Refrigeration cycle apparatus

Information

  • Patent Grant
  • 11441819
  • Patent Number
    11,441,819
  • Date Filed
    Thursday, June 25, 2020
    3 years ago
  • Date Issued
    Tuesday, September 13, 2022
    a year ago
Abstract
A refrigeration cycle apparatus that can improve operation efficiency when a refrigerant that contains at least 1,2-difluoroethylene is used is provided. An air conditioning apparatus 1 includes a compressor (21), an outdoor heat exchanger (23), an outdoor expansion valve (24), an indoor heat exchanger (31), and a suction injection pipe (40), and uses a refrigerant that contains at least 1,2-difluoroethylene. The suction injection pipe (40) allows a part of a refrigerant that flows toward the indoor heat exchanger (31) from the outdoor heat exchanger (23) to merge with a low-pressure refrigerant that is sucked into the compressor (21).
Description
TECHNICAL FIELD

The present disclosure relates to a refrigeration cycle apparatus.


BACKGROUND ART

Hitherto, a refrigeration cycle apparatus such as an air conditioning apparatus has frequently uses R410A as a refrigerant. R410A is a two-component mixed refrigerant containing (CH2F2; HFC-32 or R32) and pentafluoroethane (C2HF5; HFC-125 or R125), and is a near-azeotropic composition.


However, the global warming potential (GWP) of R410A is 2088, and, in recent years, due to increasing concern about global warming, R32, which is a refrigerant having a lower GWP, is being frequently used.


Therefore, for example, Patent Literature 1 (International Publication No. 2015/141678) proposes various low-GWP mixed refrigerants that can replace R410A.


SUMMARY OF THE INVENTION
Technical Problem

However, the operation efficiency of a refrigeration cycle when a refrigerant containing at least 1,2-difluoroethylene is used as a refrigerant having a sufficiently low GWP has not been considered at all up to this time.


The content of the present disclosure is based on the point above, and an object is to provide a refrigeration cycle apparatus that can improve operation efficiency when using a refrigerant containing at least 1,2-difluoroethylene.


Solution to Problem

A refrigeration cycle apparatus according to a first aspect includes a compressor, a condenser, a decompressor, an evaporator, and an injection flow path. The compressor sucks a low-pressure refrigerant from a suction flow path, compresses the refrigerant, and discharges a high-pressure refrigerant. The condenser condenses the high-pressure refrigerant discharged from the compressor. The decompressor decompresses the high-pressure refrigerant that has exited from the condenser. The evaporator evaporates the refrigerant decompressed at the decompressor. The injection flow path is at least either one of an intermediate injection flow path and a suction injection flow path. The intermediate injection flow path allows a part of a refrigerant that flows toward the evaporator from the condenser to merge with an intermediate-pressure refrigerant in the compressor. The suction injection flow path allows a part of a refrigerant that flows toward the evaporator from the condenser to merge with the low-pressure refrigerant that is sucked by the compressor. The refrigerant contains at least 1,2-difluoroethylene.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using the injection flow path, while sufficiently reducing GWP by using the refrigerant containing 1,2-difluoroethylene.


A refrigeration cycle apparatus according to a second aspect is the refrigeration cycle apparatus of the first aspect and further includes a branching flow path, an opening degree adjusting valve, and an injection heat exchanger. The branching flow path branches off from a main refrigerant flow path that connects the condenser and the evaporator to each other. The opening degree adjusting valve is provided in the branching flow path. The injection heat exchanger causes a refrigerant that flows in the main refrigerant flow path and a refrigerant that flows on a downstream side with respect to the opening degree adjusting valve in the branching flow path to exchange heat. A refrigerant that exits from the injection heat exchanger and flows in the branching flow path flows in the injection flow path.


The refrigeration cycle apparatus can further improve the operation efficiency of a refrigeration cycle.


A refrigeration cycle apparatus according to a third aspect is the refrigeration cycle apparatus of the first aspect or the second aspect and further includes a refrigerant storage tank that is provided in a main refrigerant flow path that connects the condenser and the evaporator to each other. A gas component of a refrigerant that accumulates in the refrigerant storage tank flows in the injection flow path.


The refrigeration cycle apparatus can improve the efficiency of a refrigeration cycle, while accumulating an excess refrigerant in the refrigerant storage tank.


A refrigeration cycle apparatus according to a fourth aspect is the refrigeration cycle apparatus of any one of the first aspect to the third aspect, in which the compressor includes a fixed scroll and a swinging scroll. The fixed scroll includes a end plate and a lap that stands spirally from the end plate. The swinging scroll forms a compression chamber by engaging with the fixed scroll. A refrigerant that flows in the injection flow path merges at the compression chamber.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle while using a scroll compressor.


A refrigeration cycle apparatus according to a fifth aspect is the refrigeration cycle apparatus according to any one of the first aspect to the fifth aspect, wherein


the refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), trifluoroethylene (HFO-1123), and 2,3,3,3-tetrafluoro-1-propene (R1234yf).


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP and having a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) and a coefficient of performance (COP) that are equivalent to those of R410A.


A refrigeration cycle apparatus according to a sixth aspect is the refrigeration cycle apparatus according to the fifth 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 AA′, A′B, BD, DC′, C′C, CO, and OA that connect the following 7 points:


point A (68.6, 0.0, 31.4),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point D (0.0, 80.4, 19.6),


point C′ (19.5, 70.5, 10.0),


point C (32.9, 67.1, 0.0), and


point O (100.0, 0.0, 0.0),


or on the above line segments (excluding the points on the line segments BD, CO, and OA);


the line segment AA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment DC′ is represented by coordinates (x, 0.0082x2−0.6671x+80.4, −0.0082x2−0.3329x+19.6),


the line segment C′C is represented by coordinates (x, 0.0067x2−0.6034x+79.729, −0.0067x2−0.3966x+20.271), and


the line segments BD, CO, and OA are straight lines.


A refrigeration cycle apparatus according to a seventh aspect is the refrigeration cycle apparatus according to the fifth 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 GI, IA, AA′, A′B, BD, DC′, C′C, and CG that connect the following 8 points:


point G (72.0, 28.0, 0.0),


point I (72.0, 0.0, 28.0),


point A (68.6, 0.0, 31.4),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point D (0.0, 80.4, 19.6),


point C′ (19.5, 70.5, 10.0), and


point C (32.9, 67.1, 0.0),


or on the above line segments (excluding the points on the line segments IA, BD, and CG);


the line segment AA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment DC′ is represented by coordinates (x, 0.0082x2−0.6671x+80.4, −0.0082x2−0.3329x+19.6),


the line segment C′C is represented by coordinates (x, 0.0067x2−0.6034x+79.729, −0.0067x2−0.3966x+20.271), and


the line segments GI, IA, BD, and CG are straight lines.


A refrigeration cycle apparatus according to an eighth aspect is the refrigeration cycle apparatus according to the fifth 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 JP, PN, NK, KA′, A′B, BD, DC′, C′C, and CJ that connect the following 9 points:


point J (47.1, 52.9, 0.0),


point P (55.8, 42.0, 2.2),


point N (68.6, 16.3, 15.1),


point K (61.3, 5.4, 33.3),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point D (0.0, 80.4, 19.6),


point C′ (19.5, 70.5, 10.0), and


point C (32.9, 67.1, 0.0),


or on the above line segments (excluding the points on the line segments BD and CJ);


the line segment PN is represented by coordinates (x, −0.1135x2+12.112x−280.43, 0.1135x2−13.112x+380.43),


the line segment NK is represented by coordinates (x, 0.2421x2−29.955x+931.91, −0.2421x2+28.955x−831.91),


the line segment KA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment DC′ is represented by coordinates (x, 0.0082x2−0.6671x+80.4, −0.0082x2−0.3329x+19.6),


the line segment C′C is represented by coordinates (x, 0.0067x2−0.6034x+79.729, −0.0067x2−0.3966x+20.271), and


the line segments JP, BD, and CG are straight lines.


A refrigeration cycle apparatus according to a ninth aspect is the refrigeration cycle apparatus according to the fifth 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 JP, PL, LM, MA′, A′B, BD, DC′, C′C, and CJ that connect the following 9 points:


point J (47.1, 52.9, 0.0),


point P (55.8, 42.0, 2.2),


point L (63.1, 31.9, 5.0),


point M (60.3, 6.2, 33.5),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point D (0.0, 80.4, 19.6),


point C′ (19.5, 70.5, 10.0), and


point C (32.9, 67.1, 0.0),


or on the above line segments (excluding the points on the line segments BD and CJ);


the line segment PL is represented by coordinates (x, −0.1135x2+12.112x−280.43, 0.1135x2−13.112x+380.43)


the line segment MA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment DC′ is represented by coordinates (x, 0.0082x2−0.6671x+80.4, −0.0082x2−0.3329x+19.6),


the line segment C′C is represented by coordinates (x, 0.0067x2−0.6034x+79.729, −0.0067x2−0.3966x+20.271), and


the line segments JP, LM, BD, and CG are straight lines.


A refrigeration cycle apparatus according to a tenth aspect is the refrigeration cycle apparatus according to the fifth 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 PL, LM, MA′, A′B, BF, FT, and TP that connect the following 7 points:


point P (55.8, 42.0, 2.2),


point L (63.1, 31.9, 5.0),


point M (60.3, 6.2, 33.5),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point F (0.0, 61.8, 38.2), and


point T (35.8, 44.9, 19.3),


or on the above line segments (excluding the points on the line segment BF);


the line segment PL is represented by coordinates (x, −0.1135x2+12.112x−280.43, 0.1135x2−13.112x+380.43),


the line segment MA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment FT is represented by coordinates (x, 0.0078x2−0.7501x+61.8, −0.0078x2−0.2499x+38.2),


the line segment TP is represented by coordinates (x, 0.00672x2−0.7607x+63.525, −0.00672x2−0.2393x+36.475), and


the line segments LM and BF are straight lines.


A refrigeration cycle apparatus according to an eleventh aspect is the refrigeration cycle apparatus according to the fifth 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 PL, LQ, QR, and RP that connect the following 4 points:


point P (55.8, 42.0, 2.2),


point L (63.1, 31.9, 5.0),


point Q (62.8, 29.6, 7.6), and


point R (49.8, 42.3, 7.9),


or on the above line segments;


the line segment PL is represented by coordinates (x, −0.1135x2+12.112x−280.43, 0.1135x2−13.112x+380.43),


the line segment RP is represented by coordinates (x, 0.00672x2−0.7607x+63.525, −0.00672x2−0.2393x+36.475), and


the line segments LQ and QR are straight lines.


A refrigeration cycle apparatus according to a twelfth aspect is the refrigeration cycle apparatus according to the fifth 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 SM, MA′, A′B, BF, FT, and TS that connect the following 6 points:


point S (62.6, 28.3, 9.1),


point M (60.3, 6.2, 33.5),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point F (0.0, 61.8, 38.2), and


point T (35.8, 44.9, 19.3),


or on the above line segments,


the line segment MA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment FT is represented by coordinates (x, 0.0078x2−0.7501x+61.8, −0.0078x2−0.2499x+38.2),


the line segment TS is represented by coordinates (x, −0.0017x2−0.7869x+70.888, −0.0017x2−0.2131x+29.112), and


the line segments SM and BF are straight lines.


A refrigeration cycle apparatus according to a thirteenth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)) and trifluoroethylene (HFO-1123) in a total amount of 99.5 mass % or more based on the entire refrigerant, and


the refrigerant comprises 62.0 mass % to 72.0 mass % of HFO-1132(E) based on the entire refrigerant.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP, having a coefficient of performance (COP) and a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) that are equivalent to those of R410A, and being classified with lower flammability (class 2L) based on the standard of American Society of Heating, Refrigerating and Air Conditioning Engineers (ASHRAE).


A refrigeration cycle apparatus according to a fourteenth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises HFO-1132(E) and HFO-1123 in a total amount of 99.5 mass % or more based on the entire refrigerant, and


the refrigerant comprises 45.1 mass % to 47.1 mass % of HFO-1132(E) based on the entire refrigerant.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP, having a coefficient of performance (COP) and a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) that are equivalent to those of R410A, and being classified with lower flammability (class 2L) based on the standard of American Society of Heating, Refrigerating and Air Conditioning Engineers (ASHRAE).


A refrigeration cycle apparatus according to a fifteenth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), trifluoroethylene (HFO-1123), 2,3,3,3-tetrafluoro-1-propene (R1234yf), and difluoromethane (R32),


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≤11.1, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines GI, IA, AB, BD′, D′C, and CG that connect the following 6 points:


point G (0.026a2−1.7478a+72.0, −0.026a2+0.7478a+28.0, 0.0),


point I (0.026a2−1.7478a+72.0, 0.0, −0.026a2+0.7478a+28.0),


point A (0.0134a2−1.9681a+68.6, 0.0, −0.0134a2+0.9681a+31.4),


point B (0.0, 0.0144a2−1.6377a+58.7, −0.0144a2+0.6377a+41.3),


point D′ (0.0, 0.0224a2+0.968a+75.4, −0.0224a2−1.968a+24.6), and


point C (−0.2304a2−0.4062a+32.9, 0.2304a2−0.5938a+67.1, 0.0),


or on the straight lines GI, AB, and D′C (excluding point G, point I, point A, point B, point D′, and point C);


if 11.1<a≤18.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines GI, IA, AB, BW, and WG that connect the following 5 points:


point G (0.02a2−1.6013a+71.105, −0.02a2+0.6013a+28.895, 0.0),


point I (0.02a2−1.6013a+71.105, 0.0, −0.02a2+0.6013a+28.895),


point A (0.0112a2−1.9337a+68.484, 0.0, −0.0112a2+0.9337a+31.516),


point B (0.0, 0.0075a2−1.5156a+58.199, −0.0075a2+0.5156a+41.801), and


point W (0.0, 100.0−a, 0.0),


or on the straight lines GI and AB (excluding point G, point I, point A, point B, and point W);


if 18.2<a≤26.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines GI, IA, AB, BW, and WG that connect the following 5 points:


point G (0.0135a2−1.4068a+69.727, −0.0135a2+0.4068a+30.273, 0.0),


point I (0.0135a2−1.4068a+69.727, 0.0, −0.0135a2+0.4068a+30.273),


point A (0.0107a2−1.9142a+68.305, 0.0, −0.0107a2+0.9142a+31.695),


point B (0.0, 0.009a2−1.6045a+59.318, −0.009a2+0.6045a+40.682), and


point W (0.0, 100.0−a, 0.0),


or on the straight lines GI and AB (excluding point G, point I, point A, point B, and point W);


if 26.7<a≤36.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines GI, IA, AB, BW, and WG that connect the following 5 points:


point G (0.0111a2−1.3152a+68.986, −0.0111a2+0.3152a+31.014, 0.0),


point I (0.0111a2−1.3152a+68.986, 0.0, −0.0111a2+0.3152a+31.014),


point A (0.0103a2−1.9225a+68.793, 0.0, −0.0103a2+0.9225a+31.207),


point B (0.0, 0.0046a2−1.41a+57.286, −0.0046a2+0.41a+42.714), and


point W (0.0, 100.0−a, 0.0),


or on the straight lines GI and AB (excluding point G, point I, point A, point B, and point W); and


if 36.7<a≤46.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines GI, IA, AB, BW, and WG that connect the following 5 points:


point G (0.0061a2−0.9918a+63.902, −0.0061a2−0.0082a+36.098, 0.0),


point I (0.0061a2−0.9918a+63.902, 0.0, −0.0061a2−0.0082a+36.098),


point A (0.0085a2−1.8102a+67.1, 0.0, −0.0085a2+0.8102a+32.9),


point B (0.0, 0.0012a2−1.1659a+52.95, −0.0012a2+0.1659a+47.05), and


point W (0.0, 100.0−a, 0.0),


or on the straight lines GI and AB (excluding point G, point I, point A, point B, and point W).


