 ≥ CO2 > 0














M
Example
W
W
Example
N


Item
0.0
5.0
10.0
10.0
14.5
18.2
















CO2 = 0 mass %
52.6
39.2
32.4
32.4
29.3
27.7









Approximate
0.132x2
0.0313x2


formula of
3.34x + 52.6
1.4551x + 43.824


E-HFO-1132




when x = R32















CO2 = 0.6 mass %
55.4
42.4
35.1
35.1
31.6
29.6









Approximate
0.114x2
0.0289x2


formula of
3.17x + 55.4
1.4866x + 47.073


E-HFO-1132




when x = R32















CO2 = 1.2 mass %
58.0
45.2
38.1
38.1
34.0
31.7









Approximate
0.114x2
0.0353x2


formula of
3.13x + 58.0
1.776x + 52.330


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.025w2
0.0122w2


formula of
0.045w + 0.132
0.0113w + 0.0313


coefficient a




Approximate
−0.1806w2 +
−0.3582w2 +


formula of
0.3917w − 3.34
0.1624w − 1.4551


coefficient b




Approximate
−0.2778w2 +
2.7889w2 +


formula of
4.8333w + 52.6
3.7417w + 43.824


coefficient c




Approximate
(0.025w2 − 0.045w +
(0.0122w2 − 0.0113w +


formula of
0.132)x2 + (−0.1806w2 +
0.0313)x2 + (−0.3582w2 +


E-HFO-1132
0.3917w − 3.34)x + (−0.2778w2 +
0.1624w − 1.4551)x + (2.7889w2 +


when x = R32,
4.8333w + 52.6)
3.7417w + 43.824)


w = CO2, and




1.2 ≥ w > 0




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
















TABLE 54







4.0 ≥ CO2 ≥ 1.2














M
Example
W
W
Example
N


Item
0.0
5.0
10.0
10.0
14.5
18.2
















CO2 = 1.2 mass %
58
45.2
38.1
38.1
34
31.7









Approximate
0.114x2
0.0353x2


formula of
3.13x + 58.0
1.776x + 52.330


E-HFO-1132




when x = R32















CO2 = 2.5 mass %
59.7
48.1
40.9
40.9
36.9
34.2









Approximate
0.088x2
0.0194x2


formula of
2.76x + 59.7
1.3644x + 52.603


E-HFO-1132




when x = R32















CO2 = 4.0 mass %
60.4
49.6
42.6
42.6
38.3
35.5









Approximate
0.076x2
0.0242x2


formula of
2.54x + 60.4
1.5495x + 55.671


E-HFO-1132




when x = R32









In the approximate formula of E-HFO-1132 ax2 + bx + c, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.0043w2
0.0055w2


formula of
0.0359w + 0.1509
0.0326w + 0.0665


coefficient a




Approximate
−0.0493w2 +
−0.1571w2 +


formula of
0.4669w − 3.6193
0.8981w − 2.6274


coefficient b




Approximate
−0.3004w2 +
0.6555w2


formula of
2.419w + 55.53
2.2153w + 54.044


coefficient c




Approximate
(0.0043w2 − 0.0359w +
(0.0055w2 − 0.0326w +


formula of
0.1509)x2 + (−0.0493w2 +
0.0665)x2 + (−0.1571w2 +


E-HFO-1132
0.4669w − 3.6193)x + (−0.3004w2 +
0.8981w − 2.6274)x + (0.6555w2 −


when x = R32,
2.419w + 55.53)
2.2153w + 54.044)


w = CO2, and




4.0 ≥ w ≥ 1.2




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
















TABLE 55







7.0 ≥ CO2 ≥ 4.0














M
Example
W
W
Example
N


Item
0.0
5.0
10.0
10.0
14.5
18.2
















CO2 = 4.0 mass %
60.4
49.6
42.6
42.6
38.3
35.5









Approximate
0.076x2
0.0242x2


formula of
2.54x + 60.4
1.5495x + 55.671


E-HFO-1132




when x = R32















CO2 = 5.5 mass %
60.7
50.3
43.3
43.3
39
36.3









Approximate
0.068x2
0.0275x2


formula of
2.42x + 60.7
1.6303x + 56.849


E-HFO-1132




when x = R32















CO2 = 7.0 mass %
60.7
50.3
43.7
43.7
39.5
36.7









Approximate
0.076x2
0.0215x2


formula of
2.46x + 60.7
1.4609x + 56.156


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.00357w2
−0.002061w2 +


formula of
0.0391w + 0.1756
0.0218w − 0.0301


coefficient a




Approximate
−0.0356w2 +
0.0556w2


formula of
0.4178w − 3.6422
0.5821w − 0.1108


coefficient b




Approximate
−0.0667w2 +
− 0.4158w2 +


formula of
0.8333w + 58.103
4.7352w + 43.383


coefficient c




Approximate
(0.00357w2 − 0.0391w +
(−0.002061w2 + 0.0218w −


formula of
0.1756)x2 + (−0.0356w2 +
0.0301)x2 + (0.0556w2


E-HFO-1132
0.4178w − 3.6422)x +
0.5821w − 0.1108)x +


when x = R32,
(−0.0667w2 + 0.8333w + 58.103)
(−0.4158w2 + 4.7352w + 43.383)


w = CO2, and




7.0 ≥ w ≥ 4.0




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2









The coordinates of points on curve NO and curve OP were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, calculation was performed as shown in Table 56 (when 0 mass %<CO2 concentration≤1.2 mass %), Table 57 (when 1.2 mass %<CO2 concentration≤4.0 mass %), and Table 58 (4.0 mass %<CO2 concentration≤7.0 mass %).









TABLE 56







1.2 ≥ CO2 > 0














N
Example
O
O
Example
P


Item
18.2
27.6
36.8
36.8
44.2
51.7
















CO2 = 0 mass %
27.7
24.5
22.6
22.6
21.2
20.5









Approximate
0.0072x2
0.0064x2


formula of
0.6701x + 37.512
0.7103x + 40.07


E-HFO-1132




when x = R32















CO2 = 0.6 mass %
29.6
26.3
24
24
22.4
20.9









Approximate
0.0054x2
0.0011x2


formula of
0.5999x + 38.719
0.3044x + 33.727


E-HFO-1132




when x = R32















CO2 = 1.2 mass %
31.7
27.9
25.4
25.4
23.7
22.1









Approximate
0.0071x2
0.0011x2


formula of
0.7306x + 42.636
0.3189x + 35.644


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.00487w2
0.0074w2


formula of
0.0059w + 0.0072
0.0133w + 0.0064


coefficient a




Approximate
−0.279w2 +
−0.5839w2 +


formula of
0.2844w − 0.6701
1.0268w − 0.7103


coefficient b




Approximate
3.7639w2
11.472w2


formula of
0.2467w + 37.512
17.455w + 40.07


coefficient c




Approximate
(0.00487w2 − 0.0059w +
(0.0074w2 − 0.0133w +


formula of
0.0072)x2 + (−0.279w2 +
0.0064)x2 + (−0.5839w2 +


E-HFO-1132
0.2844w − 0.6701)x + (3.7639w2
1.0268w − 0.7103)x + (11.472w2


when x = R32,
0.2467w + 37.512)
17.455w + 40.07)


w = CO2, and




1.2 ≥ w > 0




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
















TABLE 57







4.0 ≥ CO2 ≥ 1.2














N
Example
O
O
Example
P


Item
18.2
27.6
36.8
36.8
44.2
51.7
















CO2 = 1.2 mass %
31.7
27.9
25.4
25.4
23.7
22.1









Approximate
0.0071x2
0.0011x2


formula of
0.7306x + 42.636
0.3189x + 35.644


E-HFO-1132




when x = R32















CO2 = 2.5 mass %
34.2
29.9
27.2
27.2
25.2
23.4









Approximate
0.0088x2
0.002x2


formula of
0.8612x + 46.954
0.4348x + 40.5 


E-HFO-1132




when x = R32















CO2 = 4.0 mass %
35.5
31
28
28
25.9
23.9









Approximate
0.0082x2
0.0011x2


formula of
0.8546x + 48.335
0.3768x + 40.412


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
−0.00062w2 +
−0.000463w2 +


formula of
0.0036w + 0.0037
0.0024w − 0.0011


coefficient a




Approximate
0.0375w2
0.0457w2


formula of
0.239w − 0.4977
0.2581w − 0.075


coefficient b




Approximate
−0.8575w2 +
−1.355w2 +


formula of
6.4941w + 36.078
8.749w + 27.096


coefficient c




Approximate
(−0.00062w2 + 0.0036w +
(−0.000463w2 + 0.0024w −


formula of
0.0037)x2 + (0.0375w2
0.0011)x2 + (0.0457w2 −


E-HFO-1132
0.239w − 0.4977)x + (−0.8575w2 +
0.2581w − 0.075)x + (−1.355w2 +


when x = R32,
6.4941w + 36.078)
8.749w + 27.096)


w = CO2, and




4.0 ≥ w ≥ 1.2




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
















TABLE 58







7.0 ≥ CO2 ≥ 4.0














N
Example
O
O
Example
P


Item
18.2
27.6
36.8
36.8
44.2
51.7
















CO2 = 4.0 mass %
35.5
31.0
28.0
28.0
25.9
23.9









Approximate
0.0082x2
0.0011x2


formula of
0.8546x + 48.335
0.3768x + 40.412


E-HFO-1132




when x = R32















CO2 = 5.5 mass %
36.3
31.6
28.4
28.4
26.2
24.2









Approximate
0.0082x2
0.0021x2


formula of
0.8747x + 49.51 
0.4638x + 42.584


E-HFO-1132




when x = R32















CO2 = 7.0 mass %
36.7
31.9
28.6
28.6
26.4
24.2









Approximate
0.0082x2
0.0003x2


formula of
0.8848x + 50.097
0.3188x + 39.923


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.0082
−0.0006258w2 + 0.0066w −


formula of

0.0153


coefficient a




Approximate
0.0022w2
0.0516w2


formula of
0.0345w − 0.7521
0.5478w + 0.9894


coefficient b




Approximate
−0.1307w2 +
−1.074w2 +


formula of
2.0247w + 42.327
11.651w + 10.992


coefficient c




Approximate
0.0082x2 + (0.0022w2
(−0.0006258w2 + 0.0066w −


formula of
0.0345w − 0.7521)x + (−0.1307w2 +
0.0153)x2 + (0.0516w2 −


E-HFO-1132
2.0247w + 42.327)
0.5478w + 0.9894)x + (−1.074w2 +


when x = R32,

11.651w + 10.992)


w = CO2, and




7.0 ≥ w ≥ 4.0




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2









(1-6) Various Refrigerants 2


Hereinafter, the refrigerant 2A to the refrigerant 2E that are each the refrigerant for use in the present disclosure will be described in detail.


The following respective descriptions of the refrigerant 2A, refrigerant 2B, refrigerant 2C, refrigerant 2D and refrigerant 2E are independent, and alphabets representing points and/or line segments, and numbers of Examples and numbers of Comparative Examples are all independent among the refrigerant 2A, refrigerant 2B, refrigerant 2C, refrigerant 2D and refrigerant 2E. For example, Example 1 of the refrigerant 2A and Example 1 of the refrigerant 2B represent respective Examples about embodiments different from each other.


(1-6-1) Refrigerant 2A


Examples of the refrigerant 2A include a “refrigerant 2A1” and a “refrigerant 2A2”. Hereinafter, the refrigerant 2A1 and the refrigerant 2A2 will be each described. In the present disclosure, the refrigerant 2A1 and the refrigerant 2A2 are each a mixed refrigerant.


(1-6-1-1) Refrigerant 2A1


The refrigerant 2A1 is a mixed refrigerant including HFO-1132(E), HFC-32 and HFO-1234yf as essential components. Hereinafter, HFO-1132(E), HFC-32 and HFO-1234yf are also referred to as “three components”, in the present section.


The total concentration of the three components in the entire refrigerant 2A1 is 99.5 mass % or more. In other words, the refrigerant 2A1 includes 99.5 mass % or more of the three components in terms of the sum of the concentrations of these components.


The mass ratio of the three components in the refrigerant 2A1 is within the range of a region surrounded by a figure passing through four points:


point A (HFO-1132(E)/HFC-32/HFO-1234yf=51.8/1.0/472 mass %),


point B (HFO-1132(E)/FHFC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


point C (HFO-1132(E)/HFC-32/HFO-1234yf=10.1/18.0/71.9 mass %) and


point D (HFO-1132(E)/HFC-32/HFO-1234yf=27.8/18.0/54.2 mass %);


in a ternary composition diagram with the three components as respective apexes.


In other words, the mass ratio of the three components in the refrigerant 2A1 is within the range of a region surrounded by a straight line a, a curve b, a straight line c and a curved that connect four points:


point A (HFO-1132(E)/HFC-32/HFO-1234yf=51.8/1.0/47.2 mass %),


point B (HFO-1132(E)/HFC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


point C (HFO-1132(E)/HFC-32/HFO-1234yf=10.1/18.0/71.9 mass %) and


point D (HFO-1132(E)/HFC-32/HFO-1234yf=27.8/18.0/54.2 mass %);


indicated in a ternary composition diagram of FIG. 2A, with the three components as respective apexes.


In the present section, the ternary composition diagram with the three components as respective apexes means a three-component composition diagram where the three components (HFO-1132(E), HFC-32 and HFO-1234yf) are assumed as respective apexes and the sum of the concentrations of HFO-1132(E), HFC-32 and HFO-1234yf is 100 mass %, as represented in FIG. 2A.


The refrigerant 2A1, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (125 or less), (2) a refrigerating capacity and a coefficient of performance (COP) equivalent to or more than those of R404A when used as an alternative refrigerant of R404A, and (3) a flame velocity of 5 cm/s or less as measured according to ANSI/ASHRAE Standard 34-2013.


In the present section, the coefficient of performance (COP) equivalent to or more than that of R404A means that the COP ratio relative to that of R404A is 100% or more (preferably 102% or more, more preferably 103% or more), and the refrigerating capacity equivalent to or more than that of R404A means that the refrigerating capacity ratio relative to that of R404A is 95% or more (preferably 100% or more, more preferably 102 or more, most preferably 103% or more). A sufficiently low GWP means a GWP of 125 or less, preferably 110 or less, more preferably 100 or less, further preferably 75 or less.


The point A, the point B, the point C and the point D in FIG. 2A are each a point that is represented by a white circle (◯) and that has the above coordinates.


The technical meanings of the points A, B, C and D are as follows. The concentration (mass %) at each of the points is the same as any value determined in Examples described below.


A: any mass ratio providing a flame velocity of 5 cm/s as measured according to ANSI/ASHRAE Standard 34-2013 and a concentration (mass %) of HFC-32 of 1.0 mass %


B: any mass ratio providing a concentration (mass %) of HFC-32 of 1.0 mass % and a refrigerating capacity relative to that of R404A of 95%


C: any mass ratio providing a refrigerating capacity relative to that of R404A of 95% and a GWP of 125


D: any mass ratio providing a GWP of 125 and a flame velocity of 5 cm/s as measured according to ANSI/ASHRAE Standard 34-2013


A “flame velocity of 5 cm/s as measured according to ANSI/ASHRAE Standard 34-2013” corresponds to any numerical value half the flame velocity (10 cm/s) as a reference for classification as Class 2L (lower flammability) according to ANSI/ASHRAE Standard 34-2013, and a refrigerant having such a flame velocity means a relatively safe refrigerant, among refrigerants prescribed in Class 2L. Specifically, a refrigerant having such “any numerical value half the flame velocity (10 cm/s)” is relatively safe in that flame hardly propagates even in the case of ignition by any chance. Hereinafter, such a flame velocity as measured according to ANSI/ASHRAE Standard 342013 is also simply referred to as “flame velocity”.


The flame velocity of the mixed refrigerant of the three components in the refrigerant 2A1 is preferably more than 0 to 4.5 cm/s, more preferably more than 0 to 4 cm/s, further preferably more than 0 to 3.5 cm/s, particularly preferably more than 0 to 3 cm/s.


Both the points A and B are on the straight line a That is, a line segment AB is a part of the straight line a. The straight line a is a straight line indicating any mass ratio providing a concentration (mass %) of HFC-32 of 1.0 mass %. The mixed refrigerant of the three components has a concentration of HFC-32 of more than 1 mass % in a region close to the apex HFC-32 with respect to the straight line a in the ternary composition diagram.


The refrigerating capacity is unexpectedly high in a region close to the apex HFC-32 with respect to the straight line a in the ternary composition diagram.


In a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively, in FIG. 2A, a line segment indicating any mass ratio providing a concentration of HFC-32 of 1.0 mass % is approximated to a line segment represented by the following expressions.


The line segment indicating any mass ratio providing a concentration of HFC-32 of 1.0 mass % is a part of the straight line a that connects two points of the point A and the point B (line segment AB in FIG. 2A)

y=1.0
z=100−x−y.
35.3≤x≤51.8


Both the points B and C are on the curve b. The curve b is a curve indicating any mass ratio providing a refrigerating capacity relative to that of R404A of 95%. The mixed refrigerant of the three components has a refrigerating capacity relative to that of R404A of more than 95% in a region close to the apex HFO-1132(E) and the apex HFC-32 with respect to the curvet in the ternary composition diagram.


The curve b is determined as follows.


Table 201 represents respective four points where the refrigerating capacity ratio relative to that of R404A is 95% in a case where the mass % of HFO-1132(E) corresponds to 1.0, 10.1, 20.0 and 35.3. The curve b is indicated by a line that connects the four points, and the curve b is approximated by the expressions in Table 201, according to a least-squares method, in a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively.














TABLE 201





Item
Unit
bHFO-1132(E)=
bHFO-1132(E)=
bHFO-1132(E)=
bHFO-1132(E)=




















HFO-1132(E)
mass %
1.0
10.1
20.0
35.3


HFC-32
mass %
24.8
18.0
11.0
1.0


HFO-1234yf
mass %
74.2
71.9
69.0
63.7


Refrigerating
relative to that
95.0
95.0
95.0
95.0


capacity
of R404A (%)













x = HFO-1132(E)
mass %
Expressions of curve b


y = HFC-32
mass %
y = 0.1603x2 − 0.7552x + 0.2562


z = HFO-1234yf
mass %
z = 100 − x − y









Both the points C and D are on the straight line c. That is, a line segment CD is a part of the straight line c. The straight line c is a straight line indicating any mass ratio providing a GWP of 125. The mixed refrigerant of the three components has a GWP of less than 125 in a region close to the apex. HFO-1132(E) and the apex HFO-1234yf with respect to the straight line c in the ternary composition diagram.


In a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively, in FIG. 2A, a line segment indicating any mass ratio providing a GWP of 125 is approximated to a line segment represented by the following expressions.


The line segment indicating any mass ratio providing a GWP of 125 is a part of the straight line c that connects two points of the point C and the point D (line segment CD in FIG. 2A)

y=18.0
z=100−x−y
10.1≤x≤7.8


Both the points A and D are on the curve d. The curved is a curve indicating any mass ratio providing a flame velocity of 5 cm/s. The mixed refrigerant of the three components has a flame velocity of less than 5.0 cm/s in a region close to the apex HFO-1234yf with respect to the curve d in the ternary composition diagram.


The curve d is determined as follows.


Table 202 represents respective four points where WCF lower flammability is exhibited in a case where the mass % of HFO-1132(E) corresponds to 18.0, 30.0, 40.0 and 53.5 mass %. The curve d is indicated by a line that connects the four points, and the curve d is approximated by the expressions in Table 202, according to a least-squares method, in a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively.














TABLE 202





Item
Unit
dHFO-1132(E)=
dHFO-1132(E)=
dHFO-1132(E)=
dHFO-1132(E)=




















HFO-1132(E)
mass %
18.0
30.0
40.0
53.5


HFC-32
mass %
30.0
15.5
7.5
0.0


HFO-1234yf
mass %
52.0
54.5
52.5
46.5


Flame velocity
cm/s
5.0
5.0
5.0
5.0









x = HFO-1132(E)
mass %
Expressions of curve d


y = HFC-32
mass %
y = 1.4211x2 − 1.8563x + 0.5871


z = HFO-1234yf
mass %
z = 100 − x − y









A ternary mixed refrigerant of HFO-1132(E), HFC-32 and HFO-1234yf has a GWP of 125 or less, a refrigerating capacity ratio relative to that of R404A of 95% or more, and a flame velocity of 5 cm/s or less, at any mass ratio within the range of a region (ABCD region) surrounded by lines that connect four points of the points A, B, C and D.


The mass ratio of the three components in the refrigerant 2A1 is preferably within the range of a region surrounded by a figure passing through four points:


point A (HEO-1132(E)/HFC-32/HFO-1234yf=51.8/1.0/47.2 mass %),


point B (HFO-1132(E)/HFC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


point E (HFO-1132(E)/HFC-32/HFO-1234yf=15.2/14.3/70.5 mass %) and


point F (HFO-1132(E)/HFC-32/HFO-1234yf=31.1/14.3/54.6 mass %);


in a ternary composition diagram with the three components as respective apexes.


In other words, the mass ratio of the three components in the refrigerant 2A1 is preferably within the range of a region surrounded by a straight line a, a curve b, a straight line e and a curve d that connect four points:


point A (HFO-1132(E)/HFC-32/HFO-1234yf=51.8/1.0/47.2 mass %),


point B (HFO-1132(E)/f FC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


point E (HFO-1132(E)/HFC-32/HFO-1234yf=15.2/14.3/70.5 mass %) and


point F (HFO-1132(E)/HFC-32/HFO-1234yf=31.1/143/54.6 mass %);


indicated in a ternary composition diagram of FIG. 2A, with the three components as respective apexes.


The ternary composition diagram with the three components as respective apexes is as described above.


The point A, the point B, the point E and the point F in FIG. 2A are each a point that is represented by a white circle (◯) and that has the above coordinates.


The technical meanings of the points A and B are as described above.


The technical meanings of the points E and F are as follows. The concentration (mass %) at each of the points is the same as any value determined in Examples described below.


E: any mass ratio providing a refrigerating capacity relative to that of R404A of 95% and a GWP of 100


F: any mass ratio (GWP=100) providing a GWP of 100 and a flame velocity of 5 cm/s as measured according to ANSI/ASHRAE Standard 34-2013


The straight line a and the curve b are as described above. The point E is on the curve b.


Both the points E and F are on the straight line e. That is, a line segment EF is a part of the straight line e. The straight line e is a straight line indicating any mass ratio providing a GWP of 100. The mixed refrigerant of the three components has a GWP of less than 100 in a region close to the apex HFO-1132(E) and the apex HFO-1234yf with respect to the straight line e in the ternary composition diagram.


In a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively, in FIG. 2A, a line segment indicating any mass ratio providing a GWP of 100 is approximated to a line segment represented by the following expressions.


The line segment indicating any mass ratio providing a GWP of 100 is a part of the straight line e that connects two points of the point E and the point F (line segment EF in FIG. 2A)

y=14.3
z=100−x−y
15.2≤x≤1.1


Both the points A and F on the curve d. The curved is as described above.


A ternary mixed refrigerant of HFO-1132(E), HFC-32 and HFO-1234yf has a GWP of 100 or less, a refrigerating capacity ratio relative to that of R404A of 95% or more, and a flame velocity of 5.0 cm/s or less, at any mass ratio within the range of a region (ABEF region) surrounded by lines that connect four points of the points A, B, E and F.


The refrigerant 2A1 includes 99.5 mass % or more of HFO-1132(E), HFC-32 and HFO-1234yf in terms of the sum of the concentrations of these components, and in particular, the total amount of HFO-1132(E), HFC-32 and HFO-1234yf in the entire refrigerant 2A1 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2A1 can further include other refrigerant, in addition to HFO-1132(E), ITC-32 and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2A1 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2A1.


The refrigerant 2A1 particularly preferably consists only of HFO-1132(E), HFC-32 and HFO-1234yf. In other words, the refrigerant 2A1 particularly preferably includes HFO-1132(E), HFC-32 and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant A1.


In a case where the refrigerant 2A1 consists only of HFO-1132(E), HFC-32 and HFO-1234yf, the mass ratio of the three components is preferably within the range of a region surrounded by a figure passing through four points:


point A (HFO-1132(E)/HFC-32/HFO-1234yf=51.8/1.0/47.2 mass %),


point B (HFO-1132(E)/HFC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


point C (HFO-1132(E)/H C-32/HFO-1234yf=10.1/18.0/71.9 mass %) and


point D (HFO-1132(E)/HFC-32/FIFO-1234yf=27.8/18.0/54.2 mass %);


in the ternary composition diagram with the three components as respective apexes.


The technical meanings of the points A, B, C and D are as described above. The region surrounded by a figure passing through four points of the points A, B, C and D is as described above.


In such a case, a ternary mixed refrigerant of HFO-1132(E), HFC-32 and HFO-1234yf has a GWP of 125 or less, a refrigerating capacity ratio relative to that of R404A of 95% or more, and a flame, velocity of 5.0 cm/s or less, at any mass ratio within the range of a region (ABCD region) surrounded by lines that connect four points of the points A, B, C and D.


In a case where the refrigerant 2A1 consists only of HFO-1132(E), HFC-32 and HFO-1234yf, the mass ratio of the three components is more preferably within the range of a region surrounded by a figure passing through four points:


point A (HFO-1132(E)/HFC-32/HFO-1234yf=51.8/1.0/47.2 mass %),


point B (HFO-1132(E)/HFC-32/HFO-1234yf=35:3/1.0/63.7 mass %),


point E (HFO-1132(E)/HFC-32/HFO-1234yf=15.2/14.3/70.5 mass %) and


point F (HFO-1132(E)/HFC-32/HFO-1234yf=31.1/14.3/54.6 mass %);


in the ternary composition diagram with the three components as respective apexes.


The technical meanings of the points A, B, E and F are as described above. The region surrounded by a figure passing through four points of the points A, B, E and F is as described above.


In such a case, a ternary mixed refrigerant of HFO-1132(E), HFC-32 and HFO-1234yf has a GWP of 100 or less, a refrigerating capacity ratio relative to that of R404A of 95% or more, and a flame velocity of 5.0 cm/s or less, at any mass ratio within the range of a region (ABEF region) surrounded by lines that connect four points of the points A, B, E and E


The refrigerant 2A1 has a GWP of 125 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


(1-6-1-2) Refrigerant 2A2


The refrigerant 2A2 is a mixed refrigerant including HFO-1132(E), HFC-32 and HFO-1234yf as essential components. Hereinafter, HFO-1132(E), HFC-32 and HFO-1234yf are also referred to as “three components”, in the present section.


The total concentration of the three components in the entire refrigerant 2A2 is 99.5 mass % or more. In other words, the refrigerant 2A2 includes 99.5 mass % or more of the three components in terms of the sum of the concentrations of these components.


A composition in which the mass ratio of the three components in the refrigerant 2A2 is within the range of a region surrounded by a figure passing through five points:


point P (HFO-1132(E)/HFC 32/HFO-1234yf=45.6/1.0/53.4 mass %),


point B (HFO-1132(E)/HFC-32/UFO-1234yf=35.3/1.0/63.7 mass %),


point Q (HFO-1132(E)/HFC-32/HFO-1234yf=1.0/24.8/74.2 mass %),


point R (HFO-1132(E)/HFC-32/HFO-1234yf=1.0/29.2/69.8 mass %) and


point S (HFO-1132(E)/HFC-32/HFO-1234yf=6.5/29.2/64.3 mass %);


in a ternary composition diagram with the three components as respective apexes.


In other words, the mass ratio of the three components in the refrigerant 2A2 is within the range of a region surrounded by a straight line p, a curve q, a straight liner, a straight lines and a curve t that connect five points:


point P (HFO-1132(E)/HFC-32/HFO-1234yf=45.6/1.0/53.4 mass %),


point B (HFO-1132(E)/HFC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


point Q (HFO-1132(E)/HFC-32/HFO-1234yf=1.0/24.8/74.2 mass %),


point R (HFO-1132(E)/HFC-32/HFO-1234yf=1.0/29.2/69.8 mass %) and


point S (HFO-1132(E)/HFC-32/HFO-1234yf=6.5/29.2/64.3 mass %);


indicated in a ternary composition diagram of FIG. 2B, with the three components as respective apexes.


In the present section, the ternary composition diagram with the three components as respective apexes means a three-component composition diagram where the three components (HFO-1132(E), HFC-32 and HFO-1234yf) are assumed as respective apexes and the sum of the concentrations of HFO-1132(E), HFC-32 and HFO-1234yf is 100 mass %, as represented in FIG. 2B.


The refrigerant 2A2, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (200 or less), (2) a refrigerating capacity and a coefficient of performance (COP) equivalent to or more than those of R404A when used as an alternative refrigerant of R404A, and (3) a pressure at 40° C. of 1.85 MPa or less.


In the present section, the coefficient of performance (COP) equivalent to or more than that of R404A means that the COP ratio relative to that of R404A is 100% or more (preferably 102% or more, more preferably 103% or more). The refrigerating capacity equivalent to or more than that of R404A means that the refrigerating capacity ratio relative to that of R404A is 95% or more (preferably 100% or more, more preferably 102 or more, most preferably 103% or more). A sufficiently low GWP means a GWP of 200 or less, preferably 150 or less, more preferably 125 or less, further preferably 100 or less.


The point P, the point B, the point Q, the point R and the point S in FIG. 2 are each a point that is represented by a white circle (◯) and that has the above coordinates.


The technical meanings of the point P, the point B, the point Q, the point R and the point S are as follows. The concentration (mass %) at each of the points is the same as any value determined in Examples described below


P: any mass ratio providing a pressure at 40° C. of 1.85 MPa and a concentration (mass %) of HFC-32 of 1.0 mass %


B: any mass ratio providing a concentration (mass %) of HFC-32 of 1.0 mass % and a refrigerating capacity relative to that of R404A of 95%


Q: any mass ratio providing a refrigerating capacity relative to that of R404A of 95% and a concentration (mass %) of HFO-1132(E) of 1.0 mass %


R any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % and a GWP of 200


S: any mass ratio providing a GWP of 200 and a pressure at 40° C. of 1.85 MPa


Such “any mass ratio providing a pressure at 40° C. of 1.85 MPa” means any mass ratio providing a saturation pressure at a temperature of 40(° C.) of 1.85 MPa.


In a case where the mixed refrigerant of the three components in the refrigerant 2A2 has a saturation pressure at 40° C. of more than 1.85 MPa, there is a need for the change in design from a refrigerating apparatus for R404A. The mixed refrigerant of the three components preferably has a saturation pressure at 40° C. of 1.50 to 1.85 MPa, more preferably 1.60 to 1.85 MPa, further preferably 1.70 to 1.85 MPa, particularly preferably 1.75 to 1.85 MPa.


Both the points P and B are on the straight line p. That is, a line segment PB is a part of the straight line p. The straight line p is a straight line indicating any mass ratio providing a concentration (mass %) of HFC-32 of 1.0 mass %. The mixed refrigerant of the three components has a concentration of HFC-32 of more than 1.0 mass % in a region close to the apex HFC-32 with respect to the straight line p in the ternary composition diagram. The refrigerating capacity is unexpectedly high in a region close to the apex HFC-32 with respect to the straight line p in the ternary composition diagram.


In a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively, in FIG. 2B, a line segment indicating any mass ratio providing a concentration of HFC-32 of 1.0 mass % is approximated to a line segment represented by the following expressions.


The line segment indicating any mass ratio providing a concentration (mass %) of HFC-32 of 1.0 mass % is a part of the straight line p that connects two points of the point P and the point B (line segment PB in FIG. 2B)

y=1.0
z=100−x−y
35.3≤x≤45.6


Both the points B and Q are on the curve q. The curve q is a curve indicating any mass ratio providing a refrigerating capacity relative to that of R404A of 95%. The mixed refrigerant of the three components has a refrigerating capacity relative to that of R404A of more than 95% in a region close to the apex HFO-1132(E) and the apex HFC-32 with respect to the curve q in the ternary composition diagram.


The curve q is determined as follows.


Table 203 represents respective four points where the refrigerating capacity ratio relative to that of R404A is 95% in a case where the mass % of HFO-1132(E) corresponds to 1.0, 10.1, 20.0 and 35.3. The curve q is indicated by a line that connects the four points, and the curve q is approximated by the expressions in Table 203, according to a least-squares method, in a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively.














TABLE 203





Item
Unit
qHFO-1132(E)=
qHFO-1132(E)=
qHFO-1132(E)=
qHFO-1132(E)=




















HFO-1132(E)
mass %
1.0
10.1
20.0
35.3


HFC-32
mass %
24.8
18.0
11.0
1.0


HFO-1234yf
mass %
74.2
71.9
69.0
63.7


Refrigerating
relative to that
95
95
95
95


capacity
of R404A (%)













x = HFO-1132(E)
mass %
Expressions of curve q


y = HFC-32
mass %
y = 0.1603x2 − 0.7552x + 0.2562


z = HFO-1234yf
mass %
z = 100 − x − y









Both the points Q and R are on the straight liner. That is, a line segment QR is a part of the straight liner. The straight line r is a straight line indicating any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass %. The mixed refrigerant of the three components has a concentration of HFO-1132(E) of more than 1.0 mass % in a region close to the apex HFO-1132(E) with respect to the straight liner in the ternary composition diagram. The refrigerating capacity is unexpectedly high in a region close to the apex HFO-1132(E) with respect to the straight liner in the ternary composition diagram.


In a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively, in FIG. 2B, a line segment indicating any mass ratio providing a concentration of HFO-1132(E) of 1.0 mass % is approximated to a line segment represented by the following expressions.


The line segment indicating any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % is a part of the straight liner that connects two points of the point Q and the point R (line segment QR in FIG. 2B)

x=1.0
z=100−x−y
24.8≤y≤29.2


Both the points R and S are on the straight line s. That is, a line segment RS is a part of the straight line s. The straight line s is a straight line indicating any mass ratio providing a GWP of 200. The mixed refrigerant of the three components has a GWP of less than 200 in a region close to the apex HFO-1132(E) and the apex HFO-1234yf with respect to the straight lines in the ternary composition diagram.


In a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively, in FIG. 2B, a line segment indicating any mass ratio providing a GWP of 200 is approximated to a line segment represented by the following expressions.


The line segment indicating any mass ratio providing a GWP of 200 is a part of the straight lines that connects two points of the point R and the point S (line segment RS in FIG. 2B)

y=29.2
z=100−x−y
1.0≤x≤6.5


Both the points P and S are on the curve t. The curve t is a curve indicating any mass ratio providing a pressure at 40° C. of 1.85 MPa. The mixed refrigerant of the three components has a pressure at 40° C. of less than 1.85 MPa in a region close to the apex HFO-1234yf with respect to the curve t in the ternary composition diagram.


The curve t is determined as follows.


Table 204 represents respective four points where the pressure at 40° C. is 1.85 MPa in a case where the mass % of HFO-1132(E) corresponds to 5.95, 18.00, 32.35 and 47.80. The curve t is indicated by a line that connects the four points, and the curve t is approximated by the expressions in Table 204, according to a least-squares method, in a case where the mass % of HFO-1132(E), the mass % of HFC-32 and the mass % of HFO-1234yf are represented by x, y and z, respectively.














TABLE 204





Item
Unit
tHFO-1132(E)=
tHFO-1132(E)=
tHFO-1132(E)=
tHFO-1132(E)=




















HFO-1132(E)
mass %
5.6
17.0
30.7
45.6


HFC-32
mass %
30.0
20.0
10.0
1.0


HFO-1234yf
mass %
64.4
63.0
59.3
53.4


Pressure at 40° C.
Mpa
1.850
1.850
1.850
1.850









x = HFO-1132(E)
mass %
Expressions of curve t


y = HFC-32
mass %
y = 0.5016x2 − 0.9805x + 0.3530


z = HFO-1234yf
mass %
z = 100 − x − y









A ternary mixed refrigerant of HFO-1132(E), HFC-32 and HFO-1234yf has a GWP of 200 or less, a refrigerating capacity ratio relative to that of R404A of 95% or more, and a pressure at 40° C. of 1.85 MPa or less, at any mass ratio within the range of a region (PBQRS region) surrounded by lines that connect five points of the points P, B, Q, R and S.


The refrigerant 2A2 includes 99.5 mass % or more of HFO-1132(E), HFC-32 and HFO-1234yf in terms of the sum of the concentrations of these components, and in particular, the total amount of HFO-1132(E), HFC-32 and HFO-1234yf in the entire refrigerant 2A2 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2A2 can further include other refrigerant, in addition to HFO-1132(E), HFC-32 and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2A2 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2A2.


The refrigerant 2A2 particularly preferably consists only of HFO-1132(E), HFC-32 and HFO-1234yf. In other words, the refrigerant 2A2 particularly preferably includes HFO-1132(E), HFC-32 and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2A2.


In a case where the refrigerant 2A2 consists only of HFO-1132(E), HFC-32 and HFO-1234yf, the mass ratio of the three components is preferably within the range of a region surrounded by a figure passing through five points:


point P (HFO-1132(E)/HFC-32/HFO-1234yf=45.6/1.0/53.4 mass %),


point B (HFO-1132(E)/IBC-32/HFO-1234yf=35.3/1.0/63.7 mass %),


point Q (HFO-1132(E)/HFC-32/HFO-1234yf=1.0/24.8/74.2 mass %),


point R (HFO-1132(E)/HFC-32/HFO-1234yf=1.0/29.2/69.8 mass %) and


point S (HFO-1132(E)/HFC-32/HFO-1234yf=6.5/29.2/64.3 mass %);


in the ternary composition diagram with the three components as respective apexes.


The technical meanings of the point P, the point B, the point Q, the point R and the point S are as described above. The region surrounded by a figure passing through five points of the point P, the point B, the point Q, the point R and the point S is as described above.


In such a case, a ternary mixed refrigerant of HFO-1132(E), HFC-32 and HFO-1234yf has a GWP of 300 or less, a refrigerating capacity ratio relative to that of R404A of 95% or more, and a pressure at 40° C. of 1.85 MPa, at any mass ratio within the range of a region (PBQRS region) surrounded by lines that connect five points of the points P, B, Q, R and S.


The refrigerant 2A2 has a GWP of 200 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


Examples of Refrigerant 2A

Hereinafter, the refrigerant 2A will be described with reference to Examples in more detail. It is noted that the present disclosure is not limited to such Examples.


Test Example 1

The GWP of each mixed refrigerant represented in Examples 1-1 to 1-11, Comparative Examples 1-1 to 1-6 and Reference Example 1-1 (R404A) was evaluated based on the value in the fourth report of IPCC (Intergovernmental Panel on Climate Change).


The COP, the refrigerating capacity and the saturation pressure at 40° C. of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NISI), and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature −40° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The results in Test Example 1 are shown in Table 205 and Table 206. Tables 205 and 206 show Examples and Comparative Examples of the refrigerant 2A1 of the present disclosure. In Tables 205 and 206, the “COP ratio (relative to that of R404A)” and the “Refrigerating capacity ratio (relative to that of R404A)” each represent the proportion (%) relative to that of R404A. In Tables 205 and 206, the “saturation pressure (40° C.)” represents the saturation pressure at a saturation temperature of 40° C.


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013.


The flame velocity test was performed as follows. First, the mixed refrigerant used had a purity of 99.5% or more, and degassing was made by repeating a cycle of freezing, pumping and thawing until no trace of air was observed on a vacuum gauge. The flame velocity was measured by a closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between electrodes at the center of a sample cell. The duration of discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of any flame was visualized using a schlieren photograph. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light-transmitting acrylic windows was used as the sample cell, and a xenon lamp was used as a light source. A schlieren image of any, flame was recorded by a high-speed digital video camera at a frame rate of 600 fps, and stored in a PC. Any case where the flame velocity was unmeasurable (0 cm/s) was rated as “NA (non-flammability)”.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09. Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>


Test container: spherical container of 280 mm in diameter (internal volume: 12 L)


Test temperature: 60° C.±3° C.


Pressure: 101.3 kPa±0.7 kPa


Water content: 0.0088 g±0.0005 g per gram of dry air (water content at a relative humidity of 50% at 23° C.)


Mixing ratio of refrigerant composition/air: ±0.2 vol. % by 1 vol. %


Mixing of refrigerant composition: ±0.1 mass %


Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer


Electrode interval: 6.4 mm (¼ inches)


Spark: 0.4 seconds±0.05 seconds


Criteria for determination:






    • A case where any flame was spread at more than 90 degrees around the ignition point flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)



















TABLE 205









Reference









Example









1-1
Comparative
Comparative
Comparative
Comparative
Comparative


Item
Unit
(R404A)
Example 1-1
Example 1-2
Example 1-3
Example 14
Example 1-5


















Composition
HFO-1132(E)
mass %
0%
40.0%
30.0%
20.0%
10.0%
10.0%


proportions
HFC-32
mass %
0%
10.0%
20.0%
10.0%
10.0%
30.0%



HFO-1234yf
mass %
0%
50.0%
50.0%
70.0%
80.0%
60.0%



HFC-125
mass %
44.0%  
  0%
  0%
  0%
  0%
  0%



HFC-143a
mass %
52.0%  
  0%
  0%
  0%
  0%
  0%



HFC-134a
mass %
4.0%  
  0%
  0%
  0%
  0%
  0%














GWP

3922
74
140
72
72
206


COP ratio (relative to that of
%
100
105.2
105.8
106.1
106.6
107.5


R404A)









Refrigerating capacity ratio
%
100
116.0
121.4
93.3
81.3
113.9


(relative to that of R404A)









Saturation pressure (40° C.)
MPa
1.822
1.982
2.044
1.684
1.513
1.922


Flame velocity
cm/s
NA (non-
5.7
5.8
2.8
2.2
3.8




flammability)





















Comparative
Example
Example
Example
Example
Example



Item
Unit
Example 1-6
1-1
1-2
1-3
1-4
1-5




















Composition
HFO-1132(E)
mass %
14.0%
43.0%  
35.0%  
30.0%
24.0%
20.0%



proportions
HFC-32
mass %
21.0%
2.0%  
7.0%  
10.0%
14.0%
15.0%




HFO-1234yf
mass %
65.0%
55.0%  
58.0%  
60.0%
62.0%
65.0%




HFC-125
mass %
  0%
0%
0%
  0%
  0%
  0%




HFC-143a
mass %
  0%
0%
0%
  0%
  0%
  0%




HFC-134a
mass %
  0%
0%
0%
  0%
  0%
  0%
















GWP

146
20
53
73
100
106



COP ratio (relative to that of
%
106.8
105.1
105.4
105.6
106.0
106.3



R404A)










Refrigerating capacity ratio
%
104.6
105.3
105.3
104.8
104.8
101.8



(relative to that of R404A)










Saturation pressure (40° C.)
MPa
1.821
1.839
1.845
1.839
1.836
1.795



Flame velocity
cm/s
3.5
4.1
4.0
3.9
4.1
3.5























TABLE 206








Reference









Example
Example
Example
Example
Example
Example
Example



1-1
1-6
1-7
1-8
1-9
1-10
1-11















Item
Unit
(R404A)
A
B
C
D
E
F



















Composition
HFO-1132(E)
mass %
0%
51.8%  
35.3%  
10.1%
27.8%
15.2%
31.1%


proportions
HFC-32
mass %
0%
1.0%  
1.0%  
18.0%
18.0%
14.3%
14.3%



HFO-1234yf
mass %
0%
47.2%  
63.7%  
71.9%
54.2%
70.5%
54.6%



HFC-125
mass %
44.0%  
0%
0%
  0%
  0%
  0%
  0%



HFC-143a
mass %
52.0%  
0%
0%
  0%
  0%
  0%
  0%



HFC-134a
mass %
4.0%  
0%
0%
  0%
  0%
  0%
  0%















GWP

3922
14
13
125
125
100
100


COP ratio (relative to that of R404A)
%
100
105.0
105.3
107.0
105.9
106.5
105.7


Refrigerating capacity ratio (relative to that
%
100
113.0
95.0
95.0
115.7
95.0
113.4


of R404A)










Saturation pressure (40° C.)
MPa
1.822
1.933
1.701
1.696
1.974
1.702
1.948


Flame velocity
cm/s
NA (non-
5.0
2.5
3.0
5.0
3.0
5.0




flammability)









Test Example 2

The GWP of each mixed refrigerant represented in Examples 2-1 to 2-11, Comparative Examples 2-1 to 2-5 and Reference Example 2-1 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity and the saturation pressure at 40° C. of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NISI), and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature −40° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The results in Test Example 2 are shown in Tables 207 and 208. Tables 207 and 208 show Examples and Comparative Examples of the refrigerant 2A2 of the present disclosure. In Tables 207 and 208, the meaning of each of the terms is the same as in Test Example 1.


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 1. The flame velocity test was performed in the same manner as in Test Example 1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 1.
















TABLE 207









Reference









Example









2-1
Comparative
Comparative
Comparative
Comparative
Comparative


Item
Unit
(R404A)
Example 2-1
Example 2-2
Example 2-3
Example 2-4
Example 2-5


















Composition
HFO-1132(E)
mass %
0%
40.0%
30.0%
20.0%
10.0%
10.0%


proportions
HFC-32
mass %
0%
10.0%
20.0%
10.0%
10.0%
30.0%



HFO-1234yf
mass %
0%
50.0%
50.0%
70.0%
80.0%
60.0%



HFC-125
mass %
44.0%  
  0%
  0%
  0%
  0%
  0%



HFC-143a
mass %
52.0%  
  0%
  0%
  0%
  0%
  0%



HFC-134a
mass %
4.0%  
  0%
  0%
  0%
  0%
  0%














GWP

3922
74
140
72
72
206


COP ratio (relative to that of
%
100
105.2
105.8
106.1
106.6
107.5


R404A)









Refrigerating capacity ratio
%
100
116.0
121.4
93.3
81.3
113.9


(relative to that of R404A)









Saturation pressure (40° C.)
MPa
1.822
1.982
2.044
1.684
1.513
1.922


Flame velocity
cm/s
NA (non-
5.7
5.8
2.8
2.2
3.8




flammability)





















Example
Example
Example
Example
Example
Example



Item
Unit
2-1
2-2
2-3
24
2-5
2-6




















Composition
HFO-1132(E)
mass %
43.0%  
35.0%  
30.0%
24.0%
14.0%
20.0%



proportions
HFC-32
mass %
2.0%  
7.0%  
10.0%
14.0%
21.0%
15.0%




HFO-1234yf
mass %
55.0%  
58.0%  
60.0%
62.0%
65.0%
65.0%




HFC-125
mass %
0%
0%
  0%
  0%
  0%
  0%




HFC-143a
mass %
0%
0%
  0%
  0%
  0%
  0%




HFC-134a
mass %
0%
0%
  0%
  0%
  0%
  0%
















GWP

20
53
73
100
146
106



COP ratio (relative to that of
%
105.1
105.4
105.6
106.0
106.8
106.3



R404A)










Refrigerating capacity ratio
%
105.3
105.3
104.8
104.8
104.6
101.8



(relative to that of R404A)










Saturation pressure (40° C.)
MPa
1.839
1.845
1.839
1.836
1.821
1.795



Flame velocity
cm/s
4.1
4.0
3.9
4.1
3.5
3.5






















TABLE 208








Reference








Example
Example
Example
Example
Example
Example



2-1
2-7
2-8
2-9
2-10
2-11














Item
Unit
(R404A)
P
B
Q
R
S


















Composition
HFO-1132(E)
mass %
0%
45.6%  
35.3%  
1.0%  
1.0%  
6.5%  


proportions
HFC-32
mass %
0%
1.0%  
1.0%
24.8%  
29.2%  
29.2%  



HFO-1234yf
mass %
0%
53.4%  
63.7%  
74.2%  
69.8%  
64.3%  



HFC-125
mass %
44.0%  
0%
0%
0%
0%
0%



HFC-143a
mass %
52.0%  
0%
0%
0%
0%
0%



HFC-134a
mass %
4.0%  
0%
0%
0%
0%
0%














GWP

3922
14
13
170
200
200


COP ratio (relative to that of R404A)
%
100
105.1
105.3
108.0
108.2
107.7


Refrigerating capacity ratio (relative to that of
%
100
106.4
95.0
95.0
101.8
108.5


R404A)









Saturation pressure (40° C.)
MPa
1.822
1.850
1.701
1.674
1.757
1.850


Flame velocity
cm/s
NA (non-
4.3
2.5
2.7
2.9
3.4




flammability)










(1-6-2) Refrigerant 2B


The refrigerant 2B is a mixed refrigerant including HFO-1132(E), HFO-1123 and HFO-1234yf as essential components. Hereinafter, HFO-1132(E), HFO-1123 and HFO-1234yf are also referred to as “three components”, in the present section.


The total concentration of the three components in the entire refrigerant 2B is 99.5 mass % or more. In other words, the refrigerant 2B includes 99.5 mass % or more of the three components in terms of the sum of the concentrations of these components.


The mass ratio of the three components in the refrigerant 2B is within the range of a region surrounded by a figure passing through five points:


point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


point D (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/57.0/42.0 mass %) and


point E (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/24.1/33.4 mass %);


in a ternary composition diagram with the three components as respective apexes.


In other words, the mass ratio of the three components in the refrigerant 2B is within the range of a region surrounded by a straight line a, a curve b, a straight line c, a curve d and a straight line e that connect five points:


point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


point D (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/57.0/42.0 mass %) and


point E (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/24.1/33.4 mass %);


indicated in a ternary composition diagram of FIG. 2C, with the three components as respective apexes.


In the present section, the ternary composition diagram with the three components as respective apexes means a three-component composition diagram where the three components (HFO-1132(E), HFO-1123 and HFO-1234yf) are assumed as respective apexes and the sum of the concentrations of HFO 1132(E), HFO-1123 and HFO-1234yf is 100 mass %, as represented in FIG. 2C.


The refrigerant 2B, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (125 or less), (2) a refrigerating capacity equivalent to or more than that of R404A when used as an alternative refrigerant of R404A, (3) a coefficient of performance (COP) equivalent to or more than that of R404A, and (4) a flame velocity of 5 cm/s or less as measured according to ANSI/ASHRAE Standard 34-2013.


In the present disclosure, the coefficient of performance (COP) equivalent to or more than that of R404A means that the COP ratio relative to that of R404A is 100% or more (preferably 101% or more, more preferably 102% or more, particularly preferably 103% or more).


In the present disclosure, the refrigerating capacity equivalent to or more than that of R404A means that the refrigerating capacity ratio relative to that of R404A is 85% or more (preferably 90% or more, more preferably 95% or more, further preferably 100% or more, particularly preferably 102% or more).


In the present disclosure, a sufficiently low GWP means a GWP of 125 or less, preferably 110 or less, more preferably 100 or less, particularly preferably 75 or less.


The point A, the point B, the point C, the point D and the point E in FIG. 2C are each a point that is represented by a white circle (◯) and that has the above coordinates.


The technical meanings of the points A, B, C, D and E are as follows. The concentration (mass %) at each of the points is the same as any value determined in Examples described below


A: any mass ratio providing a flame velocity of 3.0 cm/s as measured according to ANSI/ASHRAE Standard 34-2013 and a concentration (mass %) of HFO-1123 of 1.0 mass %


B: any mass ratio providing a concentration (mass %) of HFO-1123 of 1.0 mass % and a refrigerating capacity relative to that of R404A of 85%


C: any mass ratio providing a refrigerating capacity relative to that of R404A of 85% and a concentration (mass %) of HFO-1132(E) of 1.0 mass %


D: any mass ratio providing a concentration (mass %) off-WO-1132(E) of 1.0 mass % and a saturation pressure at 40° C. of 2.25 MPa


E: any mass ratio providing a saturation pressure at 40° C. of 2.25 MPa and a flame velocity of 3.0 cm/s as measured according to ANSI/ASHRAE Standard 34-2013


A “flame velocity of 3.0 cm/s as measured according to ANSI/ASHRAE Standard 34-2013” corresponds to any numerical value less than half the flame velocity (10 cm/s) as a reference for classification as Class 2L (lower flammability) according to ANSI/ASHRAE Standard 34-2013, and a refrigerant having such a flame velocity means a relatively safe refrigerant, among refrigerants prescribed in Class 2L.


Specifically, a refrigerant having such “any numerical value less than the half the flame velocity (10 cm/s)” is relatively safe in that flame hardly propagates even in the case of ignition by any chance. Hereinafter, such a flame velocity as measured according to ANSI/ASHRAE Standard 34-2013 is also simply referred to as “flame velocity”.


The flame velocity of the mixed refrigerant of the three components in the refrigerant 2B is preferably more than 0 and 2.5 cm/s or less, more preferably more than 0 and 2.0 cm/s or less, further preferably more than 0 and 1.5 cm/s or less.


Both the points A and B are on the straight line a That is, a line segment AB is a part of the straight line a. The straight line a is a straight line indicating any mass ratio providing a concentration (mass %) of HFO-1123 of 1.0 mass %. The mixed refrigerant of the three components has a concentration of HFO-1123 of more than 1.0 mass % in a region close to the apex HFO-1123 with respect to the straight line a in the ternary composition diagram.


In a case where the mass % of HFO-1132(E), the mass % of HFO-1123 and the mass % of HFO-1234yf are represented by x, y and z, respectively, in FIG. 2C, a line segment indicating any mass ratio providing a concentration of HFO-1123 of 1.0 mass % is approximated to a line segment represented by the following expressions.


The line segment indicating any mass ratio providing a concentration (mass %) of HFO-1123 of 1.0 mass % is a part of the straight line c that connects of two points of the point A and the point B (line segment AB in FIG. 2C)

y=1.0
z=100−x−y
27.1≤x≤42.5


Both the points B and C are on the curve b. The curve b is a curve indicating any mass ratio providing a refrigerating capacity relative to that of R404A of 85%. The mixed refrigerant of the three components has a refrigerating capacity relative to that of R404A of more than 85% in a region close to the apex HFO-1132(E) and the apex HFO-1123 with respect to the curve b in the ternary composition diagram.


The curve b is determined as follows.


Table 209 represents respective three points where the refrigerating capacity ratio relative to that of R404A is 85% in a case where the mass % of HFO-1132(E) corresponds to 1.0, 15.0 and 27.1. The curve b is indicated by a line that connects the three points, and the curve b is approximated by the expressions in Table 209, according to a least-squares method, in a case where the mass % of HFO-1132(E), the mass % of HFO-1123 and the mass % of HFO-1234yf are represented by x, y and z, respectively.













TABLE 209





Item
Unit
bHFO-1132(E)=
bHFO-1132(E)=
bHFO-1132(E)=



















HFO-1132(E)
mass %
1.0
15.0
27.1


HFO-1123
mass %
30.4
14.2
1.0


HFO-1234yf
mass %
68.6
70.8
71.9


Refrigerating
relative
85.0
85.0
85.0


capacity
to that of






R404A






(%)












x = HFO-1132(E)
mass %
Expressions of curve b


y = HFC-1123
mass %
y = 0.2538x2 − 1.1977x + 0.3160


z = HFO-1234yf
mass %
z = 100 − x − y









Both the points C and D are on the straight line c. That is, a line segment CD is a part of the straight line c. The straight line c is a straight line indicating any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass %. The mixed refrigerant of the three components has a concentration of HFO-1132(E) of more than 1.0 mass % in a region close to the apex HFO-1132(E) with respect to the straight line c in the ternary composition diagram.


In a case where the mass % of HFO-1132(E), the mass % of HFO-1123 and the mass % of HFO-1234yf are represented by x, y and z, respectively, in FIG. 2C, a line segment indicating any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % is approximated to a line segment represented by the following expressions.


The line segment indicating any ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % is a part of the straight line c that connects of two points of the point C and the point D (line segment CD in FIG. 2C)

x=1.0
z=100−x−y
30.4≤y≤57.0


Both the points D and E are on the curved. The curve d is a curve indicating any mass ratio providing a saturation pressure at 40° C. of 2.25 MPa. The mixed refrigerant of the three components has a saturation pressure at 40° C. of less than 2.25 MPa in a region close to the apex HFO-1234yf with respect to the curve d in the ternary composition diagram.


The curve d is determined as follows.


Table 210 represents respective three points where the saturation pressure at 40° C. is 2.25 MPa in a case where the mass % of HFO-1132(E) corresponds to 1.0, 20.0 and 42.5. The curve d is indicated by a line that connects the three points, and the curve d is approximated by the expressions in Table 210, according to a least-squares method, in a case where the mass % of HFO-1132(E), the mass % off-TO-1123 and the mass % of HFO-1234yf are represented by x, y and z, respectively.













TABLE 210





Item
Unit
bHFO-1132(E)=
bHFO-1132(E)=
bHFO-1132(E)=



















HFO-1132(E)
mass %
1.0
20.0
42.5


HFO-1123
mass %
57.0
40.7
24.1


HFO-1234yf
mass %
42.0
39.3
33.4


Saturation pressure
MPa
2.25
2.25
2.25


at 40° C.













x = HFO-1132(E)
mass %
Expressions of curve d


y = HFC-1123
mass %
y = 0.2894x2 − 0.9187x + 0.5792


z = HFO-1234yf
mass %
z = 100 − x − y









Both the points A and E are on the straight line e. The straight line e is a straight line indicating any mass ratio providing a flame velocity of 3.0 cm/s. The mixed refrigerant of the three components has a flame velocity of less than 3.0 cm/s in a region close to the apex HFO-1234yf and the apex HFO-1123 with respect to the straight line e in the ternary composition diagram.


In a case where the mass % of HFO-1132(E), the mass % of HFO-1123 and the mass % of HFO-1234yf are represented by, x, y and z, respectively, in FIG. 2C, any mass ratio providing a flame velocity of 3.0 cm/s is approximated to a line segment represented by the following expressions.


The line segment indicating any mass ratio providing a flame velocity of 3.0 cm/s is a part of the straight line e that connects of two points of the point A and the point E (line segment AE in FIG. 2C)

x=42.5
z=100−x−y
1.0≤y≤24.1


A ternary mixed refrigerant of HFO-1132(E), HFO-1123 and HFO-1234yf has various characteristics of (1) a GWP of 125 or less, (2) a refrigerating capacity ratio relative to that of R404A of 85% or more, (3) a saturation pressure at 40° C. of 2.25 MPa or less, and (4) a flame velocity of 3.0 cm/s or less, at any mass ratio within the range of a region (ABCDE region) surrounded by lines that connect five points of the points A, B, C, D and E.


The mass ratio of the three components in the refrigerant 2B is preferably within the range of a region surrounded by a figure passing through five points:


point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


point F (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/52.2/46.8 mass %) and


point G (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/18.9/38.6 mass %);


in a ternary composition diagram with the three components as respective apexes.


In other words, the mass ratio of the three components in the refrigerant 2B is preferably within the range of a region surrounded by a straight line a, a curve b, a straight line c, a curve f and a straight line e that connect five points:


point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


point F (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/52.2/46.8 mass %) and


point G (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/18.9/38.6 mass %);


indicated in a ternary composition diagram of FIG. 2C, with the three components as respective apexes:


The ternary composition diagram with the three components as respective apexes is as described above.


The point A, the point B, the point C, the point F and the point G in FIG. 2C are each a point that is represented by a white circle (◯) and that has the above coordinates.


The technical meanings of the points A, B and C are as described above.


The technical meanings of the points F and G are as follows. The concentration (mass %) at each of the points is the same as any value determined in Examples described below.


F: any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % and a saturation pressure at 40° C. of 2.15 MPa


G: any mass ratio providing a saturation pressure at 40° C. of 2.15 MPa and a flame velocity of 3.0 cm/s as measured according to ANSI/ASHRAE Standard 34-2013


The straight line a, the curve b, the straight line c and the straight line e are as described above. The Point F is on the straight line c and the point G is on the straight line e.


Both the points F and G are on the curve f. The curve f is a curve indicating any mass ratio providing a saturation pressure at 40° C. of 2.15 MPa. The mixed refrigerant of the three components has a saturation pressure at 40° C. of less than 2.15 MPa in a region close to the apex HFO-1234yf with respect to the curve fin the ternary composition diagram.


The curve f is determined as follows.


Table 211 represents respective three points where the saturation pressure at 40° C. is 2.25 MPa in a case where the mass % of HFO-1132(E) corresponds to 1.0, 20.0 and 42.5. The curve f is indicated by a line that connects the three points, and the curve f is approximated by the expressions in Table 211, according to a least-squares method, in a case where the mass % of HFO-1132(E), the mass % of HFO-1123 and the mass % of HFO-1234yf are represented by x, y and z, respectively.













TABLE 211





Item
Unit
bHFO-1132(E)=
bHFO-1132(E)=
bHFO-1132(E)=



















HFO-1132(E)
mass %
1.0
20.0
42.5


HFO-1123
mass %
52.2
35.7
18.9


HFO-1234yf
mass %
46.8
44.3
38.6


Saturation pressure
MPa
2.15
2.15
2.15


at 40° C.













x = HFO-1132(E)
mass %
Expressions of curve f


y = HFC-1123
mass %
y = 0.2934x2 − 0.9300x + 0.5313


z = HFO-1234yf
mass %
z = 100 − x − y









A ternary mixed refrigerant of HFO-1132(E), HFO-1123 and HFO-1234yf has various characteristics of (1) a GWP of 125 or less, (2) a refrigerating capacity ratio relative to that of R404A of 85% or more, (3) a saturation pressure at 40° C. of 2.15 MPa or less, and (4) a flame velocity of 3.0 cm/s or less, at any mass ratio within the range of a region (ABCFG region) surrounded by lines that connect five points of the points A, B, C, F and G.


The mass ratio of the three components in the refrigerant 2B is preferably within the range of a region surrounded by a figure passing through six points:


point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


point B (HFO-1132(E)/HFO-1123/HFO-1234yf=271/1.0/71.9 mass %),


point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


point H (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/35.2/63.8 mass %),


point I (HFO-1132(E)/HID-1123/HEO-1234yf=27.4/29.8/42.8 mass %) and


point G (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/18.9/38.6 mass %);


in a ternary composition diagram with the three components as respective apexes.


In other words, the mass ratio of the three components in the refrigerant 2B is preferably within the range of a region surrounded by a straight line a, a curve b, a straight line c, a curve g, a curve f and a straight line e that connect six points:


point A (HFO-1132(E)/HFO-1123/HFO-1234yf=2.5/1.0/56.5 mass %),


point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


point H (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/35.2/63.8 mass %),


point I (HFO-1132(E)/HFO-1123/HFO-1234yf=27.4/29.8/42.8 mass %) and


point G (HFO 1132(E)/HFO-1123/HFO-1234yf=42.5/18.9/38.6 mass %);


indicated in a ternary composition diagram of FIG. 2C, with the three components as respective apexes.


The ternary composition diagram with the three components as respective apexes is as described above.


The point A, the point B, the point C, the point G, the point H and the point I in FIG. 2C are each a point that is represented by a white circle (◯) and that has the above coordinates.


The technical meanings of the points A, B, C and G are as described above.


The technical meanings of the points H and I are as follows. The concentration (mass %) at each of the points is the same as any value determined in Examples described below.


H: any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % and a COP relative to that of R404A of 100%


I: any mass ratio providing a COP relative to that of R404A of 100% and a saturation pressure at 40° C. of 2.15 MPa


The straight line a, the curve b, the straight line c, the straight line e and the curve fare as described above. The point H is on the straight line c and the point I is on the curve f.


Both the points H and fare on the curve g. The curve g is a curve indicating any mass ratio providing a COP relative to that of R404A of 100%. The mixed refrigerant of the three components has a COP relative to that of R404A of less than 100% in a region close to the apex HFO-1132(E) and the apex HFO-1234yf with respect to the curve g in the ternary composition diagram.


The curve g is determined as follows.


Table 212 represents respective three points where the saturation pressure at 40° C. is 2.25 MPa in a case where the mass % of HFO-1132(E) corresponds to 1.0, 20.0 and 42.5. The curve f is indicated by a line that connects the three points, and the curve f is approximated by the expressions in Table 212, according to a least-squares method, in a case where the mass % of HFO-1132(E), the mass % of HFO-1123 and the mass % of HFO-1234yf are represented by x, y and z, respectively.













TABLE 212





Item
Unit
bHFO-1132(E)=
bHFO-1132(E)=
bHFO-1132(E)=



















HFO-1132(E)
mass %
1.0
20.0
42.5


HFO-1123
mass %
35.2
30.9
28.7


HFO-1234yf
mass %
63.8
49.1
28.8


COP
relative
100.0
100.0
100.0



to that of






R404A






(%)












x = HFO-1132(E)
mass %
Expressions of curve g


y = HFC-1123
mass %
y = 0.3097x2 − 0.2914x + 0.3549


z = HFO-1234yf
mass %
z = 100 − x − y









A ternary mixed refrigerant of HFO-1132(E), HFO-1123 and HFO-1234yf has various characteristics of (1) a GWP of 125 or less, (2) a refrigerating capacity ratio relative to that of R404A of 85% or more, (3) a COP ratio relative to that of R404A of 100% or more, (4) a saturation pressure at 40° C. of 2.15 MPa or less, and (5) a flame velocity of 3.0 cm/s or less, at any mass ratio within the range of a region (ABCHIG region) surrounded by lines that connect six points of the points A, B, C, H, I and G.