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP and having a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) and a coefficient of performance (COP) that are equivalent to those of R410A.


A refrigeration cycle apparatus according to a sixteenth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), trifluoroethylene (HFO-1123), 2,3,3,3-tetrafluoro-1-propene (R1234yf), and difluoromethane (R32),


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≤11.1, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines JK′, K′B, BD′, D′C, and CJ that connect the following 5 points:


point J (0.0049a2−0.9645a+47.1, −0.0049a2−0.0355a+52.9, 0.0),


point K′ (0.0514a2−2.4353a+61.7, −0.0323a2+0.4122a+5.9, −0.0191a2+1.0231a+32.4),


point B (0.0, 0.0144a2−1.6377a+58.7, −0.0144a2+0.6377a+41.3),


point D′ (0.0, 0.0224a2+0.968a+75.4, −0.0224a2−1.968a+24.6), and


point C (−0.2304a2−0.4062a+32.9, 0.2304a2−0.5938a+67.1, 0.0),


or on the straight lines JK′, K′B, and D′C (excluding point J, point B, point D′, and point C);


if 11.1<a≤18.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines JK′, K′B, BW, and WJ that connect the following 4 points:


point J (0.0243a2−1.4161a+49.725, −0.0243a2+0.4161a+50.275, 0.0),


point K′ (0.0341a2−2.1977a+61.187, −0.0236a2+0.34a+5.636, −0.0105a2+0.8577a+33.177),


point B (0.0, 0.0075a2−1.5156a+58.199, −0.0075a2+0.5156a+41.801), and


point W (0.0, 100.0−a, 0.0),


or on the straight lines JK′ and K′B (excluding point J, point B, and point W);


if 18.2<a≤26.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines JK′, K′B, BW, and WJ that connect the following 4 points:


point J (0.0246a2−1.4476a+50.184, −0.0246a2+0.4476a+49.816, 0.0),


point K′ (0.0196a2−1.7863a+58.515, −0.0079a2−0.1136a+8.702, −0.0117a2+0.8999a+32.783),


point B (0.0, 0.009a2−1.6045a+59.318, −0.009a2+0.6045a+40.682), and


point W (0.0, 100.0−a, 0.0),


or on the straight lines JK′ and K′B (excluding point J, point B, and point W);


if 26.7<a≤36.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines JK′, K′A, AB, BW, and WJ that connect the following 5 points:


point J (0.0183a2−1.1399a+46.493, −0.0183a2+0.1399a+53.507, 0.0),


point K′ (−0.0051a2+0.0929a+25.95, 0.0, 0.0051a2−1.0929a+74.05),


point A (0.0103a2−1.9225a+68.793, 0.0, −0.0103a2+0.9225a+31.207),


point B (0.0, 0.0046a2−1.41a+57.286, −0.0046a2+0.41a+42.714), and


point W (0.0, 100.0−a, 0.0),


or on the straight lines JK′, K′A, and AB (excluding point J, point B, and point W); and


if 36.7<a≤46.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines JK′, K′A, AB, BW, and WJ that connect the following 5 points:


point J (−0.0134a2+1.0956a+7.13, 0.0134a2−2.0956a+92.87, 0.0),


point K′ (−1.892a+29.443, 0.0, 0.892a+70.557),


point A (0.0085a2−1.8102a+67.1, 0.0, −0.0085a2+0.8102a+32.9),


point B (0.0, 0.0012a2−1.1659a+52.95, −0.0012a2+0.1659a+47.05), and


point W (0.0, 100.0−a, 0.0),


or on the straight lines JK′, K′A, and AB (excluding point J, point B, and point W).


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP and having a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) and a coefficient of performance (COP) that are equivalent to those of R410A.


A refrigeration cycle apparatus according to a seventeenth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane(R32), and 2,3,3,3-tetrafluoro-1-propene (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 U, JN, NE, and EI that connect the following 4 points:


point I (72.0, 0.0, 28.0),


point J (48.5, 18.3, 33.2),


point N (27.7, 18.2, 54.1), and


point E (58.3, 0.0, 41.7),


or on these line segments (excluding the points on the line segment EI;


the line segment U is represented by coordinates (0.0236y2−1.7616y+72.0, y, −0.0236y2+0.7616y+28.0);


the line segment NE is represented by coordinates (0.012y2−1.9003y+58.3, y, −0.012y2+0.9003y+41.7); and


the line segments JN and EI are straight lines.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP, having a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) that is equivalent to that of R410A, and being classified with lower flammability (class 2L) based on the standard of American Society of Heating, Refrigerating and Air Conditioning Engineers (ASHRAE).


A refrigeration cycle apparatus according to an eighteenth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises 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 MM′, M′N, NV, VG, and GM that connect the following 5 points:


point M (52.6, 0.0, 47.4),


point M′(39.2, 5.0, 55.8),


point N (27.7, 18.2, 54.1),


point V (11.0, 18.1, 70.9), and


point G (39.6, 0.0, 60.4),


or on these line segments (excluding the points on the line segment GM);


the line segment MM′ is represented by coordinates (0.132y2−3.34y+52.6, y, −0.132y2+2.34y+47.4);


the line segment M′N is represented by coordinates (0.0596y2−2.2541y+48.98, y, −0.0596y2+1.2541y+51.02);


the line segment VG is represented by coordinates (0.0123y2−1.8033y+39.6, y, −0.0123y2+0.8033y+60.4); and


the line segments NV and GM are straight lines.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP, having a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) that is equivalent to that of R410A, and being classified with lower flammability (class 2L) based on the standard of American Society of Heating, Refrigerating and Air Conditioning Engineers (ASHRAE).


A refrigeration cycle apparatus according to a nineteenth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises 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 ON, NU, and UO that connect the following 3 points:


point O (22.6, 36.8, 40.6),


point N (27.7, 18.2, 54.1), and


point U (3.9, 36.7, 59.4),


or on these line segments;


the line segment ON is represented by coordinates (0.0072y2−0.6701y+37.512, y, −0.0072y2−0.3299y+62.488);


the line segment NU is represented by coordinates (0.0083y2−1.7403y+56.635, y, −0.0083y2+0.7403y+43.365); and


the line segment UO is a straight line.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP, having a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) that is equivalent to that of R410A, and being classified with lower flammability (class 2L) based on the standard of American Society of Heating, Refrigerating and Air Conditioning Engineers (ASHRAE).


A refrigeration cycle apparatus according to a twentieth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises 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 QR, RT, TL, LK, and KQ that connect the following 5 points:


point Q (44.6, 23.0, 32.4),


point R (25.5, 36.8, 37.7),


point T (8.6, 51.6, 39.8),


point L (28.9, 51.7, 19.4), and


point K (35.6, 36.8, 27.6),


or on these line segments;


the line segment QR is represented by coordinates (0.0099y2−1.975y+84.765, y, −0.0099y2+0.975y+15.235);


the line segment RT is represented by coordinates (0.0082y2−1.8683y+83.126, y, −0.0082y2+0.8683y+16.874);


the line segment LK is represented by coordinates (0.0049y2−0.8842y+61.488, y, −0.0049y2−0.1158y+38.512);


the line segment KQ is represented by coordinates (0.0095y2−1.2222y+67.676, y, −0.0095y2+0.2222y+32.324); and


the line segment TL is a straight line.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP, having a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) that is equivalent to that of R410A, and being classified with lower flammability (class 2L) based on the standard of American Society of Heating, Refrigerating and Air Conditioning Engineers (ASHRAE).


A refrigeration cycle apparatus according to a twenty first aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises 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 PS, ST, and TP that connect the following 3 points:


point P (20.5, 51.7, 27.8),


point S (21.9, 39.7, 38.4), and


point T (8.6, 51.6, 39.8),


or on these line segments;


the line segment PS is represented by coordinates (0.0064y2−0.7103y+40.1, y, −0.0064y2−0.2897y+59.9);


the line segment ST is represented by coordinates (0.0082y2−1.8683y+83.126, y, −0.0082y2+0.8683y+16.874); and


the line segment TP is a straight line.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP, having a refrigeration capacity (may be referred to as “cooling capacity” or “capacity”) that is equivalent to that of R410A, and being classified with lower flammability (class 2L) based on the standard of American Society of Heating, Refrigerating and Air Conditioning Engineers (ASHRAE).


A refrigeration cycle apparatus according to a twenty second aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), trifluoroethylene (HFO-1123), and difluoromethane (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 IK, KB′, B′H, HR, RG, and GI that connect the following 6 points:


point I (72.0, 28.0, 0.0),


point K (48.4, 33.2, 18.4),


point B′ (0.0, 81.6, 18.4),


point H (0.0, 84.2, 15.8),


point R (23.1, 67.4, 9.5), and


point G (38.5, 61.5, 0.0),


or on these line segments (excluding the points on the line segments B′H and GI);


the line segment IK is represented by coordinates (0.025z2−1.7429z+72.00, −0.025z2+0.7429z+28.0, z),


the line segment HR is represented by coordinates (−0.3123z2+4.234z+11.06, 0.3123z2−5.234z+88.94, z),


the line segment RG is represented by coordinates (−0.0491z2−1.1544z+38.5, 0.0491z2+0.1544z+61.5, z), and


the line segments KB′ and GI are straight lines.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP and having a coefficient of performance (COP) that is equivalent to that of R410A.


A refrigeration cycle apparatus according to a twenty third aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises 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 U, JR, RG, and GI that connect the following 4 points:


point I (72.0, 28.0, 0.0),


point J (57.7, 32.8, 9.5),


point R (23.1, 67.4, 9.5), and


point G (38.5, 61.5, 0.0),


or on these line segments (excluding the points on the line segment GI);


the line segment U is represented by coordinates (0.025z2−1.7429z+72.0, −0.025z2+0.7429z+28.0, z),


the line segment RG is represented by coordinates (−0.0491z2−1.1544z+38.5, 0.0491z2+0.1544z+61.5, z), and


the line segments JR and GI are straight lines.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP and having a coefficient of performance (COP) that is equivalent to that of R410A.


A refrigeration cycle apparatus according to a twenty fourth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises 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 MP, PB′, B′H, HR, RG, and GM that connect the following 6 points:


point M (47.1, 52.9, 0.0),


point P (31.8, 49.8, 18.4),


point B′ (0.0, 81.6, 18.4),


point H (0.0, 84.2, 15.8),


point R (23.1, 67.4, 9.5), and


point G (38.5, 61.5, 0.0),


or on these line segments (excluding the points on the line segments B′H and GM);


the line segment MP is represented by coordinates (0.0083z2−0.984z+47.1, −0.0083z2−0.016z+52.9, z),


the line segment HR is represented by coordinates (−0.3123z2+4.234z+11.06, 0.3123z2−5.234z+88.94, z),


the line segment RG is represented by coordinates (−0.0491z2−1.1544z+38.5, 0.0491z2+0.1544z+61.5, z), and


the line segments PB′ and GM are straight lines.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP and having a coefficient of performance (COP) that is equivalent to that of R410A.


A refrigeration cycle apparatus according to a twenty fifth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises 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 MN, NR, RG, and GM that connect the following 4 points:


point M (47.1, 52.9, 0.0),


point N (38.5, 52.1, 9.5),


point R (23.1, 67.4, 9.5), and


point G (38.5, 61.5, 0.0),


or on these line segments (excluding the points on the line segment GM);


the line segment MN is represented by coordinates (0.0083z2−0.984z+47.1, −0.0083z2−0.016z+52.9, z),


the line segment RG is represented by coordinates (−0.0491z2−1.1544z+38.5, 0.0491z2+0.1544z+61.5, z), and


the line segments JR and GI are straight lines.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP and having a coefficient of performance (COP) that is equivalent to that of R410A.


A refrigeration cycle apparatus according to a twenty sixth aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises 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 PS, ST, and TP that connect the following 3 points:


point P (31.8, 49.8, 18.4),


point S (25.4, 56.2, 18.4), and


point T (34.8, 51.0, 14.2),


or on these line segments;


the line segment ST is represented by coordinates (−0.0982z2+0.9622z+40.931, 0.0982z2−1.9622z+59.069, z),


the line segment TP is represented by coordinates (0.0083z2−0.984z+47.1, −0.0083z2−0.016z+52.9, z), and


the line segment PS is a straight line.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP and having a coefficient of performance (COP) that is equivalent to that of R410A.


A refrigeration cycle apparatus according to a twenty seventh aspect is the refrigeration cycle apparatus according to any of the first through fourth aspects, wherein


the refrigerant comprises 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 QB″, B″D, DU, and UQ that connect the following 4 points:


point Q (28.6, 34.4, 37.0),


point B″ (0.0, 63.0, 37.0),


point D (0.0, 67.0, 33.0), and


point U (28.7, 41.2, 30.1),


or on these line segments (excluding the points on the line segment B″D);


the line segment DU is represented by coordinates (−3.4962z2+210.71z−3146.1, 3.4962z2−211.71z+3246.1, z),


the line segment UQ is represented by coordinates (0.0135z2−0.9181z+44.133, −0.0135z2−0.0819z+55.867, z), and


the line segments QB″ and B″D are straight lines.


The refrigeration cycle apparatus can improve the operation efficiency of a refrigeration cycle by using a refrigerant having a sufficiently low GWP and having a coefficient of performance (COP) that is equivalent to that of R410A.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a schematic view of an instrument used for a flammability test.



FIG. 2 is a diagram showing points A to T and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is 100 mass %.



FIG. 3 is a diagram showing points A to C, D′, G, I, J, and K′, 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−a) mass %.



FIG. 4 is a diagram showing points A to C, D′, G, I, J, and K′, 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 92.9 mass % (the content of R32 is 7.1 mass %).



FIG. 5 is a diagram showing points A to C, D′, G, I, J, K′, and W, 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 88.9 mass % (the content of R32 is 11.1 mass %).



FIG. 6 is a diagram showing points A, B, G, I, J, K′, and W, 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 85.5 mass % (the content of R32 is 14.5 mass %).



FIG. 7 is a diagram showing points A, B, G, I, J, K′, and W, 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 81.8 mass % (the content of R32 is 18.2 mass %).



FIG. 8 is a diagram showing points A, B, G, I, J, K′, and W, 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 78.1 mass % (the content of R32 is 21.9 mass %).



FIG. 9 is a diagram showing points A, B, G, I, J, K′, and W, 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 73.3 mass % (the content of R32 is 26.7 mass %).



FIG. 10 is a diagram showing points A, B, G, I, J, K′, and W, 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 70.7 mass % (the content of R32 is 29.3 mass %).



FIG. 11 is a diagram showing points A, B, G, I, J, K′, and W, 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 63.3 mass % (the content of R32 is 36.7 mass %).



FIG. 12 is a diagram showing points A, B, G, I, J, K′, and W, 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 55.9 mass % (the content of R32 is 44.1 mass %).



FIG. 13 is a diagram showing points A, B, G, I, J, K′, and W, 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 52.2 mass % (the content of R32 is 47.8 mass %).



FIG. 14 is a view showing points A to C, E, G, and I to W; and line segments that connect points A to C, E, G, and I to W in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass %.



FIG. 15 is a view showing points A to U; and line segments that connect the points in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R32 is 100 mass %.



FIG. 16 is a schematic structural view of a refrigerant circuit according to a first embodiment.



FIG. 17 is a schematic control block structural view of a refrigeration cycle apparatus according to the first embodiment.



FIG. 18 is a schematic structural view of a refrigerant circuit according to Modification B of the first embodiment.



FIG. 19 is a side sectional view showing a schematic structure of a compressor according to the Modification B of the first embodiment.



FIG. 20 is a schematic structural view of a refrigerant circuit according to a second embodiment.



FIG. 21 is a schematic control block structural view of a refrigeration cycle apparatus according to the second embodiment.



FIG. 22 is a side sectional view showing a schematic structure of a compressor according to the second embodiment.



FIG. 23 is a plan sectional view showing the vicinity of a cylinder chamber of the compressor according to the second embodiment.



FIG. 24 is a plan sectional view of a piston of the compressor according to the second embodiment.





DESCRIPTION OF EMBODIMENTS
(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. 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.


In the present specification, a refrigerant having a “WCF lower flammability” means that the most flammable composition (worst case of formulation for flammability: WCF) has a burning velocity of 10 cm/s or less according to the US ANSI/ASHRAE Standard 34-2013. Further, in the present specification, a refrigerant having “ASHRAE lower flammability” means that the burning velocity of WCF is 10 cm/s or less, that the most flammable fraction composition (worst case of fractionation for flammability: WCFF), which is specified by performing a leakage test during storage, shipping, or use based on ANSI/ASHRAE 34-2013 using WCF, has a burning velocity of 10 cm/s or less, and that flammability classification according to the US ANSI/ASHRAE Standard 34-2013 is determined to classified as be “Class 2L.”


In the present specification, a refrigerant having an “RCL of x % or more” means that the refrigerant has a refrigerant concentration limit (RCL), calculated in accordance with the US ANSI/ASHRAE Standard 34-2013, of x % or more. RCL refers to a concentration limit in the air in consideration of safety factors. RCL is an index for reducing the risk of acute toxicity, suffocation, and flammability in a closed space where humans are present. RCL is determined in accordance with the ASHRAE Standard. More specifically, RCL is the lowest concentration among the acute toxicity exposure limit (ATEL), the oxygen deprivation limit (ODL), and the flammable concentration limit (FCL), which are respectively calculated in accordance with sections 7.1.1, 7.1.2, and 7.1.3 of the ASHRAE Standard.


In the present specification, temperature glide refers to an absolute value of the difference between the initial temperature and the end temperature in the phase change process of a composition containing the refrigerant of the present disclosure in the heat exchanger of a refrigerant system.


(2) Refrigerant

(2-1) Refrigerant Component


Any one of various refrigerants such as refrigerant A, refrigerant B, refrigerant C, refrigerant D, and refrigerant E, details of these refrigerant are to be mentioned later, can be used as the refrigerant.


(2-2) Use of Refrigerant


The refrigerant 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 HFC refrigerant such as R410A, R407C and R404 etc, or HCFC refrigerant such as R22 etc.


(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 %.


(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. A 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.


(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. Preferably, a compound that cannot be an impurity inevitably mixed in the refrigerant of the present disclosure is selected as the tracer.


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 fluorocarbon, 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)


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


The tracer compound may be present in the refrigerant composition at a total concentration of about 10 parts per million (ppm) to about 1000 ppm. Preferably, the tracer compound is present in the refrigerant composition at a total concentration of about 30 ppm to about 500 ppm, and most preferably, the tracer compound is present at a total concentration of about 50 ppm to about 300 ppm.


(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.


(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.


(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.


(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.


(4-1) Refrigeration Oil


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.


(4-2) Compatibilizing Agent


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.


(5) Various Refrigerants

Hereinafter, the refrigerants A to E, which are the refrigerants used in the present embodiment, will be described in detail.


In addition, each description of the following refrigerant A, refrigerant B, refrigerant C, refrigerant D, and refrigerant E is each independent. The alphabet which shows a point or a line segment, the number of an Examples, and the number of a comparative examples are all independent of each other among the refrigerant A, the refrigerant B, the refrigerant C, the refrigerant D, and the refrigerant E. For example, the first embodiment of the refrigerant A and the first embodiment of the refrigerant B are different embodiment from each other.


(5-1) Refrigerant A


The refrigerant A 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 A 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 A 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 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


Preferable refrigerant A is as follows:


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 AA′, A′B, BD, DC′, C′C, CO, and OA that connect the following 7 points:


point A (68.6, 0.0, 31.4),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point D (0.0, 80.4, 19.6),


point C′ (19.5, 70.5, 10.0),


point C (32.9, 67.1, 0.0), and


point O (100.0, 0.0, 0.0),


or on the above line segments (excluding the points on the line CO);


the line segment AA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3,


the line segment DC′ is represented by coordinates (x, 0.0082x2−0.6671x+80.4, −0.0082x2−0.3329x+19.6),


the line segment C′C is represented by coordinates (x, 0.0067x2−0.6034x+79.729, −0.0067x2−0.3966x+20.271), and


the line segments BD, CO, and OA are straight lines.


When the requirements above are satisfied, the refrigerant according to the present disclosure has a refrigerating capacity ratio of 85% or more relative to that of R410A, and a COP of 92.5% or more relative to that of R410A.


When the mass % of HFO-1132(E), HFO-1123, and R1234yf, based on their sum in the refrigerant A according to the present disclosure is respectively represented by x, y, and z, the refrigerant is preferably a refrigerant wherein 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 GI, IA, AA′, A′B, BD, DC′, C′C, and CG that connect the following 8 points:


point G (72.0, 28.0, 0.0),


point I (72.0, 0.0, 28.0),


point A (68.6, 0.0, 31.4),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point D (0.0, 80.4, 19.6),


point C′ (19.5, 70.5, 10.0), and


point C (32.9, 67.1, 0.0),


or on the above line segments (excluding the points on the line segment CG);


the line segment AA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment DC′ is represented by coordinates (x, 0.0082x2−0.6671x+80.4, −0.0082x2−0.3329x+19.6),


the line segment C′C is represented by coordinates (x, 0.0067x2−0.6034x+79.729, −0.0067x2−0.3966x+20.271), and


the line segments GI, IA, BD, and CG are straight lines.


When the requirements above are satisfied, the refrigerant A according to the present disclosure has a refrigerating capacity ratio of 85% or more relative to that of R410A, and a COP of 92.5% or more relative to that of R410A; furthermore, the refrigerant A has a WCF lower flammability according to the ASHRAE Standard (the WCF composition has a burning velocity of 10 cm/s or less).


When the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum in the refrigerant according to the present disclosure is respectively represented by x, y, and z, the refrigerant is preferably a refrigerant wherein 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 JP, PN, NK, KA′, A′B, BD, DC′, C′C, and CJ that connect the following 9 points:


point J (47.1, 52.9, 0.0),


point P (55.8, 42.0, 2.2),


point N (68.6, 16.3, 15.1),


point K (61.3, 5.4, 33.3),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point D (0.0, 80.4, 19.6),


point C′ (19.5, 70.5, 10.0), and


point C (32.9, 67.1, 0.0),


or on the above line segments (excluding the points on the line segment CJ);


the line segment PN is represented by coordinates (x, −0.1135x2+12.112x−280.43, 0.1135x2−13.112x+380.43),


the line segment NK is represented by coordinates (x, 0.2421x2−29.955x+931.91, −0.2421x2+28.955x−831.91),


the line segment KA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment DC′ is represented by coordinates (x, 0.0082x2−0.6671x+80.4, −0.0082x2−0.3329x+19.6),


the line segment C′C is represented by coordinates (x, 0.0067x2−0.6034x+79.729, −0.0067x2−0.3966x+20.271), and


the line segments JP, BD, and CG are straight lines.


When the requirements above are satisfied, the refrigerant A according to the present disclosure has a refrigerating capacity ratio of 85% or more relative to that of R410A, and a COP of 92.5% or more relative to that of R410A; furthermore, the refrigerant exhibits a lower flammability (Class 2L) according to the ASHRAE Standard (the WCF composition and the WCFF composition have a burning velocity of 10 cm/s or less).


When the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum in the refrigerant according to the present disclosure is respectively represented by x, y, and z, the refrigerant is preferably a refrigerant wherein 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 JP, PL, LM, MA′, A′B, BD, DC′, C′C, and CJ that connect the following 9 points:


point J (47.1, 52.9, 0.0),


point P (55.8, 42.0, 2.2),


point L (63.1, 31.9, 5.0),


point M (60.3, 6.2, 33.5),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point D (0.0, 80.4, 19.6),


point C′ (19.5, 70.5, 10.0), and


point (32.9, 67.1, 0.0),


or on the above line segments (excluding the points on the line segment CJ);


the line segment PL is represented by coordinates (x, −0.1135x2+12.112x−280.43, 0.1135x2−13.112x+380.43),


the line segment MA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment DC′ is represented by coordinates (x, 0.0082x2−0.6671x+80.4, −0.0082x2−0.3329x+19.6),


the line segment C′C is represented by coordinates (x, 0.0067x2−0.6034x+79.729, −0.0067x2−0.3966x+20.271), and


the line segments JP, LM, BD, and CG are straight lines.


When the requirements above are satisfied, the refrigerant according to the present disclosure has a refrigerating capacity ratio of 85% or more relative to that of R410A, and a COP of 92.5% or more relative to that of R410A; furthermore, the refrigerant has an RCL of 40 g/m3 or more.


When the mass % of HFO-1132(E), HFO-1123, and R1234yf based on their sum in the refrigerant A according to the present disclosure is respectively represented by x, y, and z, the refrigerant is preferably a refrigerant wherein 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 PL, LM, MA′, A′B, BF, FT, and TP that connect the following 7 points:


point P (55.8, 42.0, 2.2),


point L (63.1, 31.9, 5.0),


point M (60.3, 6.2, 33.5),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point F (0.0, 61.8, 38.2), and


point T (35.8, 44.9, 19.3),


or on the above line segments (excluding the points on the line segment BF);


the line segment PL is represented by coordinates (x, −0.1135x2+12.112x−280.43, 0.1135x2−13.112x+380.43),


the line segment MA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment FT is represented by coordinates (x, 0.0078x2−0.7501x+61.8, −0.0078x2−0.2499x+38.2),


the line segment TP is represented by coordinates (x, 0.00672x2−0.7607x+63.525, −0.00672x2−0.2393x+36.475), and


the line segments LM and BF are straight lines.


When the requirements above are satisfied, the refrigerant according to the present disclosure has a refrigerating capacity ratio of 85% or more relative to that of R410A, and a COP of 95% or more relative to that of R410A; furthermore, the refrigerant has an RCL of 40 g/m3 or more.


The refrigerant A 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 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 PL, LQ, QR, and RP that connect the following 4 points:


point P (55.8, 42.0, 2.2),


point L (63.1, 31.9, 5.0),


point Q (62.8, 29.6, 7.6), and


point R (49.8, 42.3, 7.9),


or on the above line segments;


the line segment PL is represented by coordinates (x, −0.1135x2+12.112x−280.43, 0.1135x2−13.112x+380.43),


the line segment RP is represented by coordinates (x, 0.00672x2−0.7607x+63.525, −0.00672x2−0.2393x+36.475), and


the line segments LQ and QR are straight lines.


When the requirements above are satisfied, the refrigerant according to the present disclosure has a COP of 95% or more relative to that of R410A, and an RCL of 40 g/m3 or more, furthermore, the refrigerant has a condensation temperature glide of 1° C. or less.


The refrigerant A 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 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 SM, MA′, A′B, BF, FT, and TS that connect the following 6 points:


point S (62.6, 28.3, 9.1),


point M (60.3, 6.2, 33.5),


point A′(30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point F (0.0, 61.8, 38.2), and


point T (35.8, 44.9, 19.3),


or on the above line segments,


the line segment MA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment FT is represented by coordinates (x, 0.0078x2−0.7501x+61.8, −0.0078x2−0.2499x+38.2),


the line segment TS is represented by coordinates (x, −0.0017x2−0.7869x+70.888, −0.0017x2−0.2131x+29.112), and


the line segments SM and BF are straight lines.


When the requirements above are satisfied, the refrigerant according to the present disclosure has a refrigerating capacity ratio of 85% or more relative to that of R410A, a COP of 95% or more relative to that of R410A, and an RCL of 40 g/m3 or more furthermore, the refrigerant has a discharge pressure of 105% or more relative to that of R410A.


The refrigerant A 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 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, 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, gh, and hO (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.


When the requirements above are satisfied, the refrigerant 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 A 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 it 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 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 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 A 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 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 A 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 of is represented by coordinates (−0.0134z2−1.0825z+56.692, 0.0134z2+0.0825z+43.308, z), and


the line segments fi and it are straight lines.


When the requirements above are satisfied, the refrigerant 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 A 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 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 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 A 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 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+0.1791z+22.407, z), and


the line segment jk is a straight line.


When the requirements above are satisfied, the refrigerant 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 according to the present disclosure may further comprise other additional refrigerants in addition to HFO-1132(E), HFO-1123, and R1234yf, as long as the above properties and effects are not impaired. In this respect, the refrigerant according to the present disclosure preferably comprises HFO-1132(E), HFO-1123, 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.