The refrigerant 2B includes 99.5 mass % or more of HFO-1132(E), HFO-1123 and HFO-1234yf in terms of the sum of the concentrations of these components, and in particular, the total amount of HFO-1132(E), HFO-1123 and HFO-1234yf in the entire refrigerant 2B is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2B can further include other refrigerant, in addition to HFO-1132(E), HFO-1123 and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2B is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2B.


The refrigerant 2B particularly preferably consists only of HFO-1132(E), HFO-1123 and HFO-1234yf. In other words, the refrigerant 2B particularly preferably includes HFO-1132(E), HFO-1123 and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2B.


In a case where the refrigerant 2B consists only of HFO-1132(E), HFO-1123 and HFO-1234yf, the mass ratio of the three components is preferably within the range of a region surrounded by a figure passing through five points:


point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


point C (HFO-1132(E)/HFO-1123/HFO-1234y=1.0/30.4/68.6 mass %),


point D (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/57.0/42.0 mass %) and


point E (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/24.1/33.4 mass %);


in the ternary composition diagram with the three components as respective apexes.


The technical meanings of the points A, B, C, D and E are as described above. The region surrounded by a figure passing through five points of the points A, B, C, D and E is as described above.


In such a case, a ternary mixed refrigerant of HFO-1132(E), HFO-1123 and HFO-1234yf has various characteristics of (1) a GWP of 125 or less, (2) a refrigerating capacity ratio relative to that of R404A of 85% or more, (3) a saturation pressure at 40° C. of 2.25 MPa or less, and (4) a flame velocity of 3.0 cm/s or less, at any mass ratio within the range of a region (ABCDE region) surrounded by lines that connect five points of the points A, B, C, D and E.


In a case where the refrigerant 2B consists only of HFO-1132(E), HFO-1123 and HFO-1234yf, the mass ratio of the three components is more preferably within the range of a region surrounded by a figure passing through five points:


point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


point F (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/52.2/46.8 mass %) and


point G (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/18.9/38.6 mass %);


in the ternary composition diagram with the three components as respective apexes.


The technical meanings of the points A, B, C, F and G are as described above. The region surrounded by a figure passing through five points of the points A, B, C, F and G is as described above.


In such a case, a ternary mixed refrigerant of HFO-1132(E), HFO-1123 and HFO-1234yf has various characteristics of (1) a GWP of 125 or less, (2) a refrigerating capacity ratio relative to that of R404A of 85% or more, (3) a saturation pressure at 40° C. of 2.15 MPa or less, and (4) a flame velocity of 3.0 cm/s or less, at any mass ratio within the range of a region (ABCFG region) surrounded by lines that connect five points of the points A, B, C, F and G.


In a case where the refrigerant 2B consists only of HFO-1132(E), HFO-1123 and HFO-1234yf, the mass ratio of the three components is further preferably within the range of a region surrounded by a figure passing through six points:


point A (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/1.0/56.5 mass %),


point B (HFO-1132(E)/HFO-1123/HFO-1234yf=27.1/1.0/71.9 mass %),


point C (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/30.4/68.6 mass %),


point H (HFO-1132(E)/HFO-1123/HFO-1234yf=1.0/35.2/63.8 mass %),


point I (HFO-1132(E)/HFO-1123/HFO-1234yf=27.4/29.8/42.8 mass %) and,


point G (HFO-1132(E)/HFO-1123/HFO-1234yf=42.5/18.9/38.6 mass %);


in the ternary composition diagram with the three components as respective apexes.


The technical meanings of the points A, B, C, G, H and I are as described above. The region surrounded by a figure passing through six points of the points A, B, C, H, I and G is as described above.


In such a case, a ternary mixed refrigerant of HFO-1132(E), HFO-1123 and HFO-1234yf has various characteristics of (1) a GWP of 125 or less, (2) a refrigerating capacity ratio relative to that of R404A of 85% or more, (3) a COP ratio relative to that of R404A of 100% or more, (4) a saturation pressure at 40° C. of 2.15 MPa or less, and (5) a flame velocity of 3.0 cm/s or less, at any mass ratio within the range of a region (ABCHIG region) surrounded by lines that connect six points of the points A, B, C, H, I and G.


The refrigerant 2B has a GWP of 125 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


Examples of Refrigerant 2B

Hereinafter, the refrigerant 2B will be described with reference to Examples in more detail. It is noted that the present disclosure is not limited to such Examples.


Test Example 1

The GWP of each mixed refrigerant represented in Examples 1 to 38, Comparative Examples 1 to 9 and Reference Example 1 (R404A) was evaluated based on the value in the fourth report of IPCC (Intergovernmental Panel on Climate Change).


The COP, the refrigerating capacity and the saturation pressure at 40° C. of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST), and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature −40° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The results in Test Example 1 are shown in Tables 213 to 216. In Tables 213 to 216, the “COP ratio (relative to that of R404A)” and the “Refrigerating capacity ratio (relative to that of R404A)” each represent the proportion (%) relative to that of R404A. In Tables 213 to 216, the “Saturation pressure (40° C.)” represents the saturation pressure at a saturation temperature of 40° C.


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013.


The flame velocity test was performed as follows. First, the mixed refrigerant used had a purity of 99.5% or more, and degassing was made by repeating a cycle of freezing, pumping and thawing until no trace of air was observed on a vacuum gauge. The flame velocity was measured by a closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between electrodes at the center of a sample cell. The duration of discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of any flame was visualized using a schlieren photograph. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light-transmitting acrylic windows was used as the sample cell, and a xenon lamp was used as a light source. A schlieren image of any flame was recorded by a high-speed digital video camera at a frame rate of 600 fps, and stored in a PC. Any case where the flame velocity was unmeasurable (0 cm/s) was rated as “NA (non-flammability)”.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09. Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>


Test container: spherical container of 280 mm in diameter (internal volume: 12 L)


Test temperature: 60° C.±3° C.


Pressure: 101.3 kPa±0.7 kPa


Water content 0.0088 g±0.0005 g per gram of dry air (water content at a relative humidity of 50% at 23° C.)


Mixing ratio of refrigerant composition/air: ±02 vol. % by 1 vol. %


Mixing of refrigerant composition: ±0.1 mass %


Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer


Electrode interval: 6.4 mm (¼ inches)


Spark: 0.4 seconds±0.05 seconds


Criteria for determination:






    • A case where any flame was spread at more than 90 degrees around the ignition point: flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)





















TABLE 213









Reference











Example











1
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
1
2
3
4
5
6
7




















Composition
HFO-1132(E)
mass %
0%
40.0%  
40.0%  
40.0%  
35.0%  
35.0%  
35.0%  
35.0%  


proportions
HFO-1123
mass %
0%
5.0%  
10.0%  
15.0%  
5.0%  
10.0%  
15.0%  
20.0%  



HFO-1234yf
mass %
0%
55.0%  
50.0%  
45.0%  
60.0%  
55.0%  
50.0%  
45.0%  



HFC-125
mass %
44.0%  
0%
0%
0%
0%
0%
0%
0%



HFC-143a
mass %
52.0%  
0%
0%
0%
0%
0%
0%
0%



HFC-134a
mass %
4.0%  
0%
0%
0%
0%
0%
0%
0%
















GWP

3922
6
6
6
6
6
6
6


COP ratio (relative to that of
%
100.0
104.3
103.4
102.4
104.4
103.5
102.5
101.6


R404A)











Refrigerating capacity ratio
%
100.0
104.0
109.7
115.5
98.4
104.1
109.8
115.6


(relative to that of R404A)











Saturation pressure (40° C.)
MPa
1.822
1.845
1.943
2.041
1.771
1.871
1.970
2.068


Flame velocity
cm/s
NA (non-
2.6
2.6
2.6
2.0
2.0
2.0
2.0




flammability)























Example
Example
Example
Example
Example
Example
Example
Example



Item
Unit
8
9
10
11
12
13
14
15






















Composition
HFO-1132(E)
mass %
30.0%  
30.0%  
30.0%  
30.0%  
30.0%  
25.0%  
25.0%  
25.0%  



proportions
HFO-1123
mass %
5.0%  
10.0%  
15.0%  
20.0%  
25.0%  
5.0%  
10.  0%
15.0%  




HFO-1234yf
mass %
65.0%  
60.0%  
55.0%  
50.0%  
45.0%  
70.0%  
65.0%  
60.0%  




HFC-125
mass %
0%
0%
0%
0%
0%
0%
0%
0%




HFC-143a
mass %
0%
0%
0%
0%
0%
0%
0%
0%




HFC-134a
mass %
0%
0%
0%
0%
0%
0%
0%
0%


















GWP

6
6
5
5
5
5
5
5



COP ratio (relative to that of
%
104.6
103.6
102.7
101.7
100.8
104.7
103.8
102.8



R404A)












Refrigerating capacity ratio
%
92.7
98.3
104.0
109.7
115.6
86.9
92.4
98.0



(relative to that of R404A)












Saturation pressure (40° C.)
MPa
1.694
1.795
1.895
1.994
2.093
1.613
1.715
1.816



Flame velocity
cm/s
1.6
1.6
1.6
1.6
1.6
1.5
1.5
1.5


























TABLE 214










Reference












Example 1
Example
Example
Example
Example
Example
Example
Example
















Item
Unit
(R404A)
16
17
18
19
20
21
22




















Composition
HFO-
mass %
  0%
25.0%
25.0%
25.0%
20.0%
20.0%
20.0%
20.0%


proportions
1132(E)












HFO-1123
mass %
  0%
20.0%
25.0%
30.0%
10.0%
15.0%
20.0%
25.0%



HFO-1234yf
mass %
  0%
55.0%
50.0%
45.0%
70.0%
65.0%
60.0%
55.0%



HFC-125
mass %
44.0%
  0%
  0%
  0%
  0%
  0%
  0%
  0%



HFC-143a
mass %
52.0%
  0%
  0%
  0%
  0%
  0%
  0%
  0%



HFC-134a
mass %
 4.0%
  0%
  0%
  0%
  0%
  0%
  0%
  0%
















GWP

3922
5
5
5
5
5
5
4


COP ratio
%
100.0
101.9
100.9
100.0
103.9
103.0
102.1
101.1


(relative to that of R404A)











Refrigerating capacity ratio
%
100.0
103.7
109.5
115.4
86.4
92.0
97.6
103.4


(relative to that of R404A)











Saturation pressure (40° C.)
MPa
1.822
1.917
2.017
2.117
1.632
1.734
1.835
1.936


Flame velocity
cm/s
NA (non-
1.5
1.5
1.5
1.5
1.5
1.5
1.5




flammability)






















Example
Example
Example
Example
Example
Example
Example















Item
Unit
23
24
25
26
27
28
29



















Composition
HFO-
mass %
20.0%
15.0%
15.0%
15.0%
15.0%
30.0%
20.0%


proportions
1132(E)











HFO-1123
mass %
30.0%
15.0%
20.0%
25.0%
30.0%
30.0%
40.0%



HFO-1234yf
mass %
50.0%
70.0%
65.0%
60.0%
55.0%
40.0%
40.0%



HFC-125
mass %
  0%
  0%
  0%
  0%
  0%
  0%
  0%



HFC-143a
mass %
  0%
  0%
  0%
  0%
  0%
  0%
  0%



HFC-134a
mass %
  0%
  0%
  0%
  0%
  0%
  0%
  0%















GWP

4
4
4
4
4
5
4


COP ratio
%
100.2
103.2
102.3
101.3
100.4
99.9
98.3


(relative to that of R404A)










Refrigerating capacity ratio
%
109.2
85.8
91.4
97.1
102.9
121.5
121.2


(relative to that of R404A)










Saturation pressure (40° C.)
MPa
2.037
1.648
1.750
1.851
1.953
2.192
2.237


Flame velocity
cm/s
1.5
1.5
1.5
1.5
1.5
1.6
1.5




























TABLE 215










Ref-
Com-
Com-
Com-
Com-
Com-
Com-
Com-
Com-
Com-





erence
parative
parative
parative
parative
parative
parative
parative
parative
parative





Ex-
Ex-
Ex-
Ex-
Ex-
Ex-
Ex-
Ex-
Ex-
Ex-





ample 1
ample
ample
ample
ample
ample
ample
ample
ample
ample


















Item
Unit
(R404A)
1
2
3
4
5
6
7
8
9






















Com-
HFO-
mass %
  0%
45%
15%
0%
30%
20%
10%
 0%
100%
 0%


position
1132(E)













pro-
HFO-
mass %
  0%
10%
10%
30%
40%
45%
50%
60%
 0%
 0%


portions
1123














HFO-
mass %
  0%
45%
75%
70%
30%
35%
40%
40%
 0%
100%



1234yf














HFC-125
mass %
44.0%
 0%
 0%
 0%
 0%
 0%
 0%
 0%
 0%
 0%



HFC-143a
mass %
52.0%
 0%
 0%
 0%
 0%
 0%
 0%
 0%
 0%
 0%



HFC-134a
mass %
 4.0%
 0%
 0%
 0%
 0%
 0%
 0%
 0%
 0%
 0%


















GWP

3922
7
6
6
8
8
8
7.6
10
4


COP ratio (relative
%
100.0
103.3
104.1
101.0
98.1
97.4
100.0
98.6
105.4
106.2


to that of R404A)













Refrigerating
%
100.0
115.3
80.4
83.2
133.6
127.4
100.0
98.8
155.3
52.9


capacity ratio













(relative to that













of R404A)













Saturation pressure
MPa
1.822
2.012
1.545
1.675
2.387
2.336
2.271
2.292
2.412
1.018


(40° C.)













Flame velocity
cm/s
NA
5.4
1.5
1.5
1.6
1.5
1.5
1.5
21
1.5




(non-













flam-













mability)























TABLE 216










Reference
Example
Example
Example
Example





Example 1
30
31
32
33













Item
Unit
(R404A)
A
B
C
D

















Composition
HFO-1132(E)
mass %
  0%
42.5%
27.1%
 1.0%
 1.0%


proportions
HFO-1123
mass %
  0%
 1.0%
 1.0%
30.4%
57.0%



HFO-1234yf
mass %
  0%
56.5%
71.9%
68.6%
42.0%



HFC-125
mass %
44.0%
  0%
  0%
  0%
  0%



HFC-143a
mass %
52.0%
  0%
  0%
  0%
  0%



HFC-134a
mass %
 4.0%
  0%
  0%
  0%
  0%













GWP

3922
7
6
6
7


COP ratio (relative
%
100.0
105.0
105.4
100.9
95.9


to that of R404A)








Refrigerating capacity ratio
%
100.0
102.3
85.0
85.0
116.6


(relative to that of R404A)








Saturation pressure (40° C.)
MPa
1.822
1,801
1,565
1.703
2.25


Flame velocity
cm/s
NA (non-
3.0
1.7
1.5
1.5




flammability)




















Example
Example
Example
Example
Example





34
35
36
37
38













Item
Unit
E
F
G
H
I

















Composition
HFO-1132(E)
mass %
42.5%
 1.0%
42.5%
 1.0%
27.4%


proportions
HFO-1123
mass %
24.1%
52.2%
18.9%
35.2%
29.8%



HFO-1234yf
mass %
33.4%
46.8%
38.6%
63.8%
42.8%



HFC-125
mass %
  0%
  0%
  0%
  0%
  0%



HFC-143a
mass %
  0%
  0%
  0%
  0%
  0%



HFC-134a
mass %
  0%
  0%
  0%
  0%
  0%













GWP

8
7
8
6
7


COP ratio (relative
%
100.8
96.8
101.7
100.0
100.0


to that of R404A)








Refrigerating capacity ratio
%
128.9
110.6
122.8
90.4
118.1


(relative to that of R404A)








Saturation pressure (40° C.)
MPa
2.25
2.15
2.15
1.802
2.15


Flame velocity
cm/s
3.0
1.5
3.0
1.5
1.7










(1-6-3) Refrigerant 2C


The refrigerant 2C includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 35.0 to 65.0 mass % and the content rate of HFO-1234yf is 65.0 to 35.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C1”.


(1-6-3-1) Refrigerant 2C1


The refrigerant 2C1, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP equivalent to or more than that of R404A, and (3) a refrigerating capacity equivalent to or more than that of R404A.


The content rate of HFO-1132(E) is 35.0 mass % or more based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1, thereby allowing the refrigerating capacity equivalent to or more than that of R404A to be obtained.


The content rate of HFO-1132(E) is 65.0 mass % or less based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1, thereby enabling the saturation pressure at a saturation temperature of 40° C., in the refrigeration cycle of the refrigerant 2C1, to be kept in a suitable range (in particular, 2.10 Mpa or less).


The refrigerating capacity relative to that of R404A, of the refrigerant 2C1, may be 95% or more, and is preferably 98% or more, more preferably 100% or more, further preferably 101% or more, particularly preferably 102% or more.


The refrigerant 2C1 has a GWP of 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The refrigerant 2C1 is preferably high in ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R404A, from the viewpoint of energy consumption efficiency, and specifically, the COP relative to that of R404A is preferably 98% or more, more preferably 100% or more, particularly preferably 102% or more.


Preferably, the content rate of HFO-1132(E) is 40.5 to 59.0 mass % and the content rate of HFO-1234yf is 59.5 to 41.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.75 MPa or more and 2.00 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


More preferably, the content rate of HFO-1132(E) is 41.3 to 59.0 mass % and the content rate of HFO-1234yf is 58.7 to 41.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99.5% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 2.00 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Further preferably, the content rate of HFO-1132(E) is 41.3 to 55.0 mass % and the content rate of HFO-1234yf is 58.7 to 45.0, mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99.5% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.95 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Particularly preferably, the content rate of HFO-1132(E) is 41.3 to 53.5 mass % and the content rate of HFO-1234yf is 583 to 46.5 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has various characteristics of a GWP of, 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.94 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Extremely preferably, the content rate of HFO-1132(E) is 41.3 to 51.0 mass % and the content rate of HFO-1234yf is 58.7 to 49.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.90 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Most preferably, the content rate of HFO-1132(E) is 41.3 to 49.2 mass % and the content rate of HFO-1234yf is 58.7 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity, relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The refrigerant 2C1 usually has a saturation pressure at a saturation temperature of 40° C., of 2.10 MPa or less, preferably 2.00 MPa or less, more preferably 1.95 MPa or less, further preferably 1.90 MPa or less, particularly preferably 1.88 MPa or less. The refrigerant 2C1, which has a saturation pressure at a saturation temperature of 40° C. within such a range, thus can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The refrigerant 2C1 usually has a saturation pressure at a saturation temperature of 40° C., of 1.70 MPa or more, preferably 1.73 MPa or more, more preferably 1.74 MPa or more, further preferably 1.75 MPa or more, particularly preferably 1.76 MPa or more. The refrigerant 2C1, which has a saturation pressure at a saturation temperature of 40° C. within such a range, thus can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 150° C. or less, more preferably 140° C. or less, further preferably 130° C. or less, particularly preferably 120° C. or less from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R404A is extended.


The refrigerant 2C1 is used for operating a refrigeration cycle at an evaporating temperature of −75 to −5° C., and thus, an advantage is that the refrigerating capacity equivalent to or more than that of R404A is obtained.


In a case where the evaporating temperature is more than −5° C. in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used, the compression ratio is less than 2.5 to cause the efficiency of the refrigeration cycle to be deteriorated. In a case where the evaporating temperature is less than −75° C. in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used, the evaporating pressure is less than 0.02 MPa to cause suction of the refrigerant into a compressor to be difficult. The compression ratio can be determined by the following expression.

Compression ratio Condensation pressure (Mpa)/Evaporating pressure (Mpa)


The evaporating temperature in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably −7.5° C. or less, more preferably −10° C. or less, further preferably −35° C. or less.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably −65° C. or more, more preferably −60° C. or more, further preferably −55° C. or more, particularly preferably −50° C. or more.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably −65° C. or more and −5° C. or less, more preferably −60° C. or more and −5° C. or less, further preferably −55° C. or more and −7.5° C. or less, particularly preferably −50° C. or more and −10° C. or less.


The evaporating pressure in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably 0.02 MPa or more, more preferably 0.03 MPa or more, further preferably 0.04 MPa or more, particularly preferably 0.05 MPa or more, from the viewpoint that suction of the refrigerant into a compressor is enhanced.


The compression ratio in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably 2.5 or more, more preferably 3.0 or more, further preferably 3.5 or more, particularly preferably 4.0 or more, from the viewpoint that the efficiency of the refrigeration cycle is enhanced. The compression ratio in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably 200 or less, more preferably 150 or less, further preferably 100 or less, particularly preferably 50 or less, from the viewpoint that the efficiency of the refrigeration cycle is enhanced.


The refrigerant 2C1 may usually include 99.5 mass % or more of HFO-1132(E) and HFO-1234yf in terms of the sum of the concentrations of these components. In the present disclosure, the total amount of HFO-1132(E) and HFO-1234yf in the entire refrigerant 2C1 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2C1 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C1 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C1.


The refrigerant 2C1 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C1 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C1.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 35.0 to 65.0 mass % and the content rate of HFO-1234yf is usually 65.0 to 35.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant 2C1, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP equivalent to or more than that of R404A, and (3) a refrigerating capacity equivalent to or more than that of R404A.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, preferably, the content rate of HFO-1132(E) is 40.5 to 59.0 mass % and the content rate of HFO-1234yf is 59.5 to 41.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.75 MPa or more and 2.00 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, more preferably, the content rate of HFO-1132(E) is 41.3 to 59.0 mass % and the content rate of HFO-1234yf is 58.7 to 41.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99.5% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 2.00 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 41.3 to 55.0 mass % and the content rate of HFO-1234yf is 58.7 to 45.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99.5% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.95 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, particularly preferably, the content rate of HFO 1132(E) is 41.3 to 53.5 mass % and the content rate of HFO-1234yf is 58.7 to 46.5 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.94 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, extremely preferably, the content rate of HFO-1132(E) is 41.3 to 51.0 mass % and the content rate of HFO-1234yf is 58.7 to 49.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.90 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, most preferably, the content rate of HFO-1132(E) is 41.3 to 49.2 mass % and the content rate of HFO-1234yf is 58.7 to 50.8 mass % based on the total mass off-TO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


(1-6-3-2) Refrigerant 2C2


Refrigerant 2C2 The refrigerant included in the composition of the present disclosure includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 40.5 to 492 mass % and the content rate of HFO-1234yf is 59.5 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C2”.


The refrigerant 2C2, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP equivalent to or more than that of R404A, (3) a refrigerating capacity equivalent to or more than that of R404A, and (4) lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.75 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The content rate of HFO-1132(E) is 40.5 mass % or more based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2, thereby allowing the refrigerating capacity equivalent to or more than that of R404A to be obtained.


The content rate of HFO-1132(E) is 49.2 mass % or less based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2, thereby enabling the saturation pressure at a saturation temperature of 40° C., in the refrigeration cycle of the refrigerant 2C2, to be kept in a suitable range (in particular, 2.10 Mpa or less).


The refrigerating capacity relative to that of R404A, of the refrigerant 2C2, may be 99% or more, and is preferably 100% or more, more preferably 101% or more, further preferably 102% or more, particularly preferably 103% or more.


The refrigerant 2C2 has a GWP of 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The refrigerant 2C2 is preferably high in ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R404A, from the viewpoint of energy consumption efficiency, and specifically, the COP relative to that of R404A is preferably 98% or more, more preferably 100% or more, further preferably 101% or more, particularly preferably 102% or more.


Preferably, the content rate of HFO-1132(E) is 41.3 to 49.2 mass % and the content rate of HFO-1234yf is 58.7 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


More preferably, the content rate of HFO-1132(E) is 43.0 to 49.2 mass % and the content rate of HFO-1234yf is 57.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 101% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.78 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Further preferably, the content rate of HFO-1132(E) is 44.0 to 49.2 mass % and the content rate of HFO-1234yf is 56.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 101% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.80 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Particularly preferably, the content rate of HFO-1132(E) is 45.0 to 49.2 mass % and the content rate of HFO-1234yf is 55.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 102% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Extremely preferably, the content rate of HFO-1132(E) is 45.0 to 48.0 mass % and the content rate of HFO-1234yf is 55.0 to 52.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102.5% or more, a refrigerating capacity relative to that of R404A of 102.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.87 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Most preferably, the content rate of HFO-1132(E) is 45.0 to 47.0 mass % and the content rate of HFO-1234yf is 55.0 to 53.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102.5% or more, a refrigerating capacity relative to that of R404A of 102.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.85 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The refrigerant 2C2 usually has a saturation pressure at a saturation temperature of 40° C., of 2.10 MPa or less, preferably 2.00 MPa or less, more preferably 1.95 MPa or less, further preferably 1.90 MPa or less, particularly preferably 1.88 MPa or less. The refrigerant 2C2, which has a saturation pressure at a saturation temperature of 40° C. within such a range, thus can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The refrigerant 2C2 usually has a saturation pressure at a saturation temperature of 40° C., of 1.70 MPa or more, preferably 1.73 MPa or more, more preferably 1.74 MPa or more, further preferably 1.75 MPa or more, particularly preferably 1.76 MPa or more. The refrigerant 2C2, which has a saturation pressure at a saturation temperature of 40° C. within such a range, thus can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 150° C. or less, more preferably 140° C. or less, further preferably 130° C. or less, particularly preferably 120° C. or less from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R404A is extended.


The refrigerant 2C2 is preferably used for operating a refrigeration cycle at an evaporating temperature of −75 to 15° C. in the present disclosure, from the viewpoint that the refrigerating capacity equivalent to or more than that of R404A is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably 15° C. or less, more preferably 5° C. or less, further preferably 0° C. or less, particularly preferably −5° C. or less.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably −65° C. or more, more preferably −60° C. or more, further preferably −55° C. or more, particularly preferably −50° C. or more.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably −65° C. or more and 15° C. or less, more preferably −60° C. or more and 5° C. or less, further preferably −55° C. or more and 0° C. or less, particularly preferably −50° C. or more and −5° C. or less.


The evaporating pressure in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably 0.02 MPa or more, more preferably 0.03 MPa or more, further preferably 0.04 MPa or more, particularly preferably 0.05 MPa or more, from the viewpoint that suction of the refrigerant into a compressor is enhanced.


The compression ratio in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably 2.5 or more, more preferably 3.0 or more, further preferably 3.5 or more, particularly preferably 4.0 or more, from the viewpoint that the efficiency of the refrigeration cycle is enhanced.


The refrigerant 2C2 may usually include 99.5 mass % or more of HFO-1132(E) and HFO-1234yf in terms of the sum of the concentrations of these components. In the present disclosure, the total amount of HFO-1132(E) and HFO-1234yf in the entire refrigerant 2C2 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2C2 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C2 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C2.


The refrigerant 2C2 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C2 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C2.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 40.5 to 49.2 mass % and the content rate of HFO-1234yf is usually 59.5 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant 2C2, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP equivalent to or more than that of R404A, (3) a refrigerating capacity equivalent to or more than that of R404A, and (4) lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.75 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, preferably, the content rate of HFO-1132(E) is 41.3 to 49.2 mass % and the content rate of HFO-1234yf is 58.7 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard.


Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, more preferably, the content rate of HFO-1132(E) is 43.0 to 492 mass % and the content rate of HFO-1234yf is 57.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant, 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 101% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.78 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 44.0 to 49.2 mass % and the content rate of HFO-1234yf is 56.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 101% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.80 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, particularly preferably, the content rate of HFO-1132(E) is 45.0 to 49.2 mass % and the content rate of HFO-1234yf is 55.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 102% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, extremely preferably, the content rate of HFO-1132(E) is 45.0 to 48.0 mass % and the content rate of HFO-1234yf is 55.0 to 52.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102.5% or more, a refrigerating capacity relative to that of R404A of 102.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.87 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


(1-6-3-3) Refrigerant 2C3


The refrigerant included in the composition of the present disclosure includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 31.1 to 39.8 mass % and the content rate of HFO-1234yf is 68.9 to 60.2 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C3”.


The refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R134a, (3) a refrigerating capacity relative to that of R134a of 150% or more, and (4) a discharge temperature of 90° C. or less.


The content rate of HFO-1132(E) is 31.1 mass % or more based on the total amount of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3, thereby allowing a refrigerating capacity relative to that of R134a of 150% or more to be obtained.


The content rate of HFO-1132(E) is 39.8 mass % or less based on the total amount of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3, thereby enabling the discharge temperature in the refrigeration cycle of the refrigerant 2C3 to be kept at 90° C. or less, and enabling the life of any member of a refrigerating apparatus for R134a to be kept long.


The refrigerating capacity relative to that of R134a, of the refrigerant 2C3, may be 150% or more, and is preferably 151% or more, more preferably 152% or more, further preferably 153% or more, particularly preferably 154% or more.


The refrigerant 2C3 preferably has a discharge temperature in the refrigeration cycle of 90.0° C. or less, more preferably 89.7° C. or less, further preferably 89.4° C. or less, particularly preferably 89.0° C. or less.


The refrigerant 2C3 has a GWP of 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The refrigerant 2C3 is preferably high in ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R134a, from the viewpoint of energy consumption efficiency, and specifically, the COP relative to that of R134a is preferably 90% or more, more preferably 91% or more, further preferably 91.5% or more, particularly preferably 92% or more.


The content rate of HFO-1132(E) is usually 31.1 to 39.8 mass % and the content rate of HFO-1234yf is usually 68.9 to 60.2 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3.


The refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R134a, (3) a refrigerating capacity relative to that of R134a of 150% or more, and (4) a discharge temperature of 90.0° C. or less.


Preferably, the content rate of HFO-1132(E) is 31.1 to 37.9 mass % and the content rate of HFO-1234yf is 68.9 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 150% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


More preferably, the content rate of HFO-1132(E) is 32.0 to 37.9 mass % and the content rate of HFO-1234yf is 68.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 151% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


Still more preferably, the content rate of HFO-1132(E) is 33.0 to 37.9 mass % and the content rate of HFO-1234yf is 67.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 152% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


Further preferably, the content rate of HFO-1132(E) is 34.0 to 37.9 mass % and the content rate of HFO-1234yf is 66.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 153% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


Particularly preferably, the content rate of HFO-1132(E) is 35.0 to 37.9 mass % and the content rate of HFO-1234yf is 65.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP, relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 155% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 90.0° C. or less, more preferably 89.7° C. or less, further preferably 89.4° C. or less, particularly preferably 89.0° C. or less, from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R134a is extended.


In a case where the refrigerant 2C3 is used for operating the refrigeration cycle, in the present disclosure, a process of liquefaction (condensation) of the refrigerant is required in the refrigeration cycle, and thus the critical temperature is required to be remarkably higher than the temperature of cooling water or cooling air for liquefying the refrigerant. The critical temperature in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably 80° C. or more, more preferably 81° C. or more, further preferably 81.5° C. or more, in particular, 82° C. or more, from such a viewpoint.


The refrigerant 2C3 is usually used for operating a refrigeration cycle at an evaporating temperature of −75 to 15° C. in the present disclosure, from the viewpoint that a refrigerating capacity relative to that of R134a of 150% or more is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably 15° C. or less, more preferably 5° C. or less, further preferably 0° C. or less, particularly preferably −5° C. or less.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably −65° C. or more, more preferably −60° C. or more, further preferably −55° C. or more, particularly preferably −50° C. or more.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably −65° C. or more and 15° C. or less, more preferably −60° C. or more and 5° C. or less, further preferably −55° C. or more and 0° C. or less, particularly preferably −50° C. or more and −5° C. or less.


The critical temperature of the refrigerant in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably 80° C. or more, more preferably 81° C. or more, further preferably 81.5° C. or more, particularly preferably 82° C. or more, from the viewpoint of an enhancement in performance.


The refrigerant 2C3 may usually include 99.5 mass % or more of HFO-1132(E) and HFO-1234yf in terms of the sum of the concentrations of these components. In the present disclosure, the total amount of HFO-1132(E) and HFO-1234yf in the entire refrigerant 2C3 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2C3 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C3 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C3.


The refrigerant 2C3 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C3 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C3.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 31.1 to 39.8 mass % and the content rate of HFO-1234yf is usually 68.9 to 60.2 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R134a, (3) a refrigerating capacity relative to that of R134a of 150% or more, and (4) a discharge temperature of 90° C. or less.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, preferably, the content rate of HFO-1132(E) is 31.1 to 37.9 mass % and the content rate of HFO-1234yf is 68.9 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 150% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, more preferably, the content rate of HFO-1132(E) is 32.0 to 37.9 mass % and the content rate of HFO-1234yf is 68.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 151% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 33.0 to 37.9 mass % and the content rate of HFO-1234yf is 67.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 152% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 34.0 to 37.9 mass % and the content rate of HFO-1234yf is 66.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 153% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 35.0 to 37.9 mass % and the content rate of HFO-1234yf is 65.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 155% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


(1-6-3-4) Refrigerant 2C4


The refrigerant included in the composition of the present disclosure includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 21.0 to 28.4 mass % and the content rate of HFO-1234yf is 79.0 to 71.6 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C4”.


The refrigerant 2C4, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R1234yf, and (3) a refrigerating capacity relative to that of R1234yf of 140% or more, and (4) lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.380 MPa or more and 0.420 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is 21.0 mass % or more based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4, thereby allowing a refrigerating capacity relative to that of R1234yf of 140% or more to be obtained. The content rate of HFO-1132(E) is 28.4 mass % or less based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4, thereby allowing a critical temperature of 83.5° C. or more to be easily ensured.


The refrigerating capacity relative to that of R1234yf in the refrigerant 2C4 may be 140% or more, and is preferably 142% or more, more preferably 143% or more, further preferably 145% or more, particularly preferably 146% or more.


The refrigerant 2C4 has a GWP of 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The refrigerant 2C4 is preferably high in ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R1234yf, from the viewpoint of energy consumption efficiency, and specifically, the COP relative to that of R1234yf is preferably 95% or more, more preferably 96% or more, further preferably 97% or more, particularly preferably 98% or more.


The content rate of HFO-1132(E) is preferably 21.5 to 28.0 mass % and the content rate of HFO-1234yf is preferably 78.5 to 72.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 65.0° C. or less, and a critical temperature of 83.5° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.383 MPa or more and 0.418 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is more preferably 22.0 to 27.7 mass % and the content rate of HFO-1234yf is more preferably 78.0 to 72.3 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 65.0° C. or less, and a critical temperature of 83.5° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.385 MPa or more and 0.417 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is further preferably 22.5 to 27.5 mass % and the content rate of HFO-1234yf is further preferably 77.5 to 72.5 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.388 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is particularly preferably 23.0 to 27.2 mass % and the content rate of HFO-1234yf is particularly preferably 77.0 to 72.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 141% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.390 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is extremely preferably 23.5 to 27.0 mass % and the content rate of HFO-1234yf is extremely preferably 76.5 to 73.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 142% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0390 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is most preferably 24.0 to 26.7 mass % and the content rate of HFO-1234yf is most preferably 76.0 to 73.3 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 144% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.6° C. or less, and a critical temperature of 84.0° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.396 MPa or more and 0.411 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The refrigerant 2C4 usually has a saturation pressure at a saturation temperature of −10° C., of 0.420 MPa or less, preferably 0.418 MPa or less, more preferably 0.417 MPa or less, further preferably 0.415 MPa or less, particularly preferably 0.413 MPa or less. Such a range enables the refrigerant 2C4 to be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The refrigerant 2C4 usually has a saturation pressure at a saturation temperature of −10° C., of 0.380 MPa or more, preferably 0.385 MPa or more, more preferably 0.390 MPa or more, further preferably 0.400 MPa or more, particularly preferably 0.410 MPa or more. In such a case, the refrigerant 2C4 can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 65° C. or less, more preferably 64.8° C. or less, further preferably 64.7° C. or less, particularly preferably 64.5° C. or less from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R1234yf is extended.


The refrigerant 2C4 is preferably used for operating a refrigeration cycle at an evaporating temperature of −75 to 5° C. in the present disclosure, from the viewpoint that a refrigerating capacity relative to that of R1234yf of 140% or more is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably 5° C. or less, more preferably 0° C. or less, further preferably −5° C. or less, particularly preferably −10° C. or less, from the viewpoint that a refrigerating capacity relative to that of R1234yf of 140% or more is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably −75° C. or more, more preferably −60° C. or more, further preferably −55° C. or more, particularly preferably −50° C. or more, from the viewpoint that a refrigerating capacity relative to that of R1234yf of 140% or more is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably −65° C. or more and 0° C. or less, more preferably −60° C. or more and −5° C. or less, further preferably −55° C. or more and −7.5° C.; or less, particularly preferably −50° C. or more and −10° C. or less, from the viewpoint that a refrigerating capacity relative to that of R1234yf of 140% or more is obtained.


The discharge temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably 65.0° C. or less, more preferably 64.9° C. or less, further preferably 64.8° C. or less, particularly preferably 64.7° C. or less, from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R1234yf is extended.


In a case where the refrigerant 2C4 is used for operating the refrigeration cycle, in the present disclosure, a process of liquefaction (condensation) of the refrigerant is required in the refrigeration cycle, and thus the critical temperature is required to be remarkably higher than the temperature of cooling water or cooling air for liquefying the refrigerant. The critical temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably 83.5° C. or more, more preferably 83.8° C. or more, further preferably 84.0° C. or more, particularly preferably 84.5° C. or more, from such a viewpoint.


The refrigerant 2C4 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C4 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1; mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C4.


The refrigerant 2C4 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C4 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C4.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 21.0 to 28.4 mass % and the content rate of HFO-1234yf is usually 79.0 to 71.6 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant 2C4, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R1234yf and (3) a refrigerating capacity relative to that of R1234yf of 140% or more, and (4) lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.380 MPa or more and 0.420 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is preferably 21.5 to 28.0 mass % and the content rate of HFO-1234yf is preferably 78.5 to 72.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 65.0° C. or less, and a critical temperature of 83.5° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.383 MPa, or more and 0.418 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is more preferably 22.0 to 27.7 mass % and the content rate of HFO-1234yf is more preferably 78.0 to 72.3 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 65.0° C. or less, and a critical temperature of 83.5° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.385 MPa or more and 0.417 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is further preferably 22.5 to 27.5 mass % and the content rate of HFO-1234yf is further preferably 77.5 to 72.5 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.388 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is particularly preferably 23.0 to 27.2 mass % and the content rate of HFO-1234yf is particularly preferably 77.0 to 72.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 141% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.390 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is extremely preferably 23.5 to 27.0 mass % and the content rate of HFO-1234yf is extremely preferably 76.5 to 73.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 142% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at saturation temperature of −10° C., of 0.390 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is most preferably 24.0 to 26.7 mass % and the content rate of HFO-1234yf is most preferably 76.0 to 73.3 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 144% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.6° C. or less, and a critical temperature of 84.0° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.396 MPa or more and 0.411 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


(1-6-3-5) Refrigerant 2C5


The refrigerant included in the composition of the present disclosure includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 12.1 to 72.0 mass % and the content rate of HFO-1234yf is 87.9 to 28.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C5”.


In the present disclosure, the refrigerant 2C5 is used for in-car air conditioning equipment.


The refrigerant 2C5, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R1234yf, (3) a refrigerating capacity relative to that of R1234yf of 128% or more, and (4) a flame velocity of less than 10.0 cm/s.


The content rate of HFO-1132(E) is 12.1 mass % or more based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5, and thus a boiling point of −40° C. or less can be ensured which is favorable in a case where heating is made by using a heat pump in an electric car. Herein, a boiling point of −40° C. or less means that the saturation pressure at is equal to or more than atmospheric pressure, and such a lower boiling point of −40° C. or less is preferable in the above applications. The content rate of HFO1132(E) is 72.0 mass % or less based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5, and thus a flame velocity of less than 10.0 cm/s can be ensured which contributes to safety in the case of use in in-car air conditioning equipment.


The refrigerating capacity relative to that of R1234yf in the refrigerant 2C5 may be 128% or more, and is preferably 130% or more, more preferably 140% or more, further preferably 150% or more, particularly preferably 160% or more.


The refrigerant 2C5 has a GWP of 5 or more and 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R1234yf, in the refrigerant 2C5 may be 100% or more from the viewpoint of energy consumption efficiency.


The refrigerant 2C5 is used in in-car air conditioning equipment, and thus an advantage is that heating can be made by a heat pump lower in consumption power as compared with an electric heater.


The air conditioning equipment with the refrigerant 2C5 is preferably for a gasoline-fueled car, a hybrid car, an electric car or a hydrogen-fueled car. In particular, the air conditioning equipment with the refrigerant 2C5 is particularly preferably for an electric car, from the viewpoint that not only heating in a vehicle interior is made by a heat pump, but also the travel distance of such a car is enhanced. That is, the refrigerant 2C5 is particularly preferably used in an electric car, in the present disclosure.


The refrigerant 2C5 is used in in-car air conditioning equipment, in the present disclosure. The refrigerant 2C5 is preferably used in air conditioning equipment of a gasoline-fueled car, air conditioning equipment of a hybrid car, air conditioning equipment of an electric car or air conditioning equipment of a hydrogen-fueled car, in the present disclosure. The refrigerant 2C5 is particularly preferably used in air conditioning equipment of an electric car, in the present disclosure.


Since a pressure equal to or more than atmospheric pressure at −40° C. is required in heating of a vehicle interior by a heat pump, the refrigerant 2C5 preferably has a boiling point of −51.2 to −40.0° C., more preferably-50.0 to −42.0° C., further preferably −48.0 to −44.0° C., in the present disclosure.


The content rate of HFO-1132(E) is preferably 15.0 to 65.0 mass % and the content rate of HFO-1234yf is preferably 85.0 to 35.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The content rate of HFO-1132(E) is more preferably 20.0 to 55.0 mass % and the content rate of HFO-1234yf is more preferably 80.0 to 45.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The content rate of HFO-1132(E) is further preferably 25.0 to 50.0 mass % and the content rate of HFO-1234yf is further preferably 75.0 to 50.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The content rate of HFO-1132(E) is particularly preferably 30.0 to 45.0 mass % and the content rate of HFO-1234yf is particularly preferably 70.0 to 55.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The content rate of HFO-1132(E) is most preferably 35.0 to 40.0 mass % and the content rate of HFO-1234yf is most preferably 65.0 to 60.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The refrigerant 2C5 preferably has a flame velocity of less than 10.0 cm/s, more preferably less than 5.0 cm/s, further preferably less than 3.0 cm/s, particularly preferably 2.0 cm/s, in the present disclosure.


The refrigerant 2C5 is preferably used for operating a refrigeration cycle at an evaporating temperature of −40 to 10° C. in the present disclosure, from the viewpoint that a refrigerating capacity equivalent to or more than that of R1234yf is obtained.


In a case where the refrigerant 2C5 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 79° C. or less, more preferably 75° C. or less, further preferably 70° C. or less, particularly preferably 67° C. or less.


The refrigerant 2C5 may usually include 99.5 mass % or more of HFO-1132(E) and HFO-1234yf in terms of the sum of the concentrations of these components. In the present disclosure, the total amount of HFO-1132(E) and HFO-1234yf in the entire refrigerant 2C5 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2C5 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C5 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the ark Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C5.


The refrigerant 2C5 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C5 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C5.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 12.1 to 72.0 mass % and the content rate of HFO-1234yf is usually 87.9 to 28.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is preferably 15.0 to 65.0 mass % and the content rate of HFO-1234yf is preferably 85.0 to 35.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is more preferably 20.0 to 55.0 mass % and the content rate of HFO-1234yf is more preferably 80.0 to 45.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is further preferably 25.0 to 50.0 mass % and the content rate of HFO-1234yf is further preferably 75.0 to 50.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is particularly preferably 30.0 to 45.0 mass % and the content rate of HFO-1234yf is particularly preferably 70.0 to 55.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is most preferably 35.0 to 40.0 mass % and the content rate of HFO-1234yf is most preferably 65.0 to 60.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


Examples of Refrigerant C

Hereinafter, the refrigerant C will be described with reference to Examples in more detail. It is noted that the present disclosure is not limited to such Examples.


Test Example 1-1

The GWP of each mixed refrigerant represented in Examples 1-1 to 1-13, Comparative Examples 1-1 to 1-2 and Reference Example 1-1 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NISI) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature −50° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


An “evaporating temperature of −50° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is −50° C. A “condensation temperature of 40° C.” means that the condensation temperature of such each mixed refrigerant in a condenser included in a refrigerating apparatus is 40° C.


The results in Test Example 1-1 are shown in Table 217. Table 217 shows Examples and Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 217, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R404A.


In Table 217, the “Saturation pressure (40° C.)” represents the saturation pressure at a saturation temperature of 40° C. In Table 217, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant.


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption


The compression ratio was determined by the following expression.

Compression ratio=Condensation pressure (Mpa)/Evaporating pressure (Mpa)


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. One having a flame velocity of 0 cm/s to 10 cm/s was rated as “Class 2L (lower flammability)”, one having a flame velocity of more than 10 cm/s was rated as “Class 2 (low flammability)”, and one causing no flame propagation was rated as “Class 1 (non-flammability)”. In Table 217, the “ASHRAE flammability classification” shows each result based on the criteria for determination.


The flame velocity test was performed as follows. First, the mixed refrigerant used had a purity of 99.5% or more, and degassing was made by repeating a cycle of freezing, pumping and thawing until no trace of air was observed on a vacuum gauge. The flame velocity was measured by a closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between electrodes at the center of a sample cell. The duration of discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of any flame was visualized using a schlieren photograph. A cylindrical container (inner diameter 155 mm, length: 198 mm) equipped with two light-transmitting acrylic windows was used as the sample cell, and a xenon lamp was used as a light source. A schlieren image of any, flame was recorded by a high-speed digital camera at a frame rate of 600 fps, and stored in a PC.


The flammable range of the mixed refrigerant was measured by using an apparatus (see FIG. 1T) based on ASTM E681-09.


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>


Test container: spherical container of 280 mm in diameter (internal volume: 12 L)


Test temperature: 60° C.±3° C.


Pressure: 101.3 kPa±0.7 kPa


Water content: 0.0088 g±0.0005 g per gram of dry air (water content at a humidity of 50% at 23° C.)


Mixing ratio of refrigerant composition/air: ±02 vol. % by 1 vol. %


Mixing of refrigerant composition: ±0.1 mass %


Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer


Electrode interval: 6.4 mm (¼ inches)


Spark: 0.4 seconds±0.05 seconds


Criteria for determination:






    • A case where any flame was spread at more than 90 degrees around the ignition point: flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)





















TABLE 217









Reference











Example
Comparative










1-1
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
1-1
1-1
1-2
1-3
1-4
1-5
1-6




















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge
° C.
100.6
108.6
114.7
115.0
115.5
116.5
117.6
118.8


temperature











Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.082
0.063
0.072
0.073
0.074
0.075
0.077
0.079


Compression ratio

22.2
25.3
24.1
24.0
23.9
23.8
23.6
23.4


COP ratio
%
100
106.2
106.2
106.2
106.2
106.2
106.2
106.2


(relative to that of R404A)











Refrigerating
%
100
86.2
98.5
99.1
100
102.1
104.5
106.9


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability











classification














Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
1-7
1-8
1-9
1-10
1-11
1-12
1-13
1-2




















Composition
HFO-1132(E)
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



HFC-134a
mass %
0
0
0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge
° C.
120.0
121.0
122.4
123.3
124.4
125.5
126.0
131.7


temperature











Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.081
0.083
0.085
0.086
0.088
0.090
0.091
0.099


Compression ratio

23.1
23.0
22.8
22.6
22.5
22.3
22.2
21.6


COP ratio
%
106.2
106.3
106.3
106.3
106.3
106.4
106.4
106.7


(relative to that of R404A)











Refrigerating
%
109.5
111.7
114.6
116.4
118.7
121
122.2
133.3


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


flammability











classification









Test Example 1-2

The GWP of each mixed refrigerant represented in Examples 1-14 to 1-26, Comparative Examples 1-3 to 1-4 and Reference Example 1-2 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.


Evaporating temperature −35° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meaning of each of the above terms is the same as in Test Example 1-1.


The results in Test Example 1-2 are shown in Table 218. Table 218 shows Examples and Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 218, the meaning of each of the terms is the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 1-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 1-1. The flame velocity test was performed in the same manner as in Test Example 1-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 1-1.


















TABLE 218









Reference











Example
Comparative










1-2
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
1-3
1-14
1-15
1-16
1-17
1-18
1-19




















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0)
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge
° C.
89.1
95.8
100.6
100.8
101.2
102.0
102.9
103.8


temperature











Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.165
0.131
0.148
0.149
0.151
0.154
0.157
0.160


Compression ratio

11.0
12.2
11.8
11.7
11.7
11.6
11.6
11.5


COP ratio
%
100
105.1
104.8
104.7
104.7
104.7
104.6
104.5


(relative to that of R404A)











Refrigerating
%
100
87.7
98.5
99.0
99.8
101.6
103.7
105.7


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability











classification














Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
1-20
1-21
1-22
1-23
1-24
1-25
1-26
1-4




















Composition
HFO-1132(E)
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



HFC-134a
mass %
0
0
0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge
° C.
104.7
105.5
106.6
107.3
108.1
109.0
109.5
113.9


temperature











Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.164
0.167
0.171
0.174
0.177
0.180
0.181
0.196


Compression ratio

11.4
11.4
11.3
11.2
11.2
11.1
11.1
10.8


COP ratio
%
104,5
104.4
104.4
104.4
104.3
104.3
104.3
104.3


(relative to that of R404A)











Refrigerating
%
108.0
109.8
112.3
113.8
115.7
117.7
118.6
128.0


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


flammability











classification









Test Example 1-3

The GWP of each mixed refrigerant represented in Examples 1-27 to 1-39, Comparative Examples 1-5 to 1-6 and Reference Example 1-3 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.


Evaporating temperature −10° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meaning of each of the above terms is the same as in Test Example 1-1.


The results in Test Example 1-3 are shown in Table 219. Table 219 shows Examples and Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 219, the meaning of each of the terms is the same as in Test. Example 1-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 1-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 1-1. The flame velocity test was performed in the same manner as in Test Example 1-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 1-1.


















TABLE 219









Reference











Example
Comparative










1-3
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
1-5
1-27
1-28
1-29
1-30
1-31
1-32




















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0
0
0
0)



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge
° C.
75.8
80.8
83.7
83.9
84.1
84.5
85.1
85.6


temperature











Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.434
0.357
0.399
0.401
0.404
0.411
0.419
0.427


Compression ratio

4.2
4.5
4.4
4.4
4.4
4.3
4.3
4.3


COP ratio
%
100
103.8
102.9
102.9
102.8
102.7
102.5
102.4


(relative to that of R404A)











Refrigerating
%
100
89.8
98.7
99.1
99.8
101.2
102.8
104.5


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability











classification














Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
1-33
1-34
1-35
1-36
1-37
1-38
1-39
1-6




















Composition
HFO-1132(E)
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



HFC-134a
mass %
0
0
0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge
° C.
86.2
86.6
87.3
87.7
88.2
88.7
88.9
91.5


temperature











Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.436
0.443
0.452
0.457
0.465
0.472
0.475
0.509


Compression ratio

4.3
4.3
4.3
4.3
4.3
4.2
4.2
4.2


COP ratio
%
102.2
102.1
102.0
101.9
101.8
101.7
101.6
101.3


(relative to that of R404A)











Refrigerating
%
106.2
107.7
109.6
110.8
112.3
113.8
114.5
121.7


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


flammability











classification









Test Example 1-4

The GWP of each mixed refrigerant represented in Comparative Examples 1-7 to 1-21 and Reference Example 1-4 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.


Evaporating temperature −80° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meaning of each of the above terms is the same as in Test Example 1-1.


The results in Test Example 1-4 are shown in Table 220. Table 220 shows Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 220, the meaning of each of the terms is the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 1-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 1-1. The flame velocity test was performed in the same manner as in Test Example 1-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 1-1.


















TABLE 220









Reference
Com-
Com-
Com-
Com-
Com-
Com-
Com-




Example
parative
parative
parative
parative
parative
parative
parative




1-4
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
1-7
1-8
1-9
1-10
1-11
1-12
1-13




















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge
° C.
136.7
146.0
157.7
158.1
158.8
160.4
162.1
163.9


temperature











Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1,844


(40° C.)











Evaporating pressure
MPa
0.014
0.011
0.012
0.012
0.012
0.012
0.013
0.013


Compression ratio

134.6
149.1
150.8
150.2
149.3
147.2
145.0
142.8


COP ratio
%
100
112.6
110.3
110.3
110.4
110.6
110.8
111.0


(relative to that of R404A)











Refrigerating
%
100
91.7
99.3
100.2
101.5
104.4
107.8
111.3


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability











classification







Com-
Com-
Com-
Com-
Com-
Com-
Com-
Com-




parative
parative
parative
parative
parative
parative
parative
parative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
1-14
1-15
1-16
1-17
1-18
1-19
1-20
1-21




















Composition
HFO-1132(E)
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



HFC-134a
mass %
0
0
0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge
° C.
165.8
167.4
169.6
170.9
172.6
174.3
175.2
184.0


temperature











Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.013
0.014
0.014
0.014
0.015
0.015
0.015
0.017


Compression ratio

140.5
138.7
136.3
134.9
133.2
131.5
130.7
123.8


COP ratio
%
111.3
111.4
111.7
111.9
112.1
112.3
112.4
113.5


(relative to that of R404A)











Refrigerating
%
115.1
118.2
122.5
125.2
128.6
132.1
133.8
151.0


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


flammability











classification









Test Example 1-5

The GWP of each mixed refrigerant represented in Comparative Examples 1.22 to 1-36 and Reference Example 1-5 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.


Evaporating temperature 10° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meaning of each of the above terms is the same as in Test Example 1-1.


The results in Test Example 1-5 are shown in Table 221. Table 221 shows Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 221, the meaning of each of the terms is the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 1-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 1-1. The flame velocity test was performed in the same manner as in Test Example 1-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 1-1.


















TABLE 221









Reference
Com-
Com-
Com-
Com-
Com-
Com-
Com-




Example
parative
parative
parative
parative
parative
parative
parative




1-5
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
1-22
1-23
1-24
1-25
1-26
1-27
1-28




















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge
° C.
68.5
72.4
74.0
74.1
74.2
74.4
74.7
74.9


temperature











Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.820
0.694
0.768
0.772
0.777
0.789
0.803
0.817


Compression ratio

2.2
2.3
2.3
2.3
2.3
2.3
2.3
2.3


COP ratio
%
100.0
103.1
101.9
101.8
101.7
101.5
101.3
101.1


(relative to that of R404A)











Refrigerating
%
100.0
91.2
98.9
99.3
99.8
101.0
102.5
103.8


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability











classification







Com-
Com-
Com-
Com-
Com-
Com-
Com-
Com-




parative
parative
parative
parative
parative
parative
parative
parative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
1-29
1-30
1-31
1-32
1-33
1-34
1-35
1-36




















Composition
HFO-1132(E)
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



HFC-134a
mass %
0
0
0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge
° C.
75.2
75.5
75.8
76.0
76.2
76.5
76,6
77.9


temperature











Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.832
0.844
0.860
0.870
0.882
0.895
0.901
0.959


Compression ratio

2.3
2.2
2.2
2.2
2.2
2.2
2.2
2.2


COP ratio
%
100.9
100.8
100.6
100.4
100.3
100.1
100.1
99.5


(relative to that of R404A)











Refrigerating
%
105.3
106.5
108.2
109.1
110.4
111.6
112.3
118.2


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


flammability











classification









Test Example 2-1

The GWP of each mixed refrigerant represented in Examples 2-1 to 2-6, Comparative Examples 2-1 to 2-9 and Reference Example 2-1 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature −50° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


An “evaporating temperature of −50° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is −50° C. A “condensation temperature of 40° C.” means that the condensation temperature of such each mixed refrigerant in a condenser included in a refrigerating apparatus is 40° C.


The results in Test Example 2-1 are shown in Table 222. Table 222 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 222, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R404A.


In Table 222, the “Saturation pressure (40° C.)” represents the saturation pressure at a saturation temperature of 40° C. In Table 222, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant.


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption


The compression ratio was determined by the following expression.

Compression ratio/Condensation pressure (Mpa)/Evaporating pressure (Mpa)


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. One having a flame velocity of 0 cm/s to 10 cm/s was rated as “Class 2L (lower flammability)”, one having a flame velocity of more than 10 cm/s was rated as “Class 2 (low flammability)”, and one causing no flame propagation was rated as “Class 1 (non-flammability)”. In Table 222, the “ASHRAE flammability classification” shows each result based on the criteria for determination.


The flame velocity test was performed as follows. First, the mixed refrigerant used had a purity of 99.5% or more, and degassing was made by repeating a cycle of freezing, pumping and thawing until no trace of air was observed on a vacuum gauge. The flame velocity was measured by a closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between electrodes at the center of a sample cell. The duration of discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of any flame was visualized using a schlieren photograph. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light-transmitting acrylic windows was used as the sample cell, and a xenon lamp was used as a light source. A schlieren image of any flame was recorded by a high-speed digital video camera at a frame rate of 600 fps, and stored in a PC.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09.


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>


Test container: spherical container of 280 mm in diameter (internal volume: 12 L)


Test temperature: 60° C.±3° C.


Pressure: 101.3 kPa±0.7 kPa


Water content: 0.0088 g±0.0005 g per gram of dry air (water content at a relative humidity of 50% at 23° C.)


Mixing ratio of refrigerant composition/air: ±0.2 vol. % by 1 vol. %


Mixing of refrigerant composition: ±0.1 mass %


Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer


Electrode interval: 6.4 mm (¼ inches)


Spark: 0.4 seconds±0.05 seconds


Criteria for determination:






    • A case where any flame was spread at more than 90 degrees around the ignition point flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)





















TABLE 222









Reference
Com-
Com-









Example
parative
parative









2-1
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
2-1
2-2
2-1
2-2
2-3
2-4
2-5




















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge
° C.
100.6
108.6
114.7
115.0
115.5
116.5
117.6
118.8


temperature











Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.082
0.063
0.072
0.073
0.074
0.075
0.077
0.079


Compression ratio

22.2
25.3
24.1
24.0
23.9
23.8
23.6
23.4


COP ratio
%
100
106.2
106.2
106.2
106.2
106.2
106.2
106.2


(relative to that of R404A)











Refrigerating
%
100
86.2
98,5
99.1
100
102.1
104.5
106.9


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability











classification








Com-
Com-
Com-
Com-
Com-
Com-
Com-





parative
parative
parative
parative
parative
parative
parative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
2-6
2-3
2-4
2-5
2-6
2-7
2-8
2-9




















Composition
HFO-1132(E)
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



HFC-134a
mass %
0
0
0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge
° C.
120.0
121.0
122.4
123.3
124.4
125.5
126.0
131.7


temperature











Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.081
0.083
0.085
0.086
0.088
0.090
0.091
0.099


Compression ratio

23.1
23.0
22.8
22.6
22.5
22.3
22.2
21.6


COP ratio
%
106.2
106.3
106.3
106.3
106.3
106.4
106.4
106.7


(relative to that of R404A)











Refrigerating
%
109.5
111.7
114.6
116.4
118.7
121
122.2
133.3


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


flammability











classification









Test Example 2-2

The GWP of each mixed refrigerant represented in Examples 2-7 to 2-12, Comparative Examples 2-10 to 2-18 and Reference Example 2-2 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.


Evaporating temperature −35° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meaning of each of the above terms is the same as in Test Example 2-1.


The results in Test Example 2-2 are shown in Table 223. Table 223 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 223, the meaning of each of the terms is the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 2-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 2-1. The flame velocity test was performed in the same manner as in Test Example 2-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681.09, with the same method and test conditions as in Test Example 2-1.


















TABLE 223









Reference
Com-
Com-









Example
parative
parative









2-2
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
2-10
2-11
2-7
2-8
2-9
2-10
2-11




















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge
° C.
89.1
95.8
100.6
100.8
101.2
102.0
102.9
103.8


temperature











Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.165
0.131
0.148
0.149
0.151
0,154
0.157
0.160


Compression ratio

11.0
12.2
11.8
11.7
11.7
11.6
11.6
11.5


COP ratio
%
100
105.1
104.8
104.7
104.7
104.7
104.6
104.5


(relative to that of R404A)











Refrigerating
%
100
87.7
98,5
99.0
99.8
101.6
103.7
105.7


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability











classification








Com-
Com-
Com-
Com-
Com-
Com-
Com-





parative
parative
parative
parative
parative
parative
parative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
2-12
2-12
2-13
2-14
2-15
2-16
2-17
2-18




















Composition
HFO-1132(E)
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



HFC-134a
mass %
0
0
0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge
° C.
104.7
105.5
106.6
107.3
108.1
109.0
109.5
113.9


temperature











Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.164
0.167
0.171
0.174
0.177
0.180
0.181
0.196


Compression ratio

11.4
11.4
11.3
11.2
11.2
11.1
11.1
10.8


COP ratio
%
104.5
104.4
104.4
104.4
104.3
104.3
104.3
104.3


(relative to that of R404A)











Refrigerating
%
108.0
109.8
112.3
113.8
115.7
117.7
118.6
128.0


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


flammability











classification









Test Example 2-3

The GWP of each mixed refrigerant represented in Examples 2-13 to 2-18, Comparative Examples 2-19 to 2-27 and Reference Example 2-3 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.


Evaporating temperature −10° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meaning of each of the above terms is the same as in Test Example 2-1.


The results in Test Example 2-3 are shown in Table 224. Table 224 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 224, the meaning of each of the terms is the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 2-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 2-1. The flame velocity test was performed in the same manner as in Test Example 2-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 2-1.


















TABLE 224









Reference
Com-
Com-









Example
parative
parative









2-3
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
2-19
2-20
2-13
2-14
2-15
2-16
2-17




















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge
° C.
75.8
80.8
83.7
83.9
84.1
84.5
85.1
85.6


temperature











Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.434
0.357
0.399
0.401
0.404
0.411
0.419
0.427


Compression ratio

4.2
4.5
4.4
4.4
4.4
4.3
4.3
4.3


COP ratio
%
100
103.8
102.9
102.9
102.8
102.7
102.5
102.4


(relative to that of R404A)











Refrigerating
%
100
89.8
98.7
99.1
99.8
101.2
102.8
104.5


106.2











(relative to that of











R404A)











ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability











classification








Com-
Com-
Com-
Com-
Com-
Com-
Com-





parative
parative
parative
parative
parative
parative
parative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
2-18
2-21
2-22
2-23
2-24
2-25
2-27
2-27




















Composition
HFO-1132(E)
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



HFC-134a
mass %
0
0
0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge
° C.
86.2
86.6
87.3
87.7
88.2
88.7
88.9
91.5


temperature











Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.436
0.443
0.452
0.457
0.465
0.472
0.475
0.509


Compression ratio

4.3
4.3
4.3
4.3
4.3
4.2
4.2
4.2


COP ratio
%
102.2
102.1
102.0
101.9
101.8
101.7
101.6
101.3


(relative to that of R404A)











Refrigerating
%
106.2
107.7
109.6
110.8
112.3
113.8
114.5
121.7


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


flammability











classification









Test Example 2-4

The GWP of each mixed refrigerant represented in Examples 2-19 to 2-24, Comparative Examples 2-28 to 2-36 and Reference Example 2-4 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.


Evaporating temperature −80° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meaning of each of the above terms is the same as in Test Example 2-1.


The results in Test Example 2-4 are shown in Table 225. Table 225 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 225, the meaning of each of the terms is the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 2-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 2-1. The flame velocity test was performed in the same manner as in Test Example 2-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 2-1.


