The refrigerant 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.


Additional refrigerants are not particularly limited and can be widely selected. The mixed refrigerant may contain one additional refrigerant, or two or more additional refrigerants.


(Examples of Refrigerant A)


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


The GWP of R1234yf and a composition consisting of a mixed refrigerant 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 Patent Literature 1). The refrigerating capacity of R410A and compositions each comprising a mixture of HFO-1132(E), HFO-1123, and R1234yf 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.


Further, the RCL of the mixture was calculated with the LFL of HFO-1132(E) being 4.7 vol. %, the LFL of HFO-1123 being 10 vol. %, and the LFL of R1234yf being 6.2 vol. %, in accordance with the ASHRAE Standard 34-2013.


Evaporating temperature: 5° C.


Condensation temperature: 45° C.


Degree of superheating: 5 K


Degree of subcooling: 5 K


Compressor efficiency: 70%


Tables 1 to 34 show these values together with the GWP of each mixed refrigerant.

















TABLE 1








Comp.
Comp.

Example

Comp.




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


Item
Unit
Ex. 1
O
A
1
A′
3
B























HFO-1132(E)
mass %
R410A
100.0
68.6
49.0
30.6
14.1
0.0


HFO-1123
mass %

0.0
0.0
14.9
30.0
44.8
58.7


R1234yf
mass %

0.0
31.4
36.1
39.4
41.1
41.3


GWP

2088
1
2
2
2
2
2


COP ratio
% (relative
100
99.7
100.0
98.6
97.3
96.3
95.5



to 410A)


Refrigerating
% (relative
100
98.3
85.0
85.0
85.0
85.0
85.0


capacity ratio
to 410A)


Condensation
° C.
0.1
0.00
1.98
3.36
4.46
5.15
5.35


glide


Discharge
% (relative
100.0
99.3
87.1
88.9
90.6
92.1
93.2


pressure
to 410A)


RCL
g/m3

30.7
37.5
44.0
52.7
64.0
78.6

























TABLE 2







Comp.

Example

Comp.
Comp.
Example
Comp.




Ex. 5
Example
5
Example
Ex. 6
Ex. 7
7
Ex. 8


Item
Unit
C
4
C′
6
D
E
E′
F
























HFO-1132(E)
mass %
32.9
26.6
19.5
10.9
0.0
58.0
23.4
0.0


HFO-1123
mass %
67.1
68.4
70.5
74.1
80.4
42.0
48.5
61.8


R1234yf
mass %
0.0
5.0
10.0
15.0
19.6
0.0
28.1
38.2


GWP

1
1
1
1
2
1
2
2


COP ratio
% (relative
92.5
92.5
92.5
92.5
92.5
95.0
95.0
95.0



to 410A)


Refrigerating
% (relative
107.4
105.2
102.9
100.5
97.9
105.0
92.5
86.9


capacity ratio
to 410A)


Condensation
° C.
0.16
0.52
0.94
1.42
1.90
0.42
3.16
4.80


glide


Discharge
% (relative
119.5
117.4
115.3
113.0
115.9
112.7
101.0
95.8


pressure
to 410A)


RCL
g/m3
53.5
57.1
62.0
69.1
81.3
41.9
46.3
79.0























TABLE 3







Comp.
Example
Example
Example
Example
Example




Ex. 9
8
9
10
11
12


Item
Unit
J
P
L
N
N′
K






















HFO-1132(E)
mass %
47.1
55.8
63.1
68.6
65.0
61.3


HFO-1123
mass %
52.9
42.0
31.9
16.3
7.7
5.4


R1234yf
mass %
0.0
2.2
5.0
15.1
27.3
33.3


GWP

1
1
1
1
2
2


COP ratio
% (relative
93.8
95.0
96.1
97.9
99.1
99.5



to 410A)


Refrigerating
% (relative
106.2
104.1
101.6
95.0
88.2
85.0


capacity ratio
to 410A)


Condensation
° C.
0.31
0.57
0.81
1.41
2.11
2.51


glide


Discharge
% (relative
115.8
111.9
107.8
99.0
91.2
87.7


pressure
to 410A)


RCL
g/m3
46.2
42.6
40.0
38.0
38.7
39.7
























TABLE 4







Example
Example
Example
Example
Example
Example
Example




13
14
15
16
17
18
19


Item
Unit
L
M
Q
R
S
S′
T























HFO-1132(E)
mass %
63.1
60.3
62.8
49.8
62.6
50.0
35.8


HFO-1123
mass %
31.9
6.2
29.6
42.3
28.3
35.8
44.9


R1234yf
mass %
5.0
33.5
7.6
7.9
9.1
14.2
19.3


GWP

1
2
1
1
1
1
2


COP ratio
% (relative
96.1
99.4
96.4
95.0
96.6
95.8
95.0



to 410A)









Refrigerating
% (relative
101.6
85.0
100.2
101.7
99.4
98.1
96.7


capacity ratio
to 410A)









Condensation glide
° C.
0.81
2.58
1.00
1.00
1.10
1.55
2.07


Discharge pressure
% (relative
107.8
87.9
106.0
109.6
105.0
105.0
105.0



to 410A)









RCL
g/m3
40.0
40.0
40.0
44.8
40.0
44.4
50.8




















TABLE 5







Comp.
Example
Example




Ex. 10
20
21


Item
Unit
G
H
I



















HFO-1132(E)
mass %
72.0
72.0
72.0


HFO-1123
mass %
28.0
14.0
0.0


R1234yf
mass %
0.0
14.0
28.0


GWP

1
1
2


COP ratio
% (relative
96.6
98.2
99.9



to 410A)


Refrigerating
% (relative
103.1
95.1
86.6


capacity ratio
to 410A)


Condensation
° C.
0.46
1.27
1.71


glide


Discharge
% (relative
108.4
98.7
88.6


pressure
to 410A)


RCL
g/m3
37.4
37.0
36.6

























TABLE 6







Comp.
Comp.
Example
Example
Example
Example
Example
Comp.


Item
Unit
Ex. 11
Ex. 12
22
23
24
25
26
Ex. 13
























HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


HFO-1123
mass %
85.0
75.0
65.0
55.0
45.0
35.0
25.0
15.0


R1234yf
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

1
1
1
1
1
1
1
1


COP ratio
% (relative
91.4
92.0
92.8
93.7
94.7
95.8
96.9
98.0



to 410A)










Refrigerating
% (relative
105.7
105.5
105.0
104.3
103.3
102.0
100.6
99.1


capacity ratio
to 410A)










Condensation glide
° C.
0.40
0.46
0.55
0.66
0.75
0.80
0.79
0.67


Discharge pressure
% (relative
120.1
118.7
116.7
114.3
111.6
108.7
105.6
102.5



to 410A)










RCL
g/m3
71.0
61.9
54.9
49.3
44.8
41.0
37.8
35.1

























TABLE 7







Comp.
Example
Example
Example
Example
Example
Example
Comp.


Item
Unit
Ex. 14
27
28
29
30
31
32
Ex. 15
























HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


HFO-1123
mass %
80.0
70.0
60.0
50.0
40.0
30.0
20.0
10.0


R1234yf
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


GWP

1
1
1
1
1
1
1
1


COP ratio
% (relative
91.9
92.5
93.3
94.3
95.3
96.4
97.5
98.6



to 410A)










Refrigerating
% (relative
103.2
102.9
102.4
101.5
100.5
99.2
97.8
96.2


capacity ratio
to 410A)










Condensation glide
° C.
0.87
0.94
1.03
1.12
1.18
1.18
1.09
0.88


Discharge pressure
% (relative
116.7
115.2
113.2
110.8
108.1
105.2
102.1
99.0



to 410A)










RCL
g/m3
70.5
61.6
54.6
49.1
44.6
40.8
37.7
35.0

























TABLE 8







Comp.
Example
Example
Example
Example
Example
Example
Comp.


Item
Unit
Ex. 16
33
34
35
36
37
38
Ex. 17
























HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


HFO-1123
mass %
75.0
65.0
55.0
45.0
35.0
25.0
15.0
5.0


R1234yf
mass %
15.0
15.0
15.0
15.0
15.0
15.0
15.0
15.0


GWP

1
1
1
1
1
1
1
1


COP ratio
% (relative
92.4
93.1
93.9
94.8
95.9
97.0
98.1
99.2



to 410A)










Refrigerating
% (relative
100.5
100.2
99.6
98.7
97.7
96.4
94.9
93.2


capacity ratio
to 410A)










Condensation glide
° C.
1.41
1.49
1.56
1.62
1.63
1.55
1.37
1.05


Discharge pressure
% (relative
113.1
111.6
109.6
107.2
104.5
101.6
98.6
95.5



to 410A)










RCL
g/m3
70.0
61.2
54.4
48.9
44.4
40.7
37.5
34.8
























TABLE 9







Example
Example
Example
Example
Example
Example
Example


Item
Unit
39
40
41
42
43
44
45























HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0


HFO-1123
mass %
70.0
60.0
50.0
40.0
30.0
20.0
10.0


R1234yf
mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0


GWP

2
2
2
2
2
2
2


COP ratio
% (relative
93.0
93.7
94.5
95.5
96.5
97.6
98.7



to 410A)









Refrigerating
% (relative
97.7
97.4
96.8
95.9
94.7
93.4
91.9


capacity ratio
to 410A)









Condensation glide
° C.
2.03
2.09
2.13
2.14
2.07
1.91
1.61


Discharge pressure
% (relative
109.4
107.9
105.9
103.5
100.8
98.0
95.0



to 410A)









RCL
g/m3
69.6
60.9
54.1
48.7
44.2
40.5
37.4
























TABLE 10







Example
Example
Example
Example
Example
Example
Example


Item
Unit
46
47
48
49
50
51
52























HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0


HFO-1123
mass %
65.0
55.0
45.0
35.0
25.0
15.0
5.0


R1234yf
mass %
25.0
25.0
25.0
25.0
25.0
25.0
25.0


GWP

2
2
2
2
2
2
2


COP ratio
% (relative
93.6
94.3
95.2
96.1
97.2
98.2
99.3



to 410A)









Refrigerating
% (relative
94.8
94.5
93.8
92.9
91.8
90.4
88.8


capacity ratio
to 410A)









Condensation glide
° C.
2.71
2.74
2.73
2.66
2.50
2.22
1.78


Discharge pressure
% (relative
105.5
104.0
102.1
99.7
97.1
94.3
91.4



to 410A)









RCL
g/m3
69.1
60.5
53.8
48.4
44.0
40.4
37.3























TABLE 11







Example
Example
Example
Example
Example
Example


Item
Unit
53
54
55
56
57
58






















HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0
60.0


HFO-1123
mass %
60.0
50.0
40.0
30.0
20.0
10.0


R1234yf
mass %
30.0
30.0
30.0
30.0
30.0
30.0


GWP

2
2
2
2
2
2


COP ratio
% (relative
94.3
95.0
95.9
96.8
97.8
98.9



to 410A)








Refrigerating
% (relative
91.9
91.5
90.8
89.9
88.7
87.3


capacity ratio
to 410A)








Condensation glide
° C.
3.46
3.43
3.35
3.18
2.90
2.47


Discharge pressure
% (relative
101.6
100.1
98.2
95.9
93.3
90.6



to 410A)








RCL
g/m3
68.7
60.2
53.5
48.2
43.9
40.2























TABLE 12







Example
Example
Example
Example
Example
Comp.


Item
Unit
59
60
61
62
63
Ex. 18






















HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0
60.0


HFO-1123
mass %
55.0
45.0
35.0
25.0
15.0
5.0


R1234yf
mass %
35.0
35.0
35.0
35.0
35.0
35.0


GWP

2
2
2
2
2
2


COP ratio
% (relative
95.0
95.8
96.6
97.5
98.5
99.6



to 410A)








Refrigerating
% (relative
88.9
88.5
87.8
86.8
85.6
84.1


capacity ratio
to 410A)








Condensation glide
° C.
4.24
4.15
3.96
3.67
3.24
2.64


Discharge pressure
% (relative
97.6
96.1
94.2
92.0
89.5
86.8



to 410A)








RCL
g/m3
68.2
59.8
53.2
48.0
43.7
40.1






















TABLE 13









Comp.
Comp.
Comp.


Item
Unit
Example 64
Example 65
Ex. 19
Ex. 20
Ex. 21





















HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0


HFO-1123
mass %
50.0
40.0
30.0
20.0
10.0


R1234yf
mass %
40.0
40.0
40.0
40.0
40.0


GWP

2
2
2
2
2


COP ratio
% (relative
95.9
96.6
97.4
98.3
99.2



to 410A)







Refrigerating
% (relative
85.8
85.4
84.7
83.6
82.4


capacity ratio
to 410A)







Condensation glide
° C.
5.05
4.85
4.55
4.10
3.50


Discharge pressure
% (relative
93.5
92.1
90.3
88.1
85.6



to 410A)







RCL
g/m3
67.8
59.5
53.0
47.8
43.5

























TABLE 14







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
66
67
68
69
70
71
72
73
























HFO-1132(E)
mass %
54.0
56.0
58.0
62.0
52.0
54.0
56.0
58.0


HFO-1123
mass %
41.0
39.0
37.0
33.0
41.0
39.0
37.0
35.0


R1234yf
mass %
5.0
5.0
5.0
5.0
7.0
7.0
7.0
7.0


GWP

1
1
1
1
1
1
1
1


COP ratio
% (relative
95.1
95.3
95.6
96.0
95.1
95.4
95.6
95.8



to 410A)










Refrigerating
% (relative
102.8
102.6
102.3
101.8
101.9
101.7
101.5
101.2


capacity ratio
to 410A)










Condensation glide
° C.
0.78
0.79
0.80
0.81
0.93
0.94
0.95
0.95


Discharge pressure
% (relative
110.5
109.9
109.3
108.1
109.7
109.1
108.5
107.9



to 410A)










RCL
g/m3
43.2
42.4
41.7
40.3
43.9
43.1
42.4
41.6

























TABLE 15







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
74
75
76
77
78
79
80
81
























HFO-1132(E)
mass %
60.0
62.0
61.0
58.0
60.0
62.0
52.0
54.0


HFO-1123
mass %
33.0
31.0
29.0
30.0
28.0
26.0
34.0
32.0


R1234yf
mass %
7.0
7.0
10.0
12.0
12.0
12.0
14.0
14.0


GWP

1
1
1
1
1
1
1
1


COP ratio
% (relative
96.0
96.2
96.5
96.4
96.6
96.8
96.0
96.2



to 410A)










Refrigerating
% (relative
100.9
100.7
99.1
98.4
98.1
97.8
98.0
97.7


capacity ratio
to 410A)










Condensation glide
° C.
0.95
0.95
1.18
1.34
1.33
1.32
1.53
1.53


Discharge pressure
% (relative
107.3
106.7
104.9
104.4
103.8
103.2
104.7
104.1



to 410A)










RCL
g/m3
40.9
40.3
40.5
41.5
40.8
40.1
43.6
42.9

























TABLE 16







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
82
83
84
85
86
87
88
89
























HFO-1132(E)
mass %
56.0
58.0
60.0
48.0
50.0
52.0
54.0
56.0


HFO-1123
mass %
30.0
28.0
26.0
36.0
34.0
32.0
30.0
28.0


R1234yf
mass %
14.0
14.0
14.0
16.0
16.0
16.0
16.0
16.0


GWP

1
1
1
1
1
1
1
1


COP ratio
% (relative
96.4
96.6
96.9
95.8
96.0
96.2
96.4
96.7



to 410A)










Refrigerating
% (relative
97.5
97.2
96.9
97.3
97.1
96.8
96.6
96.3


capacity ratio
to 410A)










Condensation glide
° C.
1.51
1.50
1.48
1.72
1.72
1.71
1.69
1.67


Discharge pressure
% (relative
103.5
102.9
102.3
104.3
103.8
103.2
102.7
102.1



to 410A)










RCL
g/m3
42.1
41.4
40.7
45.2
44.4
43.6
42.8
42.1

























TABLE 17







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
90
91
92
93
94
95
96
97
























HFO-1132(E)
mass %
58.0
60.0
42.0
44.0
46.0
48.0
50.0
52.0


HFO-1123
mass %
26.0
24.0
40.0
38.0
36.0
34.0
32.0
30.0


R1234yf
mass %
16.0
16.0
18.0
18.0
18.0
18.0
18.0
18.0


GWP

1
1
2
2
2
2
2
2


COP ratio
% (relative
96.9
97.1
95.4
95.6
95.8
96.0
96.3
96.5



to 410A)










Refrigerating
% (relative
96.1
95.8
96.8
96.6
96.4
96.2
95.9
95.7


capacity ratio
to 410A)










Condensation glide
° C.
1.65
1.63
1.93
1.92
1.92
1.91
1.89
1.88


Discharge pressure
% (relative
101.5
100.9
104.5
103.9
103.4
102.9
102.3
101.8



to 410A)










RCL
g/m3
41.4
40.7
47.8
46.9
46.0
45.1
44.3
43.5

























TABLE 18







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
98
99
100
101
102
103
104
105
























HFO-1132(E)
mass %
54.0
56.0
58.0
60.0
36.0
38.0
42.0
44.0


HFO-1123
mass %
28.0
26.0
24.0
22.0
44.0
42.0
38.0
36.0


R1234yf
mass %
18.0
18.0
18.0
18.0
20.0
20.0
20.0
20.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
96.7
96.9
97.1
97.3
95.1
95.3
95.7
95.9



to 410A)










Refrigerating
% (relative
95.4
95.2
94.9
94.6
96.3
96.1
95.7
95.4


capacity ratio
to 410A)










Condensation glide
° C.
1.86
1.83
1.80
1.77
2.14
2.14
2.13
2.12


Discharge pressure
% (relative
101.2
100.6
100.0
99.5
104.5
104.0
103.0
102.5



to 410A)










RCL
g/m3
42.7
42.0
41.3
40.6
50.7
49.7
47.7
46.8

























TABLE 19







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
106
107
108
109
110
111
112
113
























HFO-1132(E)
mass %
46.0
48.0
52.0
54.0
56.0
58.0
34.0
36.0


HFO-1123
mass %
34.0
32.0
28.0
26.0
24.0
22.0
44.0
42.0


R1234yf
mass %
20.0
20.0
20.0
20.0
20.0
20.0
22.0
22.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
96.1
96.3
96.7
96.9
97.2
97.4
95.1
95.3



to 410A)










Refrigerating
% (relative
95.2
95.0
94.5
94.2
94.0
93.7
95.3
95.1


capacity ratio
to 410A)










Condensation glide
° C.
2.11
2.09
2.05
2.02
1.99
1.95
2.37
2.36


Discharge pressure
% (relative
101.9
101.4
100.3
99.7
99.2
98.6
103.4
103.0



to 410A)










RCL
g/m3
45.9
45.0
43.4
42.7
41.9
41.2
51.7
50.6

























TABLE 20







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
114
115
116
117
118
119
120
121
























HFO-1132(E)
mass %
38.0
40.0
42.0
44.0
46.0
48.0
50.0
52.0


HFO-1123
mass %
40.0
38.0
36.0
34.0
32.0
30.0
28.0
26.0


R1234yf
mass %
22.0
22.0
22.0
22.0
22.0
22.0
22.0
22.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
95.5
95.7
95.9
96.1
96.4
96.6
96.8
97.0



to 410A)










Refrigerating
% (relative
94.9
94.7
94.5
94.3
94.0
93.8
93.6
93.3


capacity ratio
to 410A)










Condensation
° C.
2.36
2.35
2.33
2.32
2.30
2.27
2.25
2.21


glide











Discharge
% (relative
102.5
102.0
101.5
101.0
100.4
99.9
99.4
98.8


pressure
to 410A)










RCL
g/m3
49.6
48.6
47.6
46.7
45.8
45.0
44.1
43.4

























TABLE 21







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
122
123
124
125
126
127
128
129







HFO-1132(E)
mass %
54.0
56.0
58.0
60.0
32.0
34.0
36.0
38.0


HFO-1123
mass %
24.0
22.0
20.0
18.0
44.0
42.0
40.0
38.0


R1234yf
mass %
22.0
22.0
22.0
22.0
24.0
24.0
24.0
24.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
97.2
97.4
97.6
97.9
95.2
95.4
95.6
95.8



to 410A)










Refrigerating
% (relative
93.0
92.8
92.5
92.2
94.3
94.1
93.9
93.7


capacity ratio
to 410A)










Condensation
° C.
2.18
2.14
2.09
2.04
2.61
2.60
2.59
2.58


glide











Discharge
% (relative
98.2
97.7
97.1
96.5
102.4
101.9
101.5
101.0


pressure
to 410A)










RCL
g/m3
42.6
41.9
41.2
40.5
52.7
51.6
50.5
49.5

























TABLE 22







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
130
131
132
133
134
135
136
137
























HFO-1132(E)
mass %
40.0
42.0
44.0
46.0
48.0
50.0
52.0
54.0


HFO-1123
mass %
36.0
34.0
32.0
30.0
28.0
26.0
24.0
22.0


R1234yf
mass %
24.0
24.0
24.0
24.0
24.0
24.0
24.0
24.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
96.0
96.2
96.4
96.6
96.8
97.0
97.2
97.5



to 410A)










Refrigerating
% (relative
93.5
93.3
93.1
92.8
92.6
92.4
92.1
91.8


capacity ratio
to 410A)










Condensation
° C.
2.56
2.54
2.51
2.49
2.45
2.42
2.38
2.33


glide











Discharge
% (relative
100.5
100.0
99.5
98.9
98.4
97.9
97.3
96.8


pressure
to 410A)










RCL
g/m3
48.5
47.5
46.6
45.7
44.9
44.1
43.3
42.5

























TABLE 23







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
138
139
140
141
142
143
144
145
























HFO-1132(E)
mass %
56.0
58.0
60.0
30.0
32.0
34.0
36.0
38.0


HFO-1123
mass %
20.0
18.0
16.0
44.0
42.0
40.0
38.0
36.0


R1234yf
mass %
24.0
24.0
24.0
26.0
26.0
26.0
26.0
26.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
97.7
97.9
98.1
95.3
95.5
95.7
95.9
96.1



to 410A)










Refrigerating
% (relative
91.6
91.3
91.0
93.2
93.1
92.9
92.7
92.5


capacity ratio
to 410A)










Condensation
° C.
2.28
2.22
2.16
2.86
2.85
2.83
2.81
2.79


glide











Discharge
% (relative
96.2
95.6
95.1
101.3
100.8
100.4
99.9
99.4


pressure
to 410A)










RCL
g/m3
41.8
41.1
40.4
53.7
52.6
51.5
50.4
49.4

























TABLE 24







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
146
147
148
149
150
151
152
153
























HFO-1132(E)
mass %
40.0
42.0
44.0
46.0
48.0
50.0
52.0
54.0


HFO-1123
mass %
34.0
32.0
30.0
28.0
26.0
24.0
22.0
20.0


R1234yf
mass %
26.0
26.0
26.0
26.0
26.0
26.0
26.0
26.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
96.3
96.5
96.7
96.9
97.1
97.3
97.5
97.7



to 410A)










Refrigerating
% (relative
92.3
92.1
91.9
91.6
91.4
91.2
90.9
90.6


capacity ratio
to 410A)










Condensation
° C.
2.77
2.74
2.71
2.67
2.63
2.59
2.53
2.48


glide











Discharge
% (relative
99.0
98.5
97.9
97.4
96.9
96.4
95.8
95.3


pressure
to 410A)










RCL
g/m3
48.4
47.4
46.5
45.7
44.8
44.0
43.2
42.5

























TABLE 25







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
154
155
156
157
158
159
160
161
























HFO-1132(E)
mass %
56.0
58.0
60.0
30.0
32.0
34.0
36.0
38.0


HFO-1123
mass %
18.0
16.0
14.0
42.0
40.0
38.0
36.0
34.0


R1234yf
mass %
26.0
26.0
26.0
28.0
28.0
28.0
28.0
28.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
97.9
98.2
98.4
95.6
95.8
96.0
96.2
96.3



to 410A)










Refrigerating
% (relative
90.3
90.1
89.8
92.1
91.9
91.7
91.5
91.3


capacity ratio
to 410A)










Condensation
° C.
2.42
2.35
2.27
3.10
3.09
3.06
3.04
3.01


glide











Discharge
% (relative
94.7
94.1
93.6
99.7
99.3
98.8
98.4
97.9


pressure
to 410A)










RCL
g/m3
41.7
41.0
40.3
53.6
52.5
51.4
50.3
49.3

























TABLE 26







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
162
163
164
165
166
167
168
169
























HFO-1132(E)
mass %
40.0
42.0
44.0
46.0
48.0
50.0
52.0
54.0


HFO-1123
mass %
32.0
30.0
28.0
26.0
24.0
22.0
20.0
18.0


R1234yf
mass %
28.0
28.0
28.0
28.0
28.0
28.0
28.0
28.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
96.5
96.7
96.9
97.2
97.4
97.6
97.8
98.0



to 410A)










Refrigerating
% (relative
91.1
90.9
90.7
90.4
90.2
89.9
89.7
89.4


capacity ratio
to 410A)










Condensation
° C.
2.98
2.94
2.90
2.85
2.80
2.75
2.68
2.62


glide











Discharge
% (relative
97.4
96.9
96.4
95.9
95.4
94.9
94.3
93.8


pressure
to 410A)










RCL
g/m3
48.3
47.4
46.4
45.6
44.7
43.9
43.1
42.4

























TABLE 27







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
170
171
172
173
174
175
176
177
























HFO-1132(E)
mass %
56.0
58.0
60.0
32.0
34.0
36.0
38.0
42.0


HFO-1123
mass %
16.0
14.0
12.0
38.0
36.0
34.0
32.0
28.0


R1234yf
mass %
28.0
28.0
28.0
30.0
30.0
30.0
30.0
30.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
98.2
98.4
98.6
96.1
96.2
96.4
96.6
97.0



to 410A)










Refrigerating
% (relative
89.1
88.8
88.5
90.7
90.5
90.3
90.1
89.7


capacity ratio
to 410A)










Condensation
° C.
2.54
2.46
2.38
3.32
3.30
3.26
3.22
3.14


glide











Discharge
% (relative
93.2
92.6
92.1
97.7
97.3
96.8
96.4
95.4


pressure
to 410A)










RCL
g/m3
41.7
41.0
40.3
52.4
51.3
50.2
49.2
47.3

























TABLE 28







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
178
179
180
181
182
183
184
185
























HFO-1132(E)
mass %
44.0
46.0
48.0
50.0
52.0
54.0
56.0
58.0


HFO-1123
mass %
26.0
24.0
22.0
20.0
18.0
16.0
14.0
12.0


R1234yf
mass %
30.0
30.0
30.0
30.0
30.0
30.0
30.0
30.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
97.2
97.4
97.6
97.8
98.0
98.3
98.5
98.7



to 410A)










Refrigerating
% (relative
89.4
89.2
89.0
88.7
88.4
88.2
87.9
87.6


capacity ratio
to 410A)










Condensation
° C.
3.08
3.03
2.97
2.90
2.83
2.75
2.66
2.57


glide











Discharge
% (relative
94.9
94.4
93.9
93.3
92.8
92.3
91.7
91.1


pressure
to 410A)










RCL
g/m3
46.4
45.5
44.7
43.9
43.1
42.3
41.6
40.9

























TABLE 29







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
186
187
188
189
190
191
192
193
























HFO-1132(E)
mass %
30.0
32.0
34.0
36.0
38.0
40.0
42.0
44.0


HFO-1123
mass %
38.0
36.0
34.0
32.0
30.0
28.0
26.0
24.0


R1234yf
mass %
32.0
32.0
32.0
32.0
32.0
32.0
32.0
32.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
96.2
96.3
96.5
96.7
96.9
97.1
97.3
97.5



to 410A)










Refrigerating
% (relative
89.6
89.5
89.3
89.1
88.9
88.7
88.4
88.2


capacity ratio
to 410A)










Condensation
° C.
3.60
3.56
3.52
3.48
3.43
3.38
3.33
3.26


glide











Discharge
% (relative
96.6
96.2
95.7
95.3
94.8
94.3
93.9
93.4


pressure
to 410A)










RCL
g/m3
53.4
52.3
51.2
50.1
49.1
48.1
47.2
46.3

























TABLE 30







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
194
195
196
197
198
199
200
201
























HFO-1132(E)
mass %
46.0
48.0
50.0
52.0
54.0
56.0
58.0
60.0


HFO-1123
mass %
22.0
20.0
18.0
16.0
14.0
12.0
10.0
8.0


R1234yf
mass %
32.0
32.0
32.0
32.0
32.0
32.0
32.0
32.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
97.7
97.9
98.1
98.3
98.5
98.7
98.9
99.2



to 410A)










Refrigerating
% (relative
88.0
87.7
87.5
87.2
86.9
86.6
86.3
86.0


capacity ratio
to 410A)










Condensation
° C.
3.20
3.12
3.04
2.96
2.87
2.77
2.66
2.55


glide











Discharge
% (relative
92.8
92.3
91.8
91.3
90.7
90.2
89.6
89.1


pressure
to 410A)










RCL
g/m3
45.4
44.6
43.8
43.0
42.3
41.5
40.8
40.2

























TABLE 31







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
202
203
204
205
206
207
208
209
