TABLE 225









Reference
Com-
Com-









Example
parative
parative









2-3
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
2-28
2-29
2-19
2-20
2-21
2-21
2-22




















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge
° C.
136.7
146.0
157.7
158.1
158.8
160.4
162.1
163.9


temperature











Saturation pressure
MPa
1.822
1,592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.014
0.011
0.012
0.012
0.012
0.012
0.013
0.013


Compression ratio

134.6
149.1
150.8
150.2
149.3
147.2
145.0
142.8


COP ratio
%
100
112.6
110.3
110.3
110.4
110.6
110.8
111.0


(relative to that of R404A)











Refrigerating
%
100
91.7
99.3
100.2
101.5
104.4
107.8
111.3


106.2











(relative to that of











R404A)











ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability











classification









Com-
Com-
Com-
Com-
Com-
Com-






parative
parative
parative
parative
parative
parative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
2-23
2-24
2-31
2-32
2-33
2-34
2-35
2-36




















Composition
HFO-1132(E)
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



HFC-134a
mass %
0
0
0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge
° C.
165.8
167.4
169.6
170.9
172.6
174.3
175.2
184.0


temperature











Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.013
0.014
0.014
0.014
0.015
0.015
0.015
0.017


Compression ratio

140.5
138.7
136.3
134.9
133.2
131.5
130.7
123.8


COP ratio
%
111.3
111.4
111.7
111.9
112.1
112.3
112.4
113.5


(relative to that of R404A)











Refrigerating
%
115.1
118.2
122.5
125.2
128.6
132.1
133.8
151.0


capacity ratio











(relative to that of











R404A)











ASHRAE

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


flammability











classification









Test Example 2-5

The GWP of each mixed refrigerant represented in Examples 2-25 to 2-30, Comparative Examples 2-37 to 2-45 and Reference Example 2-5 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.


Evaporating temperature 10° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meaning of each of the above terms is the same as in Test Example 2-1.


The results in Test Example 2-5 are shown in Table 226. Table 226 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 226, the meaning of each of the terms is the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 2-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 2-1. The flame velocity test was performed in the same manner as in Test Example 2-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 2-1.


















TABLE 226









Reference
Com-
Com-









Example
parative
parative









2-5
Example
Example
Example
Example
Example
Example
Example



Unit
(R404A)
2-37
2-38
2-25
2-26
2-27
2-28
2-29




















Composition
HFO-
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
1132(E)












HFO-
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



1234yf












HFC-
mass %
4.0
0
0
0
0
0
0
0



134a












HFC-
mass %
52.0
0
0
0
0
0
0
0



143a












HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP (AR4)

3922
6
6
6
6
7
7
7


Discharge temperature

68.5
72.4
74.0
74.1
74.2
74.4
74.7
74.9


Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.820
0.694
0.768
0.772
0.777
0.789
0.803
0.817


Compression ratio

2.2
2.3
2.3
2.3
2.3
2.3
2.3
2,3


COP ratio (relative to
%
100.0
103.1
101.9
101.8
101.7
101.5
101.3
101.1


that of R404A)











Refrigerating capacity
%
100.0
91.2
98.9
99.3
99.8
101.0
102.5
103.8


ratio (relative to that of











R404A)











ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification

















Com-
Com-
Com-
Com-
Com-
Com-
Com-





parative
parative
parative
parative
parative
parative
parative




Example
Example
Example
Example
Example
Example
Example
Example



Unit
2-30
2-39
2-40
2-41
2-42
2-43
2-44
2-45




















Composition
HFO-
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0


proportions
1132(E)












HFO-
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0



1234yf












HFC-
mass %
0
0
0
0
0
0
0
0



134a












HFC-
mass %
0
0
0
0
0
0
0
0



143a












HFC-125
mass %
0
0
0
0
0
0
0
0
















GWP (AR4)

7
7
7
7
7
8
8
8


Discharge temperature

75.2
75.5
75.8
76.0
76.2
76.5
76.6
77.9


Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128


(40° C.)











Evaporating pressure
MPa
0.832
0.844
0.860
0.870
0.882
0.895
0.901
0.959


Compression ratio

2.3
2,2
2.2
2.2
2.2
2.2
2.2
2.2


COP ratio (relative to
%
100.9
100.8
100.6
100.4
100.3
100.1
100.1
99.5


that of R404A)











Refrigerating capacity
%
105.3
106.5
108.2
109.1
110.4
111.6
112,3
118.2


ratio (relative to that of











R404A)











ASHRAE flammability

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


classification


















Test Example 3

The GWP of each mixed refrigerant represented in Examples 3-1 to 3-5, Comparative Examples 3-1 to 3-5, Reference Example 3-1 (R134a) and Reference Example 3-2 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 45° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature −10° C.


Condensation temperature 45° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


An “evaporating temperature of −10° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is −10° C. A “condensation temperature of 45° C.” means that the condensation temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is 45° C.


The results in Test Example 3 are shown in Table 227. Table 227 shows Examples and Comparative Examples of the refrigerant 2C3 of the present disclosure. In Table 227, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R134a. In Table 227, the “Saturation pressure (45° C.)” represents the saturation pressure at a saturation temperature of 45° C. In Table 227, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant.


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption


The critical temperature was determined by performing calculation by using National Institute of Science and Technology (NISI) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. One having a flame velocity of 0 cm/s to 10 cm/s was rated as “Class 2L (lower flammability)”, one having a flame velocity of more than 10 cm/s was rated as “Class 2 (low flammability)”, and one causing no flame propagation was rated as “Class 1 (non-flammability)”. In Table 227, the “ASHRAE flammability classification” shows each result based on the criteria for determination.


The flame velocity test was performed as follows. First, the mixed refrigerant used had a purity of 99.5% or more, and degassing was made by repeating a cycle of freezing, pumping and thawing until no trace of air was observed on a vacuum gauge. The flame velocity was measured by a closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between electrodes at the center of a sample cell. The duration of discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of any flame was visualized using a schlieren photograph. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light-transmitting acrylic windows was used as the sample cell, and a xenon lamp was used as a light source. A schlieren image of any flame was recorded by a high-speed digital video camera at a frame rate of 600 fps, and stored in a PC.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09.


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>


Test container: spherical container of 280 mm in diameter (internal volume: 12 L)


Test temperature: 60° C.±3° C.


Pressure: 101.3 kPa±0.7 kPa


Water content: 0.0088 g±0.0005 g per gram of dry air (water content at a relative humidity of 50% at 23° C.)


Mixing ratio of refrigerant composition/air: ±0.2 vol. % by 1 vol. %


Mixing of refrigerant composition: ±0.1 mass %


Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer


Electrode interval: 6.4 mm (¼ inches)


Spark: 0.4 seconds±0.05 seconds


Criteria for determination:






    • A case where any flame was spread at more than 90 degrees around the ignition point flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)



















TABLE 227









Reference









Example 3-1
Comparative
Example 3-2





Item
Unit
(R134a)
Example 3-1
Comparative
Example 3-1
Example 3-2
Example 3-3


















Composition
HFO-1132(E)
mass %
0
20.0
30.0
31.1
33.0
35.0


proportions
HFO-1234yf
mass %
0
80.0
70.0
68.9
67.0
65.0



HFC-134a
mass %
100.0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0














GWP (AR4)

1430
5
6
6
6
6


Discharge temperature
° C.
86.9
86.3
86.9
87.2
87.9
88,5


Saturation pressure (45° C.)
MPa
1.160
1.607
1.795
1.814
1.848
1.883


Evaporating pressure
MPa
0.201
0.311
0.355
0.360
0.368
0.376


Critical temperature
° C.
101.1
84.6
83.0
82.7
82.2
81.7


COP ratio (relative
%
100.0
93.6
92.7
92.6
92.4
92.2


to that of R134a)









Refrigerating capacity ratio
%
100.0
132.3
148.3
150.0
152.8
155.8


(relative to that of R134a)









ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification



















Reference






Comparative
Comparative
Comparative
Example 3-2


Item
Unit
Example 3-4
Example 3-5
Example 3-3
Example 3-4
Example 3-5
(R404A)


















Composition
HFO-1132(E)
mass %
37.9
39.8
40.0
50.0
0.0
0


proportions
HFO-1234yf
mass %
62.1
60.2
60.0
50.0
100.0
0



HFC-134a
mass %
0
0
0
0
0
4.0



HFC-143a
mass %
0
0
0
0
0
52.0



HFC-125
mass %
0
0
0
0
0
44.0














GWP (AR4)

6
6
6
7
4
3922


Discharge temperature
° C.
89.4
90.0
90.1
93.0
72.2
81.7


Saturation pressure (45° C.)
MPa
1.930
1.963
1.966
2.123
1.154
2.052


Evaporating pressure
MPa
0.388
0.397
0.397
0.437
0.222
0.434


Critical temperature
° C.
81.0
80.5
80.5
78.7
94.7
72.0


COP ratio (relative
%
92.0
91.8
91.8
91.0
95.7
88.6


to that of R134a)









Refrigerating capacity ratio
%
159.8
162.7
162.9
176.6
96.2
164.4


(relative to that of R134a)









ASHRAE flammability

Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 1


classification
















Test Example 4

The GWP of each mixed refrigerant represented in Examples 41 to 4-7 and Comparative Examples 4-1 to 4-5 was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature and the saturation pressure at a saturation temperature of −10° C. of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature 5° C.


Condensation temperature 45° C.


Superheating temperature 5 K


Subcooling temperature 5 K


Compressor efficiency 70%


An “evaporating temperature of 5° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is 5° C. A “condensation temperature of 45° C.” means that the condensation temperature of such each mixed refrigerant in a condenser included in a refrigerating apparatus is 45° C.


The results in Test Example 4 are shown in Table 228. Table 228 shows Examples and Comparative Examples of the refrigerant 2C4 of the present disclosure. In Table 228, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R1234yf. In Table 228, the “Saturation pressure (−10° C.)” represents the saturation pressure at a saturation temperature of −10° C., as a representative evaporating temperature value under refrigeration conditions. In Table 228, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant.


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption


The critical temperature was determined by performing calculation by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. One having a flame velocity of 0 cm/s to 10 cm/s was rated as “Class 2L (lower flammability)”, one having a flame velocity of more than 10 cm/s was rated as “Class 2 (low flammability)”, and one causing no flame propagation was rated as “Class 1 (non-flammability)”. In Table 228, the “ASHRAE flammability classification” shows each result based on the criteria for determination.


The flame velocity test was performed as follows. First, the mixed refrigerant used had a purity of 99.5% or more, and degassing was made by repeating a cycle of freezing, pumping and thawing until no trace of air was observed on a vacuum gauge. The flame velocity was measured by a closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between electrodes at the center of a sample cell. The duration of discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of any flame was visualized using a schlieren photograph. A cylindrical container (inner diameter 155 mm, length: 198 mm) equipped with two light-transmitting acrylic windows was used as the sample cell, and a xenon lamp was used as a light source. A schlieren image of any flame was recorded by a high-speed digital video camera at a frame rate of 600 fps, and stored in a PC.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09.


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>


Test container: spherical container of 280 mm in diameter (internal volume: 12 L)


Test temperature: 60° C.±3° C.


Pressure: 101.3 kPa±0.7 kPa


Water content: 0.0088 g±0.0005 g per gram of dry air (water content at a relative humidity of 50% at 23° C.)


Mixing ratio of refrigerant composition/air: ±0.2 vol. % by 1 vol. %


Mixing of refrigerant composition: ±0.1 mass %


Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer


Electrode interval: 6.4 mm (¼ inches)


Spark: 0.4 seconds±0.05 seconds


Criteria for determination:






    • A case where any flame was spread at more than 90 degrees around the ignition point: flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)



















TABLE 228









Comparative
Comparative






Item
Unit
Example 4-1
Example 4-2
Example 4-1
Example 4-2
Example 4-3
Example 4-4


















Composition
HFO-1132(E)
mass %
0
15.0
21.0
23.6
24.3
25.1


proportions
HFO-1234yf
mass %
100.0
85.0
79.0
76.4
75.7
74.9














GWP (AR4)

4
5
5
5
5
6


Discharge temperature
° C.
54.4
61.3
63.1
63.8
64.0
64.2


Saturation pressure (−10° C.)
MPa
0.222
0.350
0.383
0.396
0.400
0.403


Critical temperature
° C.
94.7
88.1
85.9
85.0
84.8
84.5


COP ratio (relative to
%
100.0
99.1
98.8
98.6
98.5
98,4


that of R1234yf)









Refrigerating capacity ratio
%
100.0
129.8
140.0
144.2
145.4
146.6


(relative to that of R1234yf)









ASHRAE flammability

Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification

















Comparative
Comparative
Comparative


Item
Unit
Example 4-5
Example 4-6
Example 4-7
Example 4-3
Example 4-4
Example 4-5


















Composition
HFO-1132(E)
mass %
26.7
27.5
28.4
30.0
40.0
50.0


proportions
HFO-1234yf
mass %
73.3
72.5
71.6
70.0
60.0
50.0














GWP (AR4)

6
6
6
6
6
7


Discharge temperature
° C.
64.6
64.8
65.0
65.4
67.5
69.4


Saturation pressure (−10° C.)
MPa
0.411
0.414
0.418
0.425
0.461
0.492


Critical temperature
° C.
84.0
83.8
83.5
83.0
80.5
78.7


COP ratio (relative to
%
98.3
98.2
98.2
98.0
97.2
96.6


that of R1234yf)









Refrigerating capacity ratio
%
149.1
150.3
151.7
154.1
168.2
181.3


(relative to that of R1234yf)









ASHRAE flammability

Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification
















Test Example 5

The GWP of each mixed refrigerant represented in Examples 5-1 to 5-13, Comparative Examples 5-1 to 5-3 and Reference Example 5-1 (R134a) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the boiling point and the discharge temperature of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature −30° C.


Condensation temperature 30° C.


Superheating temperature 5 K


Subcooling temperature 5 K


Compressor efficiency 70%


An “evaporating temperature of −30° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is −30° C. A “condensation temperature of 30° C.” means that the condensation temperature of such each mixed refrigerant in a condenser included in a refrigerating apparatus is 30° C.


The results in Test Example 5 are shown in Table 229. Table 229 shows Examples and Comparative Examples of the refrigerant 2C5 of the present disclosure. In Table 229, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R1234yf. In Table 229, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant. In Table 229, the “Boiling point (° C.)” represents the temperature at which a liquid phase of such each mixed refrigerant is at atmospheric pressure (101.33 kPa). In Table 229, “Power consumption (%) of driving force” represents the electric energy used for traveling an electric car, and is represented by the ratio to the power consumption in the case of HFO-1234yf as the refrigerant. In Table 229, “Heating power consumption (%)” represents the electric energy used for operating heating by an electric car, and is represented by the ratio to the power consumption in the case of HFO-1234yf as the refrigerant. In Table 229, the “Mileage” represents the relative proportion (%) of the mileage in traveling with heating when the mileage in travelling with no heating in an electric car in which a secondary battery having a certain electric capacitance is mounted is 100% (the consumption power in heating is 0).


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. The flame velocity was measured as follows. First, the mixed refrigerant used had a purity of 99.5% or more, and degassing was made by repeating a cycle of freezing, pumping and thawing until no trace of air was observed on a vacuum gauge. The flame velocity was measured by a closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between electrodes at the center of a sample cell. The duration of discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of any flame was visualized using a schlieren photograph. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light-transmitting acrylic windows was used as the sample cell, and a xenon lamp was used as a light source. A schlieren image of any flame was recorded by a high-speed digital camera at a frame rate of 600 fps, and stored in a PC.


The heating method included using an electric heater system for heating in the case of any refrigerant having a boiling point of more than −40° C., or using a heat pump system for heating in the case of refrigerant having a boiling point of −40° C. or less.


The power consumption in use of heating was determined by the following expression.

Power consumption in use of heating=Heating capacity/Heating COP


Herein, the heating COP means “heating efficiency”.


The heating efficiency means that the heating COP is 1 in the case of an electric heater, and an electrode comparable with a driving force is consumed in heating. In other words, the consumption power in heating is expressed by E=E/(1+COP). On the other hand, the heating COP in the case of a heat pump was determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature −30° C.


Condensation temperature 30° C.


Superheating temperature 5 K


Subcooling temperature 5 K


Compressor efficiency 70%


The mileage was determined by the following expression.

Mileage=(Battery capacitance)/(Power consumption of driving force+Heating power consumption)



















TABLE 229









Reference












Example
Comparative
Comparative
Example
Example
Example
Example
Example
Example


Item
Unit
5-1
Example 5-1
Example 5-2
5-1
5-2
5-3
5-4
5-5
5-6





















Composition
HFO-
mass %
0.0
0
10.0
12.1
15.0
20.0
25.0
30.0
35.0


proportions
1132(E)













HFO-
mass %
0.0
100.0
90.0
87.9
85.0
80.0
75.0
70.0
65.0



1234yf













HFC-134a
mass %
100.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0

















GWP (AR4)

1430
4
5
5
5
5
6
6
6


COP ratio (relative to
%
105
100
100
100
100
100
100
100
100


that of R1234yf)












Refrigerating capacity
%
99
100
123
128
134
145
155
165
175


ratio (relative to that of












R1234yf)












Power consumption of
%
100
100
100
100
100
100
100
100
100


driving force












Heating power
%
95
100
100
33
33
33
33
33
33


consumption












Mileage (without heating)
%
100
100
100
100
100
100
100
100
100


Mileage (with heating)
%
50
50
50
84
84
84
84
84
84


Discharge temperature
° C.
66.0
48.0
54.8
56.0
57.5
59.8
61.9
63.9
65.8


Flame velocity
cm/s
0.0
1.5
1.5
1.5
1.5
1.5
1.5
1.5
2.0


Boiling point
° C.
−26.1
−29.5
−38.8
−40.0
−41.4
−43.3
−44.7
−45.9
−46.9


Saturation pressure at -
kPaG
−50.1
−39
−4.4
0.9
7.5
17.2
25,3
32.3
38.4


40° C.












Heating method
System
Electric
Electric
Electric
Heat
Heat
Heat
Heat
Heat
Heat




heater
heater
heater
pump
pump
pump
pump
pump
pump





















Example
Example
Example
Example
Example
Example
Example
Comparative


Item
Unit
5-7
5-8
5-9
5-10
5-11
5-12
5-13
Example 5-3




















Composition
HFO-
mass %
40.0
45.0
50.0
55.0
60.0
65.0
72.0
75.0


proportions
1132(E)












HFO-
mass %
60.0
55.0
50.0
45.0
40.0
35.0
28.0
25.0



1234yf












HFC-134a
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
















GWP (AR4)

6
7
7
7
8
8
8
9


COP ratio (relative to
%
100
100
100
100
100
100
100
100


that of R1234yf)











Refrigerating capacity
%
185
194
203
212
220
229
240
245


ratio (relative to that of











R1234yf)











Power consumption of
%
100
100
100
100
100
100
100
100


driving force











Heating power
%
33
33
33
33
33
33
33
33


consumption











Mileage (without heating)
%
100
100
100
100
100
100
100
100


Mileage (with heating)
%
84
84
84
84
84
84
84
84


Discharge temperature
0° C.
67.6
69.3
70.9
72.6
74.2
75.9
78,2
79.2


Flame velocity
cm/s
2.6
3.4
4.3
5.3
6.5
7.8
9.9
10.9


Boiling point
0
−47.7
−48.4
−49.1
−49.6
−50.2
−50.5
−51.2
−51.4


Saturation pressure at -
kPaG
43.9
48.8
53.4
57.5
61.4
65.0
69.6
71.5


40° C.











Heating method
System
Heat
Heat
Heat
Heat
Heat
Heat
Heat
Heat




pump
pump
pump
pump
pump
pump
pump
pump










(1-6-4) Refrigerant 2D


Refrigerant 2D The refrigerant 2D of the present disclosure includes difluoromethane (HFC-32), 2,3,3,3-tetrafluoropropene (HFO-1234yf), and at least one of 1,1-difluoroethylene (HFO-1132a) and tetrafluoroethylene (FO-1114). The refrigerant 2D of the present disclosure, which has such a configuration, simultaneously has three performances of any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R404A and/or and R410A, and a sufficiently low GWP.


In the present disclosure, the coefficient of performance (COP) equivalent to or more than that of R404A means that the COP ratio relative to that of R404A is 100% or more (preferably 103% or more, more preferably 105% or more), and the refrigerating capacity (Cap) equivalent to or more than that of R404A means that the Cap ratio relative to that of R404A is 80% or more (preferably 90% or more, more preferably 95% or more, most preferably 100% or more).


The coefficient of performance (COP) equivalent to or more than that of R410A means that the COP ratio relative to that of R410A is 90% or more (preferably 93% or more, more preferably 95% or more, most preferably 100% or more), and the refrigerating capacity (Cap) equivalent to or more than that of R410A means that the Cap ratio relative to that of R410A is 80% or more (preferably 95% or more, more preferably 99% or more, most preferably 100% or more).


Furthermore, a sufficiently low GWP means a GWP of 500 or less, preferably 400 or less, more preferably 300 or less, and means a GWP of 200 or less, preferably 170 or less, more preferably 150 or less, further preferably 130 or less in the case of a refrigerant 2D according to a first aspect described below.


The refrigerant 2D of the present disclosure may include HFC-32, HFO-1234yf, and at least one of HFO-1132a and FO-1114, and the composition is not limited as long as the above performances are exhibited, and in particular, is preferably any composition so that the refrigerant has a GWP of 500 or less (in particular, 170 or less in the case of a refrigerant 2D according to a first aspect described below. While at least one of HFO-1132a and FO-1114, namely, any one or both thereof may be included, HFO-1132a is preferably included in the present disclosure.


Specifically, the refrigerant 2D of the present disclosure is preferably according to an aspect where HFC-32, HFO-1234yf and HFO-1132a are included, and is preferably a mixed refrigerant including HFO-1234yf, and 15.0 to 24.0 mass % of HFC-32 and 1.0 to 7.0 mass % of HFO-1132a when the total amount of the three components is 100 mass % (the refrigerant 2D according to the first aspect; there is within the range of a quadrangle represented by X or on line segments of the quadrangle in an enlarged view of FIG. 2A). In particular, a mixed refrigerant is preferable which includes HFO-1234yf, and 19.5 to 23.5 mass % of HFC-32 and 3.1 to 3.7 mass % of HFO-1132a (a preferable refrigerant 2D according to the first aspect; there is within the range of a quadrangle represented by Y or on line segments of the quadrangle in an enlarged view of FIG. 2A). Such a composition range allows the predetermined effects of the present disclosure to be easily exerted. Such a refrigerant 2D according to the first aspect is particularly useful as an alternative refrigerant of R404A.


The refrigerant 2D of the present disclosure (the refrigerant 2D according to the fast aspect) preferably has a condensation temperature glide of 12° C. or less, more preferably 10° C. or less, further preferably 9° C. or less. The compressor outlet pressure is preferably in the range from 1.60 to 2.00 MPa, more preferably in the range from 1.73 to 1.91 MPa. The refrigerant 2D of the present disclosure, when mixed with a known refrigerator oil described below, has the properties of good miscibility with the refrigerator oil.


The composition range of the refrigerant 2D according to the first aspect encompasses that of any refrigerant 2D according to a second aspect.


The refrigerant 2D of the present disclosure (the refrigerant 2D of the second aspect) includes HFC-32, HFO-1234yf and HFO-1132a, and when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which the sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within the range of a triangle surrounded by line segments RS, ST and TR that connect three points:

    • point R (21.80, 3.95, 74.25),
    • point S (21.80, 3.05, 75.15), and
    • point T (20.95, 75.30, 3.75);


      or are on the line segments (within the range of a triangle surrounded by line segments RS, ST and TR or are on the line segments in an enlarged view of FIG. 2A).


The refrigerant 2D of the present disclosure (the refrigerant 2D of the second aspect), when satisfies the above requirements, has a coefficient of performance (COP) equivalent to or more than that of R404A and a refrigerating capacity (Cap) of 95% or more, and a GWP of 150 or less and a condensation temperature glide of 9° C. or less.


The refrigerant 2D of the present disclosure encompasses not only such any refrigerant 2D according to the first aspect and the second aspect described above, but also any refrigerant 2D according to the following third aspect to seventh aspect. Such any refrigerant 2D according to the third aspect to the seventh aspect is useful as, in particular, an alternative refrigerant of R410A.


The refrigerant 2D of the present disclosure (the refrigerant 2D of the third aspect) includes HFC-32, HFO-1234yf and HFO-1132a, wherein

    • when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which the sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within the range of a figure surrounded by line segments LF, FG, GO, OB and BL that connect five points:
    • point L (74.0, 19.9, 6.1),
    • point F (49.1, 25.9, 25.0),
    • point G (0.0, 48.6, 51.4),
    • point O (0.0, 0.0, 100), and
    • point B (73.9, 0.0, 26.1);


      or are on the line segments (but not on the line segments GO and OB),
    • the line segment LF is represented by
    • coordinate (y=0.0021x2−0.4975x+45.264),
    • the line segment FG is represented by
    • coordinate (y=0.0031x2−0.6144x+48.6), and
    • the line segments GO, OB and BL are straight lines.


The refrigerant 2D of the present disclosure (the refrigerant 2D of the third aspect), when satisfies the above requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A, and has a GWP of 500 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less. The compressor outlet pressure is preferably 3.4 MPa or less, more preferably 3.0 MPa or less.


The line segment EF (including line segment LF and line segment PF) is obtained by determining an approximate curve from three points of the point E, that in Example 24 and the point F in the Tables herein and FIG. 2B, according to a least-squares method, and the line segment FG is obtained by determining an approximate curve from three points of the point F, that in Example 26 and the point G therein, according to a least-squares method.


The refrigerant 2D of the present disclosure (the refrigerant 2D according to the fourth aspect) includes HFC-32, HFO-1234yf and HFO-1132a, wherein

    • when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which the sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within the range of a figure surrounded by line segments PF, FG, GO, OB′ and B′P that connect five points:
    • point P (59.1, 23.2, 17.7),
    • point F (49.1, 25.9, 25.0),
    • point G (0.0, 48.6, 51.4),
    • point O (0.0, 0.0, 100) and
    • point B′ (59.0, 0.0, 40.2);


      or are on the line segments (but not on the line segments GO and OB′),
    • the line segment PF is represented by
    • coordinate (y=0.0021x2−0.4975x+45.264),
    • the line segment FG is represented by
    • coordinate (y=0.0031x2−0.6144x+48.6), and
    • the line segments GO, OB′ and BP are straight lines.


The refrigerant 2D of the present disclosure (the refrigerant 2D according to the fourth aspect), when satisfies the above requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A, and has a GWP of 400 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less. The compressor outlet pressure is preferably 3.4 MPa or less, more preferably 3.0 MPa or less.


The refrigerant 2D of the present disclosure (the refrigerant 2D according to the fifth aspect) includes HFC-32, HFO-1234yf and HFO-1132a, wherein

    • when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which the sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within the range of a figure surrounded by line segments MI, IJ, JB and BM that connect four points:
    • point M (74.0, 19.5, 6.5),
    • point I (62.9, 15.5, 21.6),
    • point J (33.5, 0.0, 66.5), and
    • point B (73.9, 0.0, 26.1),


      or are on the line segments (but not on the line segment JB),
    • the line segment MI is represented by
    • coordinate (y=0.006x2+1.1837x−35.264),
    • the line segment IJ is represented by
    • coordinate (y=0.0083x2−0.2719x−0.1953), and
    • the line segments JB and BM are straight lines.


The refrigerant 2D of the present disclosure (the refrigerant 2D according to the fifth aspect), when satisfies the above requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A, and has a GWP of 500 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less, and the compressor outlet pressure is preferably 3.4 Mpa or less, more preferably 3.0 Mpa or less. The refrigerant has a condensation temperature glide and an evaporating temperature glide each being as low as 5° C. or less, and is particularly suitable as an alternative of R410A.


The line segment HI (including line segment MI) is obtained by determining an approximate curve from three points of the point H, that in Example 21 and the point I in the Tables herein and FIG. 2B, according to a least-squares method, and the line segment IJ is obtained by determining an approximate curve from three points of the point I, that in Example 23 and the point J herein, according to a least-squares method.


The refrigerant 2D of the present disclosure (the refrigerant 2D according to the sixth aspect) includes HFC-32, HFO-1234yf and HFO-1132a, wherein

    • when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which the sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within the range of a figure surrounded by line segments QJ, JB′ and B′Q that connect three points:
    • point Q (59.1, 12.7, 28.2),
    • point J (33.5, 0.0, 66.5), and
    • point B′ (59.0, 0.0, 40.2);


      or are on the line segments (but not on the line segment 7B′),
    • the line segment QJ is represented by
    • coordinate (y=0.0083x2−0.2719x−0.1953), and
    • the line segments JB′ and B′Q are straight lines.


The refrigerant 2D of the present disclosure (the refrigerant 2D according to the sixth aspect), when satisfies the above requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A, and has a GWP of 400 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less, and the compressor outlet pressure is preferably 3.4 Mpa or less, more preferably 3.0 Mpa or less. The refrigerant has an evaporating temperature glide of as low as 5° C. or less, preferably 4° C. or less, more preferably 3.5° C., or less, and is particularly suitable as an alternative of R410A.


The refrigerant 2D of the present disclosure (the refrigerant 2D according to the seventh aspect) includes HFC-32, HFO-1234yf and HFO-1132a, wherein

    • when HFC-32, HFO-1132a and HFO-1234yf in terms of mass % based on their sum in the refrigerant are represented by x, y and z, respectively, coordinates (x,y,z) in a three-component composition diagram in which the sum of HFC-32, HFO-1132a and HFO-1234yf is 100 mass % are within the range of a figure surrounded by line segments QU, UV and VQ that connect three points:
    • point Q (59.1, 12.7, 28.2),
    • point U (59.0, 5.5, 35.5), and
    • point V (52.5, 8.4, 39.1);


      or are on the line segments,
    • the line segment VQ is represented by
    • coordinate (y=0.0083x2−0.2719x−0.1953), and
    • the line segment UV is represented by
    • coordinate (y=0.0026x2−0.7385x+39.946), and
    • the line segment QU is a straight line.


The refrigerant 2D of the present disclosure (the refrigerant 2D according to the seventh aspect), when satisfies the above requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A (refrigerating capacity relative to that of R410A of 99% or more), and has a GWP of 400 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less, and the compressor outlet pressure is preferably 3.4 Mpa or less, more preferably 3.0 Mpa or less. The refrigerant has an evaporating temperature glide of as low as 5° C. or less, preferably 4° C. or less, more preferably 3.5° C. or less, and is particularly suitable as an alternative of R410A.


The line segment UV is obtained by determining an approximate curve from three points of the point U, that in Example 28 and the point V in the Tables herein and FIG. 2B, according to a least-squares method.


The present disclosure has, for the first time, proposed an alternative refrigerant of conventional refrigerants using HFO-1132a, such as R12, R22, R134a, R404A, R407A, R407C, R407F, R407H, R410A, R413A, R417A, R422A, R422B, R422C, R422D, R423A, R424A, R426A, R427A, R430A, R434A, R437A, R438A, R448A, R449A, R449B, R449C, R452A, R452B, R454A, R454B, R454C, R455A, R459A, R465A, R502, R507 and R513A, as exemplified in the refrigerant 2D according to the first aspect to the seventh aspect, and the present disclosure encompasses, in the broadest sense, the invention of “a composition including a refrigerant, wherein the refrigerant is used as an alternative refrigerant of R12, R22, R134a, R404A, R407A, R407C, R407F, R407H, R410A, R413A, R417A, R422A, R422B, R422C, R422D, R423A, R424A, R426A, R427A, R430A, R434A, R437A, R438A, R448A, R449A, R449B, R449C, R452A, R452B, R454A, R454B, R454C, R455A, R459A, R465A, R502, R507 or R513A including 1,1-difluoroethylene (HFO-1132a)”. In particular, the invention of “a composition including a refrigerant, wherein the refrigerant is used as an alternative refrigerant of R410A including 1,1-difluoroethylene (HFO-1132a)” is preferably included.


<Mixed Refrigerant Including Still Other Additional Refrigerant>


The refrigerant 2D of the present disclosure may be a mixed refrigerant including not only HFC-32, HFO-1234yf, and at least one of HFO-1132a and FO-1114, but also still other additional refrigerant, as long as the above characteristics and/or effects are not impaired. In such a case, the total amount of HFC-32, HFO-1234yf, and at least one of HFO-1132a and FO-1114 is preferably 99.5 mass % or more and less than 100 mass %, more preferably 99.75 mass % or more and less than 100 mass %, further preferably 99.9 mass % or more and less than 100 mass %, based on the entire refrigerant of the present disclosure. The additional refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. The additional refrigerant may be included singly or in combinations of two or more kinds thereof in the mixed refrigerant.


Examples of Refrigerant 2D

Hereinafter, the refrigerant 2D will be described with reference to Examples in more detail. It is noted that the present disclosure is not limited to such Examples.


Examples 1 to 16 and Comparative Example 1 (corresponding to any refrigerant 2D according to first aspect and second aspect)


Examples 17 to 87 and Comparative Examples 2 to 18 (corresponding to any refrigerant 2D according to third aspect to seventh aspect)


The GWP of each mixed refrigerant represented in Examples and Comparative Examples, and those of R404A (R125/143a/R134a=44/52/4 weight %) and R410A (R32/R125=50/50 weight %) were evaluated based on the value in the fourth report of IPCC (Intergovernmental Panel on Climate Change).


The COP and the refrigerating capacity of each mixed refrigerant shown in Examples and Comparative Examples, and the COP and the refrigerating capacity of R404A were each determined by using National Institute of Science and Technology (NIST), and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0). Specifically, those in Examples 1 to 16 and Comparative Example 1 (corresponding to the refrigerant 2D according to the first aspect and the second aspect) were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions:


Evaporating temperature −40° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


and those in Examples 17 to 87 and Comparative Examples 2 to 18 (corresponding to the refrigerant 2D according to the third aspect to the seventh aspect) were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions.


Evaporating temperature 5° C.


Condensation temperature 45° C.


Superheating temperature 5 K


Subcooling temperature 5 K


Compressor efficiency 70%


The condensation temperature glide, the evaporating temperature glide and the compressor outlet pressure in the case of use of each mixed refrigerant represented in Examples and Comparative Examples were also determined by using Refprop 9.0.


The GWP, the COP and the refrigerating capacity, calculated based on the results, are shown in Table 30 and Table 231-1 to Table 231-12. The COP ratio and the refrigerating capacity ratio here shown are represented as respective proportions (%) relative to that of R404A in Examples 1 to 16 and Comparative Example 1, and are represented as respective proportions (%) relative to that of R410A in Examples 17 to 87 and Comparative Examples 2 to 18.


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption













TABLE 230











Evaluation results




















COP ratio
Refrigerating









(%)
capacity ratio
Condensation
Compressor













Example/
Composition proportions (mass %)

(relative to
(%) (relative
temperature
outlet















Comparative


HFO-

that of
to that of
glide
pressure


Example
R32
R1234yf
1132a
GWP
R404A)
R404A)
(K)
(Mpa)
















Comparative
R404A
3922
100
100
0.3
1.82















Example 1










Example 1
21.8
77.1
1.1
150
108
91
7.5
1.64


Example 2
21.8
72.5
5.7
150
106
100
9.8
1.81


Example 3
21.5
75.5
3
148
107
94
8.5
1.70


Example 4
16.6
78.1
5.3
115
106
90
10.4
1.68


Example 5
20
75
5
138
105
95
9.8
1.75


Example 6
20
77.5
2.5
138
107
91
8.5
1.65


Example 7
20
73
7
138
105
99
10.6
1.82


Example 8
15
80
5
105
106
87
10.4
1.64


Example 9
21.5
75
3.5
148
107
95
8.8
1.72


Example 10
23.5
72.8
3.7
162
107
99
8.6
1.77


Example 11
23.5
73.4
3.1
162
107
97
8.3
1.75


Example 12
19.5
76.8
3.7
135
107
92
9.2
1.69


Example 13
19.5
77.4
3.1
135
107
91
8.9
1.67


Example 14
21.80
75.15
3.05
150
107
95
8.5
1.71


(Point S)










Example 15
21.80
74.25
3.95
150
107
96
9.0
1.75


(Point R)










Example 16
20.95
75.30
3.75
144
107
95
9.0
1.72


(Point T)









As clear from the results in Table 230, it can be particularly seen that the refrigerant 2D according to the second aspect has a coefficient of performance (COP) equivalent to or more than that of R404A and a refrigerating capacity (Cap) of 95% or more, has a GWP of 150 or less and a condensation temperature glide of 9° C. or less, and is particularly excellent as an alternative refrigerant of R404A.

















TABLE 231-1








Comparative
Example
Example
Comparative
Comparative
Example




Comparative
Example 3
17
18
Example 4
Example 5
19


Item
Unit
Example 2
A
L
M
B
A′
P























R32
mass %
R410A
74.0
74.0
74.0
73.9
59.2
59.1


R1132a
mass %

26.0
19.9
19.5
0.0
40.8
23.2


R1234yf
mass %

0.0
6.1
6.5
26.1
0.0
17.7


GWP

2088
500
500
500
500
400
400


COP ratio
% (relative
100
95
97
97
102
89
95



to that of










R410A)









Refrigerating
% (relative
100
131
124
124
99
139
121


capacity ratio
to that of










R410A)









Compressor
% (relative
100
134
125
124
95
153
125


outlet pressure
to that of









ratio
R410A)









Condensation
° C.
0
4.6
4.6
4.5
1.0
3.9
5.5


glide










Evaporation glide
° C.
0.1
5.6
5.1
5.0
0.8
6.1
6.1
























TABLE 231-2







Example
Comparative
Comparative

Example

Comparative




20
Example 6
Example 7
Example
22
Example
Example 8


Item
Unit
Q
B′
H
21
I
23
J























R32
mass %
59.1
59.0
79.2
71.2
62.9
51.0
33.5


R1132a
mass %
12.7
0.0
20.8
18.6
15.5
7.5
0.0


R1234yf
mass %
28.2
40.2
0.0
10.0
21.6
41.5
66.5


GWP

400
400
535
481
426
346
229


COP ratio
% (relative
99
102
97
97
98
100
102



to that of










R410A)









Refrigerating
% (relative
108
92
127
122
114
97
75


capacity ratio
to that of










R410A)









Compressor outlet
% (relative
109
89
128
122
115
97
75


pressure ratio
to that of










R410A)









Condensation
° C.
5.0
2.0
4.3
4.6
5.0
5.0
5.0


glide










Evaporation glide
° C.
4.8
1.8
5.0
5.0
5.0
4.6
4.8

























TABLE 231-3







Comparative

Example

Comparative
Example

Example




Example 9
Example
25
Example
Example 10
27
Example
29


Item
Unit
E
24
F
26
G
U
28
V
























R32
mass %
81.3
65.9
49.1
29.2
0.0
59.0
55.8
52.5


R1132a
mass %
18.7
21.6
25.9
33.3
48.6
5.5
6.9
8.4


R1234yf
mass %
0.0
12.5
25.0
37.5
51.4
35.5
37.3
39.1


GWP

549
446
333
199
2
400
378
36


COP ratio
% (relative
97
96
94
92
90
101
100
100



to that of











R410A)










Refrigerating
% (relative
126
122
118
113
108
99
99
99


capacity ratio
to that of











R410A)










Compressor
% (relative
125
125
125
125
125
98
99
99


outlet pressure
to that of










ratio
R410A)










Condensation
° C.
4.2
5.0
6.4
8.9
14.5
3.7
4.3
5.0


glide











Evaporation
° C.
4.7
5.6
7.1
10.3
16.7
3.3
3.9
4.6


glide

























TABLE 231-4







Example
Example
Example
Example
Example
Comparative
Example
Example


Item
Unit
30
31
32
33
34
Example 11
35
36
























R32
mass %
30.0
40.0
50.0
60.0
70.0
80.0
30.0
40.0


R1132a
mass %
5.0
5.0
5.0
5.0
5.0
5.0
10.0
10.0


R1234yf
mass %
65.0
55.0
45.0
35.0
25.0
15.0
60.0
50.0


GWP

205
272
339
406
474
541
205
272


COP ratio
% (relative
101
101
101
101
101
101
100
99



to that of











R410A)










Refrigerating
% (relative
79
86
93
99
104
109
86
93


capacity ratio
to that of











R410A)










Compressor
% (relative
80
87
93
97
101
105
88
95


outlet pressure
to that of










ratio
R410A)










Condensation
° C.
7.6
5.9
4.5
3.5
2.8
2.2
8.9
7.0


glide











Evaporation glide
° C.
6.8
5.4
4.1
3.1
2.4
2.0
8.1
6.5

























TABLE 231-5







Example
Example
Example
Comparative
Example
Example
Example
Example


Item
Unit
37
38
39
Example 12
40
41
42
43
























R32
mass %
50.0
60.0
70.0
80.0
30.0
40.0
50.0
60.0


R1132a
mass %
10.0
10.0
10.0
10.0
15.0
15.0
15.0
15.0


R1234yf
mass %
40.0
30.0
20.0
10.0
55.0
45.0
35.0
25.0


GWP

339
406
473
541
205
272
339
406


COP ratio
% (relative
99
99
99
100
98
98
98
98



to that of











R410A)










Refrigerating
% (relative
100
105
110
115
92
99
106
112


capacity ratio
to that of











R410A)










Compressor
% (relative
101
105
109
112
96
103
108
113


outlet pressure
to that of










ratio
R410A)










Condensation
° C.
5.6
4.6
3.8
3.3
9.7
7.7
6.2
5.2


glide











Evaporation glide
° C.
5.2
4.2
3.6
3.2
9.1
7.4
6.1
5.1

























TABLE 231-6







Example
Comparative
Example
Example
Example
Example
Example
Example


Item
Unit
44
Example 13
45
46
47
48
49
50
























R32
mass %
70.0
80.0
30.0
40.0
50.0
60.0
70.0
30.0


R1132a
mass %
15.0
15.0
20.0
20.0
20.0
20.0
20.0
25.0


R1234yf
mass %
15.0
5.0
50.0
40.0
30.0
20.0
10.0
45.0


GWP

473
540
205
272
339
406
473
205


COP ratio
% (relative
98
98
97
96
96
96
97
95



to that of











R410A)










Refrigerating
% (relative
117
121
98
106
112
118
122
104


capacity ratio
to that of











R410A)










Compressor
% (relative
116
119
104
111
116
120
124
112


outlet pressure
to that of










ratio
R410A)










Condensation
° C.
4.5
3.9
9.9
7.9
6.4
5.5
4.8
9.7


glide











Evaporation glide
° C.
4.5
4.1
9.8
8.0
6.7
5.8
5.2
10.2

























TABLE 231-7









Comparative
Comparative

Comparative
Comparative
Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
51
52
14
15
53
16
17
18
























R32
mass %
40.0
50.0
60.0
70.0
30.0
40.0
50.0
60.0


R1132a
mass %
25.0
25.
25.0
25.0
30.0
30.0
30.0
30.0


R1234yf
mass %
35.0
25.0
15.0
5.0
40.0
30.0
20.0
10.0


GWP

272
339
406
473
204
272
339
406


COP ratio
% (relative
95
95
95
95
93
93
93
93



to that of











R410A)










Refrigerating
% (relative
112
118
123
128
110
117
123
129


capacity
to that of










ratio
R410A)










Compressor
% (relative
119
124
128
131
120
127
132
136


outlet pressure
to that of










ratio
R410A)










Condensation
° C.
7.7
6.3
5.4
4.8
9.2
7.3
6.0
5.1


glide











Evaporation
° C.
8.3
7.0
6.2
5.7
10.3
8.4
7.1
6.4


glide

























TABLE 231-8







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
54
55
56
57
58
59
60
61
























R32
mass %
39.0
41.0
43.0
45.0
47.0
49.0
51.0
53.0


R1132a
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0


R1234yf
mass %
60.0
58.0
56.0
54.0
52.0
50.0
48.0
46.0


GWP

266
279
293
306
319
333
346
360


COP ratio
% (relative
102
102
102
102
102
102
102
102



to that of











R410A)










Refrigerating
% (relative
80
82
83
85
86
87
88
90


capacity ratio
to that of











R410A)










Compressor outlet
% (relative
80
81
83
84
85
86
87
88


pressure ratio
to that of











R410A)










Condensation
° C.
4.6
4.3
4.1
3.8
3.6
3.3
3.1
2.9


glide











Evaporation glide
° C.
4.4
4.1
3.9
3.6
3.3
3.1
2.9
2.7

























TABLE 231-9







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
62
63
64
65
66
67
68
69
























R32
mass %
55.0
57.0
59.0
45.0
47.0
49.0
51.0
53.0


R1132a
mass %
1.0
1.0
1.0
3.0
3.0
3.0
3.0
3.0


R1234yf
mass %
44.0
42.0
40.0
52.0
50.0
48.0
46.0
44.0


GWP

373
386
400
306
319
333
346
360


COP ratio
% (relative
102
102
102
101
101
101
101
101



to that of











R410A)










Refrigerating
% (relative
91
92
93
87
89
90
91
92


capacity ratio
to that of











R410A)










Compressor outlet
% (relative
89
90
91
87
88
89
90
91


pressure ratio
to that of











R410A)










Condensation
° C.
2.7
2.5
2.3
4.5
4.3
4.0
3.8
3.6


glide











Evaporation glide
° C.
2.5
2.3
2.1
4.2
3.9
3.7
3.4
3.2

























TABLE 231-10







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
70
71
72
73
74
75
76
77
























R32
mass %
55.0
57.0
59.0
47.0
49.0
51.0
53.0
55.0


R1132a
mass %
3.0
3.0
3.0
5.0
5.0
5.0
5.0
5.0


R1234yf
mass %
42.0
40.0
38.0
48.0
46.0
44.0
42.0
40.0


GWP

373
386
400
319
333
346
359
373


COP ratio
% (relative
101
101
101
101
101
101
101
101



to that of











R410A)










Refrigerating
% (relative
93
95
96
91
92
94
95
96


capacity ratio
to that of











R410A)










Compressor outlet
% (relative
92
93
94
91
92
93
94
95


pressure ratio
to that of











R410A)










Condensation
° C.
3.4
3.2
3.0
4.9
4.6
4.4
4.2
3.9


glide











Evaporation glide
° C.
3.0
2.8
2.7
4.4
4.2
4.0
3.7
3.5

























TABLE 231-11







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
78
79
80
81
82
83
84
85
























R32
mass %
57.0
59.0
53.0
55.0
57.0
59.0
55.0
57.0


R1132a
mass %
5.0
5.0
7.0
7.0
7.0
7.0
9.0
9.0


R1234yf
mass %
38.0
36.0
40.0
38.0
36.0
34.0
36.0
34.0


GWP

386
400
359
373
386
400
373
386


COP ratio
% (relative
101
101
100
100
100
100
100
100



to that of











R410A)










Refrigerating
% (relative
97
98
98
99
100
101
101
102


capacity ratio
to that of











R410A)










Compressor outlet
% (relative
96
97
97
98
99
100
101
102


pressure ratio
to that of











R410A)










Condensation
° C.
3.8
3.6
4.7
4.4
4.2
4.1
4.9
4.7


glide











Evaporation glide
° C.
3.4
3.2
4.2
4.0
3.8
3.7
4.5
4.3



















TABLE 231-12





Item
Unit
Example 86
Example 87


















R32
mass %
59.0
59.0


R1132a
mass %
9.0
11.0


R1234yf
mass %
32.0
30.0


GWP

400
400


COP ratio
% (relative to
100
99



that of R410A)




Refrigerating capacity ratio
% (relative to
104
106



that of R410A)




Compressor outlet pressure
% (relative to
103
106


ratio
that of R410A)




Condensation glide
° C.
4.5
4.8


Evaporation glide
° C.
4.1
4.5









As clear from the results in Table 231-1 to Table 231-12, it can be seen that the refrigerant 2D of the third aspect, when satisfies predetermined requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A, and has a GWP of 500 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less. It can be seen that the refrigerant 2D according to the fourth aspect, when satisfies predetermined requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A, and has a GWP of 400 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less. It can be seen that the refrigerant 2D according to the fifth aspect, when satisfies predetermined requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A, and has a GWP of 500 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less, and also has a condensation temperature glide and an evaporating temperature glide each being as low as 5° C. or less. It can also be seen that the refrigerant 2D according to the sixth aspect, when satisfies predetermined requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A, and has a GWP of 400 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less, and also has an evaporating temperature glide being as low as of 5° C. or less. It can also be seen that the refrigerant 2D according to the seventh aspect, when satisfies predetermined requirements, has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A (99% or more relative to that of R410A), and has a GWP of 400 or less, and a compressor outlet pressure based on that of R410A, of 1.25 times or less, and also has an evaporating temperature glide being as low as 5° C. or less. The refrigerants D according to the third aspect to the seventh aspect are each suitable as an alternative refrigerant of R410A, and in particular, the refrigerant 2D according to the fifth aspect or the sixth aspect, which is low in condensation temperature glide and/or evaporating temperature glide, is particularly suitable as an alternative refrigerant of R410A. Furthermore, the refrigerant 2D according to the seventh aspect, which is low in condensation temperature glide and/or evaporating temperature glide and which has any coefficient of performance (COP) and refrigerating capacity (Cap) equivalent to or more than those of R410A (99% or more relative to that of R410A), is further excellent as an alternative refrigerant of R410A.


(1-6-5) Refrigerant 2E


The refrigerant 2E of the present disclosure is a mixed refrigerant including R32, CO2, R125, R134a and R1234yf.


The refrigerant 2E of the present disclosure has various characteristics usually demanded for an alternative refrigerant of R410A, of (1) a GWP of 750 or less, (2) WCF non-flammability or ASHRAE non-flammability, and (3) a COP and refrigerating capacity equivalent to those of R410A.


The refrigerant 2E of the present disclosure has not only the above, but also a temperature glide, and thus is used in a refrigerator having a heat exchanger with the flow of a refrigerant being opposite to the flow of an external heat medium, to thereby exert the effect of improving the energy efficiency and/or refrigerating capacity.


The refrigerant 2E of the present disclosure, when satisfies the following requirements 1-1-1 to 1-3-2, is preferable because of having a GWP of 750 or less and WCF non-flammability. Hereinafter, the mass % of R32 is defined as a, the mass % of CO2 is defined as b, the mass % of R125 is defined as c1, the mass % of R134a is defined as c2, the mass % of the total of R125 and R134a is defined as c and the mass % of R1234yf is defined as x, and c1/(c1+c2) is defined as r based on the sum of R32, CO2, R125, R134a and R1234yf.


Coordinates (a,b,c) in a three-component composition diagram with, as respective apexes, a point where R32 occupies (100−x) mass %, a point where CO2 occupies (100−x) mass % and a point where the total of R125 and R134a occupies (100−x) mass % are:


Requirement 1-1-1)






    • with 43.8≥x≥41 and 0.5≥r≥0.25,


      within the range of a quadrangle surrounded by line segments that connect:

    • point A (−0.6902x+43.307, 100−a−x, 0.0),

    • point Or=0.25 to 0.5((−2.2857x+87.314)r2+(1.7143x−55.886)r+(−0.9643x+55.336), (2.2857x−112.91)r2+(−1.7143 x+104.69)r+(−0.25x+11.05), 100−a−b−x),

    • point Dr=0.25 to 0.5 (0.0, 28.8r2+54.0r+(−x+49.9), 100−b−x) and

    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.25 to 0.5Q and QA is excluded), or 1-1-2)

    • with 43.8≥x≥41 and 1.0≥r≥0.5,


      within the range of a quadrangle surrounded by line segments that connect:

    • point A (−0.6902x+43.307, 100−a−c, 0.0),

    • point Or=0.5 to 1.0((−0.2857x+8.5143)r2+(0.5x−10.9)+(−0.8571x+52.543), (−0.2857x+4.5143)r2+(0.5x+0.9)r+(−0.7143x+33.586), 100−a−b−x),

    • point Dr=0.5 to 1.0 (0.0, (−0.5714x+12.229)r2+(0.8571x−0.3429)r+(−1.2857x+66.814), 100−b−x) and

    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.5 to 1.0Q and QA is excluded), or 1-2-1)

    • with 46.5≥x≥43.8 and 0.5≥r≥0.25,


      within the range of a quadrangle surrounded by line segments that connect:

    • point A (−0.6902x+43.307, 100−a−x, 0.0),

    • point Or=0.25 to 0.5 ((1.1852x−64.711)r2+(−0.7407x+51.644)r+(=0.5556x+37.433), (−2.3704x+91.022)r2+(2.0741 x−61.244)r+(−0.963x+42.278), 100−a−b−x),

    • point to Dr=0.25 to 0.5 (0.0, 28.8r2+54.0r+(−x+49.9), 100−b−x) and

    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.25 to 0.5Q and QA is excluded), or Requirement 1-2-2)

    • with 46.5≥x≥43 and 1.0≥r≥0.5,


      within the range of a quadrangle surrounded by line segments that connect:

    • point A (−0.6902x+43.307, 100−a−x, 0.0),

    • point Or=0.5 to 1.0 ((0.2963x−16.978)r2+(−0.3704x+27.222)r+(−0.5185x+37.711), −8.0r2+22.8r+(−0.5185x+25.011), 100−a−b−x),

    • point Dr=0.5 to 1.0 (0.0, 12.8r2+37.2r+(−x+54.3), 100−b−x) and

    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.5 to 1.0Q and QA is excluded), or Requirement 1-3.1)

    • with 50≥x≥46.5 and 0.5≥r≥0.25,


      within the range of a quadrangle surrounded by line segments that connect:

    • point A (−0.6902x+43.307, 100−a−x, 0.0),

    • point Or=0.25 to 0.5 (−9.6r2+17.21+(−0.6571x+42.157); 19.2r2+(0.2286x+24.571)r+(−0.6286x+26.729), 100−a−b−x),

    • point Dr=0.25 to 0.5(0.0, (0.9143x−71.314)r2+(−0.5714x+80.571)+(−0.9143x+45.914), 100−b−x) and

    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.25 to 0.5Q and QA is excluded), or 1-3-2)

    • with 50≥x≥46.5 and 1.0≥r≥0.5,


      within the range of a quadrangle surrounded by line segments that connect:

    • point A (−0.6902x+43.307, 100−a−x, 0.0),

    • point Or=0.5 to 1.0 ((−0.2286x+7.4286)r2+(0.4x−8.6)r+(−0.8x+50.8), (0.2286x−18.629)r2+(−0.2857x+36.086)r+(−0.4286x+20.829), 100−a−b−x),

    • point Dr=0.5 to 1.0(0.0, (0.2286x−23.429)x2+(−0.4x+55.8)r+(−0.8286x+46.329), 100−b−x) and

    • point Q (0.0, 100−x, 0.0)


      or on the line segments (provided that any point on line segments Dr=0.5 to 1.0Q and QA is excluded).





The refrigerant 2E of the present disclosure, when satisfies the following requirements 2-1-1 to 2-3-2, is preferable because of having a GWP of 750 or less and ASHRAE non-flammability.


The above coordinates are


Requirement 2-1-1)






    • with 43.8≥x≥41 and 0.5≥r≥0.25,


      within the range of a triangle surrounded by line segments that connect:

    • point Fr=0.25 to 0.5 (0.0, (−1.1429x+37.257)r2+(1.2857x−38.714)r-(−1.7143x+106.89), 100−b−x),

    • point Pr=0.25 to 0.5 ((−1.1429x+34.057)r2+(1.0x−21.0)r+(−0.4643x+27.636), (2.2857x−119.31)r2+(−2.0x+122.0)x+(−0.3929x+19.907), 100−a−b−x) and

    • point Dr=0.25 to 0.5 (0.0, 28.8x2+54.0r+(−x+49.9), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.25 to 0.5Fr=0.25 to 0.5 is excluded), or 2-1-2) with 43.8≥x≥41 and 1.0≥r≥0.5,


      within the range of a triangle surrounded by line segments that connect:

    • point Fr=0.5 to 1.0 (0.0, (3.7143x−159.49)r2+(−5.0714x+222.53)r+(0.25x+25.45), 100−b−x),

    • point Pr=0.5 to 1.0((3.4286x−138.17)r2+(−5.4286x+203.57)+(1.6071 x−41.593), (−2.8571x+106.74)r2+(4.5714x−143.63)r+(−2.3929x+96.027), 100−a−b−x) and

    • point Dr=0.5 to 1.0(0.0, (−0.5714x+12.229)r2+(0.8571x−0.3429)r+(−1.2857x+66.814), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.5 to 1.0Fr=0.5 to 1.0 is excluded), or 2-2-1) with 46.5≥x≥43 and 0.5≥r≥0.25,


      within the range of a triangle surrounded by line segments that connect:

    • point Fr=0.25 to 0.5 (0.0, (9.4815x−428.09)r2+(−7.1111 x+329.07)r+(−0.2593x+43.156), 100−b−x),

    • point Pr=0.25 to 0.5 ((−8.2963x+347.38)r2+(4.8889x−191.33)r+(−0.963x+49.478), (7.1111x−330.67)r2+(−4.1481x+216.09)r+(−0.2593x+14.056), 100−a−b−x) and

    • point Dr=0.25 to 0.5 (0.0, −28.8r2+54.0r+(−x+49.9), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.25 to 0.5Fr=0.25 to 0.5 is excluded), or 2-2-2) with 46.5≥x≥43 and 1.0≥r≥0.5,


      within the range of a triangle surrounded by line segments that connect:

    • point Fr=0.25 to 0.37(0.0, (−4.7407x+210.84)r2+(6.963x−304.58)r+(−3.7407x+200.24), 100−b−x),

    • point Pr=0.25 to 0.37 ((0.2963x−0.9778)r2+(0.2222x−43.933)r+(0.7778x+62.867), (0.2963x−5.4222)r2+(−0.0741x+59.844)r+(−0.4444x+10.867), 100−a−b−x) and

    • point Dr=0.5 to 1.0(0.0; −12.8r2+37.2r+(−x+54.3), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.5 to 1.0Fr=0.5 to 1.0 is excluded), or 2-3-1) with 50≥x≥46.5 and 0.37≥r≥0.25,


      within the range of a triangle surrounded by line segments that connect:

    • point Fr=0.25 to 0.37(0.0, (−35.714x+1744.0)r2+(23.333x−1128.3)r+(−5.144x+276.32), 100−b−x),

    • point Pr=0.25 to 0.37((11.905x−595.24)r2+(−7.6189x+392.61)r+(0.9322x−39.027), (−27.778x+1305.6)r2+(17.46x−796.35)r+(−3.5147x+166.48), 100−a−b−x) and

    • point Dr=0.25 to 0.37(0.0, (0.9143x−71.314)r2+(−0.5714x+80.571)+(−0.9143x+45.914), 100−b−x)


      or on the line segments (provided that any point on line segment Dr=0.25 to 0.37Fr=0.25 to 0.37 is excluded), or 2-3-2) with 50≥x≥46.5 and 1.0≥r≥0.5,


      within the range of a triangle surrounded by line segments that connect:

    • point Fr=0.5 to 1.0(0.0, (2.2857x−115.89)r2+(−3.0857x+162.69)r+(−0.3714x+43.571), 100−b−x),

    • point Pr=0.5 to 1.0((−3.2x+161.6)r2+(4.4571x−240.86)r+(−2.0857x+123.69), (2.5143x−136.11)r2+(−3.3714x+213.17)r+(0.5429x−35.043), 100−a−b−x) and

    • point Dr=0.5 to 1.0(0.0, (0.2286x−23.429)r2+(−0.4x+55.8)x+(−0.8286x+46.329), 100−b−x)


      or on the line segments (provided that any point on line segment. Dr=0.5 to 1.0Fr=0.5 to 1.0 is excluded).





The refrigerant 2E of the present disclosure may include not only R32, CO2, R125, R134a and R1234yf, but also still other additional refrigerant and/or unavoidable impurities, as long as the above characteristics and/or effects are not impaired. The refrigerant 2E of the present disclosure here preferably includes 99.5 mass % or more in total of R32, CO2, R125, R134a and R1234yf based on the entire refrigerant 2E. The total content of such additional refrigerant and unavoidable impurities is here 0.5 mass % or less based on the entire refrigerant 2E. The refrigerant 2E more preferably includes 99.75 mass % or more, further preferably 99.9 mass % or more in total of R32, CO2, R125, R134a and R1234yf based on the entire refrigerant 2E.


The additional refrigerant is not limited, and can be widely selected. The additional refrigerant may be included singly or in combinations of two or more kinds thereof in the mixed refrigerant.


Examples of Refrigerant 2E

Hereinafter, the refrigerant 2E will be described with reference to Examples in more detail. It is noted that the present disclosure is not limited to such Examples.


1. Calculation of WCF non-flammability limit and ASHRAE non-flammability limit (WCF & WCFF non-flammability)


The composition of a mixed refrigerant consisting only of R32, CO2, R125, R134a and R1234yf is represented by as follows. That is, in a case where the mass % of R32 is defined as a, the mass % of CO2 is defined as b, the mass % of R125 is defined as c1, the mass % of R134a is defined as c2, the mass % of the total of R125 and R134a is defined as c and the mass % of R1234yf is defined as x, and c1/(c1+c2) is defined as r based on the sum of R32, CO2, R125, R134a and R1234yf in the refrigerant, the composition of the mixed refrigerant is specified by coordinates (a,b,c) in a three-component composition diagram with, as respective apexes, a point where R32 occupies (100−x) mass %, a point where CO2 occupies (100−x) mass % and a point where the total of R125 and R134a occupies (100−x) mass %.


Hereinafter, the method for specifying the WCF non-flammability limit and the ASHRAE non-flammability limit in the case of x=41 mass % and r=0.25 will be described.


It is necessary for specifying the non-flammability limit in the three-component composition diagram to first determine the non-flammability limit of a binary mixed refrigerant of a flammable refrigerant (R32, 1234yf) and a non-flammable refrigerant (CO2, R134a, R125). Hereinafter, the method for determining the non-flammability limit of the binary mixed refrigerant is shown.


[1] Non-Flammability Limit of Binary Mixed Refrigerant of Flammable Refrigerant (R32, 1234yf) and Non-Flammable Refrigerant (CO2, R134a, R125)


The non-flammability limit of the binary mixed refrigerant was determined with a measurement apparatus (FIG. 2E) and a measurement method for the flammability test based on ASTM E681-2009.


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom. The test conditions were as follows.


<Test Conditions>


Test container: spherical container of 280 mm in diameter (internal volume: 12 L)


Test temperature: 60° C.±3° C.


Pressure: 101.3 kPa±0.7 kPa


Water content: 0.0088 g+0.0005 g per gram of dry air


Mixing ratio of binary refrigerant composition/air: ±0.2 vol. % by 1 vol. %


Mixing of binary refrigerant composition: ±0.1 mass %


Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer


Electrode interval: 6.4 mm (¼ inch)


Spark: 0.4 seconds±0.05 seconds


Criteria for determination:






    • A case where any flame was spread at more than 90 degrees around the ignition point: flammability (propagation)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)





Each combination of a flammable refrigerant and a non-flammable refrigerant 2 Described in Table 232 was subjected to the test. The non-flammable refrigerant was added to the flammable refrigerant in stages, and the flammability test was performed at each stage.


Consequently, no flame propagation was observed in a mixed refrigerant of a flammable refrigerant R32 and a non-flammable refrigerant R134a after the mass % of R32 reached 43.0 and the mass % of R134a reached 57.0, and such a composition here was defined as the non-flammability limit. Moreover, no flame propagation was observed: in a mixed refrigerant of a flammable refrigerant R32 and a non-flammable refrigerant R125 after the mass % of R32 reached 63.0 mass % and the mass % of R125 reached 37.0; in a mixed refrigerant of a flammable refrigerant R32 and a non-flammable refrigerant CO2 after the mass % of R32 reached 43.5 and the mass % of CO2 reached 56.5; in a mixed refrigerant of a flammable refrigerant 1234yf and a non-flammable refrigerant R134a after the mass % of 1234yf reached 62.0 and the mass % of R134a reached 38.0; in a mixed refrigerant of a flammable refrigerant 1234yf and a non-flammable refrigerant R125 after the mass % of 1234yf reached 79.0 and the mass % of R125 reached 21.0; and in a mixed refrigerant of a flammable refrigerant 1234yf and non-flammable refrigerant CO2 after the mass % of 1234yf reached 63.0 and the mass % of CO2 reached 37.0; and such each composition here was defined as the non-flammability limit. The results were summarized in Table 232.












TABLE 232







Flammable
Non-flammable



Item
refrigerant
refrigerant








Binary mixed refrigerant
R32
R134a



combination





Non-flammability limit
43.0
57.0



(weight %)





Binary mixed refrigerant
R32
R125



combination





Non-flammability limit
63.0
37.0



(weight %)





Binary mixed refrigerant
R32
CO2



combination





Non-flammability limit
43.5
56.5



(weight %)





Binary mixed refrigerant
1234yf
R134a



combination





Non-flammability limit
62.0
38.0



(weight %)





Binary mixed refrigerant
1234yf
R125



combination





Non-flammability limit
79.0
21.0



(weight %)





Binary mixed refrigerant
1234yf
CO2



combination





Non-flammability limit
63.0
37.0



(weight %)









Next, the non-flammability limit in the case of x==41 mass % and r=0.25 was determined as follows, based on the non-flammability limit of the binary mixed refrigerant 2 Determined in [1].