HFO-1132(E)
mass %
30.0
32.0
34.0
36.0
38.0
40.0
42.0
44.0


HFO-1123
mass %
36.0
34.0
32.0
30.0
28.0
26.0
24.0
22.0


R1234yf
mass %
34.0
34.0
34.0
34.0
34.0
34.0
34.0
34.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
96.5
96.6
96.8
97.0
97.2
97.4
97.6
97.8



to 410A)










Refrigerating
% (relative
88.4
88.2
88.0
87.8
87.6
87.4
87.2
87.0


capacity ratio
to 410A)










Condensation
° C.
3.84
3.80
3.75
3.70
3.64
3.58
3.51
3.43


glide











Discharge
% (relative
95.0
94.6
94.2
93.7
93.3
92.8
92.3
91.8


pressure
to 410A)










RCL
g/m3
53.3
52.2
51.1
50.0
49.0
48.0
47.1
46.2

























TABLE 32







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
210
211
212
213
214
215
216
217
























HFO-1132(E)
mass %
46.0
48.0
50.0
52.0
54.0
30.0
32.0
34.0


HFO-1123
mass %
20.0
18.0
16.0
14.0
12.0
34.0
32.0
30.0


R1234yf
mass %
34.0
34.0
34.0
34.0
34.0
36.0
36.0
36.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
98.0
98.2
98.4
98.6
98.8
96.8
96.9
97.1



to 410A)










Refrigerating
% (relative
86.7
86.5
86.2
85.9
85.6
87.2
87.0
86.8


capacity ratio
to 410A)










Condensation
° C.
3.36
3.27
3.18
3.08
2.97
4.08
4.03
3.97


glide











Discharge
% (relative
91.3
90.8
90.3
89.7
89.2
93.4
93.0
92.6


pressure
to 410A)










RCL
g/m3
45.3
44.5
43.7
42.9
42.2
53.2
52.1
51.0

























TABLE 33







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
218
219
220
221
222
223
224
225
























HFO-1132(E)
mass %
36.0
38.0
40.0
42.0
44.0
46.0
30.0
32.0


HFO-1123
mass %
28.0
26.0
24.0
22.0
20.0
18.0
32.0
30.0


R1234yf
mass %
36.0
36.0
36.0
36.0
36.0
36.0
38.0
38.0


GWP

2
2
2
2
2
2
2
2


COP ratio
% (relative
97.3
97.5
97.7
97.9
98.1
98.3
97.1
97.2



to 410A)










Refrigerating
% (relative
86.6
86.4
86.2
85.9
85.7
85.5
85.9
85.7


capacity ratio
to 410A)










Condensation
° C.
3.91
3.84
3.76
3.68
3.60
3.50
4.32
4.25


glide











Discharge
% (relative
92.1
91.7
91.2
90.7
90.3
89.8
91.9
91.4


pressure
to 410A)










RCL
g/m3
49.9
48.9
47.9
47.0
46.1
45.3
53.1
52.0





















TABLE 34









Example
Example



Item
Unit
226
227





















HFO-1132(E)
mass %
34.0
36.0



HFO-1123
mass %
28.0
26.0



R1234yf
mass %
38.0
38.0



GWP

2
2



COP ratio
% (relative
97.4
97.6




to 410A)



Refrigerating
% (relative
85.6
85.3



capacity ratio
to 410A)



Condensation glide
° C.
4.18
4.11



Discharge pressure
% (relative
91.0
90.6




to 410A)



RCL
g/m3
50.9
49.8










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 surrounded by line segments AA′, A′B, BD, DC′, C′C, CO, and OA that connect the following 7 points:


point A (68.6, 0.0, 31.4),


point A′(30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point D (0.0, 80.4, 19.6),


point C′ (19.5, 70.5, 10.0),


point C (32.9, 67.1, 0.0), and


point O (100.0, 0.0, 0.0),


or on the above line segments (excluding the points on the line segment CO);


the line segment AA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3,


the line segment DC′ is represented by coordinates (x, 0.0082x2−0.6671x+80.4, −0.0082x2−0.3329x+19.6),


the line segment C′C is represented by coordinates (x, 0.0067x2−0.6034x+79.729, −0.0067x2−0.3966x+20.271), and


the line segments BD, CO, and OA are straight lines,


the refrigerant has a refrigerating capacity ratio of 85% or more relative to that of R410A, and a COP of 92.5% or more relative to that of R410A.


The point on the line segment AA′ was determined by obtaining an approximate curve connecting point A, Example 1, and point A′ by the least square method.


The point on the line segment A′B was determined by obtaining an approximate curve connecting point A′, Example 3, and point B by the least square method.


The point on the line segment DC′ was determined by obtaining an approximate curve connecting point D, Example 6, and point C′ by the least square method.


The point on the line segment C′C was determined by obtaining an approximate curve connecting point C′, Example 4, and point C by the least square method.


Likewise, the results indicate that when coordinates (x,y,z) are within the range of a figure surrounded by line segments AA′, A′B, BF, FT, TE, EO, and OA that connect the following 7 points:


point A (68.6, 0.0, 31.4),


point A′ (30.6, 30.0, 39.4),


point B (0.0, 58.7, 41.3),


point F (0.0, 61.8, 38.2),


point T (35.8, 44.9, 19.3),


point E (58.0, 42.0, 0.0) and


point O (100.0, 0.0, 0.0),


or on the above line segments (excluding the points on the line EO);


the line segment AA′ is represented by coordinates (x, 0.0016x2−0.9473x+57.497, −0.0016x2−0.0527x+42.503),


the line segment A′B is represented by coordinates (x, 0.0029x2−1.0268x+58.7, −0.0029x2+0.0268x+41.3),


the line segment FT is represented by coordinates (x, 0.0078x2−0.7501x+61.8, −0.0078x2−0.2499x+38.2), and


the line segment TE is represented by coordinates (x, 0.0067x2−0.7607x+63.525, −0.0067x2−0.2393x+36.475), and


the line segments BF, FO, and OA are straight lines,


the refrigerant has a refrigerating capacity ratio of 85% or more relative to that of R410A, and a COP of 95% or more relative to that of R410A.


The point on the line segment FT was determined by obtaining an approximate curve connecting three points, i.e., points T, E′, and F, by the least square method.


The point on the line segment TE was determined by obtaining an approximate curve connecting three points, i.e., points E, R, and T, by the least square method.


The results in Tables 1 to 34 clearly indicate that in a ternary composition diagram of the mixed refrigerant of HFO-1132(E), HFO-1123, and R1234yf in which the sum of these components is 100 mass %, a line segment connecting a point (0.0, 100.0, 0.0) and a point (0.0, 0.0, 100.0) is the base, the point (0.0, 100.0, 0.0) is on the left side, and the point (0.0, 0.0, 100.0) is on the right side, when coordinates (x,y,z) are on or below the line segment LM connecting point L (63.1, 31.9, 5.0) and point M (60.3, 6.2, 33.5), the refrigerant has an RCL of 40 g/m3 or more.


The results in Tables 1 to 34 clearly indicate that in a ternary composition diagram of the mixed refrigerant of HFO-1132(E), HFO-1123 and R1234yf in which their sum is 100 mass %, a line segment connecting a point (0.0, 100.0, 0.0) and a point (0.0, 0.0, 100.0) is the base, the point (0.0, 100.0, 0.0) is on the left side, and the point (0.0, 0.0, 100.0) is on the right side, when coordinates (x,y,z) are on the line segment QR connecting point Q (62.8, 29.6, 7.6) and point R (49.8, 42.3, 7.9) or on the left side of the line segment, the refrigerant has a temperature glide of 1° C. or less.


The results in Tables 1 to 34 clearly indicate that in a ternary composition diagram of the mixed refrigerant of HFO-1132(E), HFO-1123, and R1234yf in which their sum is 100 mass %, a line segment connecting a point (0.0, 100.0, 0.0) and a point (0.0, 0.0, 100.0) is the base, the point (0.0, 100.0, 0.0) is on the left side, and the point (0.0, 0.0, 100.0) is on the right side, when coordinates (x,y,z) are on the line segment ST connecting point S (62.6, 28.3, 9.1) and point T (35.8, 44.9, 19.3) or on the right side of the line segment, the refrigerant has a discharge pressure of 105% or less relative to that of 410A.


In these compositions, R1234yf contributes to reducing flammability, and suppressing deterioration of polymerization etc. Therefore, the composition preferably contains R1234yf.


Further, the burning velocity of these mixed refrigerants whose mixed formulations were adjusted to WCF concentrations 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 classified as “Class 2L (lower flammability).”


A burning velocity test was performed using the apparatus shown in FIG. 1 in the following manner. In FIG. 1, reference numeral 901 refers to a sample cell, 902 refers to a high-speed camera, 903 refers to a xenon lamp, 904 refers to a collimating lens, 905 refers to a collimating lens, and 906 refers to a ring filter. 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.


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


Tables 35 and 36 show the results.













TABLE 35





Item
Unit
G
H
I




















WCF
HFO-1132(E)
mass %
72.0
72.0
72.0



HFO-1123
mass %
28.0
9.6
0.0



R1234yf
mass %
0.0
18.4
28.0











Burning velocity (WCF)
cm/s
10
10
10























TABLE 36





Item
Unit
J
P
L
N
N′
K























WCF
HFO-
mass %
47.1
55.8
63.1
68.6
65.0
61.3



1132










(E)










HFO-
mass %
52.9
42.0
31.9
16.3
7.7
5.4



1123










R1234yf
mass %
0.0
2.2
5.0
15.1
27.3
33.3













Leak condition that results
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/


in WCFF
Shipping
Shipping
Shipping
Shipping
Shipping
Shipping,



−40° C.,
−40° C.,
−40° C.,
−40° C.,
−40° C.,
−40° C.,



92%
90%
90%
66%
12%
0%



release,
release,
release,
release,
release,
release,



liquid
liquid
gas
gas
gas
gas



phase
phase
phase
phase
phase
phase



side
side
side
side
side
side















WCFF
HFO-
mass %
72.0
72.0
72.0
72.0
72.0
72.0



1132










(E)










HFO-
mass %
28.0
17.8
17.4
13.6
12.3
9.8



1123










R1234yf
mass %
0.0
10.2
10.6
14.4
15.7
18.2














Burning
cm/s
8 or less
8 or less
8 or less
9
9
8 or less


velocity (WCF)









Burning
cm/s
10
10
10
10
10
10


velocity (WCFF)
















The results in Table 35 clearly indicate that when a mixed refrigerant of HFO-1132(E), HFO-1123, and R1234yf contains HFO-1132(E) in a proportion of 72.0 mass % or less based on their sum, the refrigerant can be determined to have a WCF lower flammability.


The results in Tables 36 clearly indicate that in a ternary composition diagram of a mixed refrigerant of HFO-1132(E), HFO-1123, and R1234yf in which their sum is 100 mass %, and a line segment connecting a point (0.0, 100.0, 0.0) and a point (0.0, 0.0, 100.0) is the base, when coordinates (x,y,z) are on or below the line segments JP, PN, and NK connecting the following 6 points:


point J (47.1, 52.9, 0.0),


point P (55.8, 42.0, 2.2),


point L (63.1, 31.9, 5.0)


point N′ (65.0, 7.7, 27.3) and


point K (61.3, 5.4, 33.3),


the refrigerant can be determined to have a WCF lower flammability, and a WCFF lower flammability.


In the diagram, the line segment PN is represented by coordinates (x, −0.1135x2+12.112x−280.43, 0.1135x2−13.112x+380.43),


and the line segment NK is represented by coordinates (x, 0.2421x2−29.955x+931.91, −0.2421x2+28.955x−831.91).


The point on the line segment PN was determined by obtaining an approximate curve connecting three points, i.e., points P, L, and N, by the least square method.


The point on the line segment NK was determined by obtaining an approximate curve connecting three points, i.e., points N, N′, and K, by the least square method.


(5-2) Refrigerant B


The refrigerant B according to the present disclosure is


a mixed refrigerant comprising trans-1,2-difluoroethylene (HFO-1132(E)) and trifluoroethylene (HFO-1123) in a total amount of 99.5 mass % or more based on the entire refrigerant, and the refrigerant comprising 62.0 mass % to 72.0 mass % or 45.1 mass % to 47.1 mass % of HFO-1132(E) based on the entire refrigerant, or


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, and the refrigerant comprising 45.1 mass % to 47.1 mass % of HFO-1132(E) based on the entire refrigerant.


The refrigerant B 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.


When the refrigerant B according to the present disclosure is a mixed refrigerant comprising 72.0 mass % or less of HFO-1132(E), it has WCF lower flammability. When the refrigerant B according to the present disclosure is a composition comprising 47.1% or less of HFO-1132(E), it has WCF lower flammability and WCFF lower flammability, and is determined to be “Class 2L,” which is a lower flammable refrigerant according to the ASHRAE standard, and which is further easier to handle.


When the refrigerant B according to the present disclosure comprises 62.0 mass % or more of HFO-1132(E), it becomes superior with a coefficient of performance of 95% or more 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. When the refrigerant B according to the present disclosure comprises 45.1 mass % or more of HFO-1132(E), it becomes superior with a coefficient of performance of 93% or more 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 B 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 according to the present disclosure preferably comprises HFO-1132(E) and HFO-1123 in a total amount of 99.75 mass % or more, and more preferably 99.9 mass % or more, based on the entire refrigerant.


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.


(Examples of Refrigerant B)


The present disclosure is described in more detail below with reference to Examples of refrigerant B. However, the refrigerant B 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 37 and 38.


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 Patent Literature 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: 5 K


Subcooling temperature: 5 K


Compressor efficiency: 70%


The composition of each mixture was defined as WCF. A leak simulation was performed using NIST Standard Reference Data Base Refleak Version 4.0 under the conditions of Equipment, Storage, Shipping, Leak, and Recharge according to the ASHRAE Standard 34-2013. The most flammable fraction was defined as WCFF.