1) Point A (a,b,0) in case of x=41 mass %, x=0.25 and c=0 mass %


In the case of a+b=59 mass %, whether or not the mixed composition was non-flammability limit composition was examined by the following procedure.

    • (1) Flammable refrigerant concentration in terms of R32=R32 concentration+R1234yf concentration×((21/79)×(63/37)+(38/62)×(43/57))/2
    • (2) Non-flammable refrigerant concentration in terms of R32 R125 concentration×(63/37)+R134a concentration×(43/57)+CO2 concentration×(43.5/56.5)


The value where the value obtained by subtracting the flammable refrigerant composition in terms of R32 from the non-flammable refrigerant composition in terms of R32 exhibited the minimum value as a positive value was defined as the calculated non-flammability limit composition. The calculation results were shown in Table 233, and the point A (15.0, 44.0, 0) corresponded to the calculated non-flammability limit composition.

















TABLE 233











Flammable
Non-flammable









refrigerant
refrigerant
Non-








concentration
concentration
flammability-



R32
R125
R1234yf
R134a
CO2
in terms
in terms of
Flammability



(a)
(c1)
(x)
(c2)
(b)
of R32
R32
(positive:


Composition
weight
weight
weight
weight
weight
weight
weight
non-


example
%
%
%
%
%
%
%
flammability)























Flammability
15.10
0.00
41.00
0.00
43.90
33.86
33.80
−0.06


limit










Non-
15.00
0.00
41.00
0.00
44.00
33.76
33.88
0.12


flammability










limit









2) Point (a,30,c) in case of x=41 mass %, r=0.25 and b=30 mass %


In the case of a+c=29 mass %, the non-flammability limit composition was determined under those conditions by the same procedure as described above. The results are shown in Table 234.

















TABLE 234











Flammable
Non-flammable









refrigerant
refrigerant
Non-








concentration
concentration
flammability-



R32
R125
R1234yf
R134a
CO2
in terms
in terms of
Flammability



(a)
(c1)
(x)
(c2)
(b)
of R32
R32
(positive:


Composition
weight
weight
weight
weight
weight
weight
weight
non-


example
%
%
%
%
%
%
%
flammability)























Flammability
16.70
3.10
41.00
9.20
30.00
35.46
35.32
−0.14


limit










Non-
16.60
3.10
41.00
9.30
30.00
35.36
35.39
0.03


flammability










limit









3) Point (a,15,c) in case of x=41 mass %, r=0.25 and b=15 mass %


In the case of a+c=44 mass %, the non-flammability limit composition was determined under those conditions by the same procedure as described above. The results are shown in Table 235.

















TABLE 235











Flammable
Non-flammable









refrigerant
refrigerant
Non-








concentration
concentration
flammability-



R32
R125
R1234yf
R134a
CO2
in terms
in terms of
Flammability



(a)
(c1)
(x)
(c2)
(b)
of R32
R32
(positive:


Composition
weight
weight
weight
weight
weight
weight
weight
non-


example
%
%
%
%
%
%
%
flammability)























Flammability
18.30
6.40
41.00
19.30
15.00
37.06
37.01
−0.05


limit










Non-
18.20
6.50
41.00
19.30
15.00
36.96
37.18
0.22


flammability










limit









4) Point Br=0.25 (a,0,c) in case of x=41 mass %, r=0.25 and b=0 mass %


In the case of a+c=59 mass %, the non-flammability limit composition was determined under those conditions by the same procedure as described above. The results are shown in Table 236.

















TABLE 236











Flammable
Non-flammable









refrigerant
refrigerant
Non-








concentration
concentration
flammability-



R32
R125
R1234yf
R134a
CO2
in terms
in terms of
Flammability



(a)
(c1)
(x)
(c2)
(b)
of R32
R32
(positive:


Composition
weight
weight
weight
weight
weight
weight
weight
non-


example
%
%
%
%
%
%
%
flammability)























Flammability
20.00
9.80
41.00
29.20
0.00
38.76
38.71
−0.04


limit










Non-
19.90
9.80
41.00
29.30
0.00
38.66
38.79
0.13


flammability










limit









The results obtained by examining the above calculated non-flammability limit composition are illustrated in a three-component composition diagram of FIG. 2O. Such points are connected to thereby form ABr=0.25 in FIG. 2O.


[2] Verification according to flammability test, of WCF non-flammability limit point determined from non-flammability limit of binary mixed refrigerant obtained in [1]


The flammability test according to ASTM E681 represented in [1] was performed on the composition shown in Table 233:

    • Flammability limit composition-1-1) (R32/CO2/R125/R134a)=(15.1/43.9/0.0/0.0),
    • Non-flammability limit composition-1-2) (R32/CO2/R125/R134a)=(15.0/44.0/0.0/0.0); and the composition shown in Table 235:
    • Flammability limit composition-2-1) (R32/CO2/R125/R134a)=(18.3/15.0/6.4/19.3),
    • Non-flammability limit composition-2-2) (R32/CO2/R125/R134a)=(18.2/15.0/6.5/19.3);


      and thus flame propagation was observed in the case of the composition-1-1) and the composition-2-1) and no flame propagation was observed in the case of the composition 1-1-2) and the composition-2-2). Accordingly, it can be said that the non-flammability limit of the mixed refrigerant 2 Determined from the non-flammability limit of the binary mixed refrigerant, represents an actual non-flammability limit


The non-flammability limit composition of the mixed refrigerant 2 Determined from the non-flammability limit of the binary mixed refrigerant, is defined as the WCF non-flammability limit point. The WCF non-flammability limit point is on the line segment ABr=0.25 as illustrated in FIG. 2O, and thus the line segment ABr=0.25, determined from two points of the point A and the point Br=0.25, is defined as the WCF non-flammable border line.


On the other hand, the ASHRAE non-flammability (WCF non-flammability and WCFF non-flammability) means non-flammability at the most flammable composition (WCFF) under the worst conditions in a case where the leak test in storage/transport, the leak test from an apparatus, and the leak/repacking test are performed with reference to the most flammable composition (WCF) and the WCF composition of the mixed refrigerant. Hereinafter, the WCFF concentration was determined by performing leak simulation under various conditions with KIST Standard Reference Data Base Refleak Version 4.0 (hereinafter, sometimes designated as “Refleak”). Whether or not the WCFF composition determined corresponded to the non flammability limit was confirmed by the method for determining the non-flammability limit of the mixed refrigerant from the non-flammability limit of the binary mixed refrigerant, represented as the WCF non-flammability limit.


The method for determining the ASHRAE non-flammability limit in the case of x=41 mass % and r=0.25 is described below.


5) Point 1325(0.0,b,c(c1+c2)) in case of x=41 mass %, r=0.25 and a=0 mass %


The leak test in storage/transport, the leak test from an apparatus, and the leak/repacking test were performed at Refleak, and thus the leak conditions in storage/transport were most flammable conditions and the conditions of leak at −40° C. were most flammable conditions. Accordingly, the ASHRAE non-flammability limit was determined according to the following procedure, by performing the leak test at −40° C. in storage/transport with leak simulation at Refleak. Table 237 shows each typical value serving as the flammability/non-flammability limit in leak simulation. In a case where the initial composition corresponded to (0.0, 39.5, 19.5(4.9+14.6)), atmospheric pressure was achieved in a release of 52% at −40° C. under transport and storage conditions, the liquid side concentration here was indicated by (0.0, 2.5, 30.5(6.1+24.4)) at x=67.0 mass %, and the non-flammability determination described above was made as the limit leading to non-flammability in a condition of atmospheric pressure. On the other hand, in a case where the initial composition corresponded to (0.0, 39.6, 19.4(4.9+14.5)), atmospheric pressure was achieved in a release of 52% at −40° C., the liquid side concentration here was indicated by (0.0, 2.6, 30.3(6.1+24.2)) at x=67.1%, and the non-flammability determination described above was made as flammability. Accordingly, in a case where an initial composition of (0.0, 39.5, 19.5(4.9+14.6)) was defined as the WCF composition, both the WCF composition and the WCFF composition were rated as non-flammability in terms of calculation, and thus a value of (0.0, 39.5, 19.5(4.9+14.6)) corresponded to the ASHRAE non-flammability limit composition.

















TABLE 237











Flammable
Non-flammable









refrigerant
refrigerant
Non-








concentration
concentration
flammability-


Leak
R32
R125
R1234yf
R134a
CO2
in terms
in terms of
Flammability


simulation in
(a)
(c1)
(x)
(c2)
(b)
of R32
R32
(positive:


storage/
weight
weight
weight
weight
weight
weight
weight
non-


transport
%
%
%
%
%
%
%
flammability)























Initial
0.0
4.9
41.0
14.6
39.5
18.76
49.77
31.01


composition (1)










(=WCF)










Liquid side
0.0
6.1
67.0
24.4
2.5
30.65
30.72
0.07


composition in










release of 52%










at −40° C.










(atmospheric










pressure










achieved)










(=WCFF)










Liquid side
0.0
6.0
67.8
24.7
1.6
31.02
30.08
−0.94


composition in










release of 54%










at −40° C.










(atmospheric










pressure or less)










Initial
0.0
4.9
41.0
14.5
39.6
18.76
49.77
31.01


composition (2)










Liquid side
0.0
6.1
67.1
24.2
2.6
30.70
30.64
−0.05


composition in










release of 52%










at −40° C.










(atmospheric










pressure










achieved)










Liquid side
0.0
6.0
67.8
24.5
1.7
31.02
30.01
−1.01


composition in










release of 54%










at −40° C.










(atmospheric










pressure or less)









6) Point Pr=0.25(a, b, c(c1+c2)) in case of x=41 mass %, r=0.25, and GWP=750 at a mass %


A point where GWP=750 was achieved in a three-component composition diagram indicated by a+b+c=100−x=59 mass %, under conditions of X=41.0 mass % and r=0.25, was on the straight line Cr=0.25Dr=0.25 for connecting the point Cr=0.25 (31.6, 0.0, 27.4(6.9+20.5)) and the point Dr=0.25(0.0, 20.6, 38.4(9.6+28.8)), as illustrated in FIG. 2O, and the straight line was represented by c1=−0.085a+9.6. Pr=0.25(a, −0.085c1+9.6,c) where the ASHRAE non-flammability limit was achieved at a GWP of 750, was used for the initial composition and simulation was made at under storage/transport conditions at Refleak, and thus the ASHRAE non-flammability limit composition was determined as in Table 238.

















TABLE 238











Flammable
Non-flammable









refrigerant
refrigerant
Non-








concentration
concentration
flammability-


Leak
R32
R125
R1234yf
R134a
CO2
in terms
in terms of
Flammability


simulation in
(a)
(c1)
(x)
(c2)
(b)
of R32
R32
(positive:


storage/
weight
weight
weight
weight
weight
weight
weight
non-


transport
%
%
%
%
%
%
%
flammability)























Initial
12.8
8.5
41.0
25.5
12.2
31.56
43.10
11.55


composition (1)










(=WCF)










Gas side
21.8
12.4
40.1
20.6
5.1
40.15
40.58
0.44


composition in










release of 38%










at −40° C.










(atmospheric










pressure










achieved)










(=WCFF)










Gas side
21.3
12.4
41.1
21.4
3.8
40.10
40.18
0.08


composition in










release of 40%










at −40° C.










(atmospheric










pressure or less)










Initial
12.9
8.5
41.0
25.5
12.1
31.66
43.03
11.37


composition (2)










Gas side
21.4
12.4
41.1
21.3
3.8
40.20
40.11
−0.10


composition in










release of 38%










at −40° C.










(atmospheric










pressure










achieved)










Gas side
20.8
12.4
42.0
22.1
2.8
40.01
39.94
−0.07


composition in










release of 40%










at −40° C.










(atmospheric










pressure or less)









7) Point (a, b, c(c1+c2)) in case of x=41 mass %, %0.25, and a=10.0 mass %


The results obtained by examining in the same manner as described above are shown in Table

















TABLE 239











Flammable
Non-flammable









refrigerant
refrigerant
Non-








concentration
concentration
flammability-


Leak
R32
R125
R1234yf
R134a
CO2
in terms
in terms of
Flammability


simulation in
(a)
(c1)
(x)
(c2)
(b)
of R32
R32
(positive:


storage/
weight
weight
weight
weight
weight
weight
weight
non-


transport
%
%
%
%
%
%
%
flammability)























Initial
10.0
7.0
41.0
20.8
21.2
28.76
43.93
15.18


composition (1)










(=WCF)










Gas side
18.3
11.2
44.6
19.5
6.4
38.70
38.71
0.004


composition in










release of 46%










at −40° C.










(atmospheric










pressure










achieved)










(=WCFF)










Gas side
17.7
11.3
46.1
20.4
4.6
38.79
38.17
−0.62


composition in










release of 48%










at −40° C.










(atmospheric










pressure or less)










Initial
10.0
6.9
41.0
20.8
21.3
28.76
43.84
15.08


composition (2)










Gas side
18.3
11.1
44.6
19.5
6.5
38.70
38.61
−0.09


composition in










release of 46%










at −40° C.










(atmospheric










pressure










achieved)










Gas side
17.1
11.1
46.1
20.4
4.6
38.19
37.83
−0.36


composition in










release of 48%










at −40° C.










(atmospheric










pressure or less)









8) Point (a, b, c(c1+c2)) in case of x=41 mass %, r=0.25, and a=5.8 mass %


The results obtained by examining in the same manner as described above are shown in Table 240.

















TABLE 240











Flammable
Non-flammable









refrigerant
refrigerant
Non-








concentration
concentration
flammability-


Leak
R32
R125
R1234yf
R134a
CO2
in terms
in terms of
Flammability


simulation in
(a)
(c1)
(x)
(c2)
(b)
of R32
R32
(positive:


storage/
weight
weight
weight
weight
weight
weight
weight
non-


transport
%
%
%
%
%
%
%
flammability)























Initial
5.8
5.8
41.0
17.4
30.0
24.56
46.10
21.54


composition (1)










(=WCF)










Liquid side
4.1
6.4
61.2
27.2
1.1
32.10
32.26
0.165


composition in










release of 50%










at −40° C.










(atmospheric










pressure










achieved)










(=WCFF)










Liquid side
3.8
6.2
61.7
27.5
0.8
32.03
31.92
−0.11


composition in










release of 52%










at −40° C.










(atmospheric










pressure or less)










Initial
5.8
5.8
41.0
17.3
30.1
24.56
46.10
21.54


composition (2)










Liquid side
4.1
6.4
61.4
27.0
1.1
32.19
32.11
−0.08


composition in










release of 50%










at −40° C.










(atmospheric










pressure










achieved)










Liquid side
3.8
6.2
61.9
27.5
0.6
32.12
31.76
−0.35


composition in










release of 52%










at −40° C.










(atmospheric










pressure or less)









[2] Verification according to flammability test, of ASHRAE non-flammability limit point determined from non-flammability limit of binary mixed refrigerant obtained as described above


The flammability test according to ASTM E681 represented in [1] was performed on the composition described below, and thus no flame propagation was observed in the case of the composition-3-1), the composition-4-1), and the composition-5-1), and flame propagation was observed in the case of the composition-3-2), the composition-4-2), and the composition-5-2). Accordingly, it can be said that the ASHRAE non-flammability limit represented by each calculation in Tables 237, 238 and 239 represents an actual non-flammability limit Composition 3-1)


Liquid side composition in a release of 52% at −40° C.: (R32/CO2/R125/R134a)=(0.0/39.5/4.9/14.6) at x=41.0 mass % of R1234yf, (R32/CO2/R125/R134a)=(0.0/2.5/6:1/24.4) at x=67.0% Composition 3-2)


Liquid side composition in a release of 52% at −40° C.: (R32/CO2/R125/R134a)=(0.0/39.6/4.9/14.5) at x=41.0 mass % of R1234yf (R32/CO2/R125/R134a)=(0.0/2.6/6:1/242) at x=67.1% Composition 4-1)


Gas side composition in a release of 38% at −40° C.: (R32/CO2/R125/R134a)=(12.8/12.2/8.5/25.5) at x==41.0 mass % of R1234yf (R32/CO2/R125/R134a)=(21.8/5.1/12.4/20.6) at x=40.1%, Composition 4-2)


Gas side composition in a release of 38% at −40° C.: (R32/CO2/R125/R134a)=(12.9/12.1/8.5/25.5) at x=41.0 mass % of R1234yf (R32/CO2/R125/R134a)=(21.4/3.8/12.4/21.3) at x=41.1%, Composition 5-1)


Liquid side composition in a release of 50% at −40° C.: (R32/CO2/R125/R134a)=(5.8/30.0/5.8/17.4) at x=41.0 mass % of R1234yf, (R32/CO2/R125/R134a) 4.1/1.1/6.4/27.2) at x=61.2%, Composition 5-2)


Liquid side composition in a release of 50% at −40° C.: (R32/CO2/R125/R134a)=(5.8/30.1/5.8/17.3) at x=41.0 mass % of R1234y f (R32/CO2/R125/R134a)=(4.1/1.1/6.4/27.0) at x=61.4%.



FIG. 2O illustrates each ASHRAE non-flammability limit point shown in Tables 237, 238, 239 and 40, and the straight line Fr=0.25Pr=0.25 that connects point Fr=0.25 and the point Pr=0.25. Such each ASHRAE non-flammability limit point is located closer to the flammable refrigerant R32 with respect to the straight line Fr=0.25Pr=0.25, as illustrated in FIG. 2O, and here the straight line Fr=0.25Pr=0.25, obtained by determining the point Fr=0.25 and the point P=0.25, is here defined as the ASHRAE non flammable border line also in consideration of safety rate.


The WCF non-flammable border line, determined from the non-flammability limit of the binary mixed refrigerant, and the ASHRAE non-flammable border line, determined from the non-flammability limit of the binary mixed refrigerant based on the WCFF composition of determined from leak simulation at Refleak are each matched with an actual non-flammable border line, and, hereinafter, each non-flammability limit is determined according to the above method, the line segment ABr is defined as the WCF non-flammable border line and the line segment FrPr is defined as the ASHRAE non-flammable border line.


Table 241 to Table 244 each show the WCF non-flammability limit point of the mixed refrigerant 2 Determined from the non-flammability limit of the binary mixed refrigerant, and Table 245 to Table 248 each show the ASHRAE non-flammability limit point, determined from the leak simulation and the non-flammability limit of the binary mixed refrigerant

















TABLE 241










Comparative
Comparative
Comparative
Comparative
Comparative
Comparative





Example 2
Example 3
Example 7
Example 11
Example 15
Example 19














Item
Unit
A
Br = 0.25
Br = 0.375
Br = 0.5
Br = 0.75
Br = 1.0


















WCF
R32
mass %
15.0
19.9
22.1
24.1
27.4
30.2


concentrations
CO2
mass %
44.0
0.0
0.0
0.0
0.0
0.0



R125
mass %
0.0
9.8
13.8
17.5
23.7
28.8



R134a
mass %
0.0
29.3
23.1
17.4
7.9
0.0



R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0













Non-flammability determination
Non-
Non-
Non-
Non-
Non-
Non-


















flammability
flammability
flammability
flammability
flammability
flammability
























TABLE 242










Comparative
Comparative
Comparative
Comparative
Comparative
Comparative





Example 23
Example 24
Example 28
Example 32
Example 36
Example 40














Item
Unit
A
Br = 0.25
Br = 0.375
Br = 0.5
Br = 0.75
Br = 1.0


















WCF
R32
mass %
13.1
17.9
20.0
21.9
25.2
27.9


concentrations
CO2
mass %
43.1
0.0
0.0
0.0
0.0
0.0



R125
mass %
0.0
9.6
13.6
17.2
23.3
28.3



R134a
mass %
0.0
28.7
22.6
17.1
7.7
0.0



R1234yf
mass %
43.8
43.8
43.8
43.8
43.8
43.8













Non-flammability determination
Non-
Non-
Non-
Non-
Non-
Non-


















flamma-
flamma-
flamma-
flamma-
flamma-
flamma-





bility
bility
bility
bility
bility
bility


























TABLE 243










Compar-
Compar-
Compar-
Compar-
Compar-
Compar-
Compar-
Compar-





ative
ative
ative
ative
ative
ative
ative
ative





Example
Example
Example
Example
Example
Example
Example
Example





44
45
49
53
57
61
65
69
















Item
Unit
A
Br = 0.25
Br = 0.375
Br = 0.5
Br = 0.75
Br = 1.0
Br = 0.31
Br = 0.37




















WCF
R32
mass %
11.2
15.9
16.9
17.9
18.0
19.9
23.1
25.8


concentrations
CO2
mass %
42.3
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R125
mass %
0.0
9.4
11.3
13.2
13.3
16.8
22.8
27.7



R134a
mass %
0.0
28.2
25.3
22.4
22.2
16.8
7.6
0.0



R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5
46.5
46.5















Non-flammability determination
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-




















flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-





bility
bility
bility
bility
bility
bility
bility
bility


























TABLE 244










Compar-
Compar-
Compar-
Compar-
Compar-
Compar-
Compar-
Compar-





ative
ative
ative
ative
ative
ative
ative
ative





Example
Example
Example
Example
Example
Example
Example
Example





73
74
78
82
86
90
94
98
















Item
Unit
A
Br = 0.25
Br = 0.375
Br = 0.5
Br = 0.75
Br = 1.0
Br = 0.31
Br = 0.37




















WCF
R32
mass %
8.8
13.4
14.4
15.3
15.4
17.3
20.4
23.0


concentrations
CO2
mass %
41.2
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R125
mass %
0.0
9.2
11.0
12.8
13.0
16.4
22.2
27.0



R134a
mass %
0.0
27.4
24.6
21.9
21.6
16.3
7.4
0.0



R1234yf
mass %
50.0
50.0
50.0
50.0
50.0
50.0
50.0
50.0















Non-flammability determination
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-




















flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-





bility
bility
bility
bility
bility
bility
bility
bility




























TABLE 245










Compar-

Compar-

Compar-

Compar-

Compar-






ative

ative

ative

ative

ative






Example
Example
Example
Example
Example
Example
Example
Example
Example
Example





6
2
10
4
14
6
18
8
22
10


















Item
Unit
Fr = 0.25
Pr = 0.25
Fr = 0.375
Pr = 0.375
Fr = 0.5
Pr = 0.5
Fr = 0.75
Pr = 0.75
Fr = 1.0
Pr = 1.0






















WCF
R32
mass %
0.0
12.8
0.0
14.3
0.0
15.4
0.0
11.4
0.0
7.7


concen-
CO2
mass %
39.5
12.2
40.5
15.2
41.2
17.4
42.6
25.1
43.1
31.5


trations
R125
mass %
4.9
8.5
6.9
11.1
8.9
13.1
12.3
16.9
15.9
19.8



R134a
mass %
14.6
25.5
11.6
18.4
8.9
13.1
4.1
5.6
0.0
0.0



R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0

















Non-flammability
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-


determination
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-






















bility
bility
bility
bility
bility
bility
bility
bility
bility
bility

















Leak conditions leading to
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/


WCFF
transport,
transport,
transport,
transport,
transport,
transport,
transport,
transport,
transport,
transport,






















−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.





52%
38%
54%
48%
56%
56%
58%
62%
62%
64%





leak,
leak,
leak,
leak,
leak,
leak,
leak,
leak,
leak,
leak,





liquid
gas
liquid
gas
liquid
gas
liquid
liquid
liquid
liquid





phase
phase
phase
phase
phase
phase
phase
phase
phase
phase


WCFF
R32
mass %
0.0
21.8
0.0
22.1
0.0
21.5
0.0
16.2
0.0
12.1


concen-
CO2
mass %
2.5
5.1
2.3
2.6
1.9
1.3
2.0
1.5
1.2
2.6


trations
R125
mass %
6.1
12.4
8.7
16.0
11.3
18.7
16.2
26.3
20.5
33.7



R134a
mass %
24.4
20.6
19.9
16.6
15.7
13.2
7.5
6.5
0.0
0.0



R1234yf
mass %
67.0
40.1
69.1
42.7
71.1
45.3
74.3
49.5
78.3
51.6

















Non-flammability
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-


determination
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-






















bility
bility
bility
bility
bility
bility
bility
bility
bility
bility




























TABLE 246










Compar-

Compar-

Compar-

Compar-

Compar-






ative

ative

ative

ative

ative






Example
Example
Example
Example
Example
Example
Example
Example
Example
Example





27
12
31
14
35
16
39
18
43
20


















Item
Unit
Fr = 0.25
Pr = 0.25
Fr = 0.375
Pr = 0.375
Fr = 0.5
Pr = 0.5
Fr = 0.75
Pr = 0.75
Fr = 1.0
Pr = 1.0






















WCF
R32
mass %
0.0
12.0
0.0
13.6
0.0
14.7
0.0
9.9
0.0
6.6


concen-
CO2
mass %
35.4
10.1
36.6
12.9
37.4
15.1
38.5
23.5
40.0
29.6


trations
R125
mass %
5.2
8.5
7.4
11.2
9.4
13.2
13.3
17.1
16.2
20.0



R134a
mass %
15.6
25.6
12.2
18.5
9.4
13.2
4.4
5.7
0.0
0.0



R1234yf
mass %
43.8
43.8
43.8
43.8
43.8
43.8
43.8
43.8
43.8
43.8

















Non-flammability
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-


determination
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-






















bility
bility
bility
bility
bility
bility
bility
bility
bility
bility

















Leak conditions leading to
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/


WCFF
transport,
transport,
transport,
transport,
transport,
transport,
transport,
transport,
transport,
transport,






















−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.





48%
36%
50%
44%
52%
52%
56%
56%
58%
60%





leak,
leak,
leak,
leak,
leak,
leak,
leak,
leak,
leak,
leak,





liquid
gas
liquid
gas
liquid
gas
liquid
liquid
liquid
liquid





phase
phase
phase
phase
phase
phase
phase
phase
phase
phase


WCFF
R32
mass %
0.0
20.5
0.0
21.5
0.0
21.1
0.0
5.4
0.0
3.5


concen-
CO2
mass %
2.4
4.3
2.3
3.0
2.1
1.6
1.4
0.4
1.5
0.4


trations
R125
mass %
6.2
12.3
8.9
16.0
11.4
18.7
16.2
17.4
20.3
21.8



R134a
mass %
24.3
20.7
19.6
15.9
15.4
12.6
7.6
9.3
0.0
0.0



R1234yf
mass %
67.1
42.2
69.2
43.6
71.1
46.0
74.8
67.5
78.2
74.3

















Non-flammability
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-
Non-


determination
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-






















bility
bility
bility
bility
bility
bility
bility
bility
bility
bility

























TABLE 247










Comparative

Comparative

Comparative

Comparative





Example

Example

Example

Example





48
Example 22
52
Example 24
56
Example 26
60















Item
Unit
Fr = 0.25
Pr = 0.25
Fr = 0.375
Pr = 0.375
Fr = 0.5
Pr = 0.5
Fr = 0.75



















WCF
R32
mass %
0.0
11.3
0.0
12.8
0.0
13.1
0.0


concentrations
CO2
mass %
31.5
7.8
32.3
10.7
33.5
13.6
35.3



R125
mass %
5.5
8.6
8.2
11.3
10.0
13.4
13.7



R134a
mass %
16.5
25.8
13.0
18.7
10.0
13.4
4.5



R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5
46.5














Non-flammability
Non-
Non-
Non-
Non-
Non-
Non-
Non-


determination
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-



bility
bility
bility
bility
bility
bility
bility


Leak conditions
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/


leading to WCFF
transport,
transport,
transport,
transport,
transport,
transport,
transport,



















−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.





44%
32%
46%
40%
48%
48%
52%





leak, liquid
leak, gas
leak, liquid
leak, gas
leak, liquid
leak, liquid
leak, liquid





phase
phase
phase
phase
phase
phase
phase


WCFF
R32
mass %
0.0
19.7
0.0
20.8
0.0
7.1
0.0


concentrations
CO2
mass %
2.5
4.5
2.2
3.4
2.1
0.3
1.7



R125
mass %
6.2
12.4
9.4
15.9
11.6
12.2
16.2



R134a
mass %
24.2
20.2
19.5
15.5
15.4
19.0
7.3



R1234yf
mass %
67.1
43.2
68.9
44.4
70.9
61.4
74.8














Non-flammability
Non-
Non-
Non-
Non-
Non-
Non-
Non-


determination
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-



bility
bility
bility
bility
bility
bility
bility























Compar-

Compar-

Compar-






Example
ative
Example
ative
Example
ative
Example





28
Example 64
30
Example 68
32
Example 72
34















Item
Unit
Pr = 0.75
Fr = 1.0
Pr = 1.0
Fr = 0.31
Pr = 0.31
Fr = 0.37
Pr = 0.37



















WCF
R32
mass %
8.7
0.0
5.9
0.0
12.2
0.0
12.8


concentrations
CO2
mass %
21.7
35.9
27.4
31.7
9.2
32.5
10.7



R125
mass %
17.3
17.6
20.2
6.8
10.0
7.8
11.1



R134a
mass %
5.8
0.0
0.0
15.0
22.1
13.2
18.9



R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5
46.5














Non-flammability
Non-
Non-
Non-
Non-
Non-
Non-
Non-


determination
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-



bility
bility
bility
bility
bility
bility
bility


Leak conditions
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/


leading to WCFF
transport,
transport,
transport,
transport,
transport,
transport,
transport,



















−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.
−40° C.





52%
54%
56%
44%
36%
46%
40%





leak, liquid
leak, liquid
leak, liquid
leak, liquid
leak, gas
leak, liquid
leak, gas





phase
phase
phase
phase
phase
phase
phase


WCFF
R32
mass %
4.9
0.0
3.2
0.0
20.5
0.0
20.8


concentrations
CO2
mass %
0.5
1.6
0.6
1.9
3.9
2,3
3.3



R125
mass %
17.4
21.1
21.7
7.6
14.2
9.0
15.7



R134a
mass %
8.9
0.0
0.0
22.3
17.7
19.8
15.7



R1234yf
mass %
68.3
77.3
74.5
68.2
43.7
68.9
44.5














Non-flammability
Non-
Non-
Non-
Non-
Non-
Non-
Non-


determination
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-
flamma-



bility
bility
bility
bility
bility
bility
bility
























TABLE 248









Comparative

Comparative

Comparative

Comparative




Example

Example

Example

Example




77
Example 36
81
Example 38
85
Example 40
89


Item
Unit
Fr=0.25
Pr=0.25
Fr=0.375
Pr=0.375
Fr=0.5
Pr=0.5
Fr=0.75



















WCF
R32
mass
0.0
10.5
0.0
11.9
0.0
10.8
0.0


concentrations

%










CO2
mass
26.1
4.7
27.6
8.0
28.8
11.8
30.4




%










R125
mass
6.0
8.7
8.5
11.3
10.6
13.7
14.7




%










R134a
mass
17.9
26.1
13.9
18.8
10.6
13.7
4.9




%










R1234yf
mass
50.0
50.0
50.0
50.0
50.0
50.0
50.0




%





















Non-flammability determination
Non-
Non-
Non-
Non-
Non-
Non-
Non-



flammability
flammability
flammability
flammability
flammability
flammability
flammability


Leak conditions leading to WCFF
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/



















transport,
transport,
transport,
transport,
transport,
transport,
transport,





−40° C., 40%
−40° C., 32%
−40° C., 42%
−40° C., 36%
40° C., 44%
−40° C., 42%
−40° C., 48%





leak, liquid
leak, gas
leak, liquid
leak, gas
leak, liquid
leak, liquid
leak, liquid





phase
phase
phase
phase
phase
phase
phase


WCFF
R32
mass
0
17.3
0
19.7
0
6.1
0


concentrations

%










CO2
mass
2
2.4
1.9
3.2
1.8
0.4
1.5




%










R125
mass
6.4
12.3
9.2
15.9
11.6
12.4
16.2




%










R134a
mass
24.4
21.3
19.5
15.1
15.3
18.2
7.4




%










R1234yf
mass
67.2
46.7
69.4
46.1
71.3
62.9
74.9




%





















Non-flammability determination
Non-
Non-
Non-
Non-
Non-
Non-
Non-



flammability
flammability
flammability
flammability
flammability
flammability
flammability























Comparative

Comparative

Comparative







Example

Example

Example






Example 42
93
Example 44
97
Example 46
101
Example 48















Item
Unit
Pr=0.75
Fr=1.0
Pr=1.0
Fr=0.31
Pr=0.31
Fr=0.37
Pr=0.37



















WCF
R32
mass
7.3
0.0
3.9
0.0
11.2
0.0
11.9


concentrations

%










CO2
mass
19.3
31.8
25.5
27.0
6.5
27.6
7.7




%










R125
mass
17.6
18.2
20.6
7.3
10.0
8.5
11.2




%










R134a
mass
5.8
0.0
0.0
15.7
22.3
13.9
19.2




%










R1234yf
mass
50.0
50.0
50.0
50.0
50.0
50.0
50.0




%





















Non-flammability determination
Non-
Non-
Non-
Non-
Non-
Non-
Non-



















flammability
flammability
flammability
flammability
flammability
flammability
flammability














Leak conditions leading to WCFF
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/



















transport,
transport,
transport,
transport,
transport,
transport,
transport,





−40° C., 48%
−40° C., 50%
−40° C., 52%
−40°C, 40%
−40° C., 38%
−40° C., 42%
−40° C., 34%





leak, liquid
leak, liquid
leak, liquid
leak, liquid
leak, gas
leak, liquid
leak, gas





phase
phase
phase
phase
phase
phase
phase


WCFF
R32
mass
4
0
2.1
0
17.2
0
20.2


concentrations

%










CO2
mass
0.5
1.6
0.7
2.3
1.7
1.9
3.9




%










R125
mass
17.2
20.7
21.5
7.9
14
9.2
15.7




%










R134a
mass
8.4
0
0
21.7
19
19.5
15




%










R1234yf
mass
69.9
77.7
75.7
68.2
48.1
69.4
45.2




%





















Non-flammability determination
Non-
Non-
Non-
Non-
Non-
Non-
Non-



flammability
flammability
flammability
flammability
flammability
flammability
flammability









Examples 1 to 222 and Comparative Examples 1 to 206

The respective GWPs of R410A, and a composition including a mixture of R32, R125, R1234yf, R134a and CO2 were evaluated based on the value in the fourth report of IPCC (Intergovernmental Panel on Climate Change). The respective refrigerating capacities of R410A, and the composition including a mixture of R32, R125, R1234yf, R134a and CO2 were determined by performing theoretical refrigeration cycle calculation with respect to each mixed refrigerant under the following conditions by using National Institute of Science and Technology (MIST) Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


Evaporating temperature −10° C.


Condensation temperature 45° C.


Superheating temperature 20 K


Subcooling temperature 5 K


Compressor efficiency 70%


The GWP, the COP and the refrigerating capacity, calculated based on the results, are shown in Tables 249 to 280. The COP and the refrigerating capacity are each represented as the proportion relative to that of R410A.


The coefficient of performance (COP) was determined according to the following expression.

COP=(Refrigerating capacity or heating capacity)/Power consumption









TABLE 249







41%R1234yf,r=0.25



















Comparative
Comparative
Comparative
Comparative
Comparative
Example
Example




Comparative
Example 2
Example 3
Example 4
Example 5
Example 6
1
2


Item
Unit
Example 1
A
Br=0.25
Cr=0.25
Dr=0.25
Fr=0.25
Or=0.25
Pr=0.25





R32
mass %
R410A
15.0
19.9
31.6
0.0
0.0
19.0
12.8


CO2
mass %

44.0
0.0
0.0
20.6
39.5
8.2
12.2


R125
mass %

0.0
9.8
6.9
9.6
4.9
7.9
8.5


R134a
mass %

0.0
29.3
20.5
28.8
14.6
23.9
25.5


R1234yf
mass %

41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

2088
103
898
750
750
382
750
750


COP ratio
% (relative
100
87.6
104.7
103.8
98.6
92.0
101.0
100.0



to that of











R410A)










Refrigerating
% (relative
100
157.7
63.8
72.8
94.9
139.9
80.6
84.9


capacity ratio
to that of











R410A)










Condensation
° C.
0.1
17.6
4.9
4.5
25.5
25.0
13.2
17.3


glide










41%R1234yf,r=0.375
















Comparative
Comparative
Comparative
Comparative






Example 7
Example 8
Example 9
Example 10
Example 3
Example 4


Item
Unit
Br=0.375
Cr=0.375
Dr=0.375
Fr=0.375
Or=0.375
Pr=0.375





R32
mass %
22.1
36.2
0.0
0.0
20.3
14.3


CO2
mass %
0.0
0.0
25.1
40.5
11.0
15.2


R125
mass %
13.8
8.6
12.7
6.9
10.4
11.1


R134a
mass %
23.1
14.2
21.2
11.6
17.3
18.4


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0


GWP

964
750
750
409
750
750


COP ratio
% (relative
104.0
103.2
96.9
91.1
99.5
98.5



to that of









R410A)








Refrigerating
% (relative
67.0
77.1
107.4
142.7
89.2
94.3


capacity ratio
to that of









R410A)








Condensation
º C.
4.8
4.0
25.6
24.3
14.2
17.8


glide

















41%R1234yf,r=0.5
















Comparative
Comparative
Comparative
Comparative






Example 11
Example 12
Example 13
Example 14
Example 5
Example 6


Item
Unit
Br=0.5
Cr=0.5
Dr=0.5
Fr=0.5
Or=0.5
Pr=0.5





R32
mass %
24.1
39.5
0.0
0.0
21.4
15.4


CO2
mass %
0.0
0.0
28.7
41.2
13.2
17.4


R125
mass %
17.5
9.8
15.2
8.9
12.2
13.1


R134a
mass %
17.4
9.7
15.1
8.9
12.2
13.1


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0


GWP

1026
750
750
441
750
750


COP ratio
% (relative
103.4
102.7
95.2
90.3
98.3
97.3



to that of









R410A)








Refrigerating
% (relative
70.0
80.2
117.3
144.8
95.9
101.3


capacity ratio
to that of









R410A)








Condensation
º C.
4.6
3.6
25.0
23.6
14.6
17.8


glide

















41%R1234yf,r=0.75
















Comparative
Comparative
Comparative
Comparative






Example 15
Example 16
Example 17
Example 18
Example 7
Example 8


Item
Unit
Br=0.75
Cr=0.75
Dr=0.75
Fr=0.75
Or=0.75
Pr=0.75





R32
mass %
27.4
43.9
0.0
0.0
22.8
11.4


CO2
mass %
0.0
0.0
33.9
42.6
16.3
25.1


R125
mass %
23.7
11.3
18.8
12.3
14.9
16.9


R134a
mass %
7.9
3.8
6.3
4.1
5.0
5.6


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0


GWP

1129
750
750
491
750
750


COP ratio
% (relative
102.4
102.2
92.2
88.8
96.6
94.3



to that of









R410A)








Refrigerating
% (relative
75.1
84.4
131.0
148.8
105.5
118.1


capacity ratio
to that of









R410A)








Condensation
° C.
4.0
2.9
23.4
22.2
14.6
19.4


glide

















41%R1234yf,r=1.0
















Comparative
Comparative
Comparative
Comparative






Example 19
Example 20
Example 21
Example 22
Example 9
Example 10


Item
Unit
Br=1.0
Cr=1.0
Dr=1.0
Fr=1.0
Or=1.0
Pr=1.0





R32
mass %
30.2
46.7
0.0
0.0
23.8
7.7


CO2
mass %
0.0
0.0
37.7
43.1
18.5
31.5


R125
mass %
28.8
12.3
21.3
15.9
16.7
19.8


R134a
mass %
0.0
0.0
0.0
0.0
0.0
0.0


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0


GWP

1213
750
750
559
750
750


COP ratio
% (relative
101.5
101.9
89.7
87.8
95.4
91.6



to that of









R410A)








Refrigerating
% (relative
79.5
87.1
140.5
150.9
112.3
131.4


capacity ratio
to that of









R410A)








Condensation
° C.
3.4
2.5
21.8
21.2
14.2
19.8


glide
















TABLE 250







43.8%R1234yf,r=0.25

















Comparative
Comparative
Comparative
Comparative
Comparative
Example
Example




Example 23
Example 24
Example 25
Example 26
Example 27
11
12


Item
Unit
A
Br=0.25
Cr=0.25
Dr=0.25
Fr=0.25
Or=0.25
Pr=0.25





R32
mass %
13.1
17.9
27.3
0.0
0.0
17.1
12.0


CO2
mass %
43.1
0.0
0.0
17.8
35.4
6.7
10.1


R125
mass %
0.0
9.6
7.2
9.6
5.2
8.1
8.5


R134a
mass %
0.0
28.7
21.7
28.8
15.6
24.3
25.6


R1234yf
mass %
43.8
43.8
43.8
43.8
43.8
43.8
43.8


GWP

91
869
750
750
407
750
750


COP ratio
% (relative
88.4
104.8
104.1
99.4
94.0
101.8
100.8



to that of










R410A)









Refrigerating
% (relative
154.6
62.2
69.6
87.7
130.7
75.7
79.3


capacity ratio
to that of










R410A)









Condensation
° C.
18.9
5.0
4.8
24.7
26.3
12.3
16.2


glide


















43.8%R1234yf,r=0.375
















Comparative
Comparative
Comparative
Comparative






Example 28
Example 29
Example 30
Example 31
Example 13
Example 14


Item
Unit
Br=0.375
Cr=0.375
Dr=0.375
Fr=0.375
Or=0.375
Pr=0.375





R32
mass %
20.0
32.1
0.0
0.0
18.5
13.6


CO2
mass %
0.0
0.0
22.3
36.6
9.4
12.9


R125
mass %
13.6
9.0
12.7
7.4
10.6
11.2


R134a
mass %
22.6
15.1
21.2
12.2
17.7
18.5


R1234yf
mass %
43.8
43.8
43.8
43.8
43.8
43.8


GWP

936
750
750
436
750
750


COP ratio
% (relative
104.2
103.4
97.8
93.1
100.3
99.4



to that of









R410A)








Refrigerating
% (relative
65.3
74.2
100.3
134.1
84.1
88.3


capacity ratio
to that of









R410A)








Condensation
° C.
4.9
4.4
25.5
25.6
13.8
17.1


glide














Comparative
Comparative
Comparative
Comparative

Example




Example 32
Example 33
Example 34
Example 35
Example 15
16


Item
Unit
Br=0.5
Cr=0.5
Dr=0.5
Fr=0.5
Or=0.5
Pr=0.5





R32
mass %
21.9
35.6
0.0
0.0
19.5
14.7


CO2
mass %
0.0
0.0
25.9
37.4
11.7
15.1


R125
mass %
17.2
10.3
15.2
9.4
12.5
13.2


R134a
mass %
17.1
10.3
15.1
9.4
12.5
13.2


R1234yf
mass %
43.8
43.8
43.8
43.8
43.8
43.8


GWP

996
750
750
466
750
750


COP ratio
% (relative
103.6
102.9
96.3
92.3
99.0
98.2



to that of









R410A)








Refrigerating
% (relative
68.2
77.6
110.3
136.6
91.0
95.3


capacity ratio
to that of









R410A)








Condensation
° C.
4.8
3.9
25.4
24.9
14.5
17.4


glide

















43.8%R1234yf,r=0.75
















Comparative
Comparative
Comparative
Comparative

Example




Example 36
Example 37
Example 38
Example 39
Example 17
18


Item
Unit
Br=0.75
Cr=0.75
Dr=0.75
Fr=0.75
Or=0.75
Pr=0.75





R32
mass %
25.2
40.3
0.0
0.0
21.0
9.9


CO2
mass %
0.0
0.0
31.2
38.5
14.9
23.5


R125
mass %
23.3
11.9
18.8
13.3
15.2
17.1


R134a
mass %
7.7
4.0
6.2
4.4
5.1
5.7


R1234yf
mass %
43.8
43.8
43.8
43.8
43.8
43.8


GWP

1097
750
750
531
750
750


COP ratio
% (relative
102.5
102.3
93.6
91.0
97.3
95.2



to that of









R410A)








Refrigerating
% (relative
73.2
82.0
124.6
140.2
100.9
113.1


capacity ratio
to that of









R410A)








Condensation
° C.
4.3
3.3
24.3
23.7
14.8
20.2


glide














43.8%R1234yf,r=1.0
















Comparative
Comparative
Comparative
Comparative

Example




Example 40
Example 41
Example 42
Example 43
Example 19
20


Item
Unit
Br=1.0
Cr=1.0
Dr=1.0
Fr=1.0
Or=1.0
Pr=1.0





R32
mass %
27.9
43.2
0.0
0.0
22.0
6.6


CO2
mass %
0.0
0.0
34.9
40.0
17.1
29.6


R125
mass %
28.3
13.0
21.3
16.2
17.1
20.0


R134a
mass %
0.0
0.0
0.0
0.0
0.0
0.0


R1234yf
mass %
43.8
43.8
43.8
43.8
43.8
43.8


GWP

1181
748
748
569
750
750


COP ratio
% (relative
101.6
101.9
91.4
89.7
96.1
92.7



to that of









R410A)








Refrigerating
% (relative
77.4
84.8
134.2
144.4
107.7
126.2


capacity ratio
to that of









R410A)








Condensation
° C.
3.7
2.8
23.0
22.6
14.6
20.8


glide
















TABLE 251







46.5%R1234yf,r=0.25

















Comparative
Comparative
Comparative
Comparative
Comparative
Example
Example




Example 44
Example 45
Example 46
Example 47
Example 48
21
22


Item
Unit
A
Br=0.25
Cr=0.25
Dr=0.25
Fr=0.25
Or=0.25
Pr=0.25





R32
mass %
11.2
15.9
23.1
0.0
0.0
15.3
11.3


CO2
mass %
42.3
0.0
0.0
15.1
31.5
5.1
7.8


R125
mass %
0.0
9.4
7.6
9.6
5.5
8.3
8.6


R134a
mass %
0.0
28.2
22.8
28.8
16.5
24.8
25.8


R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5
46.5


GWP

78
841
750
750
431
750
750


COP ratio
% (relative
89.1
104.9
104.3
100.0
95.7
102.5
101.7



to that of










R410A)









Refrigerating
% (relative
151.8
60.5
66.3
80.7
121.5
70.7
73.3


capacity ratio
to that of










R410A)









Condensation
° C.
20.2
5.0
5.0
23.4
27.2
11.1
14.4


glide


















46.5%R1234yf,r=0.375
















Comparative
Comparative
Comparative
Comparative

Example




Example 49
Example 50
Example 51
Example 52
Example 23
24


Item
Unit
Br=0.375
Cr=0.375
Dr=0.375
Fr=0.375
Or=0.375
Pr=0.375





R32
mass %
18.0
28.3
0.0
0.0
16.7
12.8


CO2
mass %
0.0
0.0
19.6
32.3
8.0
10.7


R125
mass %
13.3
9.5
12.7
8.2
10.8
11.3


R134a
mass %
22.2
15.7
21.2
13.0
18.0
18.7


R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5


GWP

906
750
750
475
750
750


COP ratio
% (relative
104.3
103.6
98.6
95.0
100.9
100.2



to that of









R410A)








Refrigerating
% (relative
63.6
71.4
93.3
124.3
79.4
82.4


capacity ratio
to that of









R410A)








Condensation
° C.
5.0
4.7
25.0
26.5
13.2
16.1


glide










46.5%R1234yf,r=0.5
















Comparative
Comparative
Comparative
Comparative

Example




Example 53
Example 54
Example 55
Example 56
Example 25
26


Item
Unit
Br=0.5
Cr=0.5
Dr=0.5
Fr=0.5
Or=0.5
Pr=0.5





R32
mass %
19.9
31.9
0.0
0.0
17.3
13.1


CO2
mass %
0.0
0.0
23.2
33.1
10.6
13.6


R125
mass %
16.8
10.8
15.2
10.2
12.8
13.4


R134a
mass %
16.8
10.8
15.1
10.2
12.8
13.4


R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5


GWP

964
750
750
505
750
750


COP ratio
% (relative
103.7
103.1
97.3
94.3
99.6
98.9



to that of









R410A)








Refrigerating
% (relative
66.4
74.9
103.4
126.8
86.7
90.4


capacity ratio
to that of









R410A)








Condensation
° C.
4.9
4.3
25.4
26.0
14.5
17.3


glide

















46.5%R1234yf,r=0.75
















Comparative
Comparative
Comparative
Comparative

Example




Example 57
Example 58
Example 59
Example 60
Example 27
28


Item
Unit
Br=0.75
Cr=0.75
Dr=0.75
Fr=0.75
Or=0.75
Pr=0.75





R32
mass %
23.1
36.8
0.0
0.0
19.3
8.7


CO2
mass %
0.0
0.0
28.5
35.3
13.5
21.7


R125
mass %
22.8
12.5
18.8
13.7
15.5
17.3


R134a
mass %
7.6
4.2
6.2
4.5
5.2
5.8


R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5


GWP

1064
750
750
546
750
750


COP ratio
% (relative
102.7
102.4
94.9
92.7
97.9
96.1



to that of









R410A)








Refrigerating
% (relative
71.3
79.6
118.0
133.0
96.3
107.8


capacity ratio
to that of









R410A)








Condensation
° C.
4.6
3.7
24.9
24.8
14.9
20.7


glide










46.5%R1234yf,r=1.0
















Comparative
Comparative
Comparative
Comparative






Example 61
Example 62
Example 63
Example 64
Example 29
Example 30


Item
Unit
Br=1.0
Cr=1.0
Dr=1.0
Fr=1.0
Or=1.0
Pr=1.0





R32
mass %
25.8
39.8
0.0
0.0
20.4
5.9


CO2
mass %
0.0
0.0
32.2
35.9
15.7
27.4


R125
mass %
27.7
13.7
21.3
17.6
17.4
20.2


R134a
mass %
0.0
0.0
0.0
0.0
0.0
0.0


R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5


GWP

1146
750
750
618
750
750


COP ratio
% (relative
101.8
102.0
92.8
91.7
96.7
93.9



to that of









R410A)








Refrigerating
% (relative
75.4
82.6
127.8
135.5
103.2
120.4


capacity ratio
to that of









R410A)








Condensation
° C.
4.1
3.2
23.9
23.9
14.8
21.6


glide























TABLE 252







46.5%R1234yf,r=0.31
















Comparative
Comparative
Comparative
Comparative






Example 65
Example 66
Example 67
Example 68
Example 31
Example 32


Item
Unit
Br=0.31
Cr=0.31
Dr=0.31
Fr=0.31
Or=0.31
Pr=0.31





R32
mass %
16.9
25.9
0.0
0.0
16.0
12.2


CO2
mass %
0.0
0.0
17.5
31.6
6.6
9.2


R125
mass %
11.3
8.6
11.2
5.5
9.6
10.0


R134a
mass %
25.3
19.0
24.8
16.4
21.3
22.1


R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5


GWP

873
750
750
429
750
750


COP ratio
% (relative to
104.6
103.9
99.3
95.7
101.7
100.9



that of R410A)








Refrigerating
% (relative to
61.9
69.1
87.4
121.8
75.1
77.9


capacity ratio
that of R410A)








Condensation
° C.
5.0
4.9
24.4
27.1
12.3
15.3


glide

















46.5%R1234yf,r=0.37
















Comparative
Comparative
Comparative
Comparative






Example 69
Example 70
Example 71
Example 72
Example 33
Example 34


Item
Unit
Br=0.37
Cr=0.37
Dr=0.37
Fr=0.37
Or=0.37
Pr=0.37





R32
mass %
17.9
28.0
0.0
0.0
16.6
12.8


CO2
mass %
0.0
0.0
19.5
31.7
8.0
10.7


R125
mass %
13.2
9.4
12.6
6.8
10.7
11.1


R134a
mass %
22.4
16.1
21.4
15.0
18.2
18.9


R1234yf
mass %
46.5
46.5
46.5
46.5
46.5
46.5


GWP

905
750
750
455
750
750


COP ratio
% (relative to
104.3
103.6
98.6
95.5
101.0
100.2



that of R410A)








Refrigerating
% (relative to
63.4
71.1
93.0
122.4
79.3
82.3


capacity ratio
that of R410A)








Condensation
° C.
5.0
4.7
25.0
26.9
13.2
16.1


glide
















TABLE 253







50%R1234yf,r=0.25

















Comparative
Comparative
Comparative
Comparative
Comparative
Example
Example




Example 73
Example 74
Example 75
Example 76
Example 77
35
36


Item
Unit
A
Br=0.25
Cr=0.25
Dr=0.25
Fr=0.25
Or=0.25
Pr=0.25





R32
mass %
8.8
13.4
17.9
0.0
0.0
13.0
10.5


CO2
mass %
41.2
0.0
0.0
11.6
26.1
3.1
4.7


R125
mass %
0.0
9.2
8.0
9.6
6.0
8.5
8.7


R134a
mass %
0.0
27.4
24.1
28.8
17.9
25.4
26.1


R1234yf
mass %
50.0
50.0
50.0
50.0
50.0
50.0
50.0


GWP

62
806
750
750
468
750
750


COP ratio
% (relative
90.3
105.0
104.7
100.9
97.7
103.5
102.9



to that of










R410A)









Refrigerating
% (relative
148.0
58.3
62.1
71.8
108.2
64.3
65.5


capacity ratio
to that of










R410A)









Condensation
° C.
22.0
4.9
5.1
20.7
27.5
9.1
11.2


glide


















50%R1234yf,r=0.375
















Comparative
Comparative
Comparative
Comparative

Example




Example 78
Example 79
Example 80
Example 81
Example 37
38


Item
Unit
Br=0.375
Cr=0.375
Dr=0.375
Fr=0.375
Or=0.375
Pr=0.375





R32
mass %
15.4
23.3
0.0
0.0
14.4
11.9


CO2
mass %
0.0
0.0
16.1
27.6
6.1
8.0


R125
mass %
13.0
10.0
12.7
8.5
11.1
11.3


R134a
mass %
21.6
16.7
21.2
13.9
18.4
18.8


R1234yf
mass %
50.0
50.0
50.0
50.0
50.0
50.0


GWP

870
750
750
499
750
750


COP ratio
% (relative
104.4
103.9
99.5
96.8
101.8
101.3



to that of









R410A)








Refrigerating
% (relative
61.2
67.5
84.1
112.7
73.1
75.2


capacity ratio
to that of









R410A)








Condensation
° C.
5.1
5.0
23.7
27.2
12.1
14.3


glide
















TABLE 254







50%R1234yf,r=0.5
















Comparative
Comparative
Comparative
Comparative






Example 82
Example 83
Example 84
Example 85
Example 39
Example 40


Item
Unit
Br=0.5
Cr=0.5
Dr=0.5
Fr=0.5
Or=0.5
Pr=0.5





R32
mass %
17.2
27.2
0.0
0.0
15.5
10.8


CO2
mass %
0.0
0.0
19.8
28.8
8.5
11.8


R125
mass %
16.4
11.4
15.1
10.6
13.0
13.7


R134a
mass %
16.4
11.4
15.1
10.6
13.0
13.7


R1234yf
mass %
50.0
50.0
50.0
50.0
50.0
50.0


GWP

926
748
747
525
748
750


COP ratio
% (relative to
103.9
103.3
98.3
96.1
100.6
99.7



that of R410A)








Refrigerating
% (relative to
63.9
71.4
94.5
116.4
80.3
84.1


capacity ratio
that of R410A)








Condensation
° C.
5.1
4.8
25.0
26.8
13.7
17.2


glide

















50%R1234yf,r=0.75
















Comparative
Comparative
Comparative
Comparative






Example 86
Example 87
Example 88
Example 89
Example 41
Example 42


Item
Unit
Br=0.75
Cr=0.75
Dr=0.75
Fr=0.75
Or=0.75
Pr=0.75





R32
mass %
20.4
32.3
0.0
0.0
17.1
7.3


CO2
mass %
0.0
0.0
25.0
30.4
11.7
19.3


R125
mass %
22.2
13.3
18.8
14.7
15.9
17.6


R134a
mass %
7.4
4.4
6.2
4.9
5.3
5.8


R1234yf
mass %
50.0
50.0
50.0
50.0
50.0
50.0


GWP

1023
750
750
587
750
750


COP ratio
% (relative to
102.9
102.6
96.3
94.9
98.8
97.2



that of R410A)








Refrigerating
% (relative to
68.7
76.4
109.1
121.6
90.3
100.7


capacity ratio
that of R410A)








Condensation
° C.
4.9
4.2
25.3
25.9
14.8
21.1


glide










50%R1234yf,r=1.0
















Comparative
Comparative
Comparative
Comparative






Example 90
Example 91
Example 92
Example 93
Example 43
Example 44


Item
Unit
Br=1.0
Cr=1.0
Dr=1.0
Fr=1.0
Or=1.0
Pr=1.0





R32
mass %
23.0
35.5
0.0
0.0
18.2
3.9


CO2
mass %
0.0
0.0
28.7
31.8
14.0
25.5


R125
mass %
27.0
14.5
21.3
18.2
17.8
20.6


R134a
mass %
0.0
0.0
0.0
0.0
0.0
0.0


R1234yf
mass %
50.0
50.0
50.0
50.0
50.0
50.0


GWP

1102
750
750
639
750
750


COP ratio
% (relative to
102.0
102.1
94.5
93.7
97.5
95.1



that of R410A)








Refrigerating
% (relative to
72.8
79.6
119.2
126.0
97.4
114.2


capacity ratio
that of R410A)








Condensation
° C.
4.5
3.7
24.8
25.0
15.1
22.9


glide










50%R1234yf,r=0.31
















Comparative
Comparative
Comparative
Comparative






Example 94
Example 95
Example 96
Example 97
Example 45
Example 46


Item
Unit
Br=0.31
Cr=0.31
Dr=0.31
Fr=0.31
Or=0.31
Pr=0.31





R32
mass %
14.4
20.6
0.0
0.0
13.8
11.2


CO2
mass %
0.0
0.0
14.0
27.0
4.6
6.5


R125
mass %
11.0
9.1
11.2
7.3
9.8
10.0


R134a
mass %
24.6
20.3
24.8
15.7
21.8
22.3


R1234yf
mass %
50.0
50.0
50.0
50.0
50.0
50.0


GWP

836
750
750
482
750
750


COP ratio
% (relative to
104.7
104.3
100.2
97.2
102.6
102.0



that of R410A)








Refrigerating
% (relative to
59.7
64.8
78.3
110.9
68.7
70.7


capacity ratio
that of R410A)








Condensation
° C.
5.0
5.1
22.6
27.4
10.7
13.1


glide

















50%R1234yf,r=0.37
















Comparative
Comparative
Comparative
Comparative






Example 98
Example 99
Example 100
Example 101
Example 47
Example 48


Item
Unit
Br=0.37
Cr=0.37
Dr=0.37
Fr=0.37
Or=0.37
Pr=0.37





R32
mass %
15.3
23.1
0.0
0.0
14.4
11.9


CO2
mass %
0.0
0.0
16.0
27.6
6.0
7.7


R125
mass %
12.8
10.0
12.6
8.5
11.0
11.2


R134a
mass %
21.9
16.9
21.4
13.9
18.6
19.2


R1234yf
mass %
50.0
50.0
50.0
50.0
50.0
50.0


GWP

866
750
749
499
750
749


COP ratio
% (relative to
104.5
103.9
99.6
96.8
101.9
101.4



that of R410A)








Refrigerating
% (relative to
61.1
67.3
83.9
112.7
72.9
74.5


capacity ratio
that of R410A)








Condensation
° C.
5.0
5.1
23.7
27.2
12.0
14.0


glide
















TABLE 255







41%R1234yf,r=0.25























Comparative







Example



Example




Item
Unit
Example 49
50
Example 51
Example 52
Example 53
102
Example 54
Example 55





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
42.0
32.0
21.0
19.0
17.0
12.0
40.0
30.0


R125
mass %
2.5
5.0
7.8
8.3
8.8
10.0
2.5
5.0


R134a
mass %
7.5
15.0
23.2
24.7
26.2
30.0
7.5
15.0


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

244
439
654
693
732
828
258
452


COP ratio
%
89.5
94.0
97.8
98.4
99.0
100.4
90.2
94.4



(relative











to that











of











R410A)










Refrigerating
%
149.0
127.2
101.4
96.5
91.7
79.7
145.9
123.9


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
21.3
23.2
22.8
22.3
21.5
18.8
21.0
22.6


glide



















41%R1234yf,r=0.25




















Comparative



Comparative






Example
Example



Example



Item
Unit
Example 56
57
103
Example 58
Example 59
Example 60
104
Example 61





R32
mass %
9.0
9.0
9.0
11.0
11.0
11.0
11.0
15.0


CO2
mass %
17.0
15.0
10.0
38.0
28.0
14.0
8.0
34.0


R125
mass %
8.3
8.8
10.0
2.5
5.0
8.5
10.0
2.5


R134a
mass %
24.7
26.2
30.0
7.5
15.0
25.5
30.0
7.5


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

706
745
841
271
466
738
855
298


COP ratio
%
98.8
99.4
101.0
90.8
94.9
99.6
101.6
92.0



(relative











to that











of











R410A)










Refrigerating
%
93.3
88.5
76.7
142.8
120.6
87.7
73.7
136.6


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
20.9
20.0
16.7
20.6
21.9
18.9
14.6
19.8


glide










41%R1234yf,r=0.25


















Comparative
Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item
Unit
Example 62
63
105
106
107
108





R32
mass %
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
24.0
14.0
4.0
24.0
14.0
4.0


R125
mass %
5.0
7.5
10.0
2.5
5.0
7.5


R134a
mass %
15.0
22.5
30.0
7.5
15.0
22.5


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0


GWP

493
687
882
365
560
755


COP ratio
%
95.9
99.2
103.0
94.9
98.4
102.4



(relative









to that









of









R410A)








Refrigerating
%
114.1
90.8
68.2
120.8
98.1
76.1


capacity ratio
(relative









to that









of









R410A)








Condensation
º C.
20.2
17.7
9.9
16.9
14.9
8.8


glide

































Comparative







Example



Example




Item
Unit
Example 64
65
Example 66
Example 67
Example 68
109
Example 69
Example 70





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
42.0
32.0
25.0
23.0
21.0
12.0
40.0
30.0


R125
mass %
3.8
7.5
10.1
10.9
11.6
15.0
3.8
7.5


R134a
mass %
6.2
12.5
16.9
18.1
19.4
25.0
6.2
12.5


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

271
490
644
689
733
932
284
504


COP ratio
%
89.3
93.6
96.1
96.7
97.3
100.0
89.9
94.1



(relative











to that











of











R410A)










Refrigerating
%
149.4
128.1
112.0
107.4
102.6
81.2
146.4
124.8


capacity ratio
(relative











to that











of











R410A)










Condensation
º C.
21.0
22.7
22.7
22.5
22.1
18.2
20.7
22.0


glide



















41%R1234yf,r=0.375





















Comparative









Example

Example






Item
Unit
Example 71
72
Example 73
110
Example 74
Example 75
Example 76
Example 77





R32
mass %
9.0
9.0
9.0
9.0
11.0
11.0
11.0
11.0


CO2
mass %
23.0
21.0
19.0
10.0
38.0
28.0
20.0
18.0


R125
mass %
10.1
10.9
11.6
15.0
3.8
7.5
10.5
11.3


R134a
mass %
16.9
18.1
19.4
25.0
6.2
12.5
17.5
18.7


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

658
703
746
945
298
517
694
739


COP ratio
%
96.5
97.1
97.7
100.5
90.6
94.5
97.2
97.9



(relative











to that











of











R410A)










Refrigerating
%
108.7
104.0
99.3
78.2
143.3
121.5
103.1
98.4


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
21.7
21.4
20.9
16.2
20.3
21.3
20.5
19.9


glide



















41%R1234yf,r=0.375


















Comparative


Comparative
Comparative
Comparative
Comparative
Comparative




Example
Example

Example
Example
Example
Example
Example


Item
Unit
111
78
Example 79
112
113
114
115
116





R32
mass %
11.0
15.0
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
8.0
34.0
24.0
14.0
4.0
24.0
14.0
4.0


R125
mass %
15.0
3.8
7.5
11.3
15.0
3.8
7.5
11.3


R134a
mass %
25.0
6.2
12.5
18.7
25.0
6.2
12.5
18.7


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

958
325
544
766
985
392
612
833


COP ratio
%
101.1
91.8
95.5
98.8
102.6
94.7
98.2
102.0



(relative











to that











of











R410A)










Refrigerating
%
75.3
137.1
115.0
92.1
69.8
121.3
99.1
77.4


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
14.1
19.5
19.7
17.1
9.6
16.6
14.5
8.5


glide
















TABLE 256







41% R1234yf, r = 0.5























Compara-











tive






Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
80
81
82
83
84
117
85
86





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
42.0
32.0
29.0
27.0
25.0
12.0
40.0
30.0


R125
mass %
5.0
10.0
11.5
12.5
13.5
20.0
5.0
10.0


R134a
mass %
5.0
10.0
11.5
12.5
13.5
20.0
5.0
10.0


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

296
542
616
665
715
1035
309
556


COP ratio
%
89.1
93.1
94.2
94.9
95.6
99.5
89.7
93.7



(relative











to that











of











R410A)










Refrigerating
%
149.8
128.9
122.2
117.7
113.2
82.8
146.8
125.6


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
20.7
22.2
22.3
22.2
22.1
17.5
20.4
21.5


glide










41% R1234yf, r = 0.5




















Compara-




Compara-






tive




tive




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
87
88
118
89
90
91
92
119





R32
mass %
9.0
9.0
9.0
11.0
11.0
11.0
11.0
11.0


CO2
mass %
25.0
23.0
10.0
38.0
28.0
23.0
21.0
8.0


R125
mass %
12.5
13.5
20.0
5.0
10.0
12.5
13.5
20.0


R134a
mass %
12.5
13.5
20.0
5.0
10.0
12.5
13,5
20.0


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

679
728
1048
323
569
692
742
1062


COP ratio
%
95.4
96.0
100.0
90.4
94.2
95.9
96.5
100.7



(relative











to that











of











R410A)










Refrigerating
%
114.4
109.8
79.8
143.7
122.3
111.1
106.6
76.9


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
21.3
21.1
15.6
20.0
20.8
20.4
20.1
13.6


glide










41% R1234yf, r = 0.5





















Compara-
Compara-
Compara-
Compara-
Compara-







tive
tive
tive
tive
tive




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
93
94
95
120
121
122
123
124





R32
mass %
13.0
15.0
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
20.0
34.0
24.0
14.0
4.0
24.0
14.0
4.0


R125
mass %
13.0
5.0
10.0
15.0
20.0
5.0
10.0
15.0


R134a
mass %
13.0
5.0
10.0
15.0
20.0
5.0
10.0
15.0


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

730
350
596
843
1089
417
664
910


COP ratio
%
96.7
91.6
95.2
98.4
102.1
94.6
97.9
101.6



(relative











to that











of











R410A)










Refrigerating
%
105.6
137.5
115.8
93.4
71.4
121.7
100.0
78.7


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
19.2
19.2
19.2
16.5
9.2
16.4
14.1
8.1


glide










41% R1234yf, r = 0.75





















Compara-


Compara-








tive


tive





Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
96
97
98
125
99
100
126
101





R32
mass %
7.0
7.0
7.0
7.0
9.0
9.0
9.0
11.0


CO2
mass %
42.0
31.0
29.0
12.0
40.0
28.0
10.0
38.0


R125
mass %
7.5
15.8
17.3
30.0
7.5
16.5
30.0
7.5


R134a
mass %
2.5
5.2
5.7
10.0
2.5
5.5
10.0
2.5


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

348
677
736
1242
361
719
1255
375


COP ratio
%
88.6
92.6
93.3
98.4
89.3
93.5
98.9
89.9



(relative











to that











of











R410A)










Refrigerating
%
150.6
128.4
124.1
86.1
147.6
123.0
83.1
144.5


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
20.1
21.1
21.0
16.2
19.8
20.4
14.4
19.4


glide



















41% R1234yf, r = 0.75




















Compara-


Compara-
Compara-
Compara-
Compara-
Compara-




Exam-
tive
Exam-
Exam-
tive
tive
tive
tive
tive




ple
Example
ple
ple
Example
Example
Example
Example
Example


Item
Unit
102
127
103
104
128
129
130
131
132





R32
mass %
11.0
11.0
15.0
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
28.0
8.0
34.0
24.0
14.0
4.0
24.0
14.0
4.0


R125
mass %
15.0
30.0
7.5
15.0
22.5
30.0
7.5
15.0
22.5


R134a
mass %
5.0
10.0
2.5
5.0
7.5
10.0
2.5
5.0
7.5


R1234yf
mass %
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0
41.0


GWP

673
1269
401
700
998
1296
469
767
1065


COP ratio
%
93.4
99.6
91.2
94.5
97.5
101.0
94.2
97.3
100.8



(relative












to that












of












R410A)











Refrigerating
%
124.0
80.2
138.4
117.6
96.0
74.6
122.7
101.9
81.4


capacity ratio
(relative












to that












of












R410A)











Condensation
° C.
19.8
12.5
18.7
18.2
15.4
8.5
15.8
13.3
7.5


glide
















TABLE 257







43% R1234yf, r = 0.25























Comparative






Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
105
106
107
108
109
133
110
111





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
40.0
30.0
19.0
17.0
15.0
10.0
38.0
28.0


R125
mass %
2.5
5.0
7.8
8.3
8.8
10.0
2.5
5.0


R134a
mass %
7.5
15.0
23.2
24.7
26.2
30.0
7.5
15.0


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

244
439
654
693
732
828
258
452


COP ratio
%
90.6
94.8
98.4
99.0
99.6
101.1
91.2
95.3



(relative











to that of











R410A)










Refrigerating
%
144.7
122.6
96.5
91.6
86.8
74.9
141.6
119.3


capacity ratio
(relative











to that of











R410A)










Condensation
° C.
22.1
23.6
22.4
21.7
20.7
17.3
21.7
22.8


glide










43% R1234yf, r = 0.25




















Comparative



Comparative
Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
112
113
134
114
115
116
135
136





R32
mass %
9.0
9.0
9.0
11.0
11.0
11.0
11.0
15.0


CO2
mass %
15.0
13.0
8.0
36.0
26.0
12.0
6.0
32.0


R125
mass %
8.3
8.8
10.0
2.5
5.0
8.5
10.0
2.5


R134a
mass %
24.7
26.2
30.0
7.5
15.0
25.5
30.0
7.5


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

706
745
842
271
466
738
855
298


COP ratio
%
99.4
100.0
101.7
91.8
95.7
100.2
102.4
92.9



(relative











to that of











R410A)










Refrigerating
%
88.4
83.6
72.0
138.5
116.0
82.9
69.2
132.1


capacity ratio
(relative











to that of











R410A)










Condensation
° C.
20.1
19.0
15.0
21.2
22.0
17.8
12.6
20.2


glide










43% R1234yf, r = 0.25


















Comparative
Comparative
Comparative
Comparative




Example
Example
Example
Example
Example
Example


Item
Unit
117
118
137
138
139
140





R32
mass %
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
22.0
12.0
2.0
22.0
12.0
2.0


R125
mass %
5.0
7.5
10.0
2.5
5.0
7.5


R134a
mass %
15.0
22.5
30.0
7.5
15.0
22.5


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0


GWP

493
687
882
365
560
755


COP ratio
%
96.6
99.9
104.0
95.6
99.2
103.3



(relative









to that of









R410A)








Refrigerating
%
109.4
86.1
63.9
116.2
93.6
71.9


capacity ratio
(relative









to that of









R410A)








Condensation
° C.
20.1
16.7
7.5
16.8
14.1
6.9


glide










43% R1234yf, r = 0.303























Comparative






Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
119
120
121
122
123
141
124
125





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
40.0
30.0
21.0
19.0
17.0
10.0
38.0
28.0


R125
mass %
3.0
6.1
8.8
9.4
10.0
12.1
3.0
6.1


R134a
mass %
7.0
13.9
20.2
21.6
23.0
27.9
7.0
13.9


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

254
462
646
687
728
872
268
475


COP ratio
%
90.5
94.7
97.7
98.3
98.8
100.9
91.1
95.1



(relative











to that of











R410A)










Refrigerating
%
144.9
123.0
101.8
97.0
92.1
75.5
141.8
119.6


capacity ratio
(relative











to that of











R410A)










Condensation
° C.
22.0
23.4
22.7
22.1
21.4
17.0
21.6
22.6


glide










43% R1234yf, r = 0.303





















Comparative



Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
126
127
128
142
129
130
131
143





R32
mass %
9.0
9.0
9.0
9.0
11.0
11.0
11.0
11.0


CO2
mass %
19.0
17.0
15.0
8.0
36.0
26.0
14.0
6.0


R125
mass %
8.8
9.4
10.0
12.1
3.0
6.1
9.7
12.1


R134a
mass %
20.2
21.6
23.0
27.9
7.0
13.9
22.3
27.9


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

660
701
742
885
281
489
735
899


COP ratio
%
98.1
98.7
99.3
101.5
91.7
95.6
99.4
102.2



(relative











to that of











R410A)










Refrigerating
%
98.5
93.7
89.0
72.6
138.6
116.3
88.2
69.8


capacity ratio
(relative











to that of











R410A)










Condensation
° C.
21.4
20.7
19.8
14.8
21.1
21.8
18.7
12.4


glide










43% R1234yf, r = 0.303




















Comparative
Comparative
Comparative
Comparative




Example
Example
Example
Example
Example
Example
Example


Item
Unit
132
133
134
144
145
146
147





R32
mass %
15.0
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
32.0
22.0
12.0
2.0
22.0
12.0
2.0


R125
mass %
3.0
6.1
9.1
12.1
3.0
6.1
9.1


R134a
mass %
7.0
13.9
20.9
27.9
7.0
13.9
20.9


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

308
515
720
925
376
583
788


COP ratio
%
92.8
96.5
99.8
103.8
95.6
99.0
103.1



(relative










to that of










R410A)









Refrigerating
%
132.3
109.8
86.6
64.5
116.4
94.0
72.4


capacity ratio
(relative










to that of










R410A)









Condensation
° C.
20.1
19.9
16.5
7.4
16.7
13.9
6.8


glide
















TABLE 258







43% R1234yf, r = 0.355























Comparative






Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
135
136
137
138
139
148
140
141





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
40.0
30.0
23.0
21.0
19.0
10.0
38.0
28.0


R125
mass %
3.6
7.1
9.6
10.3
11.0
14.2
3.6
7.1


R134a
mass %
6.4
12.9
17.4
18.7
20.0
25.8
6.4
12.9


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

267
482
634
677
720
915
280
496


COP ratio
% (relative
90.4
94.5
96.9
97.5
98.1
100.7
91.0
95.0



to that of











R410A)










Refrigerating
% (relative
145.1
123.3
107.0
102.3
97.5
76.1
142.0
120.0


capacity ratio
to that of











R410A)










Condensation
° C.
21.8
23.2
22.8
22.4
21.9
16.8
21.4
22.4


glide










43% R1234yf, r = 0.355




















Comparative




Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
142
143
149
144
145
146
147
150





R32
mass %
9.0
9.0
9.0
11.0
11.0
11.0
11.0
11.0


CO2
mass %
19.0
17.0
8.0
36.0
26.0
17.0
15.0
6.0


R125
mass %
10.3
11.0
14.2
3.6
7.1
10.3
11.0
14.2


R134a
mass %
18.7
20.0
25.8
6.4
12.9
18.7
20.0
25.8


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

691
734
928
294
509
704
747
942


COP ratio
% (relative
97.9
98.5
101.3
91.6
95.4
98.3
98.9
102.0



to that of











R410A)










Refrigerating
% (relative
99.0
94.2
73.2
138.8
116.7
95.7
91.0
70.4


capacity ratio
to that of











R410A)










Condensation
° C.
21.1
20.5
14.6
21.0
21.6
19.8
19.0
12.3


glide










43% R1234yf, r = 0.355



















Comparative
Comparative
Comparative
Comparative
Comparative




Example
Example
Example
Example
Example
Example
Example


Item
Unit
148
149
151
152
153
154
155





R32
mass %
15.0
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
32.0
22.0
12.0
2.0
22.0
12.0
2.0


R125
mass %
3.6
7.1
10.7
14.2
3.6
7.1
10.7


R134a
mass %
6.4
12.9
19.3
25.8
6.4
12.9
19.3


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

321
536
754
969
388
604
821


COP ratio
% (relative
92.7
96.3
99.6
103.6
95.5
98.9
103.0



to that of










R410A)









Refrigerating
% (relative
132.5
110.1
87.2
65.2
116.6
94.4
73.0


capacity ratio
to that of










R410A)









Condensation
° C.
20.0
19.7
16.3
7.3
16.6
13.8
6.7


glide










43% R1234yf, r = 0.375























Comparative






Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
150
151
152
153
154
156
155
156





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
40.0
30.0
23.0
21.0
19.0
10.0
38.0
28.0


R125
mass %
3.8
7.5
10.1
10.9
11.6
15.0
3.8
7.5


R134a
mass %
6.2
12.5
16.9
18.1
19.4
25.0
6.2
12.5


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

271
491
644
690
733
932
285
504


COP ratio
% (relative
90.4
94.5
96.8
97.4
98.0
100.6
91.0
94.9



to that of











R410A)










Refrigerating
% (relative
145.2
123.4
107.2
102.4
97.7
76.4
142.0
120.1


capacity ratio
to that of











R410A)










Condensation
° C.
21.8
23.1
22.7
22.3
21.8
16.7
21.4
22.3


glide










43% R1234yf, r = 0.375





















Comparative



Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
157
158
159
157
160
161
162
158





R32
mass %
9.0
9.0
9.0
9.0
11.0
11.0
11.0
11.0


CO2
mass %
21.0
19.0
17.0
8.0
36.0
26.0
16.0
6.0


R125
mass %
10.1
10.9
11.6
15.0
3.8
7.5
11.3
15.0


R134a
mass %
16.9
18.1
19.4
25.0
6.2
12.5
18.7
25.0


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

658
703
746
945
298
517
739
959


COP ratio
% (relative
97.2
97.8
98.4
101.3
91.6
95.4
98.6
101.9



to that of











R410A)










Refrigerating
% (relative
103.9
99.2
94.4
73.5
138.9
116.8
93.6
70.7


capacity ratio
to that of











R410A)










Condensation
° C.
21.6
21.0
20.4
14.5
20.9
21.5
19.3
12.2


glide










43% R1234yf, r = 0.375



















Comparative
Comparative
Comparative
Comparative
Comparative




Example
Example
Example
Example
Example
Example
Example


Item
Unit
163
164
159
160
161
162
163





R32
mass %
15.0
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
32.0
22.0
12.0
2.0
22.0
12.0
2.0


R125
mass %
3.8
7.5
11.3
15.0
3.8
7.5
11.3


R134a
mass %
6.2
12.5
18.7
25.0
6.2
12.5
18.7


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

325
544
766
985
392
612
833


COP ratio
% (relative
92.7
96.3
99.6
103.5
95.5
98.9
102.9



to that of










R410A)









Refrigerating
% (relative
132.6
110.3
87.4
65.4
116.7
94.5
73.2


capacity ratio
to that of










R410A)









Condensation
° C.
19.9
19.7
16.2
7.3
16.5
13.7
6.7


glide
















TABLE 259







43% R1234yf, r = 0.5























Comparative






Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
165
166
167
168
169
164
170
171





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
40.0
30.0
27.0
25.0
23.0
10.0
38.0
28.0


R125
mass %
5.0
10.0
11.5
12.5
13.5
20.0
5.0
10.0


R134a
mass %
5.0
10.0
11.5
12.5
13.5
20.0
5.0
10.0


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

296
542
616
665
715
1035
309
556


COP ratio
%
90.2
94.1
95.1
95.7
96.4
100.2
90.8
94.5



(relative











to that











of











R410A)










Refrigerating
%
145.5
124.2
117.5
112.9
108.3
77.9
142.4
120.9


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
21.5
22.6
22.5
22.4
22.1
16.2
21.1
21.8


glide










43% R1234yf, r = 0.5




















Comparative



Comparative





Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
172
173
165
174
175
176
166
177





R32
mass %
9.0
9.0
9.0
11.0
11.0
11.0
11.0
13.0


CO2
mass %
23.0
21.0
8.0
36.0
26.0
20.0
6.0
18.0


R125
mass %
12.5
13.5
20.0
5.0
10.0
13.0
20.0
13.0


R134a
mass %
12.5
13.5
20.0
5.0
10.0
13.0
20.0
13.0


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

679
728
1049
323
569
717
1062
731


COP ratio
%
96.2
96.8
100.8
91.4
95.0
96.9
101.5
97.4



(relative











to that











of











R410A)










Refrigerating
%
109.6
105.0
75.0
139.3
117.6
104.0
72.2
100.8


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
21.4
21.0
14.1
20.7
21.0
20.1
11.8
18.8


glide










43% R1234yf, r = 0.5



















Comparative
Comparative
Comparative
Comparative
Comparative




Example
Example
Example
Example
Example
Example
Example


Item
Unit
178
179
167
168
169
170
171





R32
mass %
15.0
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
32.0
22.0
12.0
2.0
22.0
12.0
2.0


R125
mass %
5.0
10.0
15.0
20.0
5.0
10.0
15.0


R134a
mass %
5.0
10.0
15.0
20.0
5.0
10.0
15.0


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

350
596
843
1089
417
664
910


COP ratio
%
92.5
96.0
99.2
103.0
95.3
98.6
102.5



(relative










to that










of










R410A)









Refrigerating
%
133.0
111.1
88.6
67.0
117.2
95.4
74.4


capacity ratio
(relative










to that










of










R410A)









Condensation
° C.
19.7
19.2
15.7
7.1
16.3
13.3
6.5


glide










43% R1234yf, r = 0.75





















Comparative


Comparative





Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
180
181
182
172
183
184
173
185





R32
mass %
7.0
7.0
7.0
7.0
9.0
9.0
9.0
15.0


CO2
mass %
40.0
29.0
27.0
10.0
38.0
26.0
8.0
32.0


R125
mass %
7.5
15.8
17.3
30.0
7.5
16.5
30.0
7.5


R134a
mass %
2.5
5.2
5.7
10.0
2.5
5.5
10.0
2.5


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0
43.0
43.0


GWP

348
677
736
1242
361
719
1256
402


COP ratio
%
89.7
93.6
94.2
99.1
90.3
94.4
99.7
92.1



(relative











to that











of











R410A)










Refrigerating
%
146.3
123.7
119.3
81.1
143.2
118.2
78.2
133.9


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
20.9
21.5
21.4
15.1
20.5
20.6
13.1
19.1


glide










43% R1234yf, r = 0.75

















Comparative
Comparative
Comparative
Comparative





Example
Example
Example
Example
Example
Example


Item
Unit
186
174
175
176
177
187





R32
mass %
15.0
15.0
15.0
25.0
25.0
25.0


CO2
mass %
22.0
12.0
2.0
22.0
12.0
2.0


R125
mass %
15.0
22.5
30.0
7.5
15.0
22.5


R134a
mass %
5.0
7.5
10.0
2.5
5.0
7.5


R1234yf
mass %
43.0
43.0
43.0
43.0
43.0
43.0


GWP

700
998
1296
469
767
1065


COP ratio
%
95.3
98.3
101.9
95.0
98.1
101.7



(relative









to that









of









R410A)








Refrigerating
%
112.9
91.2
70.1
118.1
97.3
77.0


capacity ratio
(relative









to that









of









R410A)








Condensation
° C.
18.2
14.6
6.7
15.8
12.6
6.0


glide
















TABLE 260







45% R1234yf, r = 0.25























Comparative






Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
188
189
190
191
192
178
193
194





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
38.0
28.0
17.0
15.0
13.0
8.0
36.0
26.0


R125
mass %
2.5
5.0
7.8
8.3
8.8
10.0
2.5
5.0


R134a
mass %
7.5
15.0
23.2
24.7
26.2
30.0
7.5
15.0


R1234yf
mass %
45.0
45.0
45.0
45.0
45.0
45.0
45.0
45.0


GWP

244
439
654
693
732
828
258
452


COP ratio
%
91.7
95.7
99.1
99.6
100.2
101.8
92.2
96.1



(relative











to that











of











R410A)










Refrigerating
%
140.4
117.9
91.5
86.7
81.9
70.1
137.2
114.5


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
22.8
23.9
21.8
20.8
19.6
15.4
22.3
23.0


glide










45% R1234yf, r = 0.25




















Comparative



Comparative
Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
195
196
179
197
198
199
180
181





R32
mass %
9.0
9.0
9.0
11.0
11.0
11.0
11.0
15.0


CO2
mass %
13.0
11.0
6.0
34.0
24.0
10.0
4.0
30.0


R125
mass %
8.3
8.8
10.0
2.5
5.0
8.5
10.0
2.5


R134a
mass %
24.7
26.2
30.0
7.5
15.0
25.5
30.0
7.5


R1234yf
mass %
45.0
45.0
45.0
45.0
45.0
45.0
45.0
45.0


GWP

706
745
842
271
466
738
855
298


COP ratio
%
100.1
100.7
102.5
92.7
96.5
100.9
103.2
93.8



(relative











to that











of











R410A)










Refrigerating
%
83.5
78.8
67.3
134.0
111.2
78.2
64.7
127.6


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
19.0
17.7
12.8
21.8
22.0
16.4
10.2
20.6


glide










45% R1234yf, r = 0.25














Comparative Example

Comparative Example
Comparative Example


Item
Unit
182
Example 200
183
184





R32
mass %
15.0
15.0
25.0
25.0


CO2
mass %
20.0
10.0
20.0
10.0


R125
mass %
5.0
7.5
2.5
5.0


R134a
mass %
15.0
22.5
7.5
15.0


R1234yf
mass %
45.0
45.0
45.0
45.0


GWP

493
687
366
560


COP ratio
%
97.3
100.6
96.3
99.9



(relative







to that







of







R410A)






Refrigerating
%
104.6
81.4
111.6
89.1


capacity ratio
(relative







to that







of







R410A)






Condensation
° C.
19.9
15.4
16.6
13.1


glide










45% R1234yf, r = 0.375























Comparative






Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
201
202
203
204
205
185
206
207





R32
mass %
7.0
7.0
7.0
7.0
7.0
7.0
9.0
9.0


CO2
mass %
38.0
28.0
21.0
19.0
17.0
8.0
36.0
26.0


R125
mass %
3.8
7.5
10.1
10.9
11.6
15.0
3.8
7.5


R134a
mass %
6.2
12.5
16.9
18.1
19.4
25.0
6.2
12.5


R1234yf
mass %
45.0
45.0
45.0
45.0
45.0
45.0
45.0
45.0


GWP

271
491
644
690
733
932
285
504


COP ratio
%
91.4
95.3
97.5
98.1
98.7
101.4
92.0
95.7



(relative











to that











of











R410A)










Refrigerating
%
140.8
118.7
102.2
97.5
92.7
71.6
137.6
115.3


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
22.5
23.4
22.5
21.9
21.2
15.0
22.0
22.5


glide










45% R1234yf, r = 0.375




















Comparative



Comparative
Comparative




Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
208
209
186
210
211
212
187
188





R32
mass %
9.0
9.0
9.0
11.0
11.0
11.0
11.0
15.0


CO2
mass %
17.0
15.0
6.0
34.0
24.0
14.0
4.0
30.0


R125
mass %
10.9
11.6
15.0
3.8
7.5
11.3
15.0
3.8


R134a
mass %
18.1
19.4
25.0
6.2
12.5
18.7
25.0
6.2


R1234yf
mass %
45.0
45.0
45.0
45.0
45.0
45.0
45.0
45.0


GWP

703
746
945
298
518
739
959
325


COP ratio
%
98.5
99.1
102.0
92.5
96.1
99.2
102.8
93.6



(relative











to that











of











R410A)










Refrigerating
%
94.2
89.5
68.8
134.4
112.0
88.7
66.1
128.0


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
20.5
19.6
12.5
21.5
21.5
18.5
10.0
20.3


glide










45% R1234yf, r = 0.375














Example
Comparative Example
Comparative Example
Comparative Example


Item
Unit
213
189
190
191





R32
mass %
15.0
15.0
25.0
25.0


CO2
mass %
20.0
10.0
20.0
10.0


R125
mass %
7.5
11.3
3.8
7.5


R134a
mass %
12.5
18.7
6.2
12.5


R1234yf
mass %
45.0
45.0
45.0
45.0


GWP

545
766
392
612


COP ratio
%
97.0
100.3
96.2
99.6



(relative







to that







of







R410A)






Refrigerating
%
105.5
82.7
112.1
90.0


capacity ratio
(relative







to that







of







R410A)






Condensation
° C.
19.4
15.0
16.3
12.8


glide
















TABLE 261







45% R1234yf, r = 0.5






















Comparative







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
214
215
216
217
192
218
219
220





R32
mass %
7.0
7.0
7.0
7.0
7.0
9.0
9.0
9.0


CO2
mass %
38.0
28.0
23.0
21.0
8.0
36.0
26.0
21.0


R125
mass %
5.0
10.0
12.5
13.5
20.0
5.0
10.0
12.5


R134a
mass %
5.0
10.0
12.5
13.5
20.0
5.0
10.0
12.5


R1234yf
mass %
45.0
45.0
45.0
45.0
45.0
45.0
45.0
45.0


GWP

296
542
666
715
1035
309
556
679


COP ratio
%
91.2
94.9
96.5
97.1
100.9
91.8
95.4
96.9



(relative











to that











of











R410A)










Refrigerating
%
141.2
119.5
108.0
103.3
73.1
138.0
116.1
104.7


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
22.2
22.9
22.4
21.9
14.5
21.7
22.0
21.2


glide










45% R1234yf, r = 0.5



















Comparative



Comparative
Comparative





Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
221
193
222
223
224
194
195
225





R32
mass %
9.0
9.0
11.0
11.0
11.0
11.0
15.0
15.0


CO2
mass %
19.0
6.0
34.0
24.0
18.0
4.0
30.0
20.0


R125
mass %
13.5
20.0
5.0
10.0
13.0
20.0
5.0
10.0


R134a
mass %
13.5
20.0
5.0
10.0
13.0
20.0
5.0
10.0


R1234yf
mass %
45.0
45.0
45.0
45.0
45.0
45.0
45.0
45.0


GWP

728
1049
323
569
717
1062
350
596


COP ratio
%
97.5
101.6
92.3
95.8
97.6
102.3
93.4
96.7



(relative











to that











of











R410A)










Refrigerating
%
100.1
70.3
134.8
112.9
99.1
67.6
128.4
106.4


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
20.7
12.2
21.2
21.1
19.7
9.7
20.0
19.0


glide










45% R1234yf, r = 0.5













Comparative Example
Comparative Example
Comparative Example


Item
Unit
196
197
198





R32
mass %
15.0
25.0
25.0


CO2
mass %
10.0
20.0
10.0


R125
mass %
15.0
5.0
10.0


R134a
mass %
15.0
5.0
10.0


R1234yf
mass %
45.0
45.0
45.0


GWP

843
417
664


COP ratio
%
99.9
96.0
99.4



(relative






to that






of






R410A)





Refrigerating
%
83.9
112.6
90.9


capacity ratio
(relative






to that






of






R410A)





Condensation
° C.
14.6
16.1
12.4


glide










45% R1234yf, r = 0.75























Comparative
Comparative








Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
226
227
199
200
228
229
230
231





R32
mass %
7.0
7.0
7.0
7.0
9.0
9.0
15.0
15.0


CO2
mass %
38.0
26.0
18.0
8.0
36.0
23.0
30.0
20.0


R125
mass %
7.5
16.5
22.5
30.0
7.5
17.3
7.5
15.0


R134a
mass %
2.5
5.5
7.5
10.0
2.5
5.7
2.5
5.0


R1234yf
mass %
45.0
45.0
45.0
45.0
45.0
45.0
45.0
45.0


GWP

348
705
944
1242
361
750
402
700


COP ratio
%
90.8
94.8
97.0
99.9
91.4
95.5
93.0
96.1



(relative











to that











of











R410A)










Refrigerating
%
142.0
116.7
98.7
76.2
138.8
111.2
129.3
108.1


capacity ratio
(relative











to that











of











R410A)










Condensation
° C.
21.7
21.7
19.8
13.6
21.2
20.6
19.5
18.1


glide



















45% R1234yf, r = 0.75













Comparative Example
Comparative Example
Comparative Example


Item
Unit
201
202
203





R32
mass %
15.0
25.0
25.0


CO2
mass %
10.0
20.0
10.0


R125
mass %
22.5
7.5
15.0


R134a
mass %
7.5
2.5
5.0


R1234yf
mass %
45.0
45.0
45.0


GWP

998
469
767


COP ratio
%
99.1
95.7
98.8



(relative






to that






of






R410A)





Refrigerating
%
86.4
113.5
92.7


capacity ratio
(relative






to that






of






R410A)





Condensation
° C.
13.6
15.6
11.8


glide









Method for determining approximate curves of point A, point Br, point Cr, point Dr, point Or, point Fr and point Pr in case of x with respect to R1234yf


Point A


The approximate expression with respect to the coordinates of the point A was determined as the function of the proportion (x) of R1234yf according to a least-squares method as follows, based on four compositions about the point A, revealed as described above. In other words, the coordinates (a,b,c) of the point A was found to be (−0.6902x+43.307, 100−a−x, 0.0).









TABLE 262





Point A





















R32
15.0
13.1
11.2
8.8



CO2
44.0
43.1
42.3
41.2



R125 + R134a
0.0
0.0
0.0
0.0



R1234yf
41.0
43.8
46.5
50.0










x = R1234yf
−0.6902x + 43.307



Approximate




expression for R32




Approximate
100 − R32 − x



expression for CO2










Point Br


The approximate expression with respect to the coordinates of the point Br was determined as the function of r and proportion (x) of R1234yf according to a least-squares method and calculation as follows, based on the compositions of the point Br, revealed as described above.










TABLE 263








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Br
R32
19.9
22.1
24.1
17.9
20.0
21.9
24.1
27.4
30.2
21.9
25.2
27.9



CO2
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R125 + R134a
39.1
36.9
34.9
38.3
36.2
34.3
34.9
31.6
28.8
34.3
31.0
28.3



R1234yf
41.0
41.0
41.0
43.8
43.8
43.8
41.0
41.0
41.0
43.8
43.8
43.8












Approximate
R32
−6.4r2 + 21.6r + 14.9
−6.4r2 + 20.8r + 13.1
−4.0r2 + 18.2r + 16
−4.8r2 + 19.2r + 13.5


expressions
CO2
0
0
0
0


for point Br
R125 + R134a
100 − R32 − x
100 − R32 − x
100 − R32 − x
100 − R32 − x


Approximate
x = R1234yf
41.0
43.8
41.0
43.8


expressions
a
−6.4
−6.4
−4.0
−4.8


for R32,
b
21.6
20.8
18.2
19.2


CO2, and
c
14.9
13.1
16.0
13.5










R125 + R134a,
Approximate
−6.4
−0.2857x + 7.7143   


represented
expression a




by r and x
Approximate
−0.2857x + 33.314
0.3571x + 3.5571 



expression b





Approximate
−0.6429x + 41.257
−0.8929x + 52.607   



expression c





Approximate
−6.4r2 + (−0.2857x + 33.314)r +
(−0.2857x + 7.7143)r2 + (0.3571x−3.5571)r +



expression for
(−0.6429x + 41.257)
(−0.8929x + 52.607)



R32





CO2
0.0
0.0



R125 + R134a
100 − R32 − x
100 − R32 − x

















TABLE 264








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Br
R32
17.9
20.0
21.9
15.9
18.0
19.9
21.9
25.2
27.9
19.9
23.1
25.8



CO2
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R125 + R134a
38.3
36.2
34.3
37.6
35.5
33.6
34.3
31.0
28.3
33.6
30.4
27.7



R1234yf
43.8
43.8
43.8
46.5
46.5
46.5
43.8
43.8
43.8
46.5
46.5
46.5












Approximate
R32
−6.4r2 + 20.8r + 13.1
−6.4r2 + 20.8r + 11.1
−4.8r2 + 19.2r + 13.5
−4.0r2 + 17.8r + 12.0


expressions
CO2
0
0
0
0


for point Br
R125 + R134a
100 − R32 − x
100 − R32 − x
100 − R32 − x
100 − R32 − x


Approximate
x = R1234yf
43.8
46.5
43.8
46.5


expressions
a
−6.4
−6.4
−4.8
−4.0


for R32,
b
20.8
20.8
19.2
17.8


CO2, and
c
13.1
11.1
13.5
12.0










R125 + R134a,
Approximate
−6.4
0.2963x − 17.778 


represented
expression a




by r and x
Approximate
20.8
−0.5185x + 41.911   



expression b





Approximate
−0.7407x + 45.544
−0.5556x + 37.833   



expression c





Approximate
−6.4r2 + 20.8r + (−0.7407x + 45.544)
(0.2963x − 17.778)r2 + (−0.5185x + 41.911)r +



expression for

(−0.5556x + 37.833)



R32





CO2
0.0
0.0



R125 + R134a
100 − R32 − x
100 − R32 − x

















TABLE 265








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Br
R32
15.9
18.0
19.9
13.4
15.4
17.3
19.9
23.1
25.8
17.3
20.4
23.0



CO2
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R125 + R134a
37.6
35.5
33.6
36.6
34.6
32.7
33.6
30.4
27.7
32.7
29.6
27.0



R1234yf
46.5
46.5
46.5
50.0
50.0
50.0
46.5
46.5
46.5
50.0
50.0
50.0












Approximate
R32
−6.4r2 + 20.8r + 11.1
−3.2r2 + 18.0r + 9.1
−4.0r2 + 17.8r + 12.0
−4.0r2 + 17.4r + 9.6


expressions
CO2
0
0
0
0


for point Br
R125 + R134a
100 − R32 − x
100 − R32 − x
100 − R32 − x
100 − R32 − x


Approximate
x = R1234yf
46.5
50.0
46.5
50.0


expressions
a
−6.4
−3.2
−4.0
−4.0


for R32,
b
20.8
18.0
17.8
17.4


CO2, and
c
11.1
9.1
12.0
9.6










R125 + R134a,
Approximate
0.9143x − 48.914 
−4.0


represented
expression a




by r and x
Approximate
−0.8x + 58.0  
−0.1143x + 23.114



expression b





Approximate
−0.5714x + 37.671   
−0.6857x + 43.886



expression c





Approximate
(0.9143x − 48.914)r2 + (−0.8x + 58) +
−4.0r2 + (−0.1143x + 23.114)r +



expression for
(−0.5714x + 37.671)
(−0.6857x + 43.886)



R32





CO2
0.0
0.0



R125 + R134a
100 − R32 − x
100 − R32 − x









Method for determining approximate curves of points Cr=0.25 to 1.0 and Dr=0.25 to 1.0


The respective approximate expressions with respect to the coordinates of the point Cr and the point Dr were each determined as the function of r and proportion (x) of R1234yf according to a least-squares method and calculation as follows, based on the compositions of the point Cr and the point Dr, revealed as described above.










TABLE 266








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Cr
R32
31.6
36.2
39.5
27.3
32.1
35.6
39.5
43.9
46.7
35.6
40.3
43.2



CO2
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R125 + R134a
27.4
22.8
19.5
28.9
24.1
20.6
19.5
15.1
12.3
20.6
15.9
13.0



R1234yf
41.0
41.0
41.0
43.8
43.8
43.8
41.0
41.0
41.0
43.8
43.8
43.8












Approximate
R32
−41.6r2 + 62.8r + 18.5
−41.6r2 + 64.4r + 13.8
−12.8r2 + 33.6r + 25.9
−14.4r2 + 36.8r + 20.8


expressions
CO2
0
0
0
0


for point Cr
R125 + R134a
100 − R32 − x
100 − R32 − x
100 − R32 − x
100 − R32 − x


Approximate
x = R1234yf
41.0
43.8
41.0
43.8


expressions
a
−41.6
−41.6
−12.8
−14.4


for R32,
b
62.8
64.4
33.6
36.8


CO2, and
c
18.5
13.8
25.9
20.8










R125 + R134a,
Approximate
−41.6
−0.5714x + 10.629   


represented
expression a




by r and x
Approximate
0.5714x + 39.371 
1.1429x − 13.257 



expression b





Approximate
−1.6786x + 87.321   
−1.8214x + 100.58   



expression c





Approximate
−41.6r2 + (0.5747x + 39.371)r +
(−0.5714x + 10.629)r2 + (1.1429x−13.257)r +



expression for
(−1.6786x + 87.321)
(−1.8214x + 100.58)



R32





CO2
0.0
0.0



R125 + R134a
100 − R32 − x
100 − R32 − x

















TABLE 267








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Cr
R32
27.3
32.1
35.6
23.1
28.3
31.9
35.6
40.3
43.2
31.9
36.8
39.8



CO2
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R125 + R134a
28.9
24.1
20.6
30.4
25.2
21.6
20.6
15.9
13.0
21.6
16.7
13.7



R1234yf
43.8
43.8
43.8
46.5
46.5
46.5
43.8
43.8
43.8
46.5
46.5
46.5












Approximate
R32
−41.6r2 + 64.4r + 13.8
−51.2r2 + 73.6r + 7.9
−14.4r2 + 36.8r + 20.8
−15.2r2 + 38.6r + 16.4


expressions
CO2
0
0
0
0


for point Cr
R125 + R134a
100 − R32 − x
100 − R32 − R1234yf
100 − R32 − x
100 − R32 − R1234yf


Approximate
x = R1234yf
43.8
46.5
43.8
46.5


expressions
a
−41.6
−51.2
−14.4
−15.2


for R32,
b
64.4
73.6
36.8
38.6


CO2, and
c
13.8
7.9
20.8
16.4










R125 + R134a,
Approximate
−3.5556x + 114.13   
−0.2963x − 1.4222   


represented
expression a




by r and x
Approximate
3.4074x − 84.844 
0.6667x + 7.6  



expression b





Approximate
−2.1852x + 109.51   
−1.6296x + 92.178   



expression c





Approximate
(−3.5556x + 114.13)r2 + (3.4074x − 84.844) +
(−0.2963x − 1.4222)r2 + (0.6667x + 7.6)r +



expression for
(−2.1852x + 109.51)
(−1.6296x + 92.178)



R32





CO2
0.0
0.0



R125 + R134a
100 − R32 − x
100 − R32 − x

















TABLE 268








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Cr
R32
23.1
28.3
31.9
17.9
23.3
27.2
31.9
36.8
39.8
27.2
32.3
35.5



CO2
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R125 + R134a
30.4
25.2
21.6
32.1
26.7
22.8
21.6
16.7
13.7
22.8
17.7
14.5



R1234yf
46.5
46.5
46.5
50.0
50.0
50.0
46.5
46.5
46.5
50.0
50.0
50.0












Approximate
R32
−51.2r2 + 73.6r + 7.9
−48.0r2 + 73.2r + 2.6
−15.2r2 + 38.6r + 16.4
−15.2r2 + 39.4r + 11.3


expressions
CO2
0
0
0
0


for point Cr
R125 + R134a
100 − R32 − R1234yf
100 − R32 − R1234yf
100 − R32 − R1234yf
100 − R32 − R1234yf


Approximate
x = R1234yf
46.5
50.0
46.5
50.0


expressions
a
−51.2
−48.0
−15.2
−15.2


for R32,
b
73.6
73.2
38.6
39.4


CO2, and
c
7.9
2.6
16.4
11.3










R125 + R134a,
Approximate
0.9143x − 93.714 
−15.2


represented
expression a




by r and x
Approximate
−0.1143x + 78.914   
0.2286x + 27.971 



expression b





Approximate
−1.5143x + 78.314   
−1.4571x + 84.157   



expression c





Approximate
(0.9143x − 93.714)r2 + (−0.1143x + 78.314) +
−15.2r2 + (0.2286x + 27.971)r +



expression for
(−1.5143x + 78.314)
(−1.4571x + 84.157)



R32





CO2
0.0
0.0



R125 + R134a
100 − R32 − x
100 − R32 − x

















TABLE 269








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Dr
R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



CO2
20.6
25.1
28.7
17.8
22.3
25.9
28.7
33.9
37.7
25.9
31.2
34.9



R125 + R134a
38.4
33.9
30.3
38.4
33.9
30.3
30.3
25.1
21.3
30.3
25.0
21.3



R1234yf
41.0
41.0
41.0
43.8
43.8
43.8
41.0
41.0
41.0
43.8
43.8
43.8












Approximate
R32
0.0
0.0
0.0
0.0


expressions
CO2
−28.8r2 + 54.0r + 8.9
−28.8r2 + 54.0r + 6.1
−11.2x2 + 34.8x + 14.1
−12.8r2 + 37.2r + 10.5


for point Dr
R125 + R134a
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x


Approximate
x = R1234yf
41.0
43.8
41.0
43.8


expressions
a
−28.8
−28.8
−11.2
−12.8


for R32,
b
54.0
54.0
34.8
37.2


CO2, and
c
8.9
6.1
14.1
10.5










R125 + R134a,
Approximate
−28.8
−0.5714x + 12.229   


represented
expression a




by r and x
Approximate
54.0
0.8571x − 0.3429 



expression b





Approximate
−x + 49.9
−1.2857x + 66.814   



expression c





Approximate
0.0
0.0



expression for





R32





CO2
−28.8r2 + 54.0r + (−x + 49.9)
(−0.5714x + 12.229)r2 + (0.8571x − 0.3429)r +





(−1.2857x + 66.814)



R125 + R134a
100 − CO2 − x
100 − CO2 − x

















TABLE 270








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Dr
R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



CO2
17.8
22.3
25.9
15.1
19.6
23.2
25.9
31.2
34.9
23.2
28.5
32.2



R125 + R134a
38.4
33.9
30.3
38.4
33.9
30.3
30.3
25.0
21.3
30.3
25.0
21.3



R1234yf
43.8
43.8
43.8
46.5
46.5
46.5
43.8
43.8
43.8
46.5
46.5
46.5












Approximate
R32
0.0
0.0
0.0
0.0


expressions
CO2
−28.8r2 + 54.0r + 6.1
−28.8r2 + 54r + 3.4
−12.8r2 + 37.2r + 10.5
−12.8r2 + 37.2r + 7.8


for point Dr
R125 + R134a
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x


Approximate
x = R1234yf
43.8
46.5
43.8
46.5


expressions
a
−28.8
−28.8
−12.8
−12.8


for R32,
b
54.0
54.0
37.2
37.2


CO2, and
c
6.1
3.4
10.5
7.8










R125 + R134a,
Approximate
−28.8
−12.8


represented
expression a




by r and x
Approximate
54.0
37.2



expression b





Approximate
−x + 49.9
−x + 54.3



expression c





Approximate
0.0
0.0



expression for





R32





CO2
−28.8r2 + 54.0r + (−x + 49.9)
−12.8r2 + 37.2r + (−x + 54.3)



R125 + R134a
100 − CO2 − x
100 − CO2 − x

















TABLE 271








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Dr
R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



CO2
15.1
19.6
23.2
11.6
16.1
19.8
23.2
28.5
32.2
19.8
25.0
28.7



R125 + R134a
38.4
33.9
30.3
38.4
33.9
30.2
30.3
25.0
21.3
30.2
25.0
21.3



R1234yf
46.5
46.5
46.5
50.0
50.0
50.0
46.5
46.5
46.5
50.0
50.0
50.0












Approximate
R32
0.0
0.0
0.0
0.0


expressions
CO2
−28.8r2 + 54r + 3.4
−25.6r2 + 52.0r + 0.2
−12.8r2 + 37.2r + 7.8
−12.0r2 + 35.8r + 4.9


for point Dr
R125 + R134a
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x


Approximate
x = R1234yf
46.5
50.0
46.5
50.0


expressions
a
−28.8
−25.6
−12.8
−12.0


for R32,
b
54.0
52.0
37.2
35.8


CO2, and
c
3.4
0.2
7.8
4.9










R125 + R134a,
Approximate
0.9143x − 71.314 
0.2286x − 23.429 


represented
expression a




by r and x
Approximate
−0.5714x + 80.571   
−0.4x + 55.8  



expression b





Approximate
−0.9143x + 45.914   
−0.8286x + 46.329   



expression c





Approximate
0.0
0.0



expression for





R32





CO2
(0.9143x − 71.314)r2 + (−0.5714x + 80.571) +
(0.2286x − 23.429)r2 + (−0.4x + 55.8)r +




(−0.9143x + 45.914)
(−0.8286x + 46.329)



R125 + R134a
100 − CO2 − x
100 − CO2 − x









Method for Determining Approximate Curve of Point Or


The point Or as the intersection of the line segment ABr and the line segment CrDr was shown in Examples and Comparative Examples, and the approximate expression with respect to the coordinates of the point Or was determined as the function of r and proportion (x) of R1234yf according to a least-squares method and calculation as follows, based on the compositions of the point Or.










TABLE 272








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Or
R32
19.0
20.3
21.4
17.1
18.5
19.5
21.4
22.8
23.8
19.5
21.0
22.0



CO2
8.2
11.0
13.2
6.7
9.4
11.7
13.2
16.3
18.5
11.7
14.9
17.1



R125 + R134a
31.8
27.7
24.4
32.4
28.3
25.0
24.4
19.9
16.7
25.0
20.3
17.1



R1234yf
41.0
41.0
41.0
43.8
43.8
43.8
41.0
41.0
41.0
43.8
43.8
43.8












Approximate
R32
−6.4r2 + 14.4r + 15.8
−12.8r2 + 19.2r + 13.1
−3.2r2 + 9.6r + 17.4
−4.0r2 + 11.0r + 15.0


expressions
CO2
−19.2r2 + 34.4r + 0.8 
−12.8r2 + 29.6r + 0.1 
−7.2r2 + 21.4r + 4.3
−8.0r2 + 22.8r + 2.3 


for point Or
R125 + R134a
100 −R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x


Calculation
x = R1234yf
41.0
43.8
41.0
43.8


of
a
−6.4
−12.8
−3.2
−4.0


approximate
b
14.4
19.2
9.6
11.0


expressions
c
15.8
13.1
17.4
15.0










for R32,
Approximate
−2.2857x + 87.314   
−0.2857x + 8.5143   


represented
expression a




by r and x
Approximate
1.7143x − 55.886 
0.5x − 10.9



expression b





Approximate
−0.9643x + 55.336   
−0.8571x + 52.543   



expression c














Calculation
x = R1234yf
41.0
43.8
41.0
43.8


of
a
−19.2
−12.8
−7.2
−8.0


approximate
b
34.4
29.6
21.4
22.8


expressions
c
0.8
0.1
4.3
2.3










for CO2,
Approximate
2.2857x − 112.91 
−0.2857x + 4.5143   


represented
expression a




by r and x
Approximate
−1.7143x + 104.69   
0.5x + 0.9 



expression b





Approximate
−0.25x + 11.05  
−0.7143x + 33.586   



expression c




Approximate
Approximate
(−2.2857x + 87.314)r2 + (1.7143x − 55.886)r +
(−0.2857x + 8.5143)r2 + (0.5x − 10.9) +


expressions
expression for
(−0.9643x + 55.336)
(−0.8571x + 52.543)


for O(r, x)
R32





Approximate
(2.2857x − 112.91)r2 + (−1.7143x + 104.69)r +
(−0.2857x + 4.5143)r2 + (0.5x + 0.9)r +



expression c
(−0.25x + 11.05)
(−0.7143x + 33.586)



for CO2





R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x

















TABLE 273








r=R125/(R125+R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Or
R32
17.1
18.5
19.5
15.3
16.7
17.8
19.5
21.0
22.0
17.8
19.3
20.4



CO2
6.7
9.4
11.7
5.1
8.0
10.3
11.7
14.9
17.1
10.3
13.5
15.7



R125 + R134a
32.4
28.3
25.0
33.1
28.8
25.4
25.0
20.3
17.1
25.4
20.7
17.4



R1234yf
43.8
43.8
43.8
46.5
46.5
46.5
43.8
43.8
43.8
46.5
46.5
46.5












Approximate
R32
−12.8r2 + 19.2r + 13.1
−9.6r2 + 17.2r + 11.6
−4.0r2 + 11.0r + 15.0
−3.2r2 + 10.0r + 13.6


expressions
CO2
−12.8r2 + 29.6r + 0.1 
−19.2r2 + 35.2r − 2.5 
−8.0r2 + 22.8r + 2.3 
−8.0r2 + 22.8r + 0.9 


for point Or
R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x


Calculation
x = R1234yf
43.8
46.5
43.8
46.5


of
a
−12.8
−9.6
−4.0
−3.2


approximate
b
19.2
17.2
11.0
10.0


expressions
c
13.1
11.6
15.0
13.6










for R32,
Approximate
1.1852x − 64.711 
0.2963x − 16.978 


represented
expression a




by r and x
Approximate
−0.7407x + 51.644   
−0.3704x + 27.222   



expression b





Approximate
−0.5556x + 37.433   
−0.5185x + 37.711   



expression c














Calculation
x = R1234yf
43.8
46.5
43.8
46.5


of
a
−12.8
−19.2
−8.0
−8.0


approximate
b
29.6
35.2
22.8
22.8


expressions
c
0.1
−2.5
2.3
0.9










for CO2,
Approximate
−2.3704x + 91.022   
−8.0


represented
expression a




by r and x
Approximate
2.0741x − 61.244 
22.8



expression b





Approximate
−0.963x + 42.278 
−0.5185x + 25.011   



expression c




Approximate
Approximate
(1.1852x − 64.711)r2 + (−0.7407x + 51.644)r +
(0.2963x − 16.978)r2 + (−0.3704x + 27.222)r +


expressions
expression for
(−0.5556x + 37.433)
(−0.5185x + 37.711)


for O(r, x)
R32





Approximate
(−2.3704x + 91.022)r2 + (2.0741x − 61.244)r +
−8.0r2 + 22.8r + (−0.5185x + 25.011)



expression c
(−0.963x + 42.278)




for CO2





R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x

















TABLE 274








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Or
R32
15.3
16.7
17.8
13.0
14.4
15.5
17.8
19.3
20.4
15.5
17.1
18.2



CO2
5.1
8.0
10.3
3.1
6.1
8.5
10.3
13.5
15.7
8.5
11.7
14.0



R125 + R134a
33.1
28.8
25.4
33,9
29.5
26.0
25.4
20.7
17.4
26.0
21.2
17.8



R1234yf
46.5
46.5
46.5
50.0
50.0
50.0
46.5
46.5
46.5
50.0
50.0
50.0












Approximate
R32
−9.6r2 + 17.2r + 11.6
−9.6r2 + 17.2r + 9.3
−3.2r2 + 10.0r + 13.6
−4.0r2 + 11.4r + 10.8


expressions
CO2
−19.2r2 + 35.2r − 2.5 
−19.2r2 + 36.0r − 4.7 
−8.0r2 + 22.8r + 0.9 
−7.2r2 + 21.8r − 0.6 


for point Or
R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x


Calculation
x = R1234yf
46.5
50.0
46.5
50.0


of
a
−9.6
−9.6
−3.2
−4.0


approximate
b
17.2
17.2
10.0
11.4


expressions
c
11.6
9.3
13.6
10.8


for R32,
Approximate














represented
expression a
−9.6
−0.2286x + 7.4286   


by r and x
Approximate
17.2
0.4x − 8.6 



expression b





Approximate
−0.6571x + 42.157   
−0.8x + 50.8  



expression c














Calculation
x = R1234yf
46.5
50.0
46.5
50.0


of
a
−19.2
−19.2
−8.0
−7.2


approximate
b
35.2
36.0
22.8
21.8


expressions
c
−2.5
−4.7
0.9
−0.6


for CO2,
Approximate














represented
expression a
−19.2
0.2286x − 18.629 


by r and x
Approximate
0.2286x + 24.571 
−0.2857x + 36.086   



expression b





Approximate
−0.6286x + 26.729   
−0.4286x + 20.829   



expression c




Approximate
Approximate
−9.6r2 + 17.2r + (−0.6571x + 42.157)
(−0.2286x + 7.4286)r2 + (0.4x − 8.6)r +


expressions
expression for

(−0.8x + 50.8)


for O(r, x)
R32





Approximate
−19.2r2 + (0.2286x + 24.571)r +
(0.2286x − 18.629)r2 + (−0.2857x + 36.086)r +



expression c
(−0.6286x + 26.729)
(−0.4286x + 20.829)



for CO2





R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x









Method for Determining Approximate Curves of Points Fr and Pr


The point Fr and the point Pr were shown in Examples and Comparative Examples, and the respective approximate expressions with respect to the coordinates of the point Fr and the point Pr were each determined as the function of r and proportion (x) of R1234yf according to a least-squares method and calculation as follows, based on each composition.










TABLE 275








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Fr
R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



CO2
39.5
40.5
41.2
35.4
36.6
37.4
41.2
42.6
43.1
37.4
38.5
40.0



R125 + R134a
19.5
18.5
17.8
20.8
19.6
18.8
17.8
16.4
15.9
18.8
17.
16.2



R1234yf
41.0
41.0
41.0
43.8
43.8
43.8
41.0
41.0
41.0
43.8
43.8
43.8












Approximate
R32
0.0
0.0
0.0
0.0


expressions
CO2
−9.6r2 + 14.0r + 36.6
−12.8r2 + 17.6r + 31.8
−7.2x2 + 14.6x + 35.7
3.2r2 + 0.4r + 36.4


for point Fr
R125 + R134a
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x


Approximate
x = R1234yf
41.0
43.8
41.0
43.8


expressions
a
−9.6
−12.8
−7.2
3.2


for R32,
b
14.0
17.6
14.6
0.4


CO2, and
c
36.6
31.8
35.7
36.4










R125 + R134a,
Approximate
−1.1429x + 37.257   
3.7143x − 159.49 


represented
expression a




by r and x
Approximate
1.2857x − 38.714 
−5.0714x + 222.53   



expression b





Approximate
−1.7143x + 106.89   
0.25x + 25.45



expression c





Approximate
0.0
0.0



expression for





R32





CO2
(−1.1429x + 37.257)r2 + (1.2857x − 38.714)r −
(3.7143x − 159.49)r2 + (−5.0714x + 222.53)r +




(−1.7143x + 106.89)
(0.25x + 25.45)



R125 + R134a
100 − CO2 − x
100 − CO2 − x

















TABLE 276








r = R125/(R125 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Fr
R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



CO2
35.4
36.6
37.4
31,5
32.3
33.5
37.4
38.5
40.0
33.5
35.3
35.9



R125 + R134a
20.8
19.6
18.8
22.0
21.2
20.0
18.8
17.7
16.2
20.0
18.2
17.6



R1234yf
43.8
43.8
43.8
46.5
46.5
46.5
43.8
43.8
43.8
46.5
46.5
46.5












Approximate
R32
0.0
0.0
0.0
0.0


expressions
CO2
−12.8r2 + 17.6r + 31.8
12.8r2 − 1.6r + 31.1
3.2r2 + 0.4r + 36.4
−9.6r2 + 19.2r + 26.3


for point Fr
R125 + R134a
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x


Approximate
x = R1234yf
43.8
46.5
43.8
46.5


expressions
a
−12.8
12.8
3.2
−9.6


for R32,
b
17.6
−1.6
0.4
19.2


CO2, and
c
31.8
31.1
36.4
26.3










R125 + R134a,
Approximate
9.4815x − 428.09 
−4.7407x + 210.84   


represented
expression a




by r and x
Approximate
−7.1111x + 329.07   
6.963x − 304.58



expression b





Approximate
−0.2593x + 43.156   
−3.7407x + 200.24   



expression c





Approximate
0.0
0.0



expression for





R32





CO2
(9.4815x − 428.09)r2 + (−7.1111x + 329.07)r +
(−4.7407x + 210.84)r2 + (6.963x − 304.58)r +




(−0.2593x + 43.156)
(−3.7407x + 200.24)



R125 + R134a
100 − CO2 − x
100 − CO2 − x

















TABLE 277








r = R125/(R125 + R134a)



















Item
0.250
0.310
0.370
0.250
0.310
0.370
0.500
0.750
1.000
0.500
0.750
1.000























Point Fr
R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



CO2
31.5
31.7
32.5
26.1
27.0
27.6
33.5
35.3
35.9
28.8
30.4
31.8



R125 + R134a
22.0
21.8
21.0
23.9
23.0
22.4
20.0
18.2
17.6
21.2
19.6
18.2



R1234yf
46.5
46.5
46.5
50.0
50.0
50.0
46.5
46.5
46.5
50.0
50.0
50.0












Approximate
R32
0.0
0.0
0.0
0.0


expressions
CO2
83.333r2 − 43.333r +
−41.667r2 + 38.333r +
−9.6r2 + 19.2r + 26.3
1.612 + 8.4r + 25.0


for point Fr

37.125
19.121





R125 + R134a
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x
100 − CO2 − x


Approximate
x = R1234yf
46.5
50.0
46.5
50.0


expressions
a
83.333
−41.667
−9.6
−1.6


for R32,
b
−43.333
38.333
19.2
8.4


CO2, and
c
37.125
19.121
26.3
25.0










R125 + R134a,
Approximate
−35.714x + 1744.0   
2.2857x − 115.89 


represented
expression a




by r and x
Approximate
23.333x − 1128.3 
−3.0857x + 162.69   



expression b





Approximate
−5.144x + 276.32 
−0.3714x + 43.571   



expression c





Approximate
0.0
0.0



expression





for R32





CO2
(−35.714x + 1744.0)r2 + (23.333x − 1128.3)r +
(2.2857x − 115.89)r2 + (−3.0857x + 162.69)r +




(−5.144x + 276.32)
(−0.3714x + 43.571)



R125 + R134a
100 − CO2 − x
100 − CO2 − x

















TABLE 278








r = R125/(R12 5 + R134a)



















Item
0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000























Point Pr
R32
12.8
14.3
15.4
12.0
13.6
14.7
15.4
11.4
7.7
14.7
9.9
6.6



CO2
12.2
15.2
17.4
10.1
12.9
15.1
17.4
25.1
31.5
15.1
23.5
29.6



R125 + R134a
34.0
29.5
26.2
53.9
56.7
58.9
26.2
22.5
19.8
58.9
67.3
73.4



R1234yf
41.0
41.0
41.0
43.8
43.8
43.8
41.0
41.0
41.0
43.8
43.8
43.8












Approximate
R32
−12.8r2 + 20.0r + 8.6
−16.0r2 + 22.8r + 7.3
2.4r2 − 19.0r + 24.3
12.0r2 − 34.2r + 28.8


expressions
CO2
−25.6r2 + 40.0r + 3.8
−19.2r2 + 34.4r + 2.7
−10.4r2 + 43.8r − 1.9
−18.4r2 + 56.6r − 8.6


for point Pr
R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x


Calculation
x = R1234yf
41.0
43.8
41.0
43.8


of
a
−12.8
−16.0
2.4
12.0


approximate
b
20.0
22.8
−19.0
−34.2


expressions
c
8.6
7.3
24.3
28.8










for R32,
Approximate
−1.1429x + 34.057
3.4286x − 138.17


represented
expression a




by r and x
Approximate
  1.0x − 21.0
−5.4286x + 203.57 



expression b





Approximate
−0.4643x + 27.636
1.6071x − 41.593



expression c














Calculation
x = R1234yf
41.0
43.8
41.0
43.8


of
a
−25.6
−19.2
−10.4
−18.4


approximate
b
40.0
34.4
43.8
56.6


expressions
c
3.8
2.7
−1.9
−8.6










for CO2,
Approximate
 2.2857x − 119.31
−2.8571x + 106.74


represented
expression a




by r and x
Approximate
  −2.0x + 122.0
 4.5714x − 143.63



expression b





Approximate
−0.3929x + 19.907
−2.3929x + 96.207



expression c




Approximate
Approximate
(−1.1429x + 34.057)r2 +
(3.4286x − 138.17)r2 +


expressions
expression
(1.0x − 21.0)r + (−0.4643x + 27.636)
(−5.4286x + 203.57) + (1.6071x − 41.593)


for P(r, x)
for R32





Approximate
(2.2857x − 119.31)r2 +
(−2.8571x + 106.74)r2 +



expression c
(−2.0x + 122.0)r + (−0.3929x + 19.907)
(4.5714x − 143.63)r + (−2.3929x + 96.027)



for CO2





R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x


















TABLE 279









r = R125/(R125 + R134a)




















Item

0.250
0.375
0.500
0.250
0.375
0.500
0.500
0.750
1.000
0.500
0.750
1.000





Point Pr
R32
12.0
13.6
14.7
11.3
12.8
13.1
14.7
9.9
6.6
13.1
8.7
5.9



CO2
10.1
12.9
15.1
7.8
10.7
13.6
15.1
23.5
29.6
13.6
21.7
27.4



R125 + R134a
53.9
56.7
58.9
34.4
30.0
26.8
58.9
67.3
73.4
26.8
23.1
20.2



R1234yf
43.8
43.8
43.8
46.5
46.5
46.5
43.8
43.8
43.8
46.5
46.5
46.5












Approximate
R32
−16.0r2 + 22.8r + 7.3
−38.4r2 + 36.0r + 4.7
12.0r2 −34.2r + 28.8
12.8r2 − 33.6r + 26.7


expressions
CO2
−19.2r2 + 34.4r + 2.7
23.2r + 2.0
−18.4r2 + 56.6r − 8.6
−19.2r2 + 56.4r − 9.8


for point Pr
R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R 32 − CO2 − x
100 − R32 − CO2 − x


Calculation
x = R1234yf
43.8
46.5
43.8
46.5


of
a
−16.0
−38.4
12.0
12.8


approximate
b
22.8
36.0
−34.2
−33.6


expressions
c
7.3
4.7
28.8
26.7










for R32,
Approximate
−8.2963x + 347.38
0.2963x − 0.9778


represented
expression a




by r and x
Approximate
 4.8889x − 191.33
0.2222x − 43.933



expression b





Approximate
−0.963x + 49.478
−0.7778x + 62.867 












expression c















Calculation
x = R1234yf
43.8
46.5
43.8
46.5


of
a
−19.2
0.0
−18.4
−19.2


approximate
b
34.4
23.2
56.6
56.4


expressions
c
2.7
2.0
−8.6
−9.8










for CO2,
Approximate
 7.1111x − 330.67
−0.2963x − 5.4222


represented
expression a




by r and x
Approximate
−4.1481x + 216.09
−0.0741x + 59.844



expression b





Approximate
−0.2593x + 14.056
−0.4444x + 10.867



expression c




Approximate
Approximate
(−8.2963x + 347.38)r2 + (4.8889x − 191.33)
(0.2963x − 0.9778)r2 + (0.2222x − 43.933)


expressions
expression
r + (−0.963x + 49.478)
r + (−0.7778x + 62.867)


for P(r, x)
for R32





Approximate
(7.1111x − 330.67)r2 + (−4.1481x + 216.09)
(−0.2963x−5.4222)r2 + (−0.0741x + 59.844)



expression c
r + (−0.2593x + 14.056)
r + (−0.4444x + 10.867)



for CO2





R125 + R134a
10 0− R32 − CO2 − x
100 − R32 − CO2 − x


















TABLE 280









r = R125/(R125 + R134a)




















Item

0.250
0.310
0.370
0.250
0.310
0.370
0.500
0.750
1.000
0.500
0.750
1.000





Point Pr
R32
11.3
12.2
12.8
10.5
11.2
11.9
13.1
8.7
5.9
10.8
6.8
3.0



CO2
7.8
9.2
10.7
4.7
6.5
7.7
13.6
21.7
27.4
11.8
19.7
26.3



R125 + R134a
34.4
32.1
30.0
34.8
32.3
30.4
26.8
23.1
20.2
27.4
23.5
20.7



R1234yf
46.5
46.5
46.5
50.0
50.0
50.0
46.5
46.5
46.5
50.0
50.0
50.0












Approximate
R32
−41.667r2 + 38.333r + 4.3208
11.667r + 7.5833
12.8r2 − 33.6r + 26.7
1.6r2 − 18.0r + 19.4


expressions
CO2
13.889r2 + 15.556r + 3.0431
−83.333r2 +
−19.2r2 + 56.4r − 9.8
−10.4r2 + 44.6r − 7.9


for point Pr


76.667r − 9.2583





R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x
100 − R32 − CO2 − x


Calculation
x = R1234yf
46.5
50.0
46.5
50.0


of
a
−41.6670
0.0000
12.8
1.6


approximate
b
38.3330
11.6670
−33.6
−18.0


expressions
c
4.3206
7.5833
26.7
19.4










for R32,
Approximate
11.905x − 595.24
−3.2x + 161.6


represented
expression a




by r and x
Approximate
−7.6189x + 392.61 
4.4571x − 240.86



expression b





Approximate
−0.9322x − 39.027 
−2.0857x + 123.69 



expression c














Calculation
x = R1234yf
46.5
50.0
46.5
50.0


of
a
13.889
−83.333
−19.2
−10.4


approximate
b
15.556
76.667
56.4
44.6


expressions
c
3.043
−9.258
−9.8
−7.9










for CO2,
Approximate
−27.778x + 1305.6
2.5143x − 136.11


represented
expression a




by r and x
Approximate
 17.46x − 796.35
−3.3714x + 213.17 



expression b





Approximate
−3.5147x + 166.48
0.5429x − 35.043



expression c




Approximate
Approximate
(11.905x − 595.24)r2 + (−7.6189x + 392.61)r +
(−3.2x + 161.6)r2 + (4.4571x − 240.86)r +


expressions
expression
(0.9322x − 39.027)
(−2.0857x + 123.69)


for P(r, x)
for R32





Approximate
(−27.778x + 1305.6)r2 + (17.46x − 796.35)r +
(2.5143x − 136.11)r2 + (−3.3714x + 213.17)r +



expression c
(−3.5147x + 166.48)
(0.5429x − 35.043)



for CO2





R125 + R134a
100 − R32 − CO2 − x
100 − R32 − CO2 − x









(1-7) Various Refrigerants 3


1. Composition


The composition of the present disclosure contains a refrigerant, and examples of the refrigerant include “refrigerant 3A” and “refrigerant 3B”. Refrigerant 3A and refrigerant 3B will each be described below. As used herein, “the refrigerant of the present disclosure” means refrigerant 3A and refrigerant 3B.