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. Both WCF and WCFF 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. 1 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 37








Comp-











Comp-
Ex-
Comp-





Comp-




Ex-
ample
arative





arative




ample
2
Ex-
Ex-
Ex-
Ex-
Ex-
Ex-
Ex-




1
HFO-
ample
ample
ample
ample
ample
ample
ample


Item
Unit
R410A
1132E
3
1
2
3
4
5
4

























HFO-1132E
mass %

100
80
72
70
68
65
62
60


(WCF)












HFO-1132
mass %

0
20
28
30
32
35
38
40


(WCF)












GWP

2088
1
1
1
1
1
1
1
1


COP ratio
%
100
99.7
97.5
96.6
96.3
96.1
95.8
95.4
95.2



(relative












to R410A)











Refrigerating
%
100
98.3
101.9
103.1
103.4
103.8
104.1
104.5
104.8


capacity
(relative











ratio
to R410A)











Discharge
Mpa
2.73
2.71
2.89
2.96
2.98
3.00
3.02
3.04
3.06


pressure












Burning
cm/sec
Non-
20
13
10
9
9
8
8 or
8 or


velocity

flam-






less
less


(WCF)

mable


































TABLE 38















Comp-












arative




Comp-
Comp-



Comp-
Comp-
Comp-
Ex-




arative
arative



arative
arative
arative
ample




Ex-
Ex-
Ex-
Ex-
Ex-
Ex-
Ex-
Ex-
10




ample
ample
ample
ample
ample
ample
ample
ample
HFO-


Item
Unit
5
6
7
8
9
7
8
9
1123

























HFO-
mass %
50
48
47.1
46.1
45.1
43
40
25
0


1132E












(WCF)












HFO-1123
mass %
50
52
52.9
53.9
54.9
57
60
75
100


(WCF)












GWP

1
1
1
1
1
1
1
1
1


COP ratio
%
94.1
93.9
93.8
93.7
93.6
93.4
93.1
91.9
90.6



(relative












to












R410A)











Refrigerating
%
105.9
106.1
106.2
106.3
106.4
106.6
106.9
107.9
108.0


capacity
(relative











ratio
to












R410A)











Discharge
Mpa
3.14
3.16
3.16
3.17
3.18
3.20
3.21
3.31
3.39


pressure


























Leakage test
Stor-
Stor-
Stor-
Stor-
Stor-
Stor-
Stor-
Stor-



conditions (WCFF)
age/
age/
age/
age/
age/
age/
age/
age/




Ship-
Ship-
Ship-
Ship-
Ship-
Ship-
Ship-
Ship-




ping
ping
ping
ping
ping
ping
ping
ping




−40° C.,
−40° C.,
−40° C.,
−40° C.,
−40° C.,
−40° C.,
−40° C.,
−40° C.,




















92%
92%
92%
92%
92%
92%
92%
92%





release,
release,
release,
release,
release,
release,
release,
release,





liquid
liquid
liquid
liquid
liquid
liquid
liquid
liquid





phase
phase
phase
phase
phase
phase
phase
phase





side
side
side
side
side
side
side
side



HFO-
mass %
74
73
72
71
70
67
63
38



1132E












(WCFF)












HFO-1123
mass %
26
27
28
29
30
33
37
62



(WCFF)












Burning
cm/sec
8 or
8 or
8 or
8 or
8 or
8 or
8 or
8 or
5


velocity

less
less
less
less
less
less
less
less



(WCF)












Burning
cm/sec
11
10.5
10.0
9.5
9.5
8.5
8 or
8 or



velocity







less
less



(WCFF)


























ASHRAE
2
2
2L
2L
2L
2L
2L
2L
2L


flammability











classification









The compositions each comprising 62.0 mass % to 72.0 mass % of HFO-1132(E) based on the entire composition are stable while having a low GWP (GWP=1), and they ensure WCF lower flammability. Further, surprisingly, they can ensure performance equivalent to that of R410A. Moreover, compositions each comprising 45.1 mass % to 47.1 mass % of HFO-1132(E) based on the entire composition are stable while having a low GWP (GWP=1), and they ensure WCFF lower flammability. Further, surprisingly, they can ensure performance equivalent to that of R410A.


(5-3) Refrigerant C


The refrigerant C according to the present disclosure is a composition comprising trans-1,2-difluoroethylene (HFO-1132(E)), trifluoroethylene (HFO-1123), 2,3,3,3-tetrafluoro-1-propene (R1234yf), and difluoromethane (R32), and satisfies the following requirements. The refrigerant C according to the present disclosure has various properties that are desirable as an alternative refrigerant for R410A; i.e. it has a coefficient of performance and a refrigerating capacity that are equivalent to those of R410A, and a sufficiently low GWP.


Requirements


Preferable refrigerant C is as follows:


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≤11.1, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines GI, IA, AB, BD′, D′C, and CG that connect the following 6 points:


point G (0.026a2−1.7478a+72.0, −0.026a2+0.7478a+28.0, 0.0),


point I (0.026a2−1.7478a+72.0, 0.0, −0.026a2+0.7478a+28.0),


point A (0.0134a2−1.9681a+68.6, 0.0, −0.0134a2+0.9681a+31.4),


point B (0.0, 0.0144a2−1.6377a+58.7, −0.0144a2+0.6377a+41.3),


point D′ (0.0, 0.0224a2+0.968a+75.4, −0.0224a2−1.968a+24.6), and


point C (−0.2304a2−0.4062a+32.9, 0.2304a2−0.5938a+67.1, 0.0),


or on the straight lines GI, AB, and D′C (excluding point G, point I, point A, point B, point D′, and point C);






    • if 11.1<a≤18.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines GI, IA, AB, BW, and WG that connect the following 5 points:


      point G (0.02a2−1.6013a+71.105, −0.02a2+0.6013a+28.895, 0.0),


      point I (0.02a2−1.6013a+71.105, 0.0, −0.02a2+0.6013a+28.895),


      point A (0.0112a2−1.9337a+68.484, 0.0, −0.0112a2+0.9337a+31.516),


      point B (0.0, 0.0075a2−1.5156a+58.199, −0.0075a2+0.5156a+41.801) and


      point W (0.0, 100.0−a, 0.0),


      or on the straight lines GI and AB (excluding point G, point I, point A, point B, and point W);





if 18.2<a≤26.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines GI, IA, AB, BW, and WG that connect the following 5 points:


point G (0.0135a2−1.4068a+69.727, −0.0135a2+0.4068a+30.273, 0.0),


point I (0.0135a2−1.4068a+69.727, 0.0, −0.0135a2+0.4068a+30.273),


point A (0.0107a2−1.9142a+68.305, 0.0, −0.0107a2+0.9142a+31.695),


point B (0.0, 0.009a2−1.6045a+59.318, −0.009a2+0.6045a+40.682) and


point W (0.0, 100.0−a, 0.0),


or on the straight lines GI and AB (excluding point G, point I, point A, point B, and point W);


if 26.7<a≤36.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines GI, IA, AB, BW, and WG that connect the following 5 points:


point G (0.0111a2−1.3152a+68.986, −0.0111a2+0.3152a+31.014, 0.0),


point I (0.0111a2−1.3152a+68.986, 0.0, −0.0111a2+0.3152a+31.014),


point A (0.0103a2−1.9225a+68.793, 0.0, −0.0103a2+0.9225a+31.207),


point B (0.0, 0.0046a2−1.41a+57.286, −0.0046a2+0.41a+42.714) and


point W (0.0, 100.0−a, 0.0),


or on the straight lines GI and AB (excluding point G, point I, point A, point B, and point W);


and


if 36.7<a≤46.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines GI, IA, AB, BW, and WG that connect the following 5 points:


point G (0.0061a2−0.9918a+63.902, −0.0061a2−0.0082a+36.098, 0.0),


point I (0.0061a2−0.9918a+63.902, 0.0, −0.0061a2−0.0082a+36.098),


point A (0.0085a2−1.8102a+67.1, 0.0, −0.0085a2+0.8102a+32.9),


point B (0.0, 0.0012a2−1.1659a+52.95, −0.0012a2+0.1659a+47.05) and


point W (0.0, 100.0−a, 0.0),


or on the straight lines GI and AB (excluding point G, point I, point A, point B, and point W). When the refrigerant according to the present disclosure satisfies the above requirements, it has a refrigerating capacity ratio of 85% or more relative to that of R410A, and a COP ratio of 92.5% or more relative to that of R410A, and further ensures a WCF lower flammability.


The refrigerant C 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,


if 0<a≤11.1, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines JK′, K′B, BD′, D′C, and CJ that connect the following 5 points:


point J (0.0049a2−0.9645a+47.1, −0.0049a2−0.0355a+52.9, 0.0),


point K′ (0.0514a2−2.4353a+61.7, −0.0323a2+0.4122a+5.9, −0.0191a2+1.0231a+32.4),


point B (0.0, 0.0144a2−1.6377a+58.7, −0.0144a2+0.6377a+41.3),


point D′ (0.0, 0.0224a2+0.968a+75.4, −0.0224a2−1.968a+24.6), and


point C (−0.2304a2−0.4062a+32.9, 0.2304a2−0.5938a+67.1, 0.0),


or on the straight lines JK′, K′B, and D′C (excluding point J, point B, point D′, and point C);


if 11.1<a≤18.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines JK′, K′B, BW, and WJ that connect the following 4 points:


point J (0.0243a2−1.4161a+49.725, −0.0243a2+0.4161a+50.275, 0.0),


point K′ (0.0341a2−2.1977a+61.187, −0.0236a2+0.34a+5.636, −0.0105a2+0.8577a+33.177),


point B (0.0, 0.0075a2−1.5156a+58.199, −0.0075a2+0.5156a+41.801) and


point W (0.0, 100.0−a, 0.0),


or on the straight lines JK′ and K′B (excluding point J, point B, and point W);


if 18.2<a≤26.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines JK′, K′B, BW, and WJ that connect the following 4 points:


point J (0.0246a2−1.4476a+50.184, −0.0246a2+0.4476a+49.816, 0.0),


point K′ (0.0196a2−1.7863a+58.515, −0.0079a2−0.1136a+8.702, −0.0117a2+0.8999a+32.783),


point B (0.0, 0.009a2−1.6045a+59.318, −0.009a2+0.6045a+40.682) and


point W (0.0, 100.0−a, 0.0),


or on the straight lines JK′ and K′B (excluding point J, point B, and point W);


if 26.7<a≤36.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines JK′, K′A, AB, BW, and WJ that connect the following 5 points:


point J (0.0183a2−1.1399a+46.493, −0.0183a2+0.1399a+53.507, 0.0),


point K′ (−0.0051a2+0.0929a+25.95, 0.0, 0.0051a2−1.0929a+74.05),


point A (0.0103a2−1.9225a+68.793, 0.0, −0.0103a2+0.9225a+31.207),


point B (0.0, 0.0046a2−1.41a+57.286, −0.0046a2+0.41a+42.714) and


point W (0.0, 100.0−a, 0.0),


or on the straight lines JK′, K′A, and AB (excluding point J, point B, and point W); and


if 36.7<a≤46.7, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines JK′, K′A, AB, BW, and WJ that connect the following 5 points:


point J (−0.0134a2+1.0956a+7.13, 0.0134a2−2.0956a+92.87, 0.0),


point K′ (−1.892a+29.443, 0.0, 0.892a+70.557),


point A (0.0085a2−1.8102a+67.1, 0.0, −0.0085a2+0.8102a+32.9),


point B (0.0, 0.0012a2−1.1659a+52.95, −0.0012a2+0.1659a+47.05) and


point W (0.0, 100.0−a, 0.0),


or on the straight lines JK′, K′A, and AB (excluding point J, point B, and point W). When the refrigerant according to the present disclosure satisfies the above requirements, it has a refrigerating capacity ratio of 85% or more relative to that of R410A, and a COP ratio of 92.5% or more relative to that of R410A. Additionally, the refrigerant has a WCF lower flammability and a WCFF lower flammability, and is classified as “Class 2L,” which is a lower flammable refrigerant according to the ASHRAE standard.


When the refrigerant C 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 in which the sum of HFO-1132(E), HFO-1123, and R1234yf is (100−a) 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−a, 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−a, 0.0, 0.0),


or on the straight lines oa, ab′, and b′c (excluding point o and point 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−a, 0.0, 0.0),


or on the straight lines oa, ab′, and b′c (excluding point o and point 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 refrigerant according to the present disclosure meets the above requirements, 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.


The refrigerant C 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 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.


The refrigerant C according to the present disclosure may comprise HFO-1132(E), HFO-1123, 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.


Additional refrigerants are not particularly limited and can be widely selected. The mixed refrigerant may contain one additional refrigerant, or two or more additional refrigerants.


(Examples of Refrigerant C)


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


Mixed refrigerants were prepared by mixing HFO-1132(E), HFO-1123, R1234yf, and R32 at mass % based on their sum shown in Tables 39 to 96.


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 Patent Literature 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.


For each of these mixed refrigerants, the COP ratio and the refrigerating capacity ratio relative to those of R410 were obtained. Calculation was conducted under the following conditions.


Evaporating temperature: 5° C.


Condensation temperature: 45° C.


Superheating temperature: 5 K


Subcooling temperature: 5 K


Compressor efficiency: 70%


Tables 39 to 96 show the resulting values together with the GWP of each mixed refrigerant. 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



















TABLE 39







Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Ex.




Ex.
Ex. 2
Ex. 3
Ex. 4
Ex. 5
Ex. 6
Ex. 7
Ex. 8
1


Item
Unit
1
A
B
C
D′
G
I
J
K′

























HFO-
Mass %
R410A
68.6
0.0
32.9
0.0
72.0
72.0
47.1
61.7


1132 (E)












HFO-
Mass %

0.0
58.7
67.1
75.4
28.0
0.0
52.9
5.9


1123












R1234yf
Mass %

31.4
41.3
0.0
24.6
0.0
28.0
0.0
32.4


R32
Mass %

0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

2088
2
2
1
2
1
2
1
2


COP
% (relative
100
100.0
95.5
92.5
93.1
96.6
99.9
93.8
99.4


ratio
to R410A)











Refrig-
% (relative
100
85.0
85.0
107.4
95.0
103.1
86.6
106.2
85.5


erating
to R410A)











capacity












ratio

























TABLE 40







Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.





Ex. 9
Ex. 10
Ex. 11
Ex. 12
Ex. 13
Ex. 14
Ex. 15
Ex. 2


Item
Unit
A
B
C
D′
G
I
J
K′
























HFO-
Mass %
55.3
0.0
18.4
0.0
60.9
60.9
40.5
47.0


1132 (E)











HFO-
Mass %
0.0
47.8
74.5
83.4
32.0
0.0
52.4
7.2


1123











R1234yf
Mass %
37.6
45.1
0.0
9.5
0.0
32.0
0.0
38.7


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

50
50
49
49
49
50
49
50


COP
%
99.8
96.9
92.5
92.5
95.9
99.6
94.0
99.2


ratio
(relative











to











R410A)










Refrig-
%
85.0
85.0
110.5
106.0
106.5
87.7
108.9
85.5


erating
(relative










capacity
to










ratio
R410A)
























TABLE 41







Comp.
Comp.
Comp.
Comp.
Comp.
Comp.