(1-7-1) Refrigerant 3A


The refrigerant contained in the composition of the present disclosure contains HFO-1132(Z) and HFO-1234yf in one embodiment. This refrigerant may be sometimes referred to as “refrigerant 3A”.


In refrigerant 3A, the content of HFO-1132(Z) is 53.0 to 59.5% by mass, and the content of HFO-1234yf is 47.0 to 40.5% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


Refrigerant 3A has such a configuration and thus refrigerant 3A has the following desired properties as an R134a alternative refrigerant: (1) having a sufficiently small GWP (100 or less), (2) having a COP equivalent to or more than that of R134a, (3) having a refrigerating capacity equivalent to or more than that of R134a, and (4) having a lower flammability (Class 2L) in the ASHRAE standard.


In the present items, the phrase “having a sufficiently small GWP” means to have a GWP of usually 100 or less, preferably 75 or less, more preferably 50 or less, and further preferably 25 or less.


When the content off-WO-1132(Z) based on the total mass of WO-1132(Z) and HFO-1234yf is more than 59.5% by mass in refrigerant 3A, a problem arises in that refrigerant 3A becomes weakly flammable.


Refrigerant 3A has a refrigerating capacity of usually 95% or more, preferably 98% or more, more preferably 99% or more, further preferably 100% or more, and particularly preferably 100.5% or more with respect to R134a, from the viewpoint of enabling reduction of power consumption during operation in comparison with a commercial R134a refrigeration apparatus.


Refrigerant 3A has a GWP of 100 or less and thus can significantly suppress the environmental load compared with other general-purpose refrigerants from the viewpoint of global warming.


Refrigerant 3A has a ratio between the power consumed in a refrigeration cycle and refrigerating capacity (coefficient of performance (COP)) of 100% or more with respect to R134a, and therefore refrigerant 3A can be applied to a commercial R134a refrigeration apparatus without a large design change.


Preferably, refrigerant 3A has a higher ratio between power consumed in a refrigeration cycle and refrigerating capacity (coefficient of performance (COP)) with respect to R134a in terms of energy consumption efficiency. Specifically, the COP with respect to R134a is preferably 98% or more, more preferably 99% or more, further preferably 100% or more, and particularly preferably 101% or more.


In refrigerant 3A, it is preferred that the content of HFO-11320 be 53.0 to 59.0% by mass, and the content of HFO-1234yf be 47.0 to 41.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


In refrigerant 3A, it is more preferred that the content of HFO-1132(Z) be 54.0 to 59.0% by mass, and the content of HFO-1234yf be 46.0 to 41.0% by mass, based on the total mass of HFO-1132(Z) and HFO-12343f.


In refrigerant 3A, it is further preferred that the content of HFO-1132(Z) be 55.0 to 59.0% by mass, and the content of HFO-1234yf be 45.0 to 41.0% by mass, based on the total mass of HFO-1132(Z) and HFO-12343f.


In refrigerant 3A, it is particularly preferred that the content of HFO-1132(Z) be 56.0 to 59.0% by mass, and the content of HFO-1234yf be 44.0 to 41.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


Refrigerant 3A may usually contain 99.5% by mass or more of HFO-1132(Z) and HFO-1234yf in terms of the sum of the concentrations of these. In the present disclosure, the total amount of HFO-1132(Z) and HFO-1234yf in the entire refrigerant 3A is preferably 99.7% by mass or more, more preferably 99.8% by mass or more, and further preferably 99.9% by mass or more.


Refrigerant 3A can further contain other refrigerants in addition to HFO-1132(Z) and HFO-1234yf within a range in which other refrigerants do not impair the above properties. In this case, the content of other refrigerants in the entire refrigerant 3A is preferably 0.5% by mass or less, more preferably 0.3% by mass or less, further preferably 0.2% by mass or less, and particularly preferably 0.1% by mass or less. Other refrigerants are not limited and can be widely selected from known refrigerants which are widely used in this field. Refrigerant 3A may comprise one other refrigerant alone or may comprise two or more other refrigerants.


In the present disclosure, refrigerant 3A is preferably used for operating a refrigeration cycle in which the evaporating temperature is −60 to 20° C., from the viewpoint of sufficiently cooling the interior of a room, and an object to be cooled.


In the refrigeration cycle in which refrigerant 3A is used, the evaporating temperature is more preferably 15° C. or lower, even more preferably 10° C. or lower, further preferably 5° C. or lower, and particularly preferably lower than 0° C. from the viewpoint of sufficiently cooling the interior of a room, and an object to be cooled.


In the refrigeration cycle in which refrigerant 3A is used, the evaporating temperature is preferably −55° C. or higher, more preferably −50° C. or higher, further preferably −45° C. or higher, and particularly preferably −40° C. or higher from the viewpoint of setting the evaporating pressure to 0.02 MPa or higher.


In the refrigeration cycle in which refrigerant 3A is used, the evaporating temperature is more preferably −55° C. or higher and 15° C. or lower, even more preferably −50° C. or higher and 10° C. or lower, further preferably −45° C. or higher and 5° C. or lower, and particularly preferably −40° C. or higher and lower than 0° C.


It is particularly preferred that refrigerant 3A consist of HFO-1132(Z) and HFO-1234yf. In other words, it is particularly preferred for refrigerant 3A that the total concentration of FIFO-1132(Z) and HFO-1234yf in the entire refrigerant 3A be 100% by mass.


When refrigerant 3A consists of HFO-1132(Z) and HFO-1234yf, it is preferred that the content of HFO-1132(Z) be 53.0 to 59.5% by mass, and the content of HFO-1234yf be 47.0 to 40.5% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


When refrigerant 3A consists of HFO-1132(Z) and HFO-1234yf, it is even more preferred that the content of HFO-1132(Z) be 54.0 to 59.0% by mass, and the content of HFO-1234yf be 46.0 to 41.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf


When refrigerant 3A consists of HFO-1132(Z) and HFO-1234yf, it is further preferred that the content of HFO-1132(Z) be 55.0 to 59.0% by mass, and the content of HFO-1234yf be 45.0 to 41.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


When refrigerant 3A consists of HFO-1132(Z) and HFO-1234yf, it is particularly preferred that the content of HFO-1132(Z) be 56.0 to 59.0% by mass, and the content of HFO-1234yf be 44.0 to 41.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


When refrigerant 3A consists of HFO-1132(Z) and HFO-1234yf, it is preferred that the content of HFO-1132(Z) be 53.0 to 59.5% by mass, and the content of HFO-1234yf be 47.0 to 40.5% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf, and refrigerant 3A be used for operating a refrigeration cycle in which the evaporating temperature is −55° C. to 15° C.


When refrigerant 3A consists of HFO-1132(Z) and HFO-1234yf, it is more preferred that the content of HFO-1132(Z) be 54.0 to 59.0% by mass, and the content of HFO-1234yf be 46.0 to 41.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf, and refrigerant 3A be used, for operating a refrigeration cycle in which the evaporating temperature is −50° C. to 10° C.


When refrigerant 3A consists of HFO-1132(Z) and HFO-1234yf, it is further preferred that the content of HFO-1132(Z) be 55.0 to 59.0% by mass, and the content of HFO-1234yf be 45.0 to 41.0% by mass, based on the total mass of WO-1132(Z) and HFO-1234yf, and refrigerant 3A be used for operating a refrigeration cycle in which the evaporating temperature is −45° C. to 5° C.


When refrigerant 3A consists of HFO-1132(Z) and HFO-1234yf, it is particularly preferred that the content of HFO-1132(Z) be 56.0 to 59.0% by mass, and the content of HFO-1234yf be 44.0 to 41.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf, and refrigerant 3A be used for operating a refrigeration cycle in which the evaporating temperature is −40° C. or higher and less than 0° C.


(1-7-2) Refrigerant 3B


1.2 Refrigerant 3B


In one embodiment, the refrigerant contained in the composition of the present disclosure contains HFO-1132(Z) and HFO-1234yf, and the content of HFO-1132(Z) is 41.0 to 49.2% by mass, and the content of HFO-1234yf is 59.0 to 50.8% by mass, based on the total mass of HFO-1132(Z) and HFO-1234y. This refrigerant is sometimes referred to as the “refrigerant 3B”.


Refrigerant 3B has such a configuration and thus has the following desired properties as an R134a alternative refrigerant: (1) having a sufficiently small GWP (100 or less), (2) having a COP equivalent to or more than that of R134a, (3) having a refrigerating capacity equivalent to or more than that of R134a, and (4) having a lower flammability (Class 2L) in the ASHRAE standard.


In the present items, the phrase “having a sufficiently small GWP” means to have a GWP of usually 100 or less, preferably 75 or less, more preferably 50 or less, and further preferably 25 or less.


Refrigerant 3B has a GWP of 100 or less and thus can significantly suppress the environmental load compared with other general-purpose refrigerants from the viewpoint of global warming.


Refrigerant 3B has a refrigerating capacity of usually 95% or more, preferably 98% or more, more preferably 99% or more, further preferably 100% or more, and particularly preferably 101% or more with respect to R134a, from the viewpoint of enabling reduction of power consumption during operation in comparison a commercial R134a refrigeration apparatus.


Refrigerant 3B has a ratio between power consumed in a refrigeration cycle and refrigerating capacity (coefficient of performance (COP)) of 100% or more with respect to R134a, and therefore refrigerant 3B can be applied to a commercial R134a refrigeration apparatus without a large design change.


Preferably, refrigerant 3B has a higher ratio between power consumed in a refrigeration cycle and refrigerating capacity (coefficient of performance (COP)) with respect to R134a in terms of energy consumption efficiency. Specifically, the COP with respect to R134a is preferably 98% or more, more preferably 99% or more, further preferably 100% or more, and particularly preferably 101% or more.


In refrigerant 3B, it is preferred that the content of HFO-1132(Z) be 42.0 to 49.2% by mass, and the content of HFO-1234yf be 58.0 to 50.8% by mass, based on the total mass of HFO-1132(Z) and HFO-12343f.


In refrigerant 3B, it is more preferred that the content of HFO-1132(Z) be 43.0 to 49.2% by mass, and the content of HFO-1234yf be 57.0 to 50.8% by mass, based on the total mass of HFO-1132(2) and HFO-1234yf.


In refrigerant 3B, it is further preferred that the content of HFO-1132(Z) be 44.0 to 49.0% by mass, and the content of HFO-1234yf be 56.0 to 51.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


Refrigerant 3B may usually contain 99.5% by mass or more of HFO-1132(Z) and HFO-1234yf in terms of the sum of the concentrations of these. In the present disclosure, the total amount of HFO-1132(Z) and HFO-1234yf in the entire refrigerant 3B is preferably 99.7% by mass or more, more preferably 99.8% by mass or more, and further preferably 99.9% by mass or more.


Refrigerant 3B can further contain other refrigerants in addition to HFO-1132(Z) and HFO-1234yf within a range in which other refrigerants do not impair the above properties. In this case, the content of other refrigerants in the entire refrigerant 3B is preferably 0.5% by mass or less, more preferably 0.3% by mass or less, further preferably 0.2% by mass or less, and particularly preferably 0.1% by mass or less. Other refrigerants are not limited and can be widely selected from known refrigerants which are widely used in this field. Refrigerant 3B may comprise one other refrigerant alone or may comprise two or more other refrigerants.


In the present disclosure, refrigerant 3B is preferably used for operating a refrigeration cycle in which the evaporating temperature is −60 to 20° C., from the viewpoint of sufficiently cooling the interior of a room, and an object to be cooled.


In the refrigeration cycle in which refrigerant 3B is used, the evaporating temperature is more preferably 15° C. or lower, even more preferably 10° C. or lower, further preferably 5° C. or lower, and particularly preferably lower than 0° C. from the viewpoint of sufficiently cooling the interior of a room, and an object to be cooled.


In the refrigeration cycle in which refrigerant 3B is used, the evaporating temperature is preferably −55° C. or higher, more preferably −50° C. or higher, further preferably −45° C. or higher, and particularly preferably −40° C. or higher from the viewpoint of setting the evaporating pressure to 0.02 MPa or higher.


In the refrigeration cycle in which refrigerant 3B is used, the evaporating temperature is more preferably −55° C. or higher and 15° C. or lower, even more preferably −50° C. or higher and 10° C. or lower, further preferably −45° C. or higher and 5° C. or lower, and particularly preferably −40° C. or higher and lower than 0° C.


It is particularly preferred that refrigerant 3B consist of HFO-1132(Z) and HFO-1234yf. In other words, it is particularly preferred for refrigerant 3B that the total concentration of HFO-1132(Z) and HFO-1234yf in the entire refrigerant 3B be 100% by mass.


When refrigerant 3B consists of HFO-1132(Z) and HFO-1234yf it is preferred that the content of HFO-1132(Z) be 41.0 to 49.2% by mass, and the content of HFO-1234yf be 59.0 to 50.8% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


When refrigerant 3B consists of HFO-1132(Z) and HFO-1234yf, it is more preferred that the content of HFO-1132(Z) is 42.0 to 49.2% by mass, and the content of HFO-1234yf is 58.0 to 50.8% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


When refrigerant 3B consists of HFO-1132(Z) and HFO-1234yf, it is further preferred that the content of HFO-1132(Z) be 43.0 to 49.2% by mass, and the content of HFO-1234yf be 57.0 to 50.8% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


When refrigerant 3B consists of HFO-1132(Z) and HFO-1234yf, it is particularly preferred that the content of HFO-1132(Z) be 44.0 to 49.0% by mass, and the content of HFO-1234yf be 56.0 to 51.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf.


When refrigerant 3B consists of HFO-1132(Z) and HFO-1234yf, it is preferred that the content of HFO-1132(Z) be 41.0 to 49.2% by mass, and the content of HFO-1234yf be 59.0 to 50.8% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf, and refrigerant 3B is used for operating a refrigeration cycle in which the evaporating temperature is −55° C. to 15° C.


When refrigerant 3B consists of HFO-1132(Z) and HFO-1234yf, it is more preferred that the content of HFO-1132(Z) be 42.0 to 49.2% by mass, and the content of HFO-1234yf be 58.0 to 50.8% by mass, based on the total mass of HFO-1132(Z) and HFO-1234y f, and refrigerant 3B be used for operating a refrigeration cycle in which the evaporating temperature is −50° C. to 10° C.


When refrigerant 3B consists of HFO-1132(Z) and HFO-1234yf, it is further preferred that the content of HFO-1132(Z) is 43.0 to 49.2% by mass, and the content of HFO-1234yf is 57.0 to 50.8% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf, and refrigerant 3B be used for operating a refrigeration cycle in which the evaporating temperature is −45° C. to 5° C.


When refrigerant 3B consists of HFO-1132(Z) and HFO-1234yf, it is particularly preferred that the content of HFO-1132(Z) be 44.0 to 49.0% by mass, and the content of HFO-1234yf be 56.0 to 51.0% by mass, based on the total mass of HFO-1132(Z) and HFO-1234yf, and refrigerant 3B be used for operating a refrigeration cycle in which the evaporating temperature is −40° C. or higher and less than 0° C.


1.3 Applications


The composition containing a refrigerant according to the present disclosure can be widely used as a working fluid in existing applications of a refrigerant in 1) a refrigeration method comprising the step of operating a refrigeration cycle, 2) a method for operating a refrigeration apparatus operating a refrigeration cycle, and the like.


Here, the above-mentioned refrigeration cycle means circulating a refrigerant (refrigerant 3A and refrigerant 3B of the present disclosure) via a compressor through the interior of a refrigeration apparatus in a state of only the refrigerant or in a state of a refrigerant composition or a refrigerator oil-containing working fluid described below to convert energy.


The present disclosure also encompasses the use of the refrigerants (or compositions comprising them) of the present disclosure in a refrigeration method, the use of the refrigerants (or compositions comprising them) of the present disclosure in a method for operating a refrigeration apparatus or the like, and further refrigeration apparatuses having the refrigerants (or compositions comprising them) of the present disclosure, and the like.


The composition containing refrigerant 3A according to the present disclosure is preferably used for operating a refrigeration cycle in which the evaporating temperature is −60 to 20° C., from the viewpoint of sufficiently cooling the interior of a room, and an object to be cooled. In addition, by using the composition containing refrigerant 3A according to the present disclosure for operating the refrigeration cycle in which the evaporating temperature is −60 to 20° C., the COP during operation increases in comparison with a commercial R134a refrigeration apparatus, and therefore the power consumption can be reduced.


In the refrigeration cycle in which the composition containing refrigerant 3A is used, the evaporating temperature is more preferably 15° C. or lower, even more preferably 10° C. or lower, further preferably 5° C. or lower, and particularly preferably lower than 0° C. from the viewpoint of sufficiently cooling the interior of a room, and an object to be cooled.


In the refrigeration cycle in which the composition containing refrigerant 3A is used, the evaporating temperature is preferably −55° C. or higher, more preferably −50° C. or higher, further preferably −45° C. or higher, and particularly preferably −40° C. or higher from the viewpoint of setting the evaporating pressure to 0.02 MPa or higher.


In the refrigeration cycle in which the composition containing refrigerant 3A is used, the evaporating temperature is more preferably −55° C. or higher and 15° C. or lower, even more preferably −50° C. or higher and 10° C. or lower, further preferably −45° C. or higher and 5° C. or lower, and particularly preferably −40° C. or higher and lower than 0° C.


The composition containing refrigerant 3A is preferably used for operating a refrigeration cycle in which the condensation temperature is 0 to 70° C.


In the refrigeration cycle in which the composition containing refrigerant 3A is used, the condensation temperature is preferably 70° C. or lower, more preferably 60° C. or lower, further preferably 55° C. or lower, and particularly preferably 50° C. or lower from the viewpoint of extending the life of a refrigeration apparatus.


In the refrigeration cycle in which the composition containing refrigerant 3A is used, the condensation temperature is preferably 0° C. or higher, more preferably 5° C. or higher, further preferably 10° C. or higher, and particularly preferably 15° C. or higher from the viewpoint of preventing dew condensation on an outdoor unit.


The present disclosure can provide an apparatus constituting a refrigeration cycle in which the composition containing refrigerant 3A is circulated via a compressor.


The composition containing refrigerant 3B is preferably used for operating a refrigeration cycle in which the evaporating temperature is −60 to 20° C., from the viewpoint of sufficiently cooling the interior of a room, and an object to be cooled.


In the refrigeration cycle in which the composition containing refrigerant 3B is used, the evaporating temperature is more preferably 15° C. or lower, even more preferably 10° C. or lower, further preferably 5° C. or lower, and particularly preferably lower than 0° C. from the viewpoint of sufficiently cooling the interior of a room, and an object to be cooled.


In the refrigeration cycle in which the composition containing refrigerant 3B is used, the evaporating temperature is preferably −55° C. or higher, more preferably −50° C. or higher, further preferably −45° C. or higher, and particularly preferably −40° C. or higher from the viewpoint of setting the evaporating pressure to 0.02 MPa or higher.


In the refrigeration cycle in which the composition containing refrigerant 3B is used, the evaporating temperature is more preferably −55° C. or higher and 15° C. or lower, even more preferably −50° C. or higher and 10° C. or lower, further preferably −45° C. or higher and 5° C. or lower, and particularly preferably −40° C. or higher and lower than 0° C.


The composition containing refrigerant 3B is preferably used for operating a refrigeration cycle in which the condensation temperature is 0 to 70° C.


In the refrigeration cycle in which the composition containing refrigerant 3B is used, the condensation temperature is preferably 70° C. or lower, more preferably 60° C. or lower, further preferably 55° C. or lower, and particularly preferably 50° C. or lower from the viewpoint of extending the life of a refrigeration apparatus.


In the refrigeration cycle in which the composition containing refrigerant 3B is used, the condensation temperature is preferably 0° C. or higher, more preferably 5° C. or higher, further preferably 10° C. or higher, and particularly preferably 15° C. or higher from the viewpoint of preventing dew condensation on an outdoor unit.


The present disclosure can provide an apparatus constituting a refrigeration cycle in which the composition containing refrigerant 3B is circulated via a compressor.


Preferred examples of the refrigeration apparatus to which refrigerant 3A and refrigerant 3B (or compositions comprising them) of the present disclosure can be applied include at least one selected from the group consisting of air conditioning equipment, a cold storage chamber, a refrigeration chamber, a water cooler, an ice maker, a cold storage showcase, a refrigeration showcase, a refrigeration and cold storage unit, a refrigerator for a refrigeration and cold storage warehouse, in-car air conditioning equipment, a turbo refrigerator, and a screw refrigerator.


The composition of the present disclosure is suitable for use as an alternative refrigerant to R134a, R22, R12, R404A, R407A, R407C, R407F, R407H, R410A, R413A, R417A, R422A, R422B, R422C, R422D, R423A, R424A, R426A, R427A, R428A, R430A, R434A, R437A, R438A, R448A, R449A, R449B, R450A, R454A, R454C, R455A, R465A, R502, R507, R513A, R513B, R515A, or R515B. Among these, the composition of the present disclosure is particularly suitable for use as an alternative refrigerant to R134a because the composition of the present disclosure has the properties of having a coefficient of performance (COP) and a Capacity equivalent to or higher than those of R134a and having a sufficiently small GWP.


2. Refrigerant Composition


The refrigerant composition of the present disclosure comprises at least the refrigerant of the present disclosure and can be used for the same applications as the refrigerant of the present disclosure.


The refrigerant composition of the present disclosure can be further used for obtaining a working fluid for a refrigeration apparatus by being mixed with at least a refrigerator oil.


The refrigerant composition of the present disclosure further contains at least one other component in addition to the refrigerant of the present disclosure. The refrigerant composition of the present disclosure may contain at least one of the other components described below as needed.


As described above, when the refrigerant composition of the present disclosure is used as a working fluid in a refrigeration apparatus, it is usually used by being mixed with at least a refrigerator oil.


Here, the refrigerant composition of the present disclosure is preferably substantially free from a refrigerator oil. Specifically, in the refrigerant composition of the present disclosure, the content of a refrigerator oil based on the entire refrigerant composition is preferably 0 to 1% by mass, more preferably 0 to 0.5% by mass, further preferably 0 to 0.25% by mass, and particularly preferably 0 to 0.1% by mass.


2.1 Water


The refrigerant composition of the present disclosure may comprise a slight amount of water.


The water content in the refrigerant composition is preferably 0 to 0.1% by mass, more preferably 0 to 0.075% by mass, further preferably 0 to 0.05% by mass, and particularly preferably 0 to 0.025% by mass based on the entire refrigerant


When the refrigerant composition comprises a slight amount of water, the intramolecular double bond of the unsaturated fluorocarbon-based compound that can be contained in the refrigerant is stabilized, and the oxidation of the unsaturated fluorocarbon-based compound is also less likely to occur, and therefore the stability of the refrigerant composition improves.


2.2 Tracer


A tracer is added to the refrigerant composition of the present disclosure at a detectable concentration so that when the refrigerant composition of the present disclosure is diluted or contaminated or undergoes some other change, the change can be traced.


The refrigerant composition of the present disclosure may contain one of the above tracer alone or may contain two or more of the above tracers.


The above tracer is not limited and can be appropriately selected from generally used tracers. Preferably, a compound that cannot be an impurity unavoidably mixed into the refrigerant of the present disclosure is selected as the tracer.


Examples of the above tracer include a hydrofluorocarbon, a hydrochlorofluorocarbon, a chlorofluorocarbon, a hydrochlorocarbon, a fluorocarbon, a deuterated hydrocarbon, a deuterated hydrofluorocarbon, a perfluorocarbon, a fluoroether, a brominated compound, an iodinated compound, an alcohol, an aldehyde, a ketone, and nitrous oxide (N2O). Among these, a hydrofluorocarbon, a hydrochlorofluorocarbon, a chlorofluorocarbon, a hydrochlorocarbon, a fluorocarbon, and a fluoroether are preferred.


As the above tracer, specifically, the following compounds (hereinafter also referred to as tracer compounds) are more preferred:


HCC-40 (chloromethane, CH3Cl),


HFC-41 (fluoromethane, CH3F),


HFC-161 (fluoroethane, CH3CH2F),


HFC-245fa (1,1,1,3,3-pentafluoropropane, CF3CH2CHF2), HFC-236fa (1,1,1,3,3,3-hexafluoropropane, CF3CH2CF3), HFC-236ea (1,1,1,2,3,3-hexafluoropropane, CF3CHFCHF2),


HCFC-22 (chlorodifluoromethane, CHClF2),


HCFC-31 (chlorofluoromethane, CH2ClF),


CFC-1113 (chlorotrifluoroethylene, CF2═CClF),


HFE-125 (trifluoromethyl-difluoromethyl ether, CF3OCHF2), HFE-134a (trifluoromethyl-fluoromethyl ether, CF3OCH2F), HFE-143a (trifluoromethyl-methyl ether, CF3OCH3), HFE-227ea (trifluoromethyl-tetrafluoroethyl ether, CF3OCHFCF3), and HFE-236fa (trifluoromethyl-trifluoroethyl ether, CF3OCH2CF3).


The above tracer compound can be present in the refrigerant composition at a total concentration of 10 parts per million (ppm) by mass to 1,000 ppm. The above tracer compound is preferably present in the refrigerant composition at a total concentration of 30 ppm to 500 ppm, more preferably present in the refrigerant composition at total concentration of 50 ppm to 300 ppm, further preferably present in the refrigerant composition at a total concentration of 75 ppm to 250 ppm, and particularly preferably present in the refrigerant composition at a total concentration of 100 ppm to 200 ppm.


2.3 Ultraviolet Fluorescent Dye


The refrigerant composition of the present disclosure may contain one ultraviolet fluorescent dye alone or may contain two or more ultraviolet fluorescent dyes.


The above ultraviolet fluorescent dye is not limited and can be appropriately selected from generally used ultraviolet fluorescent dyes.


Examples of the above ultraviolet fluorescent dye include naphthalimide, coumarin, anthracene, phenanthrene, xanthene, thioxanthene, naphthoxanthene, and fluorescein, and derivatives thereof. Among these, naphthalimide and coumarin are preferred.


2.4 Stabilizer


The refrigerant composition of the present disclosure may contain one stabilizer alone or may contain two or more stabilizers.


The above stabilizer is not limited and can be appropriately selected from generally used stabilizers.


Examples of the above stabilizer include nitro compounds, ethers, and amines.


Examples of the nitro compounds include an aliphatic nitro compound such as nitromethane or nitroethane, and an aromatic nitro compound such as nitrobenzene or nitrostyrene.


Examples of the ethers include 1,4-dioxane.


Examples of the amines include 2,2,3,3,3-pentafluoropropylamine and diphenylamine.


Examples of the above stabilizer also include butylhydroxyxylene and benzotriazole in addition to the above nitro compounds, ethers, and amines.


The content of the above stabilizer is not limited and is usually 0.01 to 5% by mass, preferably 0.05 to 3% by mass, more preferably 0.1 to 2% by mass, further preferably 0.25 to 1.5% by mass, and particularly preferably 0.5 to 1% by mass based on the entire refrigerant.


The method for evaluating the stability of the refrigerant composition of the present disclosure is not limited, and the stability can be evaluated by a generally used method. One example of such a method includes a method of evaluating according to ASHRAE Standard 97-2007 using the amount of free fluorine ions as an indicator. Another example includes a method of evaluating using a total acid number as an indicator. This method can be performed, for example, according to ASTM D 974-06.


2.5 Polymerization Inhibitor


The refrigerant composition of the present disclosure may contain one polymerization inhibitor alone or may contain two or more polymerization inhibitors.


The above polymerization inhibitor is not limited and can be appropriately selected from generally used polymerization inhibitors.


Examples of the above polymerization inhibitor include 4-methoxy-1-naphthol, hydroquinone, hydroquinone methyl ether, dimethyl-t-butylphenol, 2,6-di-tert-butyl-p-cresol, and benzotriazole.


The content of the above polymerization inhibitor is not limited and is usually 0.01 to 5% by mass, preferably 0.05 to 3% by mass, more preferably 0.1 to 2% by mass, further preferably 0.25 to 1.5% by mass, and particularly preferably 0.5 to 1% by mass based on the entire refrigerant.


2.6 Other Components that can be Contained in Refrigerant Composition


In the refrigerant composition of the present disclosure, examples of a component that can be contained also include the following components.


For example, the refrigerant composition of the present disclosure can contain a fluorinated hydrocarbon which are different from the above-described refrigerant. The fluorinated hydrocarbon as another component is not limited, and examples thereof include at least one fluorinated hydrocarbon selected from the group consisting of HCFC-1122 and HCFC-124 and CFC-1113.


As the other components, the refrigerant composition of the present disclosure can contain at least one halogenated organic compound, for example, represented by formula (A): CmHnXp wherein X each independently represents a fluorine atom, a chlorine atom, or a bromine atom, m is 1 or 2, 2m+2≥n+p, and p≥1. The above halogenated organic compound is not limited, and, for example, difluorochloromethane, chloromethane, 2-chloro-1,1,1,2,2-pentafluoroethane, 2-chloro-1,1,1,2-tetrafluoroethane, 2-chloro-1,1-difluoroethylene, and trifluoroethylene are preferred.


As the other component, the refrigerant composition of the present disclosure can contain at least one organic compound, for example, represented by formula (B): CmHnXp wherein X each independently represent an atom that is not a halogen atom, m is 1 or 2, 2m+2≥n+p, and p≥1. The above organic compound is not limited, and, for example, propane and isobutane are preferred.


The content of the fluorinated hydrocarbon, halogenated organic compound represented by the above formula (A), and organic compound represented by the above formula (B) is not limited, but the total amount of these is preferably 0.5% by mass or less, more preferably 0.3% by mass or less, and particularly preferably 0.1% by mass or less based on the total amount of the refrigerant composition.


3. Refrigerator Oil-Containing Working Fluid


The refrigerator oil-containing working fluid of the present disclosure comprises at least the refrigerant or refrigerant composition of the present disclosure and a refrigerator oil and is used as a working fluid in a refrigeration apparatus. Specifically, the refrigerator oil-containing working fluid of the present disclosure is obtained by the mixing of a refrigerator oil used in the compressor of a refrigeration apparatus and the refrigerant or the refrigerant composition with each other.


The content of the above refrigerator oil is not limited and is usually 10 to 50% by mass, preferably 12.5 to 45% by mass, more preferably 15 to 40% by mass, further preferably 17.5 to 35% by mass, and particularly preferably 20 to 30% by mass based on the entire refrigerator oil-containing working fluid.


3.1 Refrigerator Oil


The composition of the present disclosure may contain one refrigerator oil alone or may contain two or more refrigerator oils.


The above refrigerator oil is not limited and can be appropriately selected from generally used refrigerator oils. At the time, a refrigerator oil which is superior in terms of miscibility with the mixture of refrigerants of the present disclosure (the mixed refrigerant of the present disclosure) and the function of improving the stability of the mixed refrigerant of the present disclosure and the like can be appropriately selected as needed.


As the base oil of the above refrigerator oil, for example, at least one selected from the group consisting of a polyalkylene glycol (PAG), a polyol ester (POE), and a polyvinyl ether (PVE) is preferred.


The above refrigerator oil may further comprise an additive in addition to the above base oil.


The above additive may be at least one selected from the group consisting of an antioxidant, an extreme pressure agent, an acid scavenger, an oxygen scavenger, a copper deactivator, a rust preventive, an oily agent, and an antifoaming agent.


As the above refrigerator oil, one having a kinematic viscosity of 5 to 400 cSt at 40° C. is preferred in terms of lubrication.


The refrigerator oil-containing working fluid of the present disclosure may further comprise at least one additive as needed. Examples of the additive include the following compatibilizing agent.


3.2 Compatibilizing Agent


The refrigerator oil-containing working fluid of the present disclosure may contain one compatibilizing agent alone or may contain two or more compatibilizing agents.


The above compatibilizing agent is not limited and can be appropriately selected from generally used compatibilizing agents.


Examples of the above compatibilizing agent include a polyoxyalkylene glycol ether, an amide, a nitrite, a ketone, a chlorocarbon, an ester, a lactone, an aryl ether, a fluoroether, and a 1,1,1-trifluoroalkane. Among these, a polyoxyalkylene glycol ether is preferred.


EXAMPLES

The present disclosure will be described in more detail below by giving Examples. However, the present disclosure is not limited to these Examples.


Test Example 1-1

The GWPs of the mixed refrigerants shown in Examples 1-1 to 1-3, Comparative Examples 1-1 to 1-6, and Reference Example 1-1 (R134a) were evaluated based on the values stated in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using National Institute of Science and Technology (NIST) Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


<Air Conditioning Conditions>


Evaporating temperature 10° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The term “Evaporating temperature 10° C.” means that the evaporating temperature of each mixed refrigerant in an evaporator provided in a refrigeration apparatus is 10° C. The term “Condensation temperature 40° C.” means that the condensation temperature of each mixed refrigerant in a condenser provided in a refrigeration apparatus is 40° C.


The results of Test Example 1-1 are shown in Table 401. Table 401 shows Examples and Comparative Examples of refrigerant 3A of the present disclosure. In Table 401, “COP ratio” and “Refrigerating capacity ratio” represent proportions (%) with respect to R134a. In Table 401, the term “Saturation pressure (40° C.)” represents saturation pressure at a saturation temperature of 40° C. In Table 401, the term “Discharge temperature (° C.)” represents the highest temperature during the refrigeration cycle in the above theoretical refrigeration cycle calculations of the mixed refrigerants.


The coefficient of performance (COP) was obtained by the following formula.

COP=(refrigerating capacity or heating capacity)/power consumption


The compression ratio was obtained by the following formula.

Compression ratio=condensation pressure (Mpa)/evaporating pressure (Mpa)


The flammability of each mixed refrigerant was determined by considering the mixing composition of the mixed refrigerant as the WCF concentration and measuring the combustion rate according to the ANSI/ASHRAE 34-2013 standard. The flammability of R134a was determined by considering the composition of R134a as the WCF concentration and measuring the combustion rate according to the ANSI/ASHRAE 34-2013 standard.


A mixed refrigerant having a combustion rate of 0 cm/s to 10 cm/s was considered to be “Class 2L (slightly flammable)”, and a mixed refrigerant having a combustion rate of more than 10 cm/s was considered to be “Class 2 (weakly flammable)”. For R134a, no flame propagation occurred, and therefore R134a was considered to be “Class 1 (nonflammable)”. In Table 401, “ASHRAE flammability classification” represents a result based on these determination criteria.


The combustion rate test was performed as follows. First, the mixed refrigerant used had a purity of 99.5% or more and was degassed by repeating the cycle of freezing, pumping, and thawing until no trace of air was observed on a vacuum gauge. The combustion rate was measured by a closed method. The initial temperature was ambient temperature. The ignition was performed by producing an electric spark between the electrodes at the center of a sample cell. The duration of the discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of the flame was visualized using a schlieren photograph. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two acrylic windows that transmitted light was used as the sample cell, and as the light source, a xenon lamp was used. A schlieren image of the flame was recorded at a framing rate of 600 fps by a high speed digital video camera and stored in a PC.


The flammable range of each mixed refrigerant was measured using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of combustion could be visually observed and video-recorded, and the glass flask was adapted so that gas could be released from the upper lid when excessive pressure was generated by combustion. For the ignition method, a spark was generated by discharge from electrodes held at height of ⅓ from the bottom.


<Test Conditions>


Test container: 280 mm ϕ spherical shape (internal volume: 12 L)


Test temperature: 60° C.±3° C.


Pressure: 101.3 kPa±0.7 kPa


Water: 0.0088 g±0.0005 g per g of dry air (the amount of water at a relative humidity of 50% at 23° C.) Refrigerant composition/air mixing ratio: 1 vol. % increments±0.2 vol. %


Refrigerant composition mixture: ±0.1% by mass


Ignition method: alternating current discharge, voltage 15 kV, current 30 mA, neon transformer


Electrode spacing: 6.4 mm (¼ inch)


Spark: 0.4 s±0.05 s


Determination criteria:






    • When the flame extended at an angle of 90° or more from the ignition point, it was evaluated as having flame propagation (flammable)

    • When the flame extended at an angle of 90° or less from the ignition point, it was evaluated as having no flame propagation (nonflammable)


















TABLE 401









Reference








Example 1-1
Comparative
Comparative
Comparative
Example


Item
Unit
(R134a)
Example 1−1
Example 1−2
Example 1-3
1−1

















Composition
HFO-1132(Z)
% by mass
0
30.0
40.0
51.0
53.0


ratio
HFO-1234yf
% by mass
0
70.0
60.0
49.0
47.0



HFC-134a
% by mass
100
0
0
0
0













GWP(AR4)

1430
6
6
7
7


Discharge temperature
° C.
70.7
70.7
73.4
76.3
76.9


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.991
0.990


Evaporating pressure
MPa
0.415
0.427
0.422
0.418
0.417


Compression ratio

2.5
2.4
2.4
2.4
2.4


COP ratio (to R134a)
%
100.0
100.0
100.2
100.3
100.4


Refrigerating capacity
%
100.0
98.0
98.1
98.3
98.3


ratio (to R134a)








ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L


classification
















Example
Example
Comparative
Comparative
Comparative













Item
Unit
1-2
1-3
Example 1-4
Example 1-5
Example 1-6

















Composition
HFO-1132(Z)
% by mass
56.0
59.0
60.0
70.0
100


ratio
HFO-1234yf
% by mass
44.0
41.0
40.0
30.0
0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
8
8
8
10


Discharge temperature
° C.
77.7
78.5
78.8
81.6
90.3


Saturation pressure (40° C.)
MPa
0.988
0.987
0.986
0.981
0.968


Evaporating pressure
MPa
0.416
0.415
0.415
0.411
0.402


Compression ratio

2.4
2.4
2.4
2.4
2.4


COP ratio (to R134a)
%
100.4
100.4
100.4
100.5
100.4


Refrigerating capacity ratio (to R134a)
%
98.3
98.3
98.3
98.4
98.5


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 1-2

The GWPs of the mixed refrigerants shown in Examples 1-4 to 1-6, Comparative Examples 1-7 to 1-12, and Reference Example 1-2 (R134a) were evaluated based on the values stated in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 45° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature 5° C.


Condensation temperature 45° C.


Superheating temperature 5 K


Subcooling temperature 5 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 1-1.


The results of Test Example 1-2 are shown in Table 402. Table 402 shows Examples and Comparative Examples of refrigerant 3A of the present disclosure. In Table 402, the meanings of the terms are the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 1-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test. Example 1-1. The combustion rate test was performed in the same manner as in Test Example 1-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 1-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).
















TABLE 402










Reference









Example 1-2
Comparative
Comparative
Comparative
Example













Item
Unit
(R134a)
Example 1-7
Example 1-8
Example 1-9
1-4

















Composition
HFO-1132(Z)
% by mass
0
30.0
40.0
51.0
53.0


ratio
HFO-1234yf
% by mass
0
70.0
60.0
49.0
47.0



HFC-134a
% by mass
100
0
0
0
0













GWP(AR4)

1430
6
6
7
7


Discharge temperature
° C.
63.8
63.9
67.3
71.2
71.9


Saturation pressure (45° C.)
MPa
1.160
1.139
1.133
1.126
1.125


Evaporating pressure
MPa
0.350
0.363
0.359
0.355
0.354


Compression ratio

3.3
3.1
3.2
3.2
3.2


COP ratio (to R134a)
%
100.0
100.0
100.7
101.4
101.5


Refrigerating capacity ratio (to R134a)
%
100.0
98.8
99.7
100.5
100.6


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L






















Comparative
Comparative
Comparative





Example
Example
Example
Example
Example













Item
Unit
1-5
1-6
1-10
1-11
1-12

















Composition
HFO-1132(Z)
% by mass
56.0
59.0
60.0
70.0
100


ratio
HFO-1234yf
% by mass
44.0
41.0
40.0
30.0
0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
8
8
8
10


Discharge temperature
° C.
72.9
74.0
74.4
78.0
89.4


Saturation pressure (45° C.)
MPa
1.123
1.121
1.121
1.115
1.101


Evaporating pressure
MPa
0.353
0.352
0.352
0.349
0.340


Compression ratio

3.2
3.2
3.2
3.2
3.2


COP ratio (to R134a)
%
101.6
101.8
101.8
102.2
102.7


Refrigerating capacity ratio (to R134a)
%
100.8
101.0
101.1
101.6
102.8


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 1-3

The GWPs of the mixed refrigerants shown in Examples 1-7 to 1-9, Comparative Examples 1-13 to 1-18, and Reference Example 1-3 (R134a) were evaluated based on the values in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature −10° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 1-1.


The results of Test Example 1-3 are shown in Table 403. Table 403 shows Examples and Comparative Examples of refrigerant 3A of the present disclosure. In Table 403, the meanings of the terms are the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 1-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test Example 1-1. The combustion rate test was performed in the same manner as in Test Example 1-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 1-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).
















TABLE 403










Reference
Comparative
Comparative
Comparative






Example 1-3
Example
Example
Example
Example


Item

Unit
(R134a)
1-13
1-14
1-15
1-7





Composition
HFO-1132(Z)
% by mass
0
30.0
40.0
51.0
53.0


ratio
HFO-1234yf
% by mass
0
70.0
60.0
49.0
47.0



HFC-134a
% by mass
100
0
0
0
0













GWP(AR4)

1430
6
6
7
7


Discharge temperature
° C.
80.8
80.7
85.5
90.8
91.8


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.991
0.990


Evaporating pressure
MPa
0.201
0.215
0.212
0.209
0.208


Compression ratio

5.1
4.7
4.7
4.7
4.7


COP ratio (to R134a)
%
100.0
100.2
100.9
101.5
101.6


Refrigerating capacity ratio (to R134a)
%
100.0
101.6
102.4
103.0
103.1


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L






















Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
1-8
1-9
1-16
1-17
1-18





Composition
HFO-1132(Z)
% by mass
56.0
59.0
60.0
70.0
100


ratio
HFO-1234yf
% by mass
44.0
41.0
40.0
30.0
0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
8
8
8
10


Discharge temperature
° C.
93.3
94.8
95.3
100.3
115.9


Saturation pressure (40° C.)
MPa
0.988
0.987
0.986
0.981
0.968


Evaporating pressure
MPa
0.208
0.207
0.207
0.204
0.198


Compression ratio

4.8
4.8
4.8
4.8
4.9


COP ratio (to R134a)
%
101.7
101.8
101.8
102.0
102.4


Refrigerating capacity ratio (to R134a)
%
103.2
103.3
103.4
103.6
104.4


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 1-4

The GWPs of the mixed refrigerants shown in Examples 1-10 to 1-12, Comparative Examples 1-19 to 1-24, and Reference Example 1-4 (R134a) were evaluated based on the values in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature −35° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 1-1.


The results of Test Example 1-4 are shown in Table 404. Table 404 shows Examples and Comparative Examples of refrigerant 3A of the present disclosure. In Table 404, the meanings of the terms are the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 1-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test Example 1-1. The combustion rate test was performed in the same manner as in Test Example 1-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 1-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).
















TABLE 404










Reference
Comparative
Comparative
Comparative






Example 1-4
Example
Example
Example
Example


Item

Unit
(R134a)
1-19
1-20
1-21
1-10





Composition
HFO-1132(Z)
% by mass
0
30.0
40.0
51.0
53.0


ratio
HFO-1234yf
% by mass
0
70.0
60.0
49.0
47.0



HFC-134a
% by mass
100
0
0
0
0













GWP(AR4)

1430
6
6
7
7


Discharge temperature
° C.
99.1
98.5
106.5
115.5
117.2


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.991
0.990


Evaporating pressure
MPa
0.066
0.076
0.075
0.073
0.073


Compression ratio

15.4
13.2
13.4
13.6
13.6


COP ratio (to R134a)
%
100.0
100.7
102.2
100.2
100.4


Refrigerating capacity ratio (to R134a)
%
100.0
108.8
110.4
100.2
100.4


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L






















Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
1-11
1-12
1-22
1-23
1-24





Composition
HFO-1132(Z)
% by mass
56.0
59.0
60.0
70.0
100


ratio
HFO-1234yf
% by mass
44.0
41.0
40.0
30.0
0.0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
8
8
8
10


Discharge temperature
° C.
119.7
122.2
123.1
131.5
157.8


Saturation pressure (40° C.)
MPa
0.988
0.987
0.986
0.981
0.968


Evaporating pressure
MPa
0.073
0.072
0.072
0.071
0.068


Compression ratio

13.6
13.7
13.7
13.8
14.2


COP ratio (to R134a)
%
100.6
100.8
100.9
100.0
100.7


Refrigerating capacity ratio (to R134a)
%
100.6
100.9
100.9
100.0
101.3


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 1-5

The GWPs of the mixed refrigerants shown in Examples 1-13 to 1-15, Comparative Examples 1-25 to 1-30, and Reference Example 1-5 (R134a) were evaluated based on the values in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature −50° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 1-1.


The results of Test Example 1-5 are shown in Table 405. Table 405 shows Examples and Comparative Examples of refrigerant 3A of the present disclosure. In Table 405, the meanings of the terms are the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 1-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test Example 1-1. The combustion rate test was performed in the same manner as in Test Example 1-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 1-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).
















TABLE 405










Reference
Comparative
Comparative
Comparative






Example 1-5
Example
Example
Example
Example


Item

Unit
(R134a)
1-25
1-26
1-27
1-13





Composition
HFO-1132(Z)
% by mass
0
30.0
40.0
51.0
53.0


ratio
HFO-1234yf
% by mass
0
70.0
60.0
49.0
47.0



HFC-134a
% by mass
100
0
0
0
0













GWP(AR4)

1430
6
6
7
7


Discharge temperature
° C.
114.6
113.5
123.8
135.6
137.7


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.991
0.990


Evaporating pressure
MPa
0.029
0.036
0.035
0.034
0.034


Compression ratio

34.5
28.1
28.5
29.0
29.0


COP ratio (to R134a)
%
100.0
101.2
103.2
100.3
100.5


Refrigerating capacity ratio (to R134a)
%
100.0
115.2
117.5
100.2
100.5


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L






















Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
1-14
1-15
1-28
1-29
1-30





Composition
HFO-1132(Z)
% by mass
56.0
59.0
60.0
70.0
100


ratio
HFO-1234yf
% by mass
44.0
41.0
40.0
30.0
0.0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
8
8
8
10


Discharge temperature
° C.
141.0
144.2
145.3
156.4
190.6


Saturation pressure (40° C.)
MPa
0.988
0.987
0.986
0.981
0.968


Evaporating pressure
MPa
0.034
0.034
0.034
0.033
0.031


Compression ratio

29.2
29.3
29.3
29.7
30.9


COP ratio (to R134a)
%
100.8
101.1
101.2
100.0
101.0


Refrigerating capacity ratio (to R134a)
%
100.8
101.1
101.2
100.0
101.6


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 1-6

The GWPs of the mixed refrigerants shown in Examples 1-16 to 1-18, Comparative Examples 1-31 to 1-36, and Reference Example 1-6 (R134a) were evaluated based on the values in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature −65° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 1-1.


The results of Test Example 1-6 are shown in Table 406. Table 406 shows Examples and Comparative Examples of refrigerant 3A of the present disclosure. In Table 406, the meanings of the terms are the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 1-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test Example 1-1. The combustion rate test was performed in the same manner as in Test Example 1-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 1-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).
















TABLE 406










Reference
Comparative
Comparative
Comparative






Example 1-6
Example
Example
Example
Example


Item

Unit
(R134a)
1-31
1-32
1-33
1-16





Composition
HFO-1132(Z)
% by mass
0
30.0
40.0
51.0
53.0


ratio
HFO-1234yf
% by mass
0
70.0
60.0
49.0
47.0



HFC-134a
% by mass
100
0
0
0
0













GWP(AR4)

1430
6
6
7
7


Discharge temperature
° C.
134.8
132.8
146.1
161.0
163.8


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.991
0.990


Evaporating pressure
MPa
0.011
0.015
0.015
0.014
0.014


Compression ratio

89.3
67.4
68.7
70.1
70.4


COP ratio (to R134a)
%
100.0
101.9
104.5
106.6
106.9


Refrigerating capacity ratio (to R134a)
%
100.0
124.4
127.4
129.9
130.3


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L






















Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
1-17
1-18
1-34
1-35
1-36





Composition
HFO-1132(Z)
% by mass
56.0
59.0
60.0
70.0
100


ratio
HFO-1234yf
% by mass
44.0
41.0
40.0
30.0
0.0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
8
8
8
10


Discharge temperature
° C.
168.0
172.1
173.5
187.7
231.5


Saturation pressure (40° C.)
MPa
0.988
0.987
0.986
0.981
0.968


Evaporating pressure
MPa
0.014
0.014
0.014
0.014
0.013


Compression ratio

70.8
71.2
71.3
72.6
76.3


COP ratio (to R134a)
%
107.4
107.8
107.9
108.9
110.2


Refrigerating capacity ratio (to R134a)
%
130.8
131.3
131.4
132.7
134.9


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 2-1

The GWPs of the mixed refrigerants shown in Examples 2-1 to 2-4, Comparative Examples 2-1 to 2-6, and Reference Example 2-1 (R134a) were evaluated based on the values stated in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using National Institute of Science and Technology (NIST) Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


<Air Conditioning Conditions>


Evaporating temperature 10° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The term “Evaporating temperature 10° C.” means that the evaporating temperature of each mixed refrigerant in an evaporator provided in a refrigeration apparatus is 10° C. The term “Condensation temperature 40° C.” means that the condensation temperature of each mixed refrigerant in a condenser provided in a refrigeration apparatus is 40° C.


The results of Test Example 2-1 are shown in Table 407. Table 407 shows Examples and Comparative Examples of refrigerant 3B of the present disclosure. In Table 407, the terms “COP ratio” and “refrigerating capacity ratio” represent proportions (%) with respect to R134a. In Table 407, The term “Saturation pressure (40° C.)” represents saturation pressure at a saturation temperature of 40° C. In Table 407, the terms “Discharge temperature (° C.)” represents the highest temperature during the refrigeration cycle in the above refrigeration cycle theoretical calculation of the mixed refrigerants.


The coefficient of performance (COP) was obtained by the following formula

COP=(refrigerating capacity or heating capacity)/power consumption


The compression ratio was obtained by the following formula

Compression ratio=condensation pressure (Mpa)/evaporating pressure (Mpa)


The flammability of each mixed refrigerant was determined by considering the mixing composition of the mixed refrigerant as the WCF concentration and measuring the combustion rate according to the ANSI/ASHRAE 34-2013 standard. The flammability of R134a was determined by considering the composition of R134a as the WCF concentration and measuring the combustion rate according to the ANSI/ASHRAE 34-2013 standard.


A mixed refrigerant having a combustion rate of 0 cm/s to 10 cm/s was considered to be “Class 2L (slightly flammable)”, and a mixed refrigerant having a combustion rate of more than 10 cm/s was considered to be “Class 2 (weakly flammable)”. For R134a, no flame propagation occurred, and therefore R134a was considered to be “Class 1 (nonflammable)”. In Table 407, “ASHRAE flammability classification” represents a result based on these determination criteria.


The combustion rate test was performed as follows. First, the mixed refrigerant used had a purity of 99.5% or more and was degassed by repeating the cycle of freezing, pumping, and thawing until no trace of air was observed on a vacuum gauge. The combustion rate was measured by a closed method. The initial temperature was ambient temperature. The ignition was performed by producing an electric spark between electrodes at the center of a sample cell. The duration of the discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of the flame was visualized using a schlieren photograph. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two acrylic windows that transmitted light was used as the sample cell, and as the light source, a xenon lamp was used. A schlieren image of the flame was recorded at a framing rate of 600 fps by a high speed digital video camera and stored in a PC.


The flammable range of each mixed refrigerant was measured using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of combustion could be visually observed and video-recorded, and the glass flask was adapted so that gas could be released from the upper lid when excessive pressure was generated by combustion. For the ignition method, a spark was generated by discharge from electrodes held at a height of ⅓ from the bottom.


<Test Conditions>


Test container: 280 mm ϕ spherical shape (internal volume: 12 L)


Test temperature: 60° C.±3° C.


Pressure: 101.3 kPa±0.7 kPa


Water: 0.0088 g±0.0005 g per g of dry air (the amount of water at a relative humidity of 50% at 23° C.) Refrigerant composition/air mixing ratio: 1 vol. % increments±0.2 vol. %


Refrigerant composition mixture: ±0.1% by mass


Ignition method: alternating current discharge, voltage 15 kV, current 30 mA, neon transformer


Electrode spacing: 6.4 mm (¼ inch)


Spark: 0.4 s±0.05 s


Determination criteria:






    • When the flame extended at an angle of 90° or more from the ignition point, it was evaluated as having flame propagation (flammable)

    • When the flame extended at an angle of 90° or less from the ignition point; it was evaluated as having no flame propagation (nonflammable)




















TABLE 407










Reference
Comparative
Comparative








Example2 -1
Example
Example
Example
Example
Example


Item

Unit
(R134a)
2-1
2-2
2-1
2-2
2-3





Composition ratio
HFO-1132(Z)
% by mass
0
30.0
40.0
41.0
44.0
47.0



HFO-1234yf
% by mass
0
70.0
60.0
59.0
56.0
53.0



HFC-134a
% by mass
100
0
0
0
0
0














GWP(AR4)

1430
6
6
6
7
7


Discharge temperature
° C.
70.7
70.7
73.4
73.6
74.4
75.3


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.997
0.995
0.994


Evaporating pressure
MPa
0.415
0.427
0.422
0.422
0.421
0.420


Compression ratio

2.5
2.4
2.4
2.4
2.4
2.4


COP ratio (to R134a)
%
100.0
100.0
100.2
100.2
100.2
100.3


Refrigerating capacity ratio (to R134a)
%
100.0
98.0
98.1
98.2
98.2
98.2


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L





















Comparative
Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
2-4
2-3
2-4
2-5
2-6





Composition ratio
HFO-1132(Z)
% by mass
49.0
51.0
60.0
70.0
100



HFO-1234yf
% by mass
51.0
49.0
40.0
30.0
0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
7
8
8
10


Discharge temperature
° C.
75.8
76.3
78.8
81.6
90.3


Saturation pressure (40° C.)
MPa
0.992
0.991
0.986
0.981
0.968


Evaporating pressure
MPa
0.419
0.418
0.415
0.411
0.402


Compression ratio

2.4
2.4
2.4
2.4
2.4


COP ratio (to R134a)
%
100.3
100.3
100.4
100.5
100.4


Refrigerating capacity ratio (to R134a)
%
98.2
98.3
98.3
98.4
98.5


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 2-2

The GWPs of the mixed refrigerants shown in Examples 2-5 to 2-8, Comparative Examples 2-7 to 2-12, and Reference Example 2-2 (R134a) were evaluated based on the values stated in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 45° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature 5° C.


Condensation temperature 45° C.


Superheating temperature 5 K


Subcooling temperature 5 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 2-1.


The results of Test Example 2-2 are shown in Table 408. Table 408 shows Examples and Comparative Examples of refrigerant 3B of the present disclosure. In Table 408, the meanings of the terms are the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 2-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test Example 2-1. The combustion rate test was performed in the same manner as in Test Example 2-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 2-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).

















TABLE 408










Reference
Comparative
Comparative








Example 2-2
Example
Example
Example
Example
Example


Item

Unit
(R134a)
2-7
2-8
2-5
2-6
2-7





Composition ratio
HFO-1132(Z)
% by mass
0
30.0
40.0
41.0
44.0
47.0



HFO-1234yf
% by mass
0
70.0
60.0
59.0
56.0
53.0



HFC-134a
% by mass
100
0
0
0
0
0














GWP(AR4)

1430
6
6
6
7
7


Discharge temperature
° C.
63.8
63.9
67.3
67.7
68.7
69.7


Saturation pressure (45° C.)
MPa
1.160
1.139
1.133
1.132
1.130
1.129


Evaporating pressure
MPa
0.350
0.363
0.359
0.359
0.358
0.357


Compression ratio

3.3
3.1
3.2
3.2
3.2
3.2


COP ratio (to R134a)
%
100.0
100.0
100.7
100.8
101.0
101.2


Refrigerating capacity ratio (to R134a)
%
100.0
98.8
99.7
99.8
100.0
100.2


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L





















Comparative
Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
2-8
2-9
2- 10
2-11
2-12





Composition ratio
HFO-1132(Z)
% by mass
49.0
51.0
60.0
70.0
100



HFO-1234yf
% by mass
51.0
49.0
40.0
30.0
0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
7
8
8
10


Discharge temperature
° C.
70.4
71.2
74.4
78.0
89.4


Saturation pressure (45° C.)
MPa
1.127
1.126
1.121
1.115
1.101


Evaporating pressure
MPa
0.356
0.355
0.352
0.349
0.340


Compression ratio

3.2
3.2
3.2
3.2
3.2


COP ratio (to R134a)
%
101.3
101.4
101.8
102.2
102.7


Refrigerating capacity ratio (to R134a)
%
100.4
100.5
101.1
101.6
102.8


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 2-3

The GWPs of the mixed refrigerants shown in Examples 2-9 to 2-12, Comparative Examples 2-13 to 2-18, and Reference Example 2-3 (R134a) were evaluated based on the values stated in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature −10° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 2-1.


The results of Test Example 2-3 are shown in Table 409. Table 409 shows Examples and Comparative Examples of refrigerant 3B of the present disclosure. In Table 409, the meanings of the terms are the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 2-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test Example 2-1. The combustion rate test was performed in the same manner as in Test Example 2-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 2-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).

















TABLE 409










Reference
Comparative
Comparative








Example 2-3
Example
Example
Example
Example
Example


Item

Unit
(R134a)
2-13
2-14
2-9
2-10
2-11





Composition ratio
HFO-1132(Z)
% by mass
0
30.0
40.0
41.0
44.0
47.0



HFO-1234yf
% by mass
0
70.0
60.0
59.0
56.0
53.0



HFC-134a
% by mass
100
0
0
0
0
0)














GWP(AR4)

1430
6
6
6
7
7


Discharge temperature
° C.
80.8
80.7
85.5
85.9
87.4
88.8


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.997
0.995
0.994


Evaporating pressure
MPa
0.201
0.215
0.212
0.212
0.211
0.210


Compression ratio

5.1
4.7
4.7
4.7
4.7
4.7


COP ratio (to R134a)
%
100.0
100.2
100.9
101.0
101.1
101.3


Refrigerating capacity ratio (to R134a)
%
100.0
101.6
102.4
102.4
102.6
102.8


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L





















Comparative
Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
2-12
2-15
2-16
2-17
2-18





Composition ratio
HFO-1132(Z)
% by mass
49.0
51.0
60.0
70.0
100



HFO-1234yf
% by mass
51.0
49.0
40.0
30.0
0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
7
8
8
10


Discharge temperature
° C.
89.8
90.8
95.3
100.3
115.9


Saturation pressure (40° C.)
MPa
0.992
0.991
0.986
0.981
0.968


Evaporating pressure
MPa
0.209
0.209
0.207
0.204
0.198


Compression ratio

4.7
4.7
4.8
4.8
4.9


COP ratio (to R134a)
%
101.4
101.5
101.8
102.0
102.4


Refrigerating capacity ratio (to R134a)
%
102.9
103.0
103.4
103.6
104.4


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 2-4

The GWPs of the mixed refrigerants shown in Examples 2-13 to 2-16, Comparative Examples 2-19 to 2-24, and Reference Example 2-4 (R134a) were evaluated based on the values in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature −35° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 2-1.


The results of Test Example 2-4 are shown in Table 410. Table 410 shows Examples and Comparative Examples of refrigerant 3B of the present disclosure. In Table, 410, the meanings of the terms are the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 2-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test Example 2-1. The combustion rate test was performed in the same manner as in Test Example 2-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 2-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).

















TABLE 410










Reference
Comparative
Comparative








Example 2-4
Example
Example
Example
Example
Example


Item

Unit
(R134a)
2-19
2-20
2-13
2-14
2-15





Composition ratio
HFO-1132(Z)
% by mass
0
30.0
40.0
41.0
44.0
47.0



HFO-1234yf
% by mass
0
70.0
60.0
59.0
56.0
53.0



HFC-134a
% by mass
100
0
0
0
0
0














GWP(AR4)

1430
6
6
6
7
7


Discharge temperature
° C.
99.1
98.5
106.5
107.3
109.8
112.2


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.997
0.995
0.994


Evaporating pressure
MPa
0.066
0.076
0.075
0.074
0.074
0.074


Compression ratio

15.4
13.2
13.4
13.4
13.5
13.5


COP ratio (to R134a)
%
100.0
100.7
102.2
102.3
102.7
103.0


Refrigerating capacity ratio (to R134a)
%
100.0
108.8
110.4
110.5
110.9
111.3


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L





















Comparative
Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
2-16
2-21
2-22
2-23
2-24





Composition ratio
HFO-1132(Z)
% by mass
49.0
51.0
60.0
70.0
100



HFO-1234yf
% by mass
51.0
49.0
40.0
30.0
0.0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
7
8
8
10


Discharge temperature
° C.
113.9
115.5
123.1
131.5
157.8


Saturation pressure (40° C.)
MPa
0.992
0.991
0.986
0.981
0.968


Evaporating pressure
MPa
0.073
0.073
0.072
0.071
0.068


Compression ratio

13.5
13.6
13.7
13.8
14.2


COP ratio (to R134a)
%
100.0
100.2
100.9
100.0
100.7


Refrigerating capacity ratio (to R134a)
%
100.0
100.2
100.9
100.0
101.3


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 2-5

The GWPs of the mixed refrigerants shown in Examples 2-17 to 2-20, Comparative Examples 2-25 to 2-30, and Reference Example 2-5 (R134a) were evaluated based on the values in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature −50° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 2-1.


The results of Test Example 2-5 are shown in Table 411. Table 411 shows Examples and Comparative Examples of refrigerant 3B of the present disclosure. In Table 411, the meanings of the terms are the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 2-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test Example 2-1. The combustion rate test was performed in the same manner as in Test. Example 2-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 2-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).

















TABLE 411










Reference
Comparative
Comparative








Example 2-5
Example
Example
Example
Example
Example


Item

Unit
(R134a)
2-25
2-26
2-17
2-18
2-19





Composition ratio
HFO-1132(Z)
% by mass
0
30.0
40.0
41.0
44.0
47.0



HFO-1234yf
% by mass
0
70.0
60.0
59.0
56.0
53.0



HFC-134a
% by mass
100
0
0)
0
0
0














GWP(AR4)

1430
6
6
6
7
7


Discharge temperature
° C.
114.6
113.5
123.8
124.9
128.1
131.3


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.997
0.995
0.994


Evaporating pressure
MPa
0.029
0.036
0.035
0.035
0.035
0.035


Compression ratio

34.5
28.1
28.5
28.5
28.7
28.8


COP ratio (to R134a)
%
100.0
101.2
103.2
103.4
103.9
104.3


Refrigerating capacity ratio (to R134a)
%
100.0
115.2
117.5
117.7
118.2
118.7


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L





















Comparative
Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
2-20
2-27
2-28
2-29
2-30





Composition ratio
HFO-1132(Z)
% by mass
49.0
51.0
60.0
70.0
100



HFO-1234yf
% by mass
51.0
49.0
40.0
30.0
0.0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
7
8
8
10


Discharge temperature
° C.
133.4
135.6
145.3
156.4
190.6


Saturation pressure (40° C.)
MPa
0.992
0.991
0.986
0.981
0.968


Evaporating pressure
MPa
0.034
0.034
0.034
0.033
0.031


Compression ratio

28.9
29.0
29.3
29.7
30.9


COP ratio (to R134a)
%
100.0
100.3
101.2
100.0
101.0


Refrigerating capacity ratio (to R134a)
%
100.0
100.2
101.2
100.0
101.6


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









Test Example 2-6

The GWPs of the mixed refrigerants shown in Examples 2-21 to 2-24, Comparative Examples 2-31 to 2-36, and Reference Example 2-6 (R134a) were evaluated based on the values in the IPCC Fourth Report.


The COPs, refrigerating capacities, discharge temperatures, saturation pressures at a saturation temperature of 40° C., condensation pressures, and evaporating pressures of these mixed refrigerants were obtained by carrying out the theoretical refrigeration cycle calculations for the mixed refrigerants under the following conditions using NIST Refprop 9.0.


<Air Conditioning Conditions>


Evaporating temperature −65° C.


Condensation temperature 40° C.


Superheating temperature 20 K


Subcooling temperature 0 K


Compressor efficiency 70%


The meanings of the above terms are the same as in Test Example 2-1.


The results of Test Example 2-6 are shown in Table 412. Table 412 shows Examples and Comparative Examples of refrigerant 3B of the present disclosure. In Table 412, the meanings of the terms are the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were obtained in the same manner as in Test Example 2-1.


The flammability of each mixed refrigerant was determined in the same manner as in Test Example 2-1. The combustion rate test was performed in the same manner as in Test Example 2-1.


The flammable range of each mixed refrigerant was measured with the same method and test conditions as in Test Example 2-1 using a measuring apparatus based on ASTM E681-09 (see FIG. 1T).

















TABLE 412










Reference
Comparative
Comparative








Example 2-6
Example
Example
Example
Example
Example


Item

Unit
(R134a)
2-31
2-32
2-21
2-22
2-23





Composition ratio
HFO-1132(Z)
% by mass
0
30.0
40.0
41.0
44.0
47.0



HFO-1234yf
% by mass
0
70.0
60.0
59.0
56.0
53.0



HFC-134a
% by mass
100
0
0
0
0
0














GWP(AR4)

1430
6
6
6
7
7


Discharge temperature
° C.
134.8
132.8
146.1
147.4
151.5
155.6


Saturation pressure (40° C.)
MPa
1.017
1.004
0.998
0.997
0.995
0.994


Evaporating pressure
MPa
0.011
0.015
0.015
0.014
0.014
0.014


Compression ratio

89.3
67.4
68.7
68.8
69.2
69.6


COP ratio (to R134a)
%
100.0
101.9
104.5
104.7
105.3
105.9


Refrigerating capacity ratio (to R134a)
%
100.0
124.4
127.4
127.7
128.4
129.1


ASHRAE flammability classification

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L





















Comparative
Comparative
Comparative
Comparative





Example
Example
Example
Example
Example


Item

Unit
2-24
2-33
2-34
2-35
2-36





Composition ratio
HFO-1132(Z)
% by mass
49.0
51.0
60.0
70.0
100



HFO-1234yf
% by mass
51.0
49.0
40.0
30.0
0.0



HFC-134a
% by mass
0
0
0
0
0













GWP(AR4)

7
7
8
8
10


Discharge temperature
° C.
158.3
161.0
173.5
187.7
231.5


Saturation pressure (40° C.)
MPa
0.992
0.991
0.986
0.981
0.968


Evaporating pressure
MPa
0.014
0.014
0.014
0.014
0.013


Compression ratio

69.9
70.1
71.3
72.6
76.3


COP ratio (to R134a)
%
106.3
106.6
107.9
108.9
110.2


Refrigerating capacity ratio (to R134a)
%
129.5
129.9
131.4
132.7
134.9


ASHRAE flammability classification

Class 2L
Class 2L
Class 2
Class 2
Class 2









(2) Refrigerating Machine Oil

(2) Refrigerating Machine Oil


A refrigerating oil can improve the lubricity in the refrigeration cycle apparatus and can also achieve efficient cycle performance by performing a refrigeration cycle such as a refrigeration cycle together with a refrigerant composition.


Examples of the refrigerating oil include oxygen-containing synthetic oils (e.g., ester-type refrigerating oils and ether-type refrigerating oils) and hydrocarbon refrigerating oils. In particular, ester-type refrigerating oils and ether-type refrigerating oils are preferred from the viewpoint of miscibility with refrigerants or refrigerant compositions. The refrigerating oils may be used alone or in combination of two or more.


The kinematic viscosity of the refrigerating oil at 40° C. is preferably 1 mm2/s or more and 750 mm2/s or less and more preferably 1 mm2/s or more and 400 mm2/s or less from at least one of the viewpoints of suppressing the deterioration of the lubricity and the hermeticity of compressors, achieving sufficient miscibility with refrigerants under low-temperature conditions, suppressing the lubrication failure of compressors, and improving the heat exchange efficiency of evaporators. Herein, the kinematic viscosity of the refrigerating oil at 100° C. may be, for example, 1 mm2/s or more and 100 mm2/s or less and is more preferably 1 mm2/s or more and 50 mm2/s or less.


The refrigerating oil preferably has an aniline point of −100° C. or higher and 0° C. or lower. The term “aniline point” herein refers to a numerical value indicating the solubility of, for example, a hydrocarbon solvent, that is, refers to a temperature at which when equal volumes of a sample (herein, refrigerating oil) and aniline are mixed with each other and cooled, turbidity appears because of their immiscibility (provided in JIS K 2256). Note that this value is a value of the refrigerating oil itself in a state in which the refrigerant is not dissolved. By using a refrigerating oil having such an aniline point, for example, even when bearings constituting resin functional components and insulating materials for electric motors are used at positions in contact with the refrigerating oil, the suitability of the refrigerating oil for the resin functional components can be improved. Specifically, if the aniline point is excessively low, the refrigerating oil readily infiltrates the bearings and the insulating materials, and thus the bearings and the like tend to swell. On the other hand, if the aniline point is excessively high, the refrigerating oil does not readily infiltrate the bearings and the insulating materials, and thus the bearings and the like tend to shrink. Accordingly, the deformation of the bearings and the insulating materials due to swelling or shrinking can be prevented by using the refrigerating oil having an aniline point within the above-described predetermined range (100° C. or higher and 0° C. or lower). If the bearings deform through swelling, the desired length of a gap at a sliding portion cannot be maintained. This may result in an increase in sliding resistance. If the bearings deform through shrinking, the hardness of the bearings increases, and consequently the bearings may be broken because of vibration of a compressor. In other words, the deformation of the bearings through shrinking may decrease the rigidity of the sliding portion. Furthermore, if the insulating materials (e.g., insulating coating materials and insulating films) of electric motors deform through swelling, the insulating properties of the insulating materials deteriorate. If the insulating materials deform through shrinking, the insulating materials may also be broken as in the case of the bearings, which also deteriorates the insulating properties. In contrast, when the refrigerating oil having an aniline point within the predetermined range is used as described above, the deformation of bearings and insulating materials due to swelling or shrinking can be suppressed, and thus such a problem can be avoided.


The refrigerating oil is used as a working fluid for a refrigerating machine by being mixed with a refrigerant composition. The content of the refrigerating oil relative to the whole amount of working fluid fora refrigerating machine is preferably 5 mass % or more and 60 mass % or less and more preferably 10 mass % or more and 50 mass % or less.


(2-1) Oxygen-Based Synthetic Oil


(2-1) Oxygen-Containing Synthetic Oil


An ester-type refrigerating oil or an ether-type refrigerating oil serving as an oxygen-containing synthetic oil is mainly constituted by carbon atoms and oxygen atoms. In the ester-type refrigerating oil or the ether-type refrigerating oil, an excessively low ratio (carbon/oxygen molar ratio) of carbon atoms to oxygen atoms increases the hygroscopicity, and an excessively high ratio of carbon atoms to oxygen atoms deteriorates the miscibility with a refrigerant. Therefore, the molar ratio is preferably 2 or more and 7.5 or less.

    • (2-1-1) Ester-Based Refrigerating Machine Oil


      (2-1-1) Ester-Type Refrigerating Oil


Examples of base oil components of the ester-type refrigerating oil include dibasic acid ester oils of a dibasic acid and a monohydric alcohol, polyol ester oils of a polyol and a fatty acid, complex ester oils of a polyol, a polybasic acid, and a monohydric alcohol (or a fatty acid), and polyol carbonate oils from the viewpoint of chemical stability.


(Dibasic Acid Ester Oil)


The dibasic acid ester oil is preferably an ester of a dibasic acid such as oxalic acid, malonic acid, succinic acid, glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, sebacic acid, phthalic acid, isophthalic acid, or terephthalic acid, in particular, a dibasic acid having 5 to 10 carbon atoms (e.g., glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, or sebacic acid) and a monohydric alcohol having a linear or branched alkyl group and having 1 to 15 carbon atoms (e.g., methanol, ethanol, propanol, butanol, pentanol, hexanol, heptanol, octanol, nonanol, decanol, undecanol, dodecanol, tridecanol, tetradecanol, or pentadecanol). Specific examples of the dibasic acid ester oil include ditridecyl glutarate, di(2-ethylhexyl) adipate, diisodecyl adipate, ditridecyl adipate, and di(3-ethylhexyl) sebacate.


(Polyol Ester Oil)


The polyol ester oil is an ester synthesized from a polyhydric alcohol and a fatty acid (carboxylic acid), and has a carbon/oxygen molar ratio oft or more and 7.5 or less, preferably 3.2 or more and 5.8 or less.


The polyhydric alcohol constituting the polyol ester oil is a diol (e.g., ethylene glycol, 1,3-propanediol, propylene glycol, 1,4-butanediol, 1,2-butanediol, 2-methyl-1,3-propanediol, 1,5-pentanediol, neopentyl glycol, 1,6-hexanediol, 2-ethyl-2-methyl-1,3-propanediol, 1,7-heptanediol, 2-methyl-2-propyl-1,3-propanediol, 2,2-diethyl-1,3-propanediol, 1,8-octanediol, 1,9-nonanediol, 1,10-decanediol, 1,11-undecanediol, or 1,12-dodecanediol) or a polyol having 3 to 20 hydroxyl groups (trimethylolethane, trimethylolpropane, trimethylolbutane, di-(trimethylolpropane), tri-(trimethylolpropane), pentaerythritol, di-(pentaerythritol), tri-(pentaerythritol), glycerol, polyglycerol (glycerol dimer or trimer), 1,3,5-pentanetriol, sorbitol, sorbitan, a sorbitol-glycerol condensate, a polyhydric alcohol such as adonitol, arabitol, xylitol, or mannitol, a saccharide such as xylose, arabinose, ribose, rhamnose, glucose, fructose, galactose, mannose, sorbose, cellobiose, maltose, isomaltose, trehalose, sucrose, raffinose, gentianose, or melezitose, or a partially etherified product of the foregoing). One or two or more polyhydric alcohols may constitute an ester.


For the fatty acid constituting the polyol ester, the number of carbon atoms is not limited, but is normally 1 to 24. A linear fatty acid or a branched fatty acid is preferred. Examples of the linear fatty acid include acetic acid, propionic acid, butanoic acid, pentanoic acid, hexanoic acid, heptanoic acid, octanoic acid, nonanoic acid, decanoic acid, undecanoic acid, dodecanoic acid, tridecanoic acid, tetradecanoic acid, pentadecanoic acid, hexadecanoic acid, heptadecanoic acid, octadecanoic acid, nonadecanoic acid, eicosanoic acid, oleic acid, linoleic acid, and linolenic acid. The hydrocarbon group that bonds to a carboxy group may have only a saturated hydrocarbon or may have an unsaturated hydrocarbon. Examples of the branched fatty acid include 2-methylpropionic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2-dimethylpropionic acid, 2-methylpentanoic acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, 2-methylhexanoic acid, 3-methylhexanoic acid, 4-methylhexanoic acid, 5-methylhexanoic acid, 2,2-dimethylpentanoic acid, 2,3-dimethylpentanoic acid, 2,4-dimethylpentanoic acid, 3,3-dimethylpentanoic acid, 3,4-dimethylpentanoic acid, 4,4 dimethylpentanoic acid, 2-ethylpentanoic acid, 3-ethylpentanoic acid, 2,2,3-trimethylbutanoic acid, 2,3,3-trimethylbutanoic acid, 2-ethyl-2-methylbutanoic acid, 2-ethyl-3-methylbutanoic acid, 2-methylheptanoic acid, 3-methylheptanoic acid, 4-methylheptanoic acid, 5-methylheptanoic acid, 6-methylheptanoic acid, 2-ethylhexanoic acid, 3-ethylhexanoic acid, 4-ethylhexanoic acid, 2,2-dimethylhexanoic acid, 2,3-dimethylhexanoic acid, 2,4 dimethylhexanoic acid, 2,5-dimethylhexanoic acid, 3,3-dimethylhexanoic acid, 3,4-dimethylhexanoic acid, 3,5-dimethylhexanoic acid, 4,4-dimethylhexanoic acid, 4,5-dimethylhexanoic acid, 5,5-dimethylhexanoic acid, 2-propylpentanoic acid, 2-methyloctanoic acid, 3-methyloctanoic acid, 4-methyloctanoic acid, 5-methyloctanoic acid, 6-methyloctanoic acid, 7-methyloctanoic acid, 2,2-dimethylheptanoic acid, 2,3-dimethylheptanoic acid, 2,4-dimethylheptanoic acid, 2,5-dimethylheptanoic acid, 2,6-dimethylheptanoic acid, 3,3-dimethylheptanoic acid, 3,4-dimethylheptanoic acid, 3,5-dimethylheptanoic acid, 3,6-dimethylheptanoic acid, 4,4-dimethylheptanoic acid, 4,5-dimethylheptanoic acid, 4,6-dimethylheptanoic acid, 5,5-dimethylheptanoic acid, 5,6-dimethylheptanoic acid, 6,6-dimethylheptanoic acid, 2-methyl-2-ethylhexanoic acid, 2-methyl-3-ethylhexanoic acid, 2 methyl-4-ethylhexanoic acid, 3-methyl-2-ethylhexanoic acid, 3-methyl-3-ethylhexanoic acid, 3-methyl-4-ethylhexanoic acid, 4-methyl-2-ethylhexanoic acid, 4-methyl-3-ethylhexanoic acid, 4-methyl-4-ethylhexanoic acid, 5-methyl-2-ethylhexanoic acid, 5-methyl-3-ethylhexanoic acid, 5-methyl-4-ethylhexanoic acid, 2-ethylheptanoic acid, 3-methyloctanoic acid, 3,5,5-trimethylhexanoic acid, 2-ethyl-2,3,3-trimethylbutyric acid, 2,2,4,4-tetramethylpentanoic acid, 2,2,3,3-tetramethylpentanoic acid, 2,2,3,4-tetramethylpentanoic acid, and 2,2-diisopropylpropanoic acid. One or two or more fatty acids selected from the foregoing may constitute an ester.


One polyhydric alcohol may be used to constitute an ester or a mixture of two or more polyhydric alcohols may be used to constitute an ester. The fatty acid constituting an ester may be a single component, or two or more fatty acids may constitute an ester. The fatty acids may be individual fatty acids of the same type or may be two or more types of fatty acids as a mixture. The polyol ester oil may have a free hydroxyl group.


Specifically, the polyol ester oil is more preferably an ester of a hindered alcohol such as neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, di-(trimethylolpropane), tri-(trimethylolpropane), pentaerythritol, di-(pentaerythritol), or tri-(pentaerythritol); further preferably an ester of neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, pentaerythritol, or di-(pentaerythritol); and preferably an ester of neopentyl glycol, trimethylolpropane, pentaerythritol, di-(pentaerythritol), or the like and a fatty acid having 2 to 20 carbon atoms.


The fatty acid constituting such a polyhydric alcohol fatty acid ester may be only a fatty acid having a linear alkyl group or may be selected from fatty acids having a branched structure. A mixed ester of linear and branched fatty acids may be employed. Furthermore, two or more fatty acids selected from the above fatty acids may be used to constitute an ester.


Specifically, for example, in the case of a mixed ester of linear and branched fatty acids, the molar ratio of a linear fatty acid having 4 to 6 carbon atoms and a branched fatty acid having 7 to 9 carbon atoms is 15:85 to 90:10, preferably 15:85 to 85:15, more preferably 20:80 to 80:20, further preferably 25:75 to 75:25, and most preferably 30:70 to 70:30. The total content of the linear fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester is preferably 20 mol % or more. The fatty acid preferably has such a composition that both of sufficient miscibility with a refrigerant and viscosity required as a refrigerating oil are achieved. The content of a fatty acid herein refers to a value relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester contained in the refrigerating oil.


In particular, the refrigerating oil preferably contains an ester (hereafter referred to as a “polyhydric alcohol fatty acid ester (A)”) in which the molar ratio of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms is 15:85 to 90:10, the fatty acid having 4 to 6 carbon atoms contains 2-methylpropionic acid, and the total content of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms relative to the whole amount of fatty acid constituting the above ester is 20 mol % or more.


The polyhydric alcohol fatty acid ester (A) includes a complete ester in which all hydroxyl groups of a polyhydric alcohol are esterified, a partial ester in which some hydroxyl groups of a polyhydric alcohol are left without being esterified, and a mixture of a complete ester and a partial ester. The hydroxyl value of the polyhydric alcohol fatty acid ester (A) is preferably 10 mgKOH/g or less, more preferably 5 mgKOH/g or less, and most preferably 3 mgKOH/g or less.


For the fatty acid constituting the polyhydric alcohol fatty acid ester (A), the molar ratio of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms is 15:85 to 90:10, preferably 15:85 to 85:15, more preferably 20:80 to 80:20, further preferably 25:75 to 75:25, and most preferably 30:70 to 70:30. The total content of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester (A) is 20 mol % or more. In the case where the above conditions for the composition of the fatty acid are not satisfied, if difluoromethane is contained in the refrigerant composition, both of sufficient miscibility with the difluoromethane and viscosity required as a refrigerating oil are not easily achieved at high levels. The content of a fatty acid refers to a value relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester contained in the refrigerating oil.


Specific examples of the fatty acid having 4 to 6 carbon atoms include butanoic acid, 2-methylpropionic acid, pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2 dimethylpropionic acid, 2-methylpentanoic acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, and hexanoic acid. Among them, a fatty acid having a branched structure at an alkyl skeleton, such as 2-methylpropionic acid, is preferred.


Specific examples of the branched fatty acid having 7 to 9 carbon atoms include 2 methylhexanoic acid, 3-methylhexanoic acid, 4-methylhexanoic acid, 5-methylhexanoic acid, 2,2-dimethylpentanoic acid, 2,3-dimethylpentanoic acid, 2,4-dimethylpentanoic acid, 3,3-dimethylpentanoic acid, 3,4-dimethylpentanoic acid, 4,4-dimethylpentanoic acid, 2-ethylpentanoic acid, 3-ethylpentanoic acid, 1,1,2-trimethylbutanoic acid, 1,2,2-trimethylbutanoic acid, 1-ethyl-1-methylbutanoic acid, 1-ethyl-2-methylbutanoic acid, octanoic acid, 2-ethylhexanoic acid, 3-ethylhexanoic acid, 3,5-dimethylhexanoic acid, 2,4-dimethylhexanoic acid, 3,4-dimethylhexanoic acid, 4,5-dimethylhexanoic acid, 2,2-dimethylhexanoic acid, 2-methylheptanoic acid, 3-methylheptanoic acid, 4-methylheptanoic acid, 5-methylheptanoic acid, 6-methylheptanoic acid, 2-propylpentanoic acid, nonanoic acid, 2,2-dimethyiheptanoic acid, 2-methyloctanoic acid, 2-ethylheptanoic acid, 3-methyloctanoic acid, 3,5,5-trimethylhexanoic acid, 2-ethyl-2,3,3-trimethylbutyric acid, 2,2,4,4-tetramethylpentanoic acid, 2,2,3,3-tetramethylpentanoic acid, 2,2,3,4-tetramethylpentanoic acid, and 2,2-diisopropylpropanoic acid.


The polyhydric alcohol fatty acid ester (A) may contain, as an acid constituent component, a fatty acid other than the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms as long as the molar ratio of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms is 15:85 to 90:10 and the fatty acid having 4 to 6 carbon atoms contains 2-methylpropionic acid.


Specific examples of the fatty acid other than the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms include fatty acids having 2 or 3 carbon atoms, such as acetic acid and propionic acid; linear fatty acids having 7 to 9 carbon atoms, such as heptanoic acid, octanoic acid, and nonanoic acid; and fatty acids having 10 to 20 carbon atoms, such as decanoic acid, undecanoic acid, dodecanoic acid, tridecanoic acid, tetradecanoic acid, pentadecanoic acid, hexadecanoic acid, heptadecanoic acid, octadecanoic acid, nonadecanoic acid, eicosanoic acid, and oleic acid.


When the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms are used in combination with fatty acids other than these fatty acids, the total content of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester (A) is preferably 20 mol % or more, more preferably 25 mol % or more, and further preferably 30 mol % or more. When the content is 20 mol % or more, sufficient miscibility with difluoromethane is achieved in the case where the difluoromethane is contained in the refrigerant composition.


A polyhydric alcohol fatty acid ester (A) containing, as acid constituent components, only 2-methylpropionic acid and 3,5,5-trimethylhexanoic acid is particularly preferred from the viewpoint of achieving both necessary viscosity and miscibility with difluoromethane in the case where the difluoromethane is contained in the refrigerant composition.


The polyhydric alcohol fatty acid ester may be a mixture of two or more esters having different molecular structures. In this case, individual molecules do not necessarily satisfy the above conditions as long as the whole fatty acid constituting a pentaerythritol fatty acid ester contained in the refrigerating oil satisfies the above conditions.


As described above, the polyhydric alcohol fatty acid ester (A) contains the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms as essential acid components constituting the ester and may optionally contain other fatty acids as constituent components. In other words, the polyhydric alcohol fatty acid ester (A) may contain only two fatty acids as acid constituent components or three or more fatty acids having different structures as acid constituent components, but the polyhydric alcohol fatty acid ester preferably contains, as an acid constituent component, only a fatty acid whose carbon atom (α-position carbon atom) adjacent to carbonyl carbon is not quaternary carbon. If the fatty acid constituting the polyhydric alcohol fatty acid ester contains a fatty acid whose α-position carbon atom is quaternary carbon, the lubricity in the presence of difluoromethane in the case where the difluoromethane is contained in the refrigerant composition tends to be insufficient.


The polyhydric alcohol constituting the polyol ester according to this embodiment is preferably a polyhydric alcohol having 2 to 6 hydroxyl groups.


Specific examples of the dihydric alcohol (diol) include ethylene glycol, 1,3-propanediol, propylene glycol, 1,4-butanediol, 1,2-butanediol, 2-methyl-1,3-propanediol, 1,5-pentanediol, neopentyl glycol, 1,6-hexanediol, 2-ethyl-2-methyl-1,3-propanediol, 1,7-heptanediol, 2-methyl-2-propyl-1,3-propanediol, 2,2-diethyl-1,3-propanediol, 1,8-octanediol, 1,9-nonanediol, 1,10-decanediol, 1,11-undecanediol, and 1,12-dodecanediol. Specific examples of the trihydric or higher alcohol include polyhydric alcohols such as trimethylolethane, trimethylolpropane, trimethylolbutane, di-(trimethylolpropane), tri-(trimethylolpropane), pentaerythritol, di-(pentaerythritol), tri-(pentaerythritol), glycerol, polyglycerol (glycerol dimer or trimer), 1,3,5-pentanetriol, sorbitol, sorbitan, sorbitol glycerol condensates, adonitol, arabitol, xylitol, and mannitol; saccharides such as xylose, arabinose, ribose, rhamnose, glucose, fructose, galactose, mannose, sorbose, and cellobiose; and partially etherified products of the foregoing. Among them, in terms of better hydrolysis stability, an ester of a hindered alcohol such as neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, di-(trimethylolpropane), tri-(trimethylolpropane), pentaerythritol, di-(pentaerythritol), or tri-(pentaerythritol) is preferably used; an ester of neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, pentaerythritol, or di-(pentaerythritol) is more preferably used; and neopentyl glycol, trimethylolpropane, pentaerythritol, or di-(pentaerythritol) is further preferably used. In terms of excellent miscibility with a refrigerant and excellent hydrolysis stability, a mixed ester of pentaerythritol, di-(pentaerythritol), or pentaerythritol and di-(pentaerythritol) is most preferably used.


Preferred examples of the acid constituent component constituting the polyhydric alcohol fatty acid ester (A) are as follows:


(i) a combination of 1 to 13 acids selected from butanoic acid, 2-methylpropionic acid, pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2-dimethylpropionic acid, 2-methylpentanoic, acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, and hexanoic acid and 1 to 13 acids selected from 2-methylhexanoic acid, 3-methylhexanoic acid, 4-methylhexanoic acid, 5-methylhexanoic acid, 2,2-dimethylpentanoic acid, 2,3-dimethylpentanoic acid, 2,4-dimethylpentanoic acid, 3,3-dimethylpentanoic acid, 3,4-dimethylpentanoic acid, 4,4-dimethylpentanoic acid, 2-ethylpentanoic acid, 3-ethylpentanoic acid, and 2-ethyl-3 methylbutanoic acid;


(ii) a combination of 1 to 13 acids selected, from butanoic acid, 2-methylpropionic acid, pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2-dimethylpropionic acid, 2-methylpentanoic acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, and hexanoic acid and 1 to 25 acids selected from 2-methylheptanoic acid, 3-methylheptanoic acid, 4-methylheptanoic acid, 5-methylheptanoic acid, 6-methylheptanoic acid, 2,2-dimethylhexanoic acid, 3,3-dimethylhexanoic acid, 4,4-dimethylhexanoic acid, 5,5-dimethylhexanoic acid, 2,3-dimethylhexanoic acid, 2,4-dimethylhexanoic acid, 2,5-dimethylhexanoic acid, 3,4-dimethylhexanoic acid, 3,5-dimethylhexanoic acid, 4,5-dimethylhexanoic acid, 2,2,3 trimethylpentanoic acid, 2,3,3-trimethylpentanoic acid, 2,4,4-trimethylpentanoic acid, 3,4,4-trimethylpentanoic acid, 2-ethylhexanoic acid, 3-ethylhexanoic acid, 2-propylpentanoic acid, 2-methyl-2-ethylpentanoic acid, 2-methyl-3-ethylpentanoic acid, and 3-methyl-3-ethylpentanoic acid; and


(iii) a combination of 1 to 13 acids selected from butanoic acid, 2-methylpropionic acid, pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2-dimethylpropionic acid, 2-methylpentanoic acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, and hexanoic acid and 1 to 50 acids selected from, 2-methyloctanoic acid, 3-methyloctanoic acid, 4-methyloctanoic acid, 5-methyloctanoic acid, 6-methyloctanoic acid, 7-methyloctanoic acid, 8-methyloctanoic acid, 2,2-dimethylheptanoic acid, 3,3-dimethylheptanoic acid, 4,4-dimethylheptanoic acid, 5,5-dimethylheptanoic acid, 6,6-dimethylheptanoic acid, 2,3-dimethylheptanoic acid, 2,4-dimethylheptanoic acid, 2,5-dimethylheptanoic acid, 2,6-dimethylheptanoic acid, 3,4-dimethylheptanoic acid, 3,5-dimethylheptanoic acid, 3,6-dimethylheptanoic acid, 4,5-dimethylheptanoic acid, 4,6-dimethylheptanoic acid, 2-ethylheptanoic acid, 3-ethylheptanoic acid, 4-ethylheptanoic acid, 5-ethylheptanoic acid, 2-propylhexanoic acid, 3-propylhexanoic acid, 2-butylpentanoic acid, 2,2,3-trimethylhexanoic acid, 2,2,3-trimethylhexanoic acid, 2,2,4-trimethylhexanoic acid, 2,2,5-trimethylhexanoic acid, 2,3,4-trimethylhexanoic acid, 2,3,5 trimethylhexanoic acid, 3,3,4-trimethylhexanoic acid, 3,3,5-trimethylhexanoic acid, 3,5,5-trimethylhexanoic acid, 4,4,5-trimethylhexanoic acid, 4,5,5-trimethylhexanoic acid, 2,2,3,3-tetramethylpentanoic acid, 2,2,3,4-tetramethylpentanoic acid, 2,2,4,4-tetramethylpentanoic acid, 2,3,4,4-tetramethylpentanoic acid, 3,3,4,4-tetramethylpentanoic acid, 2,2-diethylpentanoic acid, 2,3-diethylpentanoic acid, 3,3-diethylpentanoic acid, 2-ethyl-2,3,3-trimethylbutyric acid, 3-ethyl-2,2,3-trimethylbutyric acid, and 2,2-diisopropylpropionic acid.


Further preferred examples of the acid constituent component constituting the polyhydric alcohol fatty acid ester are as follows:


(i) a combination of 2-methylpropionic acid and 1 to 13 acids selected from 2-methylhexanoic acid, 3-methylhexanoic acid, 4-methylhexanoic acid, 5-methylhexanoic acid, 2,2 dimethylpentanoic acid, 2,3-dimethylpentanoic acid, 2,4-dimethylpentanoic acid, 3,3-dimethylpentanoic acid, 3,4-dimethylpentanoic acid, 4,4-dimethylpentanoic acid, 2-ethylpentanoic acid, 3-ethylpentanoic acid, and 2-ethyl-3-methylbutanoic acid;


(ii) a combination of 2-methylpropionic acid and 1 to 25 acids selected from 2-methylheptanoic acid, 3-methylheptanoic acid, 4-methylheptanoic acid, 5-methylheptanoic acid, 6 methylheptanoic acid, 2,2-dimethylhexanoic acid, 3,3-dimethylhexanoic acid, 4,4-dimethylhexanoic acid, 5,5-dimethylhexanoic acid, 2,3-dimethylhexanoic acid, 2,4-dimethylhexanoic acid, 2,5-dimethylhexanoic acid, 3,4-dimethylhexanoic acid, 3,5-dimethylhexanoic acid, 4,5-dimethylhexanoic acid, 2,2,3-trimethylpentanoic acid, 2,3,3-trimethylpentanoic acid, 2,4,4-trimethylpentanoic acid, 3,4,4-trimethylpentanoic acid, 2 ethylhexanoic acid, 3-ethylhexanoic acid, 2-propylpentanoic acid, 2-methyl-2-ethylpentanoic acid, 2-methyl-3-ethylpentanoic acid, and 3-methyl-3-ethylpentanoic acid; and


(iii) a combination of 2-methylpropionic acid and 1 to 50 acids selected from 2-methyloctanoic acid, 3-methyloctanoic acid, 4-methyloctanoic acid, 5-methyloctanoic acid, 6-methyloctanoic acid, 7-methyloctanoic acid, 8-methyloctanoic acid, 2,2-dimethylheptanoic acid, 3,3-dimethylheptanoic acid, 4,4-dimethylheptanoic acid, 5,5-dimethylheptanoic acid, 6,6-dimethylheptanoic acid, 2,3-dimethylheptanoic acid, 2,4-dimethylheptanoic acid, 2,5-dimethylheptanoic acid, 2,6-dimethylheptanoic acid, 3,4-dimethylheptanoic acid, 3,5-dimethylheptanoic acid, 3,6-dimethylheptanoic acid, 4,5-dimethylheptanoic acid, 4,6-dimethylheptanoic acid, 2-ethylheptanoic acid, 3-ethylheptanoic acid, 4-ethylheptanoic acid, 5-ethylheptanoic acid, 2-propylhexanoic acid, 3-propylhexanoic acid, 2-butylpentanoic acid, 2,2,3-trimethylhexanoic acid, 2,2,3-trimethylhexanoic acid, 2,2,4-trimethylhexanoic acid, 2,2,5-trimethylhexanoic acid, 2,3,4-trimethylhexanoic acid, 2,3,5-trimethylhexanoic acid, 3,3,4-trimethylhexanoic acid, 3,3,5-trimethylhexanoic acid, 3,5,5-trimethylhexanoic acid, 4,4,5-trimethylhexanoic acid, 4,5,5-trimethylhexanoic acid, 2,2,3,3-tetramethylpentanoic acid, 2,2,3,4-tetramethylpentanoic acid, 2,2,4,4-tetramethylpentanoic acid, 2,3,4,4-tetramethylpentanoic acid, 3,3,4,4-tetramethylpentanoic acid, 2,2-diethylpentanoic acid, 2,3-diethylpentanoic acid, 3,3-diethylpentanoic acid, 2-ethyl-2,3,3-trimethylbutyric acid, 3-ethyl-2,2,3-trimethylbutyricacid, and 2,2-diisopropylpropionic acid.


The content of the polyhydric alcohol fatty acid ester (A) is 50 mass % or more, preferably 60 mass % or more, more preferably 70 mass % or more, and further preferably 75 mass % or more relative to the whole amount of the refrigerating oil. The refrigerating oil according to this embodiment may contain a lubricating base oil other than the polyhydric alcohol fatty acid ester (A) and additives as described later. However, if the content of the polyhydric alcohol fatty acid ester (A) is less than 50 mass %, necessary viscosity and miscibility cannot be achieved at high levels.


In the refrigerating oil according to this embodiment, the polyhydric alcohol fatty acid ester (A) is mainly used as a base oil. The base oil of the refrigerating oil according to this embodiment may be a polyhydric alcohol fatty acid ester (A) alone (i.e., the content of the polyhydric alcohol fatty acid ester (A) is 100 mass %). However, in addition to the polyhydric alcohol fatty acid ester (A), a base oil other than the polyhydric alcohol fatty acid ester (A) may be further contained to the degree that the excellent performance of the polyhydric alcohol fatty acid ester (A) is not impaired. Examples of the base oil other than the polyhydric alcohol fatty acid ester (A) include hydrocarbon oils such as mineral oils, olefin polymers, alkyldiphenylalkanes, alkylnaphthalenes, and alkylbenzenes; and esters other than the polyhydric alcohol fatty acid ester (A), such as polyol esters, complex esters, and alicyclic dicarboxylic acid esters, and oxygen-containing synthetic oils (hereafter, may be referred to as “other oxygen-containing synthetic oils”) such as polyglycols, polyvinyl ethers, ketones, polyphenyl ethers, silicones, polysiloxanes, and perfluoroethers.


Among them, the oxygen-containing synthetic oil is preferably an ester other than the polyhydric alcohol fatty acid ester (A), a polyglycol, or a polyvinyl ether and particularly preferably a polyol ester other than the polyhydric alcohol fatty acid ester (A). The polyol ester other than the polyhydric alcohol fatty acid ester (A) is an ester of a fatty acid and a polyhydric alcohol such as neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, pentaerythritol, or dipentaerythritol and is particularly preferably an ester of neopentyl glycol and a fatty acid, an ester of pentaerythritol and a fatty acid, or an ester of dipentaerythritol and a fatty acid.


The neopentyl glycol ester is preferably an ester of neopentyl glycol and a fatty acid having 5 to 9 carbon atoms. Specific examples of the neopentyl glycol ester include neopentyl glycol di(3,5,5-trimethylhexanoate), neopentyl glycol di(2-ethylhexanoate), neopentyl glycol di(2-methylhexanoate), neopentyl glycol di(2-ethylpentanoate), an ester of neopentyl glycol and 2-methylhexanoic acid·2-ethylpentanoic acid, an ester of neopentyl glycol and 3-methylhexanoic acid·5-methylhexanoic acid, an ester of neopentyl glycol and 2-methylhexanoic acid·2-ethylhexanoic acid, an ester of neopentyl glycol and 3,5-dimethylhexanoic acid·4,5-dimethylhexanoic acid·3,4-dimethylhexanoic acid, neopentyl glycol dipentanoate, neopentyl glycol di(2-ethylbutanoate), neopentyl glycol di(2-methylpentanoate), neopentyl glycol di(2-methylbutanoate), and neopentyl glycol di(3-methylbutanoate).


The pentaerythritol ester is preferably an ester of pentaerythritol and a fatty acid having 5 to 9 carbon atoms. The pentaerythritol ester is, specifically, an ester of pentaerythritol and at least one fatty acid selected from pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, hexanoic acid, 2-methylpentanoic acid, 2-ethylbutanoic acid, 2-ethylpentanoic acid, 2-methylhexanoic acid, 3,5,5-trimethylhexanoic acid, and 2-ethylhexanoic acid.


The dipentaerythritol ester is preferably an ester of dipentaerythritol and a fatty acid having 5 to 9 carbon atoms. The dipentaerythritol ester is, specifically, an ester of dipentaerythritol and at least, one fatty acid selected from pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, hexanoic acid, 2-methylpentanoic acid, 2-ethylbutanoic acid, 2-ethylpentanoic acid, 2-methylhexanoic acid, 3,5,5-trimethylhexanoic acid, and 2-ethylhexanoic acid.


When the refrigerating oil according to this embodiment contains an oxygen-containing synthetic oil other than the polyhydric alcohol fatty acid ester (A), the content of the oxygen-containing synthetic oil other than the polyhydric alcohol fatty acid ester (A) is not limited as long as excellent lubricity and miscibility of the refrigerating oil according to this embodiment are not impaired. When a polyol ester other than the polyhydric alcohol fatty acid ester (A) is contained, the content of the polyol ester is preferably less than 50 mass %, more preferably 45 mass % or less, still more preferably 40 mass % or less, even more preferably 35 mass % or less, further preferably 30 mass % or less, and most preferably 25 mass % or less relative to the whole amount of the refrigerating oil. When an oxygen-containing synthetic oil other than the polyol ester is contained, the content of the oxygen-containing synthetic oil is preferably less than 50 mass %, more preferably 40 mass % or less, and further preferably 30 mass % or less relative to the whole amount of the refrigerating oil. If the content of the polyol ester other than the pentaerythritol fatty acid ester or the oxygen-containing synthetic oil is excessively high, the above-described effects are not sufficiently produced.


The polyol ester other than the polyhydric alcohol fatty acid ester (A) may be a partial ester in which some hydroxyl groups of a polyhydric alcohol are left without being esterified, a complete ester in which all hydroxyl groups are esterified, or a mixture of a partial ester and a complete ester. The hydroxyl value is preferably 10 mgKOH/g or less, more preferably 5 mgKOH/g or less, and most preferably 3 mgKOH/g or less.


When the refrigerating oil and the working fluid for a refrigerating machine according to this embodiment contain a polyol ester other than the polyhydric alcohol fatty acid ester (A), the polyol ester may contain one polyol ester having a single structure or a mixture of two or more polyol esters having different structures.


The polyol ester other than the polyhydric alcohol fatty acid ester (A) may any of an ester of one fatty acid and one polyhydric alcohol, an ester of two or more fatty acids and one polyhydric alcohol, an ester of one fatty acid and two or more polyhydric alcohols, and an ester of two or more fatty acids and two or more polyhydric alcohols.


The refrigerating oil according to this embodiment may be constituted by only the polyhydric alcohol fatty acid ester (A) or by the polyhydric alcohol fatty acid ester (A) and other base oils. The refrigerating oil may further contain various additives described later. The working fluid for a refrigerating machine according to this embodiment may also further contain various additives. In the following description, the content of additives is expressed relative to the whole amount of the refrigerating oil, but the content of these components in the working fluid for a refrigerating machine is desirably determined so that the content is within the preferred range described later when expressed relative to the whole amount of the refrigerating oil.


To further improve the abrasion resistance and load resistance of the refrigerating oil and the working fluid for a refrigerating machine according to this embodiment, at least one phosphorus compound selected from the group consisting of phosphoric acid esters, acidic phosphoric acid esters, thiophosphoric acid esters, amine salts of acidic phosphoric acid esters, chlorinated phosphoric acid esters, and phosphorous acid esters can be added. These phosphorus compounds are esters of phosphoric acid or phosphorous acid and alkanol or polyether-type alcohol, or derivatives thereof.


Specific examples of the phosphoric acid ester include tributyl phosphate, tripentyl phosphate, trihexyl phosphate, triheptyl phosphate, trioctyl phosphate, trinonyl phosphate, tridecyl phosphate, triundecyl phosphate, tridodecyl phosphate, tritridecyl phosphate, tritetradecyl phosphate, tripentadecyl phosphate, trihexadecyl phosphate, triheptadecyl phosphate, trioctadecyl phosphate, trioleyl phosphate, triphenyl phosphate, tricresyl phosphate, trixylenyl phosphate, cresyldiphenyl phosphate, and xylenyldiphenyl phosphate.


Examples of the acidic phosphoric acid ester include monobutyl acid phosphate, monopentyl acid phosphate, monohexyl acid phosphate, monoheptyl acid phosphate, monooctyl acid phosphate, monononyl acid phosphate, monodecyl acid phosphate, monoundecyl acid phosphate, monododecyl acid phosphate, monotridecyl acid phosphate, monotetradecyl acid phosphate, monopentadecyl acid phosphate, monohexadecyl acid phosphate, monoheptadecyl acid phosphate, monooctadecyl acid phosphate, monooleyl acid phosphate, dibutyl acid phosphate, dipentyl acid phosphate, dihexyl acid phosphate, diheptyl acid phosphate, dioctyl acid phosphate, dinonyl acid phosphate, didecyl acid phosphate, diundecyl acid phosphate, didodecyl acid phosphate, ditridecyl acid phosphate, ditetradecyl acid phosphate, dipentadecyl acid phosphate, dihexadecyl acid phosphate, diheptadecyl acid phosphate, dioctadecyl acid phosphate, and dioleyl acid phosphate.


Examples of the thiophosphoric acid ester include tributyl phosphorothionate, tripentyl phosphorothionate, trihexyl phosphorothionate, triheptyl phosphorothionate, trioctyl phosphorothionate, trinonyl phosphorothionate, tridecyl phosphorothionate, triundecyl phosphorothionate, tridodecyl phosphorothionate, tritridecyl phosphorothionate, tritetradecyl phosphorothionate, tripentadecyl phosphorothionate, trihexadecyl phosphorothionate, triheptadecyl phosphorothionate, trioctadecyl phosphorothionate, trioleyl phosphorothionate, triphenyl phosphorothionate, tricresyl phosphorothionate, trixylenyl phosphorothionate, cresyldiphenyl phosphorothionate, and xylenyldiphenyl phosphorothionate.


The amine salt of an acidic phosphoric acid ester is an amine salt of an acidic phosphoric acid ester and a primary, secondary, or tertiary amine that has a linear or branched alkyl group and that has 1 to 24 carbon atoms, preferably 5 to 18 carbon atoms.


For the amine constituting the amine salt of an acidic phosphoric acid ester, the amine salt is a salt of an amine such as a linear or branched methylamine, ethylamine, propylamine, butylamine, pentylamine, hexylamine, heptylamine, octylamine, nonylamine, decylamine, undecylamine, dodecylamine, tridecylamine, tetradecylamine, pentadecylamine, hexadecylamine, heptadecylamine, octadecylamine, oleylamine, tetracosylamine, dimethylamine, diethylamine, dipropylamine, dibutylamine, dipentylamine, dihexylamine, diheptylamine, dioctylamine, dinonylamine, didecylamine, diundecylamine, didodecylamine, ditridecylamine, ditetradecylamine, dipentadecylamine, dihexadecylamine, diheptadecylamine, dioctadecylamine, dioleylamine, ditetracosylamine, trimethylamine, triethylamine, tripropylamine, tributylamine, tripentylamine, trihexylamine, triheptylamine, trioctylamine, trinonylamine, tridecylamine, triundecylamine, tridodecylamine, tritridecylamine, tritetradecylamine, tripentadecylamine, trihexadecylamine, triheptadecylamine, trioctadecylamine, trioleylamine, or tritetracosylamine. The amine may be a single compound or a mixture of two or more compounds.


Examples of the chlorinated phosphoric acid ester include tris(dichloropropyl) phosphate, tris(chloroethyl) phosphate, tris(chlorophenyl) phosphate, and polyoxyalkylene·bis[di(chloroaklyl)] phosphate. Examples of the phosphorous acid ester include dibutyl phosphite, dipentyl phosphite, dihexyl phosphite, diheptyl phosphite, dioctyl phosphite, dinonyl phosphite, didecyl phosphite, diundecyl phosphite, didodecyl phosphite, dioleyl phosphite, diphenyl phosphite, dicresyl phosphite, tributyl phosphite, tripentyl phosphite, trihexyl phosphite, triheptyl phosphite, trioctyl phosphite, trinonyl phosphite, tridecyl phosphite, triundecyl phosphite, tridodecyl phosphite, trioleyl phosphite, triphenyl phosphite, and tricresyl phosphite. Mixtures of these compounds can also be used.


When the refrigerating oil and the working fluid for a refrigerating machine according to this embodiment contain the above-described phosphorus compound, the content of the phosphorus compound is not limited, but is preferably 0.01 to 5.0 mass % and more preferably 0.02 to 3.0 mass % relative to the whole amount of the refrigerating oil (relative to the total amount of the base oil and all the additives). The above-described phosphorus compounds may used alone or in combination of two or more.


The refrigerating oil and the working fluid for a refrigerating machine according to this embodiment may contain a terpene compound to further improve the thermal and chemical stability. The “terpene compound” in the present invention refers to a compound obtained by polymerizing isoprene and a derivative thereof, and a dimer to an octamer of isoprene are preferably used. Specific examples of the terpene compound include monoterpenes such as geraniol, nerol, linalool, citral (including geranial), citronellol, menthol, limonene, terpinerol, carvone, ionone, thujone, camphor, and borneol; sesquiterpenes such as farnesene, farnesol, nerolidol, juvenile hormone, humulene, caryophyllene, elemene, cadinol, cadinene, and tutin; diterpenes such as geranylgeraniol, phytol, abietic acid, pimaragen, daphnetoxin, taxol, and pimaric acid; sesterterpenes such as geranylfarnesene; triterpenes such as squalene, limonin, camelliagenin, hopane, and lanosterol; and tetraterpenes such as carotenoid.


Among these terpene compounds, the terpene compound is preferably monoterpene, sesquiterpene, or diterpene, more preferably sesquiterpene, and particularly preferably a farnesene (3,7,11-trimethyldodeca-1,3,6,10-tetraene) and/or β-farnesene (7,11-dimethyl-3-methylidenedodeca-1,6,10-triene). In the present invention, the terpene compounds may be used alone or in combination of two or more.


The content of the terpene compound in the refrigerating oil according to this embodiment is not limited, but is preferably 0.001 to 10 mass %, more preferably 0.01 to 5 mass %, and further preferably 0.05 to 3 mass % relative to the whole amount of the refrigerating oil. If the content of the terpene compound is less than 0.001 mass %, an effect of improving the thermal and chemical stability tends to be insufficient. If the content is more than 10 mass %, the lubricity tends to be insufficient. The content of the terpene compound in the working fluid for a refrigerating machine according to this embodiment is desirably determined so that the content is within the above preferred range when expressed relative to the whole amount of the refrigerating oil.


The refrigerating oil and the working fluid for a refrigerating machine according to this embodiment may contain at least one epoxy compound selected from phenyl glycidyl ether-type epoxy compounds, alkyl glycidyl ether-type epoxy compounds, glycidyl ester-type epoxy compounds, allyloxirane compounds, alkyloxirane compounds, alicyclic epoxy compounds, epoxidized fatty acid monoesters, and epoxidized vegetable oils to further improve the thermal and chemical stability.


Specific examples of the phenyl glycidyl ether-type epoxy compound include phenyl glycidyl ether and alkylphenyl glycidyl ethers. The alkylphenyl glycidyl ether herein is an alkylphenyl glycidyl ether having 1 to 3 alkyl groups with 1 to 13 carbon atoms. In particular, the alkylphenyl glycidyl ether is preferably an alkylphenyl glycidyl ether having one alkyl group with 4 to 10 carbon atoms, such as n-butylphenyl glycidyl ether, i-butylphenyl glycidyl ether, sec-butylphenyl glycidyl ether, tert-butylphenyl glycidyl ether, pentylphenyl glycidyl ether, hexylphenyl glycidyl ether, heptylphenyl glycidyl ether, octylphenyl glycidyl ether, nonylphenyl glycidyl ether, or decylphenyl glycidyl ether.


Specific examples of the alkyl glycidyl ether-type epoxy compound include decyl glycidyl ether, undecyl glycidyl ether, dodecyl glycidyl ether, tridecyl glycidyl ether, tetradecyl glycidyl ether, 2-ethylhexyl glycidyl ether, neopentyl glycol diglycidyl ether, trimethylolpropane triglycidyl ether, pentaerythritol tetraglycidyl ether, 1,6-hexanediol diglycidyl ether, sorbitol polyglycidyl ether, polyalkylene glycol monoglycidyl ether, and polyalkylene glycol diglycidyl ether.


Specific examples of the glycidyl ester-type epoxy compound include phenyl glycidyl ester, alkyl glycidyl esters, and alkenyl glycidyl esters. Preferred examples of the glycidyl ester-type epoxy compound include glycidyl-2,2-dimethyloctanoate, glycidyl benzoate, glycidyl acrylate, and glycidyl methacrylate.


Specific examples of the allyloxirane compound include, 1,2-epoxystyrene and alkyl-1,2-epoxystyrenes.


Specific examples of the alkyloxirane compound include 1,2-epoxybutane, 1,2-epoxypentane, 1,2-epoxyhexane, 1,2-epoxyheptane, 1,2-epoxyoctane, 1,2-epoxynonane, 1,2-epoxydecane, 1,2-epoxyundecane, 1,2-epoxydodecane, 1,2-epoxytridecane, 1,2-epoxytetradecane, 1,2-epoxypentadecane, 1,2-epoxyhexadecane, 1,2-epoxyheptadecane, 1,1,2-epoxyoctadecane, 2-epoxynonadecane, and 1,2-epoxyeicosane.


Specific examples of the alicyclic epoxy compound include 1,2-epoxycyclohexane, 1,2-epoxycyclopentane, 3,4-epoxycyclohexylmethyl-3,4-epoxycyclohexane carboxylate, bis(3,4-epoxycyclohexylmethyl) adipate, exo-2,3-epoxynorbornane, bis(3,4-epoxy-6-methylcyclohexylmethyl) adipate, 2-(7-oxabicyclo[4.1.0]hept-3-yl)-spiro(1,3-dioxane-5,3′-[7]oxabicyclo[4.1.0]heptane, 4-(1′-methylepoxyethyl)-1,2-epoxy-2-methylcyclohexane, and 4-epoxyethyl-1,2-epoxycyclohexane.


Specific examples of the epoxidized fatty acid monoester include esters of an epoxidized fatty acid having 12 to 20 carbon atoms and an alcohol having 1 to 8 carbon atoms, phenol, or an alkylphenol. In particular, butyl, hexyl, benzyl, cyclohexyl, methoxyethyl, octyl, phenyl, and butyl phenyl esters of epoxystearic acid are preferably used.


Specific examples of the epoxidized vegetable oil include epoxy compounds of vegetable oils such as soybean oil, linseed oil, and cottonseed oil.


Among these epoxy compounds, phenyl glycidyl ether-type epoxy compounds, alkyl glycidyl ether-type epoxy compounds, glycidyl ester-type epoxy compounds, and alicyclic epoxy compounds are preferred.


When the refrigerating oil and the working fluid for a refrigerating machine according to this embodiment contain the above-described epoxy compound, the content of the epoxy compound is not limited, but is preferably 0.01 to 5.0 mass % and more preferably 0.1 to 3.0 mass % relative to the whole amount of the refrigerating oil. The above-described epoxy compounds may be, used alone or in combination of two or more.


The kinematic viscosity of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) at 40° C. is preferably 20 to 80 mm2/s, more preferably 25 to 75 mm2/s, and most preferably 30 to 70 mm2/s. The kinematic viscosity at 100° C. is preferably 2 to 20 mm2/s and more preferably 3 to 10 mm2/s. When the kinematic viscosity is more than or equal to the lower limit, the viscosity required as a refrigerating oil is easily achieved. On the other hand, when the kinematic viscosity is less than or equal to the upper limit, sufficient miscibility with difluoromethane in the case where the difluoromethane is contained as a refrigerant composition can be achieved.


The volume resistivity of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) is not limited, but is preferably 1.0×1012 Ω·cm or more, more preferably 1.0×1013 Ω·cm or more, and most preferably 1.0×1014 Ω·cm or more. In particular, when the refrigerating oil is used for sealed refrigerating machines, high electric insulation tends to be required. The volume resistivity refers to a value measured at 25° C. in conformity with JIS C 2101 “Testing methods of electrical insulating oils”.


The water content of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) is not limited, but is preferably 200 ppm or less, more preferably 100 ppm or less, and most preferably 50 ppm or less relative to the whole amount of the refrigerating oil. In particular, when the refrigerating oil is used for sealed refrigerating machines, the water content needs to be low from the viewpoints of the thermal and chemical stability of the refrigerating oil and the influence on electric insulation.


The acid number of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) is not limited, but is preferably 0.1 mgKOH/g or less and more preferably 0.05 mgKOH/g or less to prevent corrosion of metals used for refrigerating machines or pipes. In the present invention, the acid number refers to an acid number measured in conformity with JIS K 2501 “Petroleum products and lubricants—Determination of neutralization number”.


The ash content of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) is not limited, but is preferably 100 ppm or less and more preferably 50 ppm or less to improve the thermal and chemical stability of the refrigerating oil and suppress the generation of sludge and the like. The ash content refers to an ash content measured in conformity with JIS K 2272 “Crude oil and petroleum products—Determination of ash and sulfated ash”.


(Complex Ester Oil)


The complex ester oil is an ester of a fatty acid and a dibasic acid, and a monohydric alcohol and a polyol. The above-described fatty acid, dibasic acid, monohydric alcohol, and polyol can be used.


Examples of the fatty acid include the fatty acids mentioned in the polyol ester.


Examples of the dibasic acid include oxalic acid, malonic acid, succinic acid, glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, sebacic acid, phthalic acid, isophthalic acid, and terephthalic acid.


Examples of the polyol include the polyhydric alcohols in the polyol ester. The complex ester is an ester of such a fatty acid, dibasic acid, and polyol, each of which may be constituted by a single component or a plurality of components.


(Polyol Carbonate Oil)


The polyol carbonate oil is an ester of a carbonic acid and a polyol.


Examples of the polyol include the above-described diols and polyols.


The polyol carbonate oil may be a ring-opened polymer of a cyclic alkylene carbonate.

    • (2-1-2) Ether-Based Refrigerating Machine Oil


      (2-1-2) Ether-Type Refrigerating Oil


The ether-type refrigerating oil is, for example, a polyvinyl ether oil or a polyoxyalkylene oil.


(Polyvinyl Ether Oil)


Examples of the polyvinyl ether oil include polymers of a vinyl ether monomer, copolymers of a vinyl ether monomer and a hydrocarbon monomer having an olefinic double bond, and copolymers of a monomer having an olefinic double bond and a polyoxyalkylene chain and a vinyl ether monomer.


The carbon/oxygen molar ratio of the polyvinyl ether oil is preferably 2 or more and 7.5 or less and more preferably 2.5 or more and 5.8 or less. If the carbon/oxygen molar ratio is smaller than the above range, the hygroscopicity increases. If the carbon/oxygen molar ratio is larger than the above range, the miscibility deteriorates. The weight-average molecular weight of the polyvinyl ether is preferably 200 or more and 3000 or less and more preferably 500 or more and 1500 or less.


The pour point of the polyvinyl ether oil is preferably −30° C. or lower. The surface tension of the polyvinyl ether oil at 20° C. is preferably 0.02 N/m or more and 0.04 N/m or less. The density of the polyvinyl ether oil at 15° C. is preferably 0.8 g/cm3 or more and 1.8 g/cm3 or less. The saturated water content of the polyvinyl ether oil at a temperature of 30° C. and a relative humidity of 90% is preferably 2000 ppm or more.


The refrigerating oil may contain polyvinyl ether as a main component. In the case where HFO-1234yf is contained as a refrigerant, the polyvinyl ether serving as a main component of the refrigerating oil has miscibility with HFO-1234yf. When the refrigerating oil has a kinematic viscosity at 40° C. of 400 mm2/s or less, HFO-1234yf is dissolved in the refrigerating oil to some extent. When the refrigerating oil has a pour point of −30° C. or lower, the flowability of the refrigerating oil is easily ensured even at positions at which the temperature of the refrigerant composition and the refrigerating oil is low in the refrigerant circuit. When the refrigerating oil has a surface tension at 20° C. of 0.04 N/m or less, the refrigerating oil discharged from a compressor does not readily form large droplets of oil that are not easily carried away by a refrigerant composition. Therefore, the refrigerating oil discharged from the compressor is dissolved in HFO-1234yf and is easily returned to the compressor together with HFO-1234yf.


When the refrigerating oil has a kinematic viscosity at 40° C. of 30 mm2/s or more, an insufficient oil film strength due to excessively low kinematic viscosity is suppressed, and thus good lubricity is easily achieved. When the refrigerating oil has a surface tension at 20° C. of 0.02 N/m or more, the refrigerating oil does not readily form small droplets of oil in a gas refrigerant inside the compressor, which can suppress discharge of a large amount of refrigerating oil from the compressor. Therefore, a sufficient amount of refrigerating oil is easily stored in the compressor.


When the refrigerating oil has a saturated water content at 30° C./90% RH of 2000 ppm or more, a relatively high hygroscopicity of the refrigerating oil can be achieved. Thus, when HFO-1234yf is contained as a refrigerant, water in HFO-1234yf can be captured by the refrigerating oil to some extent. HFO-1234yf has a molecular structure that is easily altered or deteriorated because of the influence of water contained. Therefore, the hydroscopic effects of the refrigerating oil can suppress such deterioration.


Furthermore, when a particular resin functional component is disposed in the sealing portion or sliding portion that is in contact with a refrigerant flowing through the refrigerant circuit and the resin functional component is formed of any of polytetrafluoroethylene, polyphenylene sulfide, phenolic resin, polyamide resin, chloroprene rubber, silicon rubber, hydrogenated nitrile rubber, fluororubber, and hydrin rubber, the aniline point of the refrigerating oil is preferably set within a particular range in, consideration of the adaptability with the resin functional component. By setting the aniline point in such a manner, for example, the adaptability of bearings constituting the resin functional component with the refrigerating oil is improved. Specifically, if the aniline point is excessively low, the refrigerating oil readily infiltrates bearings or the like, and the bearings or the like readily swell. On the other hand, if the aniline point is excessively high, the refrigerating oil does not readily infiltrate bearings or the like, and the bearings or the like readily shrink. Therefore, by setting the aniline point of the refrigerating oil within a particular range, the swelling or shrinking of the bearings or the like can be prevented. Herein, for example, if each of the bearings or the like deforms through swelling or shrinking, the desired length of a gap at a sliding portion cannot be maintained. This may increase the sliding resistance or decrease the rigidity of the sliding portion. However, when the aniline point of the refrigerating oil is set within a particular range as described above, the deformation of the bearings or the like through swelling or shrinking is suppressed, and thus such a problem can be avoided.


The vinyl ether monomers may be used alone or in combination of two or more. Examples of the hydrocarbon monomer having an olefinic double bond include ethylene, propylene, various butenes, various pentenes, various hexenes, various heptenes, various octenes, diisobutylene, triisobutylene, styrene, α-methylstyrene, and various alkyl-substituted styrenes. The hydrocarbon monomers having an olefinic double bond may be used alone or in combination of two or more.


The polyvinyl ether copolymer may be a block copolymer or a random copolymer. The polyvinyl ether oils may be used alone or in combination of two or more.


A polyvinyl ether oil preferably used has a structural unit represented by general formula (1) below.




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(In the formula, R1, R2, and R3 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 8 carbon atoms, R4 represents a divalent hydrocarbon group having 1 to 10 carbon atoms or an ether bond oxygen-containing divalent hydrocarbon group having 2 to 20 carbon atoms, R5 represents a hydrocarbon group having 1 to 20 carbon atoms, m represents a number at which the average of m in the polyvinyl ether is 0 to 10, R1 to R5 may be the same or different in each of structural units, and when m represents 2 or more in one structural unit, a plurality of R4O may be the same or different.)


At least one of R1, R2, and R3 in the general formula (1) preferably represents a hydrogen atom. In particular, all of R1, R2, and R3 preferably represent a hydrogen atom. In the general formula (1), m preferably represents 0 or more and 10 or less, particularly preferably 0 or more and 5 or less, further preferably 0. R5 in the general formula (1) represents a hydrocarbon group having 1 to 20 carbon atoms. Specific examples of the hydrocarbon group include alkyl groups such as a methyl group, an ethyl group, a n-propyl group, an isopropyl group, a n-butyl group, an isobutyl group, a sec-butyl group, a tert-butyl group, various pentyl groups, various hexyl groups, various heptyl groups, and various octyl groups; cycloalkyl groups such as a cyclopentyl group, a cyclohexyl group, various methylcyclohexyl groups, various ethylcyclohexyl groups, and various dimethylcyclohexyl groups; aryl groups such as a phenyl group, various methylphenyl groups, various ethylphenyl groups, and various dimethylphenyl groups; and arylalkyl groups such as a benzyl group, various phenylethyl groups, and various methylbenzyl groups. Among the alkyl groups, the cycloalkyl groups, the phenyl group, the aryl groups, and the arylalkyl groups, alkyl groups, in particular, alkyl groups having 1 to 5 carbon atoms are preferred. For the polyvinyl ether oil contained, the ratio of a polyvinyl ether oil with R5 representing an alkyl group having 1 or 2 carbon atoms and a polyvinyl ether oil with R5 representing an alkyl group having 3 or 4 carbon atoms is preferably 40%:60% to 100%:0%.


The polyvinyl ether oil according to this embodiment may be a homopolymer constituted by the same structural unit represented by the general formula (1) or a copolymer constituted by two or more structural units. The copolymer may be a block copolymer or a random copolymer.


The polyvinyl ether oil according to this embodiment may constituted by only the structural unit represented by the general formula (1) or may be a copolymer further including a structural unit represented by general formula (2) below. In this case, the copolymer may be a block copolymer or a random copolymer.




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(In the formula, R6 to R9 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 20 carbon atoms.)


The vinyl ether monomer is, for example, a compound represented by general formula (3) below.




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(In the formula, R1, R2, R3, R4, R5, and m have the same meaning as R1, R2, R3, R4, R5, and m in the general formula (1), respectively.)


Examples of various polyvinyl ether compounds corresponding to the above polyvinyl ether compound include vinyl methyl ether; vinyl ethyl ether; vinyl-n-propyl ether; vinyl-isopropyl ether; vinyl-n-butyl ether; vinyl-isobutyl ether; vinyl-sec-butyl ether; vinyl-tert-butyl ether; vinyl-n-pentyl ether; vinyl-n-hexyl ether; vinyl-2-methoxyethyl ether; vinyl-2-ethoxyethyl ether; vinyl-2-methoxy-1-methylethyl ether; vinyl-2-methoxy-propyl ether; vinyl-3,6-dioxaheptyl ether; vinyl-3,6,9-trioxadecyl ether; vinyl-1,4-dimethyl-3,6-dioxaheptyl ether; vinyl-1,4,7-trimethyl-3,6,9-trioxadecyl ether; vinyl-2,6-dioxa-4-heptyl ether; vinyl-2,6,9-trioxa-4-decyl ether; 1-methoxypropene; 1-ethoxypropene; 1-n-propoxypropene; 1-isopropoxypropene; 1-n-butoxypropene; 1-isobutoxypropene; 1-sec-butoxypropene; 1-tert-butoxypropene; 2-methoxypropene; 2-ethoxypropene; 2-n-propoxypropene; 2-isopropoxypropene; 2-n-butoxypropene; 2-isobutoxypropene; 2-sec-butoxypropene; 2-tert-butoxypropene; 1-methoxy-1-butene; 1-ethoxy-1-butene; 1-n-propoxy-1-butene; 1-isopropoxy-1-butene; 1-n-butoxy-1-butene; 1-isobutoxy-1-butene; 1-sec-butoxy-1-butene; 1-tert-butoxy-1-butene; 2-methoxy-1-butene; 2-ethoxy-1-butene; 2-n-propoxy-1-butene; 2-isopropoxy-1-butene; 2-n-butoxy-1-butene; 2-isobutoxy-1-butene; 2-sec-butoxy-1-butene; 2-tert-butoxy-1-butene; 2-methoxy-2-butene; 2-ethoxy-2-butene; 2-n-propoxy-2-butene; 2-isopropoxy-2-butene; 2-n-butoxy-2-butene; 2-isobutoxy-2-butene; 2-sec-butoxy-2-butene; and 2-tert-butoxy-2-butene. These vinyl ether monomers can be produced by a publicly known method.