Ex. 16
Ex. 17
Ex. 18
Ex. 19
Ex. 20
Ex. 21
Ex. 3


Item
Unit
A
B
C = D′
G
I
J
K′























HFO-
Mass %
48.4
0.0
0.0
55.8
55.8
37.0
41.0


1132 (E)










HFO-
Mass %
0.0
42.3
88.9
33.1
0.0
51.9
6.5


1123










R1234yf
Mass %
40.5
46.6
0.0
0.0
33.1
0.0
41.4


R32
Mass %
11.1
11.1
11.1
11.1
11.1
11.1
11.1


GWP

77
77
76
76
77
76
77


COP
%
99.8
97.6
92.5
95.8
99.5
94.2
99.3


ratio
(relative










to










R410A)









Refrigerating
%
85.0
85.0
112.0
108.0
88.6
110.2
85.4


capacity
(relative









ratio
to R410A)























TABLE 42







Comp.
Comp.
Comp.
Comp.
Comp.





Ex. 22
Ex. 23
Ex. 24
Ex. 25
Ex. 26
Ex. 4


Item
Unit
A
B
G
I
J
K′






















HFO-
Mass %
42.8
0.0
52.1
52.1
34.3
36.5


1132 (E)









HFO-
Mass %
0.0
37.8
33.4
0.0
51.2
5.6


1123









R1234yf
Mass %
42.7
47.7
0.0
33.4
0.0
43.4


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5


GWP

100
100
99
100
99
100


COP
%
99.9
98.1
95.8
99.5
94.4
99.5


ratio
(relative









to









R410A)








Refrig-
%
85.0
85.0
109.1
89.6
111.1
85.3


erating
(relative








capacity
to








ratio
R410A)























TABLE 43







Comp.
Comp.
Comp.
Comp.
Comp.





Ex. 27
Ex. 28
Ex. 29
Ex. 30
Ex. 31
Ex. 5


Item
Unit
A
B
G
I
J
K′






















HFO-
Mass %
37.0
0.0
48.6
48.6
32.0
32.5


1132 (E)









HFO-
Mass %
0.0
33.1
33.2
0.0
49.8
4.0


1123









R1234yf
Mass %
44.8
48.7
0.0
33.2
0.0
45.3


R32
Mass %
18.2
18.2
18.2
18.2
18.2
18.2


GWP

125
125
124
125
124
125


COP
%
100.0
98.6
95.9
99.4
94.7
99.8


ratio
(relative









to









R410A)








Refrig-
%
85.0
85.0
110.1
90.8
111.9
85.2


erating
(relative








capacity
to








ratio
R410A)























TABLE 44







Comp.
Comp.
Comp.
Comp.
Comp.





Ex. 32
Ex. 33
Ex. 34
Ex. 35
Ex. 36
Ex. 6


Item
Unit
A
B
G
I
J
K′






















HFO-
Mass %
31.5
0.0
45.4
45.4
30.3
28.8


1132 (E)









HFO-
Mass %
0.0
28.5
32.7
0.0
47.8
2.4


1123









R1234yf
Mass %
46.6
49.6
0.0
32.7
0.0
46.9


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9


GWP

150
150
149
150
149
150


COP
%
100.2
99.1
96.0
99.4
95.1
100.0


ratio
(relative









to









R410A)








Refrig-
%
85.0
85.0
111.0
92.1
112.6
85.1


erating
(relative








capacity
to








ratio
R410A)























TABLE 45







Comp.
Comp.
Comp.
Comp.
Comp.
Comp.




Ex. 37
Ex. 38
Ex. 39
Ex. 40
Ex. 41
Ex. 42


Item
Unit
A
B
G
I
J
K′






















HFO-
Mass %
24.8
0.0
41.8
41.8
29.1
24.8


1132 (E)









HFO-
Mass %
0.0
22.9
31.5
0.0
44.2
0.0


1123









R1234yf
Mass %
48.5
50.4
0.0
31.5
0.0
48.5


R32
Mass %
26.7
26.7
26.7
26.7
26.7
26.7


GWP

182
182
181
182
181
182


COP
%
100.4
99.8
96.3
99.4
95.6
100.4


ratio
(relative









to









R410A)








Refrig-
%
85.0
85.0
111.9
93.8
113.2
85.0


erating
(relative








capacity
to








ratio
R410A)























TABLE 46







Comp.
Comp.
Comp.
Comp.
Comp.
Comp.




Ex. 43
Ex. 44
Ex. 45
Ex. 46
Ex. 47
Ex. 48


Item
Unit
A
B
G
I
J
K′






















HFO-
Mass %
21.3
0.0
40.0
40.0
28.8
24.3


1132 (E)









HFO-
Mass %
0
19.9
30.7
0.0
41.9
0.0


1123









R1234yf
Mass %
49.4
50.8
0.0
30.7
0.0
46.4


R32
Mass %
29.3
29.3
29.3
29.3
29.3
29.3


GWP

200
200
198
199
198
200


COP
%
100.6
100.1
96.6
99.5
96.1
100.4


ratio
(relative









to









R410A)








Refrig-
%
85.0
85.0
112.4
94.8
113.6
86.7


erating
(relative








capacity
to








ratio
R410A)























TABLE 47







Comp.
Comp.
Comp.
Comp.
Comp.
Comp.




Ex. 49
Ex. 50
Ex. 51
Ex. 52
Ex. 53
Ex. 54


Item
Unit
A
B
G
I
J
K′






















HFO-
Mass %
12.1
0.0
35.7
35.7
29.3
22.5


1132 (E)









HFO-
Mass %
0.0
11.7
27.6
0.0
34.0
0.0


1123









R1234yf
Mass %
51.2
51.6
0.0
27.6
0.0
40.8


R32
Mass %
36.7
36.7
36.7
36.7
36.7
36.7


GWP

250
250
248
249
248
250


COP
%
101.2
101.0
96.4
99.6
97.0
100.4


ratio
(relative









to









R410A)








Refrig-
%
85.0
85.0
113.2
97.6
113.9
90.9


erating
(relative








capacity
to








ratio
R410A)























TABLE 48







Comp.
Comp.
Comp.
Comp.
Comp.
Comp.




Ex. 55
Ex. 56
Ex. 57
Ex. 58
Ex. 59
Ex. 60


Item
Unit
A
B
G
I
J
K′






















HFO-
Mass %
3.8
0.0
32.0
32.0
29.4
21.1


1132 (E)









HFO-
Mass %
0.0
3.9
23.9
0.0
26.5
0.0


1123









R1234yf
Mass %
52.1
52.0
0.0
23.9
0.0
34.8


R32
Mass %
44.1
44.1
44.1
44.1
44.1
44.1


GWP

300
300
298
299
298
299


COP
%
101.8
101.8
97.9
99.8
97.8
100.5


ratio
(relative









to









R410A)








Refrig-
%
85.0
85.0
113.7
100.4
113.9
94.9


erating
(relative








capacity
to








ratio
R410A)






















TABLE 49







Comp.
Comp.
Comp.
Comp.
Comp.




Ex. 61
Ex. 62
Ex. 63
Ex. 64
Ex. 65


Item
Unit
A = B
G
I
J
K′





















HFO-1132 (E)
Mass %
0.0
30.4
30.4
28.9
20.4


HFO-1123
Mass %
0.0
21.8
0.0
23.3
0.0


R1234yf
Mass %
52.2
0.0
21.8
0.0
31.8


R32
Mass %
47.8
47.8
47.8
47.8
47.8


GWP

325
323
324
323
324


COP ratio
% (relative
102.1
98.2
100.0
98.2
100.6



to R410A)







Refrigerating
% relative
85.0
113.8
101.8
113.9
96.8


capacity
to R410A)







ratio

























TABLE 50







Comp.











Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
66
7
8
9
10
11
12
13
























HFO-
Mass %
5.0
10.0
15.0
20.0
25.0
30.0
35.0
40.0


1132 (E)











HFO-1123
Mass %
82.9
77.9
72.9
67.9
62.9
57.9
52.9
47.9


R1234yf
Mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

49
49
49
49
49
49
49
49


COP ratio
%
92.4
92.6
92.8
93.1
93.4
93.7
94.1
94.5



(relative











to R410A)










Refrigerating
%
108.4
108.3
108.2
107.9
107.6
107.2
106.8
106.3


capacity
(relative










ratio
to R410A)

























TABLE 51











Comp.







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
14
15
16
17
67
18
19
20
























HFO-
Mass %
45.0
50.0
55.0
60.0
65.0
10.0
15.0
20.0


1132 (E)











HFO-1123
Mass %
42.9
37.9
32.9
27.9
22.9
72.9
67.9
62.9


R1234yf
Mass %
5.0
5.0
5.0
5.0
5.0
10.0
10.0
10.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

49
49
49
49
49
49
49
49


COP ratio
%
95.0
95.4
95.9
96.4
96.9
93.0
93.3
93.6



(relative to











R410A)










Refrigerating
%
105.8
105.2
104.5
103.9
103.1
105.7
105.5
105.2


capacity
(relative










ratio
to R410A)

























TABLE 52







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
21
22
23
24
25
26
27
28
























HFO-1132(E)
Mass %
25.0
30.0
35.0
40.0
45.0
50.0
55.0
60.0


HFO-1123
Mass %
57.9
52.9
47.9
42.9
37.9
32.9
27.9
22.9


R1234yf
Mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

49
49
49
49
49
49
49
49


COP ratio
% (relative
93.9
94.2
94.6
95.0
95.5
96.0
96.4
96.9



to R410A)


Refrigerating
% (relative
104.9
104.5
104.1
103.6
103.0
102.4
101.7
101.0


capacity ratio
to R410A)

























TABLE 53







Comp.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
Ex. 68
29
30
31
32
33
34
35
























HFO-1132(E)
Mass %
65.0
10.0
15.0
20.0
25.0
30.0
35.0
40.0


HFO-1123
Mass %
17.9
67.9
62.9
57.9
52.9
47.9
42.9
37.9


R1234yf
Mass %
10.0
15.0
15.0
15.0
15.0
15.0
15.0
15.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

49
49
49
49
49
49
49
49


COP ratio
% (relative
97.4
93.5
93.8
94.1
94.4
94.8
95.2
95.6



to R410A)


Refrigerating
% (relative
100.3
102.9
102.7
102.5
102.1
101.7
101.2
100.7


capacity ratio
to R410A)

























TABLE 54







Ex.
Ex.
Ex.
Ex.
Comp.
Ex.
Ex.
Ex.


Item
Unit
36
37
38
39
Ex. 69
40
41
42
























HFO-1132(E)
Mass %
45.0
50.0
55.0
60.0
65.0
10.0
15.0
20.0


HFO-1123
Mass %
32.9
27.9
22.9
17.9
12.9
62.9
57.9
52.9


R1234yf
Mass %
15.0
15.0
15.0
15.0
15.0
20.0
20.0
20.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

49
49
49
49
49
49
49
49


COP ratio
% (relative
96.0
96.5
97.0
97.5
98.0
94.0
94.3
94.6



to R410A)


Refrigerating
% (relative
100.1
99.5
98.9
98.1
97.4
100.1
99.9
99.6


capacity ratio
to R410A)

























TABLE 55







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
43
44
45
46
47
48
49
50
























HFO-1132(E)
Mass %
25.0
30.0
35.0
40.0
45.0
50.0
55.0
60.0


HFO-1123
Mass %
47.9
42.9
37.9
32.9
27.9
22.9
17.9
12.9


R1234yf
Mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
20.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

49
49
49
49
49
49
49
49


COP ratio
% (relative
95.0
95.3
95.7
96.2
96.6
97.1
97.6
98.1



to R410A)


Refrigerating
% (relative
99.2
98.8
98.3
97.8
97.2
96.6
95.9
95.2


capacity ratio
to R410A)

























TABLE 56







Comp.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
Ex. 70
51
52
53
54
55
56
57
























HFO-1132(E)
Mass %
65.0
10.0
15.0
20.0
25.0
30.0
35.0
40.0


HFO-1123
Mass %
7.9
57.9
52.9
47.9
42.9
37.9
32.9
27.9


R1234yf
Mass %
20.0
25.0
25.0
25.0
25.0
25.0
25.0
25.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

49
50
50
50
50
50
50
50


COP ratio
% (relative
98.6
94.6
94.9
95.2
95.5
95.9
96.3
96.8



to R410A)


Refrigerating
% (relative
94.4
97.1
96.9
96.7
96.3
95.9
95.4
94.8


capacity ratio
to R410A)

























TABLE 57







Ex.
Ex.
Ex.
Ex.
Comp.
Ex.
Ex.
Ex.


Item
Unit
58
59
60
61
Ex. 71
62
63
64
























HFO-1132(E)
Mass %
45.0
50.0
55.0
60.0
65.0
10.0
15.0
20.0


HFO-1123
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


R1234yf
Mass %
25.0
25.0
25.0
25.0
25.0
30.0
30.0
30.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

50
50
50
50
50
50
50
50


COP ratio
% (relative
97.2
97.7
98.2
98.7
99.2
95.2
95.5
95.8



to R410A)


Refrigerating
% (relative
94.2
93.6
92.9
92.2
91.4
94.2
93.9
93.7


capacity ratio
to R410A)

























TABLE 58







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
65
66
67
68
69
70
71
72
























HFO-1132(E)
Mass %
25.0
30.0
35.0
40.0
45.0
50.0
55.0
60.0


HFO-1123
Mass %
37.9
32.9
27.9
22.9
17.9
12.9
7.9
2.9


R1234yf
Mass %
30.0
30.0
30.0
30.0
30.0
30.0
30.0
30.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

50
50
50
50
50
50
50
50


COP ratio
% (relative
96.2
96.6
97.0
97.4
97.9
98.3
98.8
99.3



to R410A)


Refrigerating
% (relative
93.3
92.9
92.4
91.8
91.2
90.5
89.8
89.1


capacity ratio
to R410A)

























TABLE 59







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
73
74
75
76
77
78
79
80
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0


HFO-1123
Mass %
47.9
42.9
37.9
32.9
27.9
22.9
17.9
12.9


R1234yf
Mass %
35.0
35.0
35.0
35.0
35.0
35.0
35.0
35.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

50
50
50
50
50
50
50
50


COP ratio
% (relative
95.9
96.2
96.5
96.9
97.2
97.7
98.1
98.5



to R410A)


Refrigerating
% (relative
91.1
90.9
90.6
90.2
89.8
89.3
88.7
88.1


capacity ratio
to R410A)

























TABLE 60







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
81
82
83
84
85
86
87
88
























HFO-1132(E)
Mass %
50.0
55.0
10.0
15.0
20.0
25.0
30.0
35.0


HFO-1123
Mass %
7.9
2.9
42.9
37.9
32.9
27.9
22.9
17.9


R1234yf
Mass %
35.0
35.0
40.0
40.0
40.0
40.0
40.0
40.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

50
50
50
50
50
50
50
50


COP ratio
% (relative
99.0
99.4
96.6
96.9
97.2
97.6
98.0
98.4



to R410A)


Refrigerating
% (relative
87.4
86.7
88.0
87.8
87.5
87.1
86.6
86.1


capacity ratio
to R410A)

























TABLE 61







Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.
Comp.


Item
Unit
Ex. 72
Ex. 73
Ex. 