The end of the polyvinyl ether compound having the structural unit represented by the general formula (1) can be converted into a desired structure by a method described in the present disclosure and a publicly known method. Examples of the group introduced by conversion include saturated hydrocarbons, ethers, alcohols, ketones, amides, and nitriles.


The polyvinyl ether compound preferably has the following end structures.




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(In the formula, R11, R21, and R31 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 8 carbon atoms, R41 represents a divalent hydrocarbon group having 1 to 10 carbon atoms or an ether bond oxygen-containing divalent hydrocarbon group having 2 to 20 carbon atoms, R51 represents a hydrocarbon group having 1 to 20 carbon atoms, m represents a number at which the average of m in the polyvinyl ether is 0 to 10, and when m represents 2 or more, a plurality of R41O may the same or different.)




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(In the formula, R61, R71, R81, and R91 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 20 carbon atoms.)




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(In the formula, R12, R22, and R32 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 8 carbon atoms, R42 represents a divalent hydrocarbon group having 1 to 10 carbon atoms or an ether bond oxygen-containing divalent hydrocarbon group having 2 to 20 carbon atoms, R52 represents a hydrocarbon group having 1 to 20 carbon atoms, m represents a number at which the average of m in the polyvinyl ether is 0 to 10, and when m represents 2 or more, a plurality of R42O may be the same or different.)




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(In the formula, R62, R72, R82, and R92 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 20 carbon atoms.)




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(In the formula, R13, R23, and R33 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 8 carbon atoms.)


The polyvinyl ether oil according to this embodiment can be produced by polymerizing the above-described monomer through, for example, radical polymerization, cationic polymerization, or radiation-induced polymerization. After completion of the polymerization reaction, a typical separation/purification method is performed when necessary to obtain a desired polyvinyl ether compound having a structural unit represented by the general formula (1).


(Polyoxyalkylene Oil)


The polyoxyalkylene oil is a polyoxyalkylene compound obtained by, for example, polymerizing an alkylene oxide having 2 to 4 carbon atoms (e.g., ethylene oxide or propylene oxide) using water or a hydroxyl group-containing compound as an initiator. The hydroxyl group of the polyoxyalkylene compound may be etherified or esterified. The polyoxyalkylene oil may contain an oxyalkylene unit of the same type or two or more oxyalkylene units in one molecule. The polyoxyalkylene oil preferably contains at least an oxypropylene unit in one molecule.


Specifically, the polyoxyalkylene oil is, for example, a compound represented by general formula (9) below.

R101[(R102)k—OR103]l  (9)

(In the formula, R101 represents a hydrogen atom, an alkyl group having 1 to 10 carbon atoms, an acyl group having 2 to 10 carbon atoms, or an aliphatic hydrocarbon group having 2 to 6 bonding sites and 1 to 10 carbon atoms, R102 represents an alkylene group having 2 to 4 carbon atoms, R103 represents a hydrogen atom, an alkyl group having 1 to 10 carbon atoms, or an acyl group having 2 to 10 carbon atoms, 1 represents an integer of 1 to 6, and k represents a number at which the average of k×1 is 6 to 80.)


In the general formula (9), the alkyl group represented by R101 and R103 may be a linear, branched, or cyclic alkyl group. Specific examples of the alkyl group include a methyl group, an ethyl group, a n-propyl group, an isopropyl group, various butyl groups, various pentyl groups, various hexyl groups, various heptyl groups, various octyl groups, various nonyl groups, various decyl groups, a cyclopentyl group, and a cyclohexyl group. If the number of carbon atoms of the alkyl group exceeds 10, the miscibility with a refrigerant 2 Deteriorates, which may cause phase separation. The number of carbon atoms of the alkyl group is preferably 1 to 6.


The acyl group represented by R101 and R103 may have a linear, branched, or cyclic alkyl group moiety. Specific examples of the alkyl group moiety of the acyl group include various groups having 1 to 9 carbon atoms that are mentioned as specific examples of the alkyl group. If the number of carbon atoms of the acyl group exceeds 10, the miscibility with a refrigerant 2 Deteriorates, which may cause phase separation. The number of carbon atoms of the acyl group is preferably 2 to 6.


When R101 and R103 each represent an alkyl group or an acyl group, R101 and R103 may be the same or different.


Furthermore, when 1 represents 2 or more, a plurality of R103 in one molecule may be the same or different.


When R101 represents an aliphatic hydrocarbon group having 2 to 6 bonding sites and 1 to 10 carbon atoms, the aliphatic hydrocarbon group may be a linear group or a cyclic group. Examples of the aliphatic hydrocarbon group having two bonding sites include an ethylene group, a propylene group, a butylene group, a pentylene group, a hexylene group, a heptylene group, an octylene group, a nonylene group, a decylene group, a cyclopentylene group, and a cyclohexylene group. Examples of the aliphatic hydrocarbon group having 3 to 6 bonding sites include residual groups obtained by removing hydroxyl groups from polyhydric alcohols such as trimethylolpropane, glycerol, pentaerythritol, sorbitol, 1,2,3-trihydroxycyclohexane, and 1,3,5-trihydroxycyclohexane.


If the number of carbon atoms of the aliphatic hydrocarbon group exceeds 10, the miscibility with a refrigerant 2 Deteriorates, which may cause phase separation. The number of carbon atoms is preferably 2 to 6.


R102 in the general formula (9) represents an alkylene group having 2 to 4 carbon atoms. Examples of the oxyalkylene group serving as a repeating unit include an oxyethylene group, an oxypropylene group, and an oxybutylene group. The polyoxyalkylene oil may contain an oxyalkylene group of the same type or two or more oxyalkylene groups in one molecule, but preferably contains at least an oxypropylene unit in one molecule. In particular, the content of the oxypropylene unit in the oxyalkylene unit is suitably 50 mol % or more.


In the general formula (9), 1 represents an integer of 1 to 6, which can be determined in accordance with the number of bonding sites of R101. For example, when R101 represents an alkyl group or an acyl group, 1 represents 1. When R101 represents an aliphatic hydrocarbon group having 2, 3, 4, 5, and 6 bonding sites, 1 represents 2, 3, 4, 5, and 6, respectively. Preferably, 1 represents 1 or 2. Furthermore, k preferably represents a number at which the average of k×1 is 6 to 80.


For the structure of the polyoxyalkylene oil, a polyoxypropylene diol dimethyl ether represented by general formula (10) below and a poly(oxyethylene/oxypropylene) diol dimethyl ether represented by general formula (11) below are suitable from the viewpoints of economy and the above-described effects. Furthermore, a polyoxypropylene diol monobutyl ether represented by general formula (12) below, a polyoxypropylene diol monomethyl ether represented by general formula (13) below, a poly(oxyethylene/oxypropylene) diol monomethyl ether represented by general formula (14) below, a poly(oxyethylene/oxypropylene) diol monobutyl ether represented by general formula (15) below, and a polyoxypropylene diol diacetate represented by general formula (16) below are suitable from the viewpoint of economy and the like.

CH3O—(C3H6O)h—CH3  (10)

(In the formula, h represents 6 to 80.)

CH3O—(C2H4O)i—(C3H6O)j—CH3  (11)

(In the formula, i and j each represent 1 or more and the sum of i and j is 6 to 80.)

C4H9O—(C3H6O)h—H  (12)

(In the formula, h represents 6 to 80.)

CH3O—(C3H6O)h—H  (13)

(In the formula, h represents 6 to 80.)

CH3O—(C2H4O)i—(C3H6O)j—H  (14)

(In the formula, i and j each represent 1 or more and the sum of i and j is 6 to 80.)

C4H9O—(C2H4O)i—(C3H6O)j—H  (15)

(In the formula, i and j each represent 1 or more and the sum of i and j is 6 to 80.)

CH3COO—(C3H6O)h—COCH3  (16)

(In the formula, h represents 6 to 80.)


The polyoxyalkylene oils may be used alone or in combination of two or more.


(2-2) Hydrocarbon-Based Refrigerating Machine Oil


(2-2) Hydrocarbon Refrigerating Oil


The hydrocarbon refrigerating oil that can be used is, for example, an alkylbenzene.


The alkylbenzene that can be used is a branched alkylbenzene synthesized from propylene polymer and benzene serving as raw materials using a catalyst such as hydrogen fluoride or a linear alkylbenzene synthesized from normal paraffin and benzene serving as raw materials using the same catalyst. The number of carbon atoms of the alkyl group is preferably 1 to 30 and more preferably 4 to 20 from the viewpoint of achieving a viscosity appropriate as a lubricating base oil. The number of alkyl groups in one molecule of the alkylbenzene is dependent on the number of carbon atoms of the alkyl group, but is preferably 1 to 4 and more preferably 1 to 3 to control the viscosity within the predetermined range.


The hydrocarbon refrigerating oil preferably circulates through a refrigeration cycle system together with a refrigerant. Although it is most preferable that the refrigerating oil is soluble with a refrigerant, for example, a refrigerating oil (e.g., a refrigerating oil disclosed in Japanese Patent No. 2803451) having low solubility can also be used as long as the refrigerating oil is capable of circulating through a refrigeration cycle system together with a refrigerant. To allow the refrigerating oil to circulate through a refrigeration cycle system, the refrigerating oil is required to have a low kinematic viscosity. The kinematic viscosity of the hydrocarbon refrigerating oil at 40° C. is preferably 1 mm2/s or more and 50 mmz/s or less and more preferably 1 mm2/s or more and 25 mm2/s or less.


These refrigerating oils may be used alone or in combination of two or more.


The content of the hydrocarbon refrigerating oil in the working fluid for a refrigerating machine may be, for example, 10 parts by mass or more and 100 parts by mass or less and is more preferably 20 parts by mass or more and 50 parts by mass or less relative to 100 parts by mass of the refrigerant composition.


(2-3) Additives


(2-3) Additive


The refrigerating oil may contain one or two or more additives.


Examples of the additives include an acid scavenger, an extreme pressure agent, an antioxidant, an antifoaming agent, an oiliness improver, a metal deactivator such as a copper deactivator, an anti-wear agent, and a compatibilizer.


Examples of the acid scavenger that can be used include epoxy compounds such as phenyl glycidyl ether, alkyl glycidyl ether, alkylene glycol glycidyl ether, cyclohexene oxide, α-olefin oxide, and epoxidized soybean oil; and carbodiimides. Among them, phenyl glycidyl ether, alkyl glycidyl ether, alkylene glycol glycidyl ether, cyclohexene oxide, and α-olefin oxide are preferred from the viewpoint of miscibility. The alkyl group of the alkyl glycidyl ether and the alkylene group of the alkylene glycol glycidyl ether may have a branched structure. The number of carbon atoms may be 3 or more and 30 or less, and is more preferably 4 or more and 24 or less and further preferably 6 or more and 16 or less. The total number of carbon atoms of the α-olefin oxide may be 4 or more and 50 or less, and is more preferably 4 or more and 24 or less and further preferably 6 or more and 16 or less. The acid scavengers may be used alone or in combination of two or more.


The extreme pressure agent may contain, for example, a phosphoric acid ester. Examples of the phosphoric acid ester that can be used include phosphoric acid esters, phosphorous acid esters, acidic phosphoric acid esters, and acidic phosphorous acid esters. The extreme pressure agent may contain an amine salt of a phosphoric acid ester, a phosphorous acid ester, an acidic phosphoric acid ester, or an acidic phosphorous acid ester.


Examples of the phosphoric acid ester include triaryl phosphates, trialkyl phosphates, trialkylaryl phosphates, triarylalkyl phosphates, and trialkenyl phosphates. Specific examples of the phosphoric acid ester include triphenyl phosphate, tricresyl phosphate, benzyl diphenyl phosphate, ethyl diphenyl phosphate, tributyl phosphate, ethyl dibutyl phosphate, cresyl diphenyl phosphate, dicresyl phenyl phosphate, ethylphenyl diphenyl phosphate, diethylphenyl phenyl phosphate, propylphenyl diphenyl phosphate, dipropylphenyl phenyl phosphate, triethylphenyl phosphate, tripropylphenyl phosphate, butylphenyl diphenyl phosphate, dibutylphenyl phenyl phosphate, tributylphenyl phosphate, trihexyl phosphate, tri(2-ethylhexyl) phosphate, tridecyl phosphate, trilauryl phosphate, trimyristyl phosphate, tripalmityl phosphate, tristearyl phosphate, and trioleyl phosphate.


Specific examples of the phosphorous acid ester include triethyl phosphite, tributyl phosphite, triphenyl phosphite, tricresyl phosphite, tri(nonylphenyl) phosphite, tri(2-ethylhexyl) phosphite, tridecyl phosphite, trilauryl phosphite, triisooctyl phosphite, diphenylisodecyl phosphite, tristearyl phosphite, and trioleyl phosphite.


Specific examples of the acidic phosphoric acid ester include 2-ethylhexyl acid phosphate, ethyl acid phosphate, butyl acid phosphate, oleyl acid phosphate, tetracosyl acid phosphate, isodecyl acid phosphate, lauryl acid phosphate, tridecyl acid phosphate, stearyl acid phosphate, and isostearyl acid phosphate.


Specific examples of the acidic phosphorous acid ester include dibutyl hydrogen phosphite, dilauryl hydrogen phosphite, dioleyl hydrogen phosphite, distearyl hydrogen phosphite, and diphenyl hydrogen phosphite. Among the phosphoric acid esters, oleyl acid phosphate and stearyl acid phosphate are suitably used.


Among amines used for amine salts of phosphoric acid esters, phosphorous acid esters, acidic phosphoric acid esters, or acidic phosphorous acid esters, specific examples of mono-substituted amines include butylamine, pentylamine, hexylamine, cyclohexylamine, octylamine, laurylamine, stearylamine, oleylamine, and benzylamine. Specific examples of di-substituted amines include dibutylamine, dipentylamine, dihexylamine, dicyclohexylamine, dioctylamine, dilaurylamine, distearylamine, dioleylamine, dibenzylamine, stearyl·monoethanolamine, decyl·monoethanolamine, hexyl·monopropanolamine, benzyl·monoethanolamine, phenyl·monoethanolamine, and tolyl·monopropanolamine. Specific examples of tri-substituted amines include tributylamine, tripentylamine, trihexylamine, tricyclohexylamine, trioctylamine, trilaurylamine, tristearylamine, trioleylamine, tribenzylamine, dioleyl·monoethanolamine, dilauryl·monopropanolamine, dioctyl·monoethanolamine, dihexyl·monopropanolamine, dibutyl·monopropanolamine, oleyldiethanolamine, stearyl·dipropanolamine, lauryl·diethanolamine, octyl·dipropanolamine, butyl·diethanolamine, benzyl·diethanolamine, phenyl·diethanolamine, tolyl·dipropanolamine, xylyl diethanolamine, triethanolamine, and tripropanolamine.


Examples of extreme pressure agents other than the above-described extreme pressure agents include extreme pressure agents based on organosulfur compounds such as monosulfides, polysulfides, sulfoxides, sulfones, thiosulfinates, sulfurized fats and oils, thiocarbonates, thiophenes, thiazoles, and methanesulfonates; extreme pressure agents based on thiophosphoric acid esters such as thiophosphoric acid triesters; extreme pressure agents based on esters such as higher fatty acids, hydroxyaryl fatty acids, polyhydric alcohol esters, and acrylic acid esters; extreme pressure agents based on organochlorine compounds such as chlorinated hydrocarbons, e.g., chlorinated paraffin and chlorinated carboxylic acid derivatives; extreme pressure agents based on fluoroorganic compounds such as fluorinated aliphatic carboxylic acids, fluorinated ethylene resins, fluorinated alkylpolysiloxanes, and fluorinated graphites; extreme pressure agents based on alcohols such as higher alcohols; and extreme pressure agents based on metal compounds such as naphthenic acid salts (e.g., lead naphthenate), fatty acid salts (e.g., lead fatty acid), thiophosphoric acid salts (e.g., zinc dialkyldithiophosphate), thiocarbamic acid salts, organomolybdenum compounds, organotin compounds, organogermanium compounds, and boric acid esters.


The antioxidant that can be used is, for example, a phenol-based antioxidant or an amine-based antioxidant. Examples of the phenol-based antioxidant include 2,6-di-tert-butyl-4-methylphenol (DBPC), 2,6-di-tert-butyl-4-ethylphenol, 2,2′-methylenebis(4-methyl-6-tert-butylphenol), 2,4-dimethyl-6-tert-butylphenol, 2,6-di-tert-butylphenol, di-tert-butyl-p-cresol, and bisphenol A. Examples of the amine-based antioxidant include N,N′-diisopropyl-p-phenylenediamine, N,N′-di-sec-butyl-p-phenylenediamine, phenyl-α-naphthylamine, N,N′-di-phenyl-p-phenylenediamine, and N,N-di(2-naphthyl)-p-phenylenediamine. An oxygen scavenger that captures oxygen can also be used as the antioxidant.


The antifoaming agent that can be used is, for example, a silicon compound.


The oiliness improver that can be used is, for example, a higher alcohol or a fatty acid.


The metal deactivator such as a copper deactivator that can be used is, for example, benzotriazole or a derivative thereof.


The anti-wear agent that can be used is, for example, zinc dithiophosphate.


The compatibilizer is not limited, and can be appropriately selected from commonly used compatibilizers. The compatibilizers may be used alone or in combination of two or more. Examples of the compatibilizer include polyoxyalkylene glycol ethers, amides, nitriles, ketones, chlorocarbons, esters, lactones, aryl ethers, fluoroethers, and 1,1,1-trifluoroalkanes. The compatibilizer is particularly preferably a polyoxyalkylene glycol ether.


The refrigerating oil may optionally contain, for example, a load-bearing additive, a chlorine scavenger, a detergent dispersant, a viscosity index improver, a heat resistance improver, a stabilizer, a corrosion inhibitor, a pour-point depressant, and an anticorrosive.


The content of each additive in the refrigerating oil may be 0.01 mass % or more and 5 mass % or less and is preferably 0.05 mass % or more and 3 mass % or less. The content of the additive in the working fluid for a refrigerating machine constituted by the refrigerant composition and the refrigerating oil is preferably 5 mass % or less and more preferably 3 mass % or less.


The refrigerating oil preferably has a chlorine concentration of 50 ppm or less and preferably has a sulfur concentration of 50 ppm or less.


(3) First Embodiment of Refrigeration Cycle Device for Vehicle

An air conditioner for a vehicle using any one of the refrigerant 1A, the refrigerant 1B, the refrigerant 1C, the refrigerant 1D, the refrigerant 1E, the refrigerant 2A, the refrigerant 2B, the refrigerant 2C, the refrigerant 2D, the refrigerant 2E, the refrigerant 3A, and the refrigerant 3B, and the refrigerating machine oil above is described below. The air conditioner for a vehicle is a refrigeration cycle device for a vehicle.


(3-1) Configuration of Air Conditioner 1 for Vehicle



FIG. 3 is a schematic view of a configuration of the air conditioner 1 for a vehicle according to a first embodiment of the present disclosure. In FIG. 3, the air conditioner 1 for a vehicle is a vapor-compression refrigeration cycle device for a vehicle. The “refrigeration cycle device for a vehicle” is one type of refrigeration cycle device that is used in a vehicle, such as a gasoline vehicle, a hybrid vehicle, an electric vehicle, or a hydrogen vehicle.


The air conditioner 1 for a vehicle includes a refrigerant circuit 10, an air-conditioning unit 30, and a controlling device 60, which is controlling means.


The refrigerant circuit 10 is a vapor-compression refrigerant circuit that adjusts the temperature of blowing air that is blown into the interior of a vehicle.


The air-conditioning unit 30 blows the blowing air whose temperature has been adjusted by the refrigerant circuit 10 into the interior of a vehicle. The controlling device 60 controls the operation of various structural units of the air conditioner 1 for a vehicle.


The refrigerant circuit 10 is capable of being switched between a refrigerant circuit for a cooling mode (a cooling operation), in which the interior of the vehicle is cooled by cooling the blowing air, and a refrigerant circuit for a heating mode (a heating operation), in which the interior of the vehicle is heated by heating the blowing air.


(3-2) Refrigerant Circuit 10



FIG. 4 is a schematic view of the configuration of the air conditioner 1 for a vehicle, and illustrates a circulation path of a refrigerant in the heating mode. In FIG. 4, a portion in which the refrigerant in the heating mode circulates is indicated by a solid line, and a portion in which the circulation of the refrigerant is stopped is indicated by a broken line.



FIG. 5 is a schematic view of the configuration of the air conditioner 1 for a vehicle, and illustrates a circulation path of a refrigerant in the cooling mode. A portion in which the refrigerant in the cooling mode circulates is indicated by a solid line, and a portion in which the circulation of the refrigerant is stopped is indicated by a broken line.


The refrigerant circuit 10 includes, for example, a compressor 80, a first heat exchanger 85, an outside-air heat exchanger 82, a second heat exchanger 86, an accumulator 80a, a heating control valve 83, a cooling control valve 87, an, electromagnetic valve 23, and a check valve 24.


The compressor 80 compresses and discharges a sucked-in refrigerant. The first heat exchanger 85 is a heat exchanger that heats blowing air. The second heat exchanger 86 is a heat exchanger that cools the blowing air. The heating control valve 83 and the cooling control valve 87 constitute a decompressing device that decompresses and expands the refrigerant. The electromagnetic valve 23 is refrigerant-circuit switching means that switches the refrigerant circuit between the refrigerant circuit in the cooling mode and the refrigerant circuit in the heating mode.


(3-2-1) Compressor 80


In the compressor 80, a compression mechanism is driven by a motor. As the motor, for example, an alternating current motor whose number of rotations is controlled by using an alternating voltage that is output from an inverter is used.


The inverter outputs an alternating voltage having a frequency that is in accordance with a control signal that is output from the controlling device 60. A refrigerant 2 Discharge capacity of the compressor 80 is changed by using the number-of-rotations control output. As the compressor 80, various compressors, such as a swash-plate compressor, a scroll compressor, a multi-vane compressor, and a rotary compressor, can be used.


(3-2-2) Outside-Air Heat, Exchanger 82


The outside-air heat exchanger 82 causes a refrigerant that circulates therein and vehicle outdoor air blown from an outdoor fan 90 to exchange heat with each other. The outside-air heat exchanger 82 functions as an evaporator at the time of the heating mode. The outside-air heat exchanger 82 also functions as a heat dissipater at the time of the cooling mode. The number of rotations of the outdoor fan 90 is controlled by using a control voltage that is output from the controlling device 60.


(3-2-3) Heating Control Valve 83


The heating control valve 83 that decompresses a refrigerant at the time of the heating mode is connected to a location between a refrigerant outlet of the first heat exchanger 85 and a refrigerant inlet of the outside-air heat exchanger 82. Although the heating control valve 83 is, for example, an electrically powered expansion valve, the heating control valve 83 is not limited thereto.


(3-2-4) First Heat Exchanger 85


A discharge port of the compressor 80 and a refrigerant inlet of the first heat exchanger 85 are connected to each other by a discharge pipe. The first heat exchanger 85 is disposed in an air-conditioning duct 31 that forms an air passage for blowing air that; is blown into the interior of a vehicle in the air-conditioning unit 30.


The first heat exchanger 85 heats the blowing air by causing a refrigerant that circulates therein and the blowing air to exchange heat with each other.


(3-2-5) Second Heat Exchanger 86


The second heat exchanger 86 is a cooling heat exchanger that is disposed on an upstream side of the flow of the blowing air at the first heat exchanger 85 in the air-conditioning duct 31 and that cools the blowing air by causing a refrigerant that circulates therein and the blowing air to exchange heat with each other. A refrigerant outlet of the second heat exchanger 86 and an inlet of the accumulator 80a are connected to each other by a pipe. The accumulator 80a is a gas-liquid separator that separates a gas-liquid of a refrigerant that has flowed therein and that accumulates an excessive refrigerant in a cycle. Further, a gas-phase refrigerant outlet of the accumulator 80a and an intake port of the compressor 80 are connected to each other by an intake pipe.


(3-2-6) Cooling Control Valve 87


The cooling control valve 87 that decompresses a refrigerant at the time of the cooling mode is connected to a location between a refrigerant outlet of the outside-air heat exchanger 82 and a refrigerant inlet of the second heat exchanger 86.


The cooling control valve 87 is, for example, an electrically powered expansion valve. However, as long as the cooling control valve 87 is capable of performing its function of decompressing the refrigerant at the time of the cooling mode, the cooling control valve 87 is not limited thereto. For the cooling control valve 87, a fixed aperture, such as an orifice or a capillary tube, can be used.


(3-2-7) Bypass 22


A bypass 22 that bypasses the check valve 24, the cooling control valve 87, and the second heat exchanger 86 is provided between the refrigerant outlet of the outside-air heat exchanger 82 and the refrigerant outlet of the second heat exchanger 86. The electromagnetic valve 23 is provided in the bypass 22.


(3-2-8) Electromagnetic Valve 23


The electromagnetic valve 23 is an on/off valve. The electromagnetic valve 23 is refrigerant-circuit switching means that switches the refrigerant circuit between the refrigerant circuit in the cooling mode and the refrigerant circuit in the heating mode. The operation of the electromagnetic valve 23 is controlled by using a control signal that is output from the controlling device 60. The electromagnetic valve 23 is closed at the time of the cooling mode and is open at the time of the heating mode.


(3-2-9) Check Valve 24


The check valve 24 is provided in a refrigerant passage that connects the refrigerant outlet of the outside-air heat exchanger 82 and the refrigerant inlet of the second heat exchanger 86. The check valve 24 allows a refrigerant to circulate into the refrigerant inlet of the second heat exchanger 86 from the refrigerant outlet of the outside-air heat exchanger 82, and does not allow the refrigerant to circulate in the opposite direction.


(3-3) Air-Conditioning Unit 30


The air-conditioning unit 30 is disposed on an inner side of an instrument panel at a front portion in the interior of a vehicle. The air-conditioning unit 30 accommodates such as a fan 32, the second heat exchanger 86, the first heat exchanger 85, and an air mix door 34 in the air-conditioning duct 31 that forms the outer shell of the air-conditioning unit 30.


(3-3-1) Air-Conditioning Duct 31


The air-conditioning duct 31 is molded out of a resin (such as polypropylene) having some elasticity and having excellent strength. An air passage for blowing air that is blown into the interior of a vehicle is formed in the air-conditioning duct 31. An air take-in mechanism 33 that introduces air in the interior of the vehicle (inside air) or outside air into a case by switching between the inside air and the outside air is disposed on an uppermost stream side of the flow of the blowing air of the air-conditioning duct 31.


(3-3-2) Air Take-in Mechanism 33


The air take-in mechanism 33 has an inside-air take-in port 33a that takes in the inside air and an outside-air take-in port 33b that takes in the outside air. The inside-air take-in port 33a is opened and closed by an inside-air door 43a. The outside-air take-in port 33b is opened and closed by an outside-air door 43b. For example, when the inside-air door 43a and the outside-air door 43b are driven by a motor, the opening degree of the inside-air door 43a and the opening degree of the outside-air door 43b are adjusted by controlling the rotation amount of the motor by the controlling device 60. As a result, the ratio between the flow rates of the inside air and the outside air that flow into the air-conditioning duct 31 is adjusted.


The fan 32 that blows air sucked in via the air take-in mechanism 33 toward the interior of a vehicle is disposed on a downstream side of the flow of air of the air take-in mechanism 33. The fan 32, which is blowing means, is for example an electrically powered fan in which a centrifugal multi-blade fan is driven by an electrically powered motor, and whose number of rotations is controlled by a control voltage that is output from the controlling device 60.


The second heat exchanger 86 and the first heat exchanger 85 are such that the second heat exchanger 86 and the first heat exchanger 85 are sequentially disposed with respect to the flow of blowing air on a downstream side of the flow of air of the fan 32. The air mix door 34 that adjusts, with regard to blowing air that has passed through the second heat exchanger 86, the ratio between the airflow volume to be passed through the first heat exchanger 85 and the airflow volume not to be passed through the first heat exchanger 85 is disposed in the air-conditioning duct 31.


(3-3-3) Air Mix Door 34


The air mix door 34 is driven by, for example, a motor. The operation of the motor is controlled by using a control signal that is output from the controlling device 60.


In the embodiment, at the time of the heating mode, as shown in FIG. 4, the air mix door 34 is moved to a heating position at which the entire airflow volume of the blowing air that has passed through the second heat exchanger 86 is caused to flow into the first heat exchanger 85.


Therefore, the blowing air that has passed through the second heat exchanger 86 passes through the first heat exchanger 85, flows through a warm-air passage, and reaches an air mix section formed on an upstream side with respect to a plurality of blow-out opening portions.


At the time of the cooling mode, as shown in FIG. 5, the air mix door 34 is moved to a cooling position at which the entire airflow volume of the blowing air that has passed through the second heat exchanger 86 is caused to bypass the first heat exchanger 85.


Therefore, the blowing air that has passed through the second heat exchanger 86 flows into a cool-air passage and reaches the air mix section formed on the upstream side with respect to the plurality of blow-out opening portions.


An opening for blowing out into the interior of a vehicle, which is a space to be air-conditioned, the blowing air that has passed through the first heat exchanger 85 or the blowing air that has bypassed the first heat exchanger 85 is formed in a downmost stream portion of the flow of air of the air-conditioning duct 31.


Therefore, at the time of the cooling mode, the temperature of the blowing air that is blown out into the interior of the vehicle from the blow-out opening may be adjusted by adjusting the opening degree of the air mix door 34 and re-heating at the first heat exchanger 85 a part of the blowing air cooled at the second heat exchanger 86.


(3-4) Controlling Device 60



FIG. 6 is a block diagram of the controlling device 60. In FIG. 6, the controlling device 60 is constituted by a known microcomputer and peripheral circuits thereof, the microcomputer including a CPU, ROM, RAM, etc. Based on an air-conditioning control program stored in ROM, various calculations and processing operations are performed to control the operations of, for example, the compressor 80, the heating control valve 83, the cooling control valve 87, the electromagnetic valve 23, and the fan 32, which are connected to an output side of the controlling device 60.


At the time of the heating mode, the controlling device 60 causes the electromagnetic valve 23 to open and the cooling control valve 87 to close to circulate a refrigerant in the refrigerant circuit 10 as shown in FIG. 4.


At the time of the cooling mode, the controlling device 60 causes the electromagnetic valve 23 to close and the heating control valve 83 to open fully to circulate a refrigerant in the refrigerant circuit 10 as shown in FIG. 5.


Detection signals of a group of air-conditioning control sensors such as a pressure sensor 61, a refrigerant temperature sensor 62, a blow-out temperature sensor 63, and an indoor temperature sensor 64 are input to an input side of the controlling device 60.


The pressure sensor 61 detects the temperature and the pressure of a refrigerant that has flowed out from the first heat exchanger 85 and that has not yet flowed into the heating control valve 83. The refrigerant temperature sensor 62 detects' the temperature of a refrigerant that is at the outlet of the outside-air heat exchanger and that flows out from the outside-air heat exchanger 82. The blow-out temperature sensor 63 detects the temperature of air that is blown into the interior of a vehicle immediately after that air has passed through the first heat exchanger 85. The indoor temperature sensor 64 detects the temperature of air in the interior of a vehicle.


(3-5) Operation of Air Conditioner 1 for Vehicle


(3-5-1) Cooling Mode


In the cooling mode, the controlling device 60 closes the electromagnetic valve 23 and fully opens the heating control valve 83 to cause the cooling control valve 87 to be in an aperture state that allows it to decompress a refrigerant. Therefore, in the cooling mode, as indicated by a solid-line arrow in FIG. 5, a refrigerant circulates in the compressor 80, the first heat exchanger 85, the heating control valve 83, the outside-air heat exchanger 82, the cooling control valve 87, the second heat exchanger 86, the accumulator 80a, and the intake port of the compressor 80 in this order.


The opening degree of the air mix door 34 is determined so that the air mix door 34 allows the air-conditioning duct 31 to be fully open and so that the entire flow rate of the blowing air that has passed through the second heat exchanger 86 passes through the air-conditioning duct 31.


In the cooling mode, the refrigerant 2 Discharged from the compressor 80 flows into the first heat exchanger 85. Here, in the cooling mode, since the air mix door 34 allows the air-conditioning duct 31 to be fully open, the refrigerant that has flowed into the first heat exchanger 85 flows out from the first heat exchanger 85 without dissipating heat to the blowing air.


The refrigerant that has flowed out from the first heat exchanger 85 passes through the fully open heating control valve 83 and flows into the outside-air heat exchanger 82. The refrigerant that has flowed into the outside-air heat exchanger 82 exchanges heat with outside air blown from the fan 32 to dissipate heat.


Since the electromagnetic valve 23 is closed, the refrigerant that has flowed out from the outside-air heat exchanger 82 flows into the cooling control valve 87 and is decompressed. The refrigerant 2Decompressed at the cooling control valve 87 flows into the second heat exchanger 86.


The refrigerant that has flowed into the second heat exchanger 86 absorbs heat from the blowing air blown from the fan 32 and evaporates. Therefore, the blowing air is cooled.


The refrigerant that has flowed out from the second heat exchanger 86 flows into the accumulator 80a and is subjected to gas-liquid separation. A gas-phase refrigerant separated at the accumulator 80a is sucked into the compressor 80 and is compressed again.


In the air conditioner 1 for a vehicle in the cooling mode, the interior of the vehicle can be cooled by blowing out into the interior of the vehicle the blowing air cooled at the second heat exchanger 86.


(3-5-2) Heating Mode


In the heating mode, the controlling device 60 causes the heating control valve 83 to be in an aperture state, fully closes the cooling control valve 87, and opens the electromagnetic valve 23. Therefore, in the heating mode, as indicated by a solid-line arrow in FIG. 4, a refrigerant circulates in the compressor 80, the first heat exchanger 85, the heating control valve 83, the outside-air heat exchanger 82, the bypass 22, the accumulator 80a, and the intake port of the compressor 80 in this order.


The opening degree of the air mix door 34 is such that the air mix door 34 allows the air-conditioning duct 31 to be fully closed and the entire flow rate of the blowing air that has passed through the second heat exchanger 86 passes through the first heat exchanger 85.


In the heating mode, the refrigerant 2 Discharged from the compressor 80 flows into the first heat exchanger 85. The refrigerant that has flowed into the first heat exchanger 85 exchanges heat with the blowing air that has passed through the second heat exchanger 86 to dissipate heat. Therefore, the blowing air is heated.


The refrigerant that has flowed out from the first heat exchanger 85 flows into the heating control valve 83 and is decompressed. The refrigerant 2Decompressed at the heating control valve 83 flows into the outside-air heat exchanger 82.


The refrigerant that has flowed into the outside-air heat exchanger 82 absorbs heat from outside air blown from the outdoor fan 90 and evaporates.


The refrigerant that has flowed out from the outside-air heat exchanger 82 passes through the bypass 22 and flows into the accumulator 80a. The refrigerant that has flowed into the accumulator 80a is subjected to gas-liquid separation. A gas-phase refrigerant separated at the accumulator 80a is sucked into the compressor 80 and is compressed again.


In the air conditioner 1 for a vehicle in the heating mode, the interior of the vehicle can be heated by blowing out into the interior of the vehicle the blowing air heated at the first heat exchanger 85.


(3-5-3) Dehumidifying Heating Mode


In a dehumidifying heating mode, the controlling device 60 causes the heating control valve 83 to be in an aperture state, and fully opens the cooling control valve 87 or causes the cooling control valve 87 to be in an aperture state, and closes the electromagnetic valve 23. Therefore, in the dehumidifying heating mode, as indicated by the solid-line arrow in FIG. 5, a refrigerant circulates in the compressor 80, the first heat exchanger 85, the heating control valve 83, the outside-air heat exchanger 82, the cooling control valve 87, the second heat exchanger 86, the accumulator 80a, and the intake port of the compressor 80 in this order. That is, the refrigerant 2Essentially circulates similarly to the refrigerant in the cooling mode.


The opening degree of the air mix door 34 is such that the air mix door 34 allows the air-conditioning duct 31 to be fully closed as in the heating mode.


In the dehumidifying heating mode, the refrigerant 2 Discharged from the compressor 80 flows into the first heat exchanger 85, exchanges heat with blowing air that has been cooled and dehumidified at the second heat exchanger 86, and dissipates heat. Therefore, the blowing air is heated.


The refrigerant that has flowed out from the first heat exchanger 85 flows into the heating control valve 83 and is decompressed. The refrigerant 2Decompressed at the heating control valve 83 flows into the outside-air heat exchanger 82.


A low-pressure refrigerant that has flowed into the outside-air heat exchanger 82 absorbs heat from outside air blown from the outdoor fan 90 and evaporates.


Since the electromagnetic valve 23 is closed, the refrigerant that has flowed out from the outside-air heat exchanger 82 flows into the cooling control valve 87 and is decompressed. The refrigerant 2Decompressed at the cooling control valve 87 flows into the second heat exchanger 86.


The refrigerant that has flowed into the second heat exchanger 86 absorbs heat from the blowing air blown from a fan 84 and evaporates. Therefore, the blowing air is cooled.


The refrigerant that has flowed out from the second heat exchanger 86 flows into the accumulator 80a and is subjected to gas-liquid separation. A gas-phase refrigerant separated at the accumulator 80a is sucked into the compressor 80 and is compressed again.


In the air conditioner 1 for a vehicle, in the dehumidifying heating mode, the interior of a vehicle can be dehumidified and heated by re-heating at the first heat exchanger 85 the blowing air cooled and dehumidified at the second heat exchanger 86, and by blowing out the re-heated blowing air into the interior of the vehicle.


(3-5-4) Defrosting Mode


When the air conditioner 1 for a vehicle performs a defrosting operation, the air mix door 34 closes an air-flow path that extends toward the first heat exchanger 85. The electromagnetic valve 23 is in an open state. The heating control valve 83 is in a fully open state. The cooling control valve 87 is in a fully closed state.


A refrigerant compressed at the compressor 80 becomes a high-temperature, high-pressure refrigerant, and is discharged. The refrigerant 2 Discharged from the compressor 80 passes through the first heat exchanger 85.


Since the air mix door 34 closes the air-flow path that extends toward the first heat exchanger 85, the heat-dissipation amount of the refrigerant is smaller than the heat-dissipation amount of the refrigerant at the time of the heating operation.


The refrigerant that has passed through the first heat exchanger 85 passes through the fully open heating control valve 83 and flows into the outside-air heat exchanger 82. Therefore, the refrigerant 2Dissipates heat at the outside-air heat exchanger 82, as a result of which it is possible to raise the temperature of and defrost the outside-air heat exchanger 82.


The refrigerant that has flowed out from the outside-air heat exchanger 82 passes through the bypass 22 and flows into the accumulator 80a. The refrigerant that has flowed into the accumulator 80a is separated into a gas-phase refrigerant and a liquid-phase refrigerant, and the gas-phase refrigerant sucked into the compressor 80.


(3-6) Modifications


In the first embodiment, when the refrigerant that has flowed out from the outside-air heat exchanger 82 is caused to flow through the bypass 22, the electromagnetic valve 23 is in an open state and the cooling control valve 87 is in a fully closed state. In addition, when the refrigerant that has flowed out from the outside-air heat exchanger 82 is caused to flow through the second heat exchanger 86, the electromagnetic valve 23 is in a closed state and the cooling control valve 87 is in an aperture state.


However, the switching of a flow path in the refrigerant circuit is not limited to the methods above, and thus the flow path may be switched by using a three-way valve.



FIG. 7 is a schematic view of a configuration of an air conditioner 1 for a vehicle according to a modification of the first embodiment. In FIG. 7, the modification differs from the first embodiment in that the electromagnetic valve 23 of the first embodiment is not used, and in that a three-way valve 25 is provided at a connection portion at which the bypass 22 and a pipe that is connected to an outlet of the outside-air heat exchanger 82 are connected to each other.


A flow of a refrigerant that has flowed out from the outside-air heat exchanger 82 is selected to be either one of a flow toward the bypass 22 and a flow toward the second heat exchanger 86 by the three-way valve 25.


(3-7) Features


(3-7-1)


The air conditioner 1 for a vehicle includes the refrigerant circuit 10 in which a refrigerant that contains at least 1,2-difluoroethylene is sealed.


(3-7-2)


The air conditioner 1 for a vehicle includes the refrigerant circuit 10 in which a mixed refrigerant that contains at least 1132(E), 1234yf, and R32 is sealed.


(3-7-3)


The air conditioner 1 for a vehicle includes the refrigerant circuit 10 in which a refrigerant that contains at least 1132(E), 1123, and R1234yf is sealed.


(3-7-4)


The air conditioner 1 for a vehicle includes the refrigerant circuit 10 in which a refrigerant that contains at least 1132(E)/1234yf is sealed.


(3-7-5)


The air conditioner 1 for a vehicle includes the refrigerant circuit 10 in which a refrigerant that contains at least 1132a, R32, and R1234yf is sealed.


(3-7-6)


The air conditioner 1 for a vehicle includes the refrigerant circuit 10 in which a refrigerant that contains at least R32, R125, R1234yf, R134a, and CO2 is sealed.


(4) Second Embodiment of Refrigeration Cycle Device for Vehicle

An air conditioner for a vehicle using any one of the refrigerant 1A, the refrigerant 1B, the refrigerant 1C, the refrigerant 1D, the refrigerant 1E, the refrigerant 2A, the refrigerant 2B, the refrigerant 2C, the refrigerant 2D, the refrigerant 2E, the refrigerant 3A, and the refrigerant 3B, and the refrigerating machine oil above is described below. The air conditioner for a vehicle is a refrigeration cycle device for a vehicle.


(4-1) Configuration of Air Conditioner 101 for Vehicle



FIG. 8 is a schematic view of a configuration of an air conditioner 101 for a vehicle according to a second embodiment of the present disclosure. In FIG. 8, the air conditioner 101 for a vehicle includes a refrigerant circuit 110 and a controlling device 160. The controlling device 160 controls various units. In the air conditioner 101 for a vehicle, the controlling device 160 controls the various units of the air conditioner to thereby perform air-conditioning (such as cooling, heating, and dehumidifying and heating) in the interior of the vehicle.


(4-2) Refrigerant Circuit 110


As shown in FIG. 8, the refrigerant circuit 110 of the air conditioner 101 for a vehicle is a vapor-compression refrigerant circuit that primarily includes a compressor 180, a four-way switching valve 181, an outside-air heat exchanger 182, a first heat exchanger 185, and a second heat exchanger 186. The refrigerant circuit 110 also includes a branch portion 128.


The branch portion 128 is a portion at which a branch pipe 122 branches off from a main circuit 121 in the refrigerant circuit 110.


The branch pipe 122 is connected at one end to a first refrigerant pipe 123, and is connected at the other end to an intake-side refrigerant pipe 124 that connects the four-way switching valve 181 and an intake portion of the compressor 180 to each other. Therefore, even if a direction of circulation of a refrigerant in the main circuit 121 is changed, the refrigerant flows into the branch pipe 122 in the same one direction toward an intake side of the compressor 180 from the first refrigerant pipe 123.


Note that, in the embodiment, the one end of the branch pipe 122 is connected to a refrigerant pipe 123a that is a part of the first refrigerant pipe 123 and that connects a first control valve 183 and the first heat exchanger 185 to each other.


A second control valve 187, which is an expansion mechanism, and the second heat exchanger 186 are sequentially connected to the branch pipe 122.


As shown in FIG. 8, the compressor 180, the outside-air heat exchanger 182 that exchanges heat with outside air, the first control valve 183, and the first heat exchanger 185 for air-conditioning the interior of a vehicle are sequentially connected to the main circuit 121.


(4-2-1) Compressor 180


The compressor 180 is an inverter compressor whose number of rotations is variable, and is provided for compressing a gas refrigerant that has been sucked in.


As the compressor 180, various compressors, such as a swash-plate compressor, a scroll compressor, a multi-vane compressor, and a rotary compressor, can be used.


(4-2-2) Four-Way Switching Valve 181


The four-way switching valve 181 that is connected to the main circuit 121 constitutes a switching mechanism that changes a flow path of a refrigerant that flows in the main circuit 121.



FIG. 9 is a schematic view of the configuration of the air conditioner 101 for a vehicle, and illustrates a circulation path of a refrigerant in the cooling mode. FIG. 10 is a schematic view of the configuration of the air conditioner 101 for a vehicle, and illustrates a circulation path of a refrigerant in the heating mode.


The four-way switching valve 181 is configured to switch between a first state (see the solid line in FIG. 8) and a second state (see the broken line in FIG. 8) to thereby allow a direction of circulation of a refrigerant in the main circuit 121 to be reversible (see FIGS. 9 and 10). The first state is a state in which the four-way switching valve 181 connects a discharge side of the compressor 180 and the outside-air heat exchanger 182 to each other and connects the first heat exchanger 185 and the intake side of the compressor 180 to each other. The second state is a state in which the four-way switching valve 181 connects the discharge side of the compressor 180 and the first heat exchanger 185 to each other and connects the outside-air heat exchanger 182 and the intake-side of the compressor 180 to each other.


(4-2-3) Outside-Air Heat Exchanger 182


The outside-air heat exchanger 182 is provided for causing heat to be exchanged between outside air and a refrigerant that flows in the outside-air heat exchanger 182.


(4-2-4) First Control Valve 183


The first control valve 183 is an electrically powered expansion valve for, for example, adjusting a refrigerant pressure or a refrigerant flow rate of a refrigerant that flows in the first refrigerant pipe 123 that connects the outside-air heat exchanger 182 and the first heat exchanger 185 to each other.


(4-2-5) First Heat Exchanger 185


The first, heat exchanger 185 is provided for allowing air in the interior of a vehicle as a heat source to exchange heat with a refrigerant. A fan 184 generates a flow of air that comes into contact with the first heat exchanger 185 to thereby make it possible for the air in the interior of the vehicle and the refrigerant that flows in the first heat exchanger 185 to exchange heat with each other.


(4-2-6) Second Heat Exchanger 186


Similarly to the first heat exchanger 185, the second heat exchanger 186 is provided for allowing air in the interior of a vehicle as a heat source to exchange heat with a refrigerant. The fan 184 generates a flow of air that comes into contact with the second heat exchanger 186 to thereby make it possible for the air in the interior of the vehicle and the refrigerant that flows in the second heat exchanger 186 to exchange heat with each other.


(4-2-7) Second Control Valve 187


The second control valve 187 is an electrically powered expansion valve for, for example, adjusting a refrigerant pressure or a refrigerant flow rate of a refrigerant that flows into the second heat exchanger 186 from the first refrigerant pipe 123, and is capable of causing the second heat exchanger 186 to function as an evaporator by adjusting a valve opening degree of the second control valve 187. The second control valve 187 is disposed on an intake side of the second heat exchanger 186.


In the embodiment, the refrigerant circuit 110 is designed so that, when a refrigerant flows toward the first heat exchanger 185 and the second heat exchanger 186 from the outside-air heat exchanger 182, the flow rate of the refrigerant that flows in the first heat exchanger 185 and the flow rate of the refrigerant that flows in the second heat exchanger 186 become a predetermined proportion. In the embodiment, when the heating capacity is insufficient at the time of dehumidifying and heating or at the time of heating the interior of a vehicle, a heater 188 is used as a heat source for heating the air in the interior of the vehicle. An output of the heater 188 is controlled, by the controlling device 60 based on the result of detection of the various sensors.


(4-3) Configuration of Controlling Device 160



FIG. 11 is a block diagram of the controlling device 160. In FIG. 11, the controlling device 160 is constituted by a known microcomputer and peripheral circuits thereof, the microcomputer including a CPU, ROM, RAM, etc. Based on an air-conditioning control program stored in ROM, various calculations and processing operations are performed to control the operations of, for example, the compressor 180, the four-way switching valve 181, the first control valve 183, the fan 184, the second control valve 187, and the heater 188, which are connected to an output side of the controlling device 160.


Detection signals of a group of air-conditioning control sensors such as a pressure sensor 161, a refrigerant temperature sensor 162, a blow-out temperature sensor 163, and an indoor temperature sensor 164 are input to an input side of the controlling device 160.


The pressure sensor 161 detects the temperature and the pressure of a refrigerant that has flowed out from the first heat exchanger 185 and that has not yet flowed into the first control valve 183. The refrigerant temperature sensor 162 detects the temperature of a refrigerant that is at an outlet of the outside-air heat exchanger and that flows out from the outside-air heat exchanger 182. The blow-out temperature sensor 163 detects the temperature of air that is blown into the interior of a vehicle immediately after that air has passed through the first heat exchanger 185. The indoor temperature sensor 164 detects the temperature of air in the interior of a vehicle.


The controlling device 160 performs control to adjust the valve opening degrees of the first control valve 183 and the second control valve 187 and to adjust the number of rotations of the fan 184 to thereby control the amounts of heat exchange at the first heat exchanger 185 and the second heat exchanger 186.


(4-4) Operation of Air Conditioner 101 for Vehicle


Next, the operations of the air conditioner 101 for a vehicle when, as an air-conditioning operation of the interior of the vehicle, a cooling operation is performed, a humidifying and heating operation is performed, a heating operation is performed, and a defrosting operation is performed are described.


(4-4-1) Cooling Mode


The arrows in FIG. 9 indicate flows of a refrigerant in the refrigerant circuit 110 at the time of the cooling mode. At the time of the cooling mode, the four-way switching valve 181 is switched to the first state, and the number of rotations of the compressor 180 is adjusted in accordance with the cooling capacity or the dehumidifying capacity in the interior of the vehicle.


The valve opening degree of the first control valve 183 is controlled so that the degree of superheating on an outlet side of the first heat exchanger 185 becomes a predetermined value. Further, the valve opening degree of the second control valve 187 is controlled so that the degree of superheating on an outlet side of the second heat exchanger 186 becomes a predetermined value.


A high-pressure gas refrigerant 2 Discharged from the compressor 180 exchanges heat with outside air at the outside-air heat exchanger 182, is cooled, and is condensed. After a high-pressure liquid refrigerant that has flowed out from the outside-air heat exchanger 182 has been decompressed at the first control valve 183, the refrigerant flows through the refrigerant pipe 123a, and reaches the first heat exchanger 185 or flows through the branch pipe 122 at a location partway in the refrigerant pipe 123a.


The refrigerant that has reached the first heat exchanger 185 exchanges heat with air in the interior of the vehicle that is blown by the fan 184, and the liquid refrigerant 2Evaporates and cools the air, as a result of which the interior of the vehicle is cooled. An evaporated gas refrigerant is sucked into the compressor 180 via the four-way switching valve 181.


On the other hand, the liquid refrigerant that has reached the branch pipe 122 flows into the second heat exchanger 186 via the second control valve 187. Then, the refrigerant that has flowed into the second heat exchanger 186 exchanges heat with air in the interior of the vehicle that is blown by the fan 184, and the liquid refrigerant 2Evaporates and cools the air, as a result of which the interior of the vehicle is cooled. An evaporated gas refrigerant merges with a refrigerant that flows in the intake-side refrigerant pipe 124, and is sucked into the compressor 180.


The refrigerant circulates in the refrigerant circuit 110 in this way, and the first heat exchanger 185 and the second heat, exchanger 186 function as evaporators, as a result of which the interior of the vehicle can be cooled or dehumidified.


(4-4-2) Dehumidifying Heating Mode


The arrows in FIG. 10 indicate flows of a refrigerant in the refrigerant circuit 110 in the dehumidifying heating mode. In the dehumidifying heating mode, the four-way switching valve 181 is switched to the second state, and the number of rotations of the compressor 180 is adjusted in accordance with the heating capacity in the interior of the vehicle.


The valve opening degree of the first control valve 183 is controlled so that the degree of superheating on an outlet side of the outside-air heat exchanger 182 becomes a predetermined value. Further, the valve opening degree of the second control valve 187 is adjusted in accordance with the dehumidifying capacity in the interior of the vehicle.


A high-pressure gas refrigerant 2 Discharged from the compressor 180 exchanges heat with, at the first heat exchanger 185, air in the interior of the vehicle that is blown by the fan 184, and is condensed and heats the air, as a result of which the interior of the vehicle is heated. The high-pressure liquid refrigerant that has flowed out from the first heat exchanger 185 flows through the refrigerant pipe 123a, and reaches the first control valve 183 or flows through the branch pipe 122 at a location partway in the refrigerant pipe 123a.


After the liquid refrigerant that has reached the first control valve 183 has been decompressed at the first control valve 183, the liquid refrigerant flows into the outside-air heat exchanger 182. In the outside-air heat exchanger 182, the liquid refrigerant that has flowed in evaporates by exchanging heat with outside air. An evaporated gas refrigerant is sucked into the compressor 180 via the four-way switching valve 181.


On the other hand, after the liquid refrigerant that has flowed into the branch pipe 122 has been decompressed at the second control valve 187, the liquid refrigerant flows into the second heat exchanger 186. Then, the refrigerant that has flowed into the second heat exchanger 186 exchanges heat, with air in the interior of the vehicle that is blown by the fan 184, and the liquid refrigerant 2Evaporates and cools the air, as a result of which the interior of the vehicle is dehumidified. An evaporated gas refrigerant merges with a refrigerant that flows in the intake-side refrigerant pipe 124, and is sucked into the compressor 180.


The refrigerant circulates in the refrigerant circuit 110 in this way; and the first heat exchanger 185 functions as a condenser, as a result of which the interior of the vehicle can be heated, and the second heat exchanger 186 functions as an evaporator, as a result of which the interior of the vehicle can be dehumidified.


(4-4-3) Heating Mode


Since the heating mode is a mode in which the dehumidifying operation in the dehumidifying heating mode in FIG. 10 is not performed, the heating mode is described with reference to FIG. 10. In the heating mode, the four-way switching valve 181 is switched to the second state, and the number of rotations of the compressor 180 is adjusted in accordance with the heating capacity in the interior of a vehicle.


The valve opening degree of the first control valve 183 is controlled so that the degree of superheating on the outlet side of the outside-air heat exchanger 182 becomes a predetermined value. The second control valve 187 is in a fully closed state.


A high-pressure gas refrigerant 2 Discharged from the compressor 180 exchanges heat with, at the first heat exchanger 185, air in the interior of the vehicle that is blown by the fan 184, and is condensed and heats the air, as a result of which the interior of the vehicle is heated. The high-pressure liquid refrigerant that has flowed out from the first heat exchanger 185 flows into the refrigerant pipe 123a and reaches the first control valve 183. Note that since the second control valve 187 is in a fully closed state, the refrigerant will not flow into the branch pipe 122 at a location partway in the refrigerant pipe 123a.


After the liquid refrigerant that has reached the first control valve 183 has been decompressed at the first control valve 183, the liquid refrigerant flows into the outside-air heat exchanger 182. In the outside-air heat exchanger 182, the liquid refrigerant that has flowed in evaporates by exchanging heat with outside air. An evaporated gas refrigerant is sucked into the compressor 180 via the four-way switching valve 181.


The refrigerant circulates in the refrigerant circuit 110 in this way and the first heat exchanger 185 functions as a condenser, as a result of which the interior of the vehicle can be heated.


(4-4-4) Defrosting Mode


Since the defrosting mode is a mode in which the first control valve 183 and the second control valve 187 are in a fully open state in the flow of the refrigerant in the cooling mode in FIG. 9, the defrosting mode is described with reference to FIG. 9.


A refrigerant compressed at the compressor 180 is discharged as a high-temperature, high-pressure refrigerant. The refrigerant 2 Discharged from the compressor 180 flows into the outside-air heat exchanger 182. Therefore, the refrigerant 2Dissipates heat at the outside-air heat exchanger 182, as a result of which it is possible to raise the temperature of the outside-air heat exchanger 182 and perform defrosting.


The refrigerant that has flowed out from the outside-air heat exchanger 182 flows through the fully-open first control valve 183, the refrigerant pipe 123a, and the first heat exchanger 185, and is sucked into the compressor 180 via the four-way switching valve 181.


On the other hand, a liquid refrigerant that has reached the branch pipe 122 flows through the fully-open second control valve 187 and the second heat exchanger 186, merges with a refrigerant that flows through the intake-side refrigerant pipe 124, and is sucked into the compressor 180.


(4-5) Modifications


In the second embodiment, the first heat exchanger 185 and the second heat exchanger 186 are provided side by side as heat exchangers for inside air, the first heat exchanger 185 is caused to function as a condenser, and the second heat exchanger 186 is caused to function as an evaporator to make it possible to dehumidify and heat, at the same time.


However, the configuration is not limited thereto. Two heat exchangers may be provided in series, and an expansion mechanism may provided between these two heat exchangers.



FIG. 12 is a schematic view of a configuration of an air conditioner 101 for a vehicle according to a modification of the second embodiment. In FIG. 12, in a refrigerant circuit 210, a first heat exchanger 285, a second heat exchanger 286, and an outside-air heat exchanger 282 are provided in series, and a control valve 287 is provided as an expansion mechanism between the first heat exchanger 285 and the second heat exchanger 286. Note that, in FIG. 12, units labelled with the same reference numerals as those in the second embodiment have the same functions and are not described below.


Here, an operation in the dehumidifying heating mode is described as an example. In the air conditioner 101 for a vehicle, a refrigerant is decompressed by the control valve 287, the first heat exchanger 285 is caused to function as a condenser, and the second heat exchanger 286 and the outside-air heat exchanger 282 are caused to function as evaporators. Therefore, it is possible to dehumidify and heat the interior of the vehicle.


(4-6) Features


(4-6-1)


The air conditioner 101 for a vehicle includes the refrigerant circuit 110 in which a refrigerant that contains at least 1,2-difluoroethylene is sealed.


(4-6-2)


The air conditioner 101 for a vehicle includes the refrigerant circuit 110 in which a mixed refrigerant that contains at least 1132(E), 1234yf, and R32 is sealed.


(4-6-3)


The air conditioner 101 for a vehicle includes the refrigerant, circuit 110 in which a refrigerant that contains at least 1132(E), 1123, and R1234yf is sealed.


(4-6-4)


The air conditioner 101 for a vehicle includes the refrigerant circuit 110 in which a refrigerant that contains at least 1132(E)/1234yf is sealed.


(4-6-5)


The air conditioner 101 for a vehicle includes the refrigerant circuit 110 in which a refrigerant that contains at least 1132a, R32, and R1234yf is sealed.


(4-6-6)


The air conditioner 101 for a vehicle includes the refrigerant circuit 110 in which a refrigerant that contains at least R32, R125, R1234yf, R134a, and CO2 is sealed.


Other Embodiments

The refrigerant circuit may be a refrigerant circuit that uses an economizer heat exchanger and an injection valve.


The economizer heat exchanger has a first flow path and a second flow path, and is configured to exchange heat with a refrigerant that flows in the first flow path and a refrigerant that flows in the second flow path.


The first flow path constitutes a part of a liquid refrigerant pipe. The second flow path constitutes a part of an injection flow path. The injection flow path is a refrigerant flow path that connects the liquid refrigerant pipe and a compression chamber during compression of the compressor to each other. The injection flow path is a refrigerant flow path that branches off from the liquid refrigerant pipe, and that communicates with the compression chamber during compression of the compression mechanism of the compressor.


The injection valve is, for example, an electrically powered valve whose opening degree is capable of being adjusted. The injection valve is provided at a portion, at which the liquid refrigerant pipe and the second flow path of the economizer heat exchanger are connected to each other, of the injection flow path.


When the injection valve is opened, a refrigerant that has branched off from the liquid refrigerant pipe and that has passed through the injection valve flows into the second flow path of the economizer heat exchanger. Then, the refrigerant that has flowed into the second flow path exchanges heat with a refrigerant that flows in the first flow path, becomes a gas-phase refrigerant, and is supplied to the compression chamber during the compression of the compression mechanism of the compressor.


Although the embodiments of the present disclosure are described above, it is to be understood that various changes can be made in the forms and details without departing from the spirit and the scope of the present disclosure described in the claims.


REFERENCE SIGNS LIST






    • 1 air conditioner for vehicle (refrigeration cycle device for vehicle)


    • 10 refrigerant circuit


    • 80 compressor


    • 82 outside-air heat exchanger (condenser, evaporator)


    • 83 heating control valve (decompressor)


    • 85 first, heat exchanger (condenser)


    • 86 second heat exchanger (evaporator)


    • 87 cooling control valve (decompressor)


    • 101 air conditioner for vehicle (refrigeration cycle device for vehicle)


    • 110 refrigerant circuit


    • 180 compressor


    • 182 outside-air heat exchanger (condenser, evaporator)


    • 183 first control valve (decompressor)


    • 185 first heat exchanger (evaporator, condenser)


    • 186 second heat exchanger (evaporator)


    • 187 second control valve (decompressor)


    • 210 refrigerant circuit





CITATION LIST
Patent Literature





    • PTL 1: International Publication No. 2005/105947

    • PTL 2: International Publication No. 2015/141678

    • PTL 3: Japanese Unexamined Patent Application Publication No. 2018-184597




Claims
  • 1. A refrigeration method comprising operating a refrigeration cycle device for a vehicle, wherein the operating comprises applying a refrigerant as an alternative refrigerant for R1234yf alone,wherein a first equipment designed for operation using R1234yf alone is operated using the alternative refrigerant, optionally with changes of a few parts and adjustment of the first equipment, ora second equipment designed for operation using the alternative refrigerant is operated for the same use as an existing use with R1234yf by using the alternative refrigerant,wherein:the refrigeration cycle device comprises a refrigerant circuit,the refrigerant circuit comprises a compressor, a condenser, a decompressor, and an evaporator;the refrigerant is sealed in the refrigerant circuit,the refrigerant comprises at least trans-1,2-difluoroethylene (HFO-1132(E)) and 2,3,3,3-tetrafluoropropene (HFO-1234yf), andthe refrigerant comprises HFO-1132(E) and HFO-1234yf in such amounts that the sum of HFO-1132(E) and HFO-1234yf is 99.7 mass % or more.
  • 2. The refrigeration method according to claim 1, wherein the refrigerant comprises HFO-1132(E) and HFO-1234yf,a content rate of HFO-1132(E) is 35.0 to 65.0 mass % and a content rate of HFO-1234yf is 65.0 to 35.0 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf, andan evaporating temperature is −75 to −5° C.
  • 3. The refrigeration method according to claim 1, wherein a content rate of HFO-1132(E) is 41.3 to 53.5 mass % and a content rate of HFO-1234yf is 58.7 to 46.5 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.
  • 4. The refrigeration method according to claim 2, wherein the refrigerant consists only of HFO-1132(E) and HFO-1234yf.
  • 5. The refrigeration method according to claim 1, wherein the refrigerant comprises HFO-1132(E) and HFO-1234yf, anda content rate of HFO-1132(E) is 40.5 to 49.2 mass % and a content rate of HFO-1234yf is 59.5 to 50.8 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.
  • 6. The refrigeration method according to claim 5, wherein the refrigerant consists only of HFO-1132(E) and HFO-1234yf.
  • 7. The refrigeration method according to claim 1, wherein the refrigerant comprises HFO-1132(E) and HFO-1234yf, anda content rate of HFO-1132(E) is 31.1 to 39.8 mass % and a content rate of HFO-1234yf is 68.9 to 60.2 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.
  • 8. The refrigeration method according to claim 1, wherein a content rate of HFO-1132(E) is 31.1 to 37.9 mass % and a content rate of HFO-1234yf is 68.9 to 62.1 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.
  • 9. The refrigeration method according to claim 7, wherein the refrigerant consists only of HFO-1132(E) and HFO-1234yf.
  • 10. The refrigeration method according to claim 1, wherein the refrigerant comprises HFO-1132(E) and HFO-1234yf, anda content of HFO-1132(E) is 21.0 to 28.4 mass % and a content of HFO-1234yf is 79.0 to 71.6 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.
  • 11. The refrigeration method according to claim 10, wherein the refrigerant consists only of HFO-1132(E) and HFO-1234yf.
  • 12. The refrigeration method according to claim 1, wherein the refrigerant comprises HFO-1132(E) and HFO-1234yf, a content of HFO-1132(E) is 12.1 to 72.0 mass % and a content of HFO-1234yf is 87.9 to 28.0 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf, andthe device is in-car air conditioning equipment.
Priority Claims (12)
Number Date Country Kind
2018-134448 Jul 2018 JP national
2018-227398 Dec 2018 JP national
2018-230259 Dec 2018 JP national
2019-013974 Jan 2019 JP national
2019-013979 Jan 2019 JP national
2019-018617 Feb 2019 JP national
2019-019701 Feb 2019 JP national
2019-078133 Apr 2019 JP national
2019-084708 Apr 2019 JP national
2019-112408 Jun 2019 JP national
2019-115584 Jun 2019 JP national
PCT/JP2019/027031 Jul 2019 WO international
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2019/027988 7/16/2019 WO
Publishing Document Publishing Date Country Kind
WO2020/017520 1/23/2020 WO A
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20210309902 A1 Oct 2021 US
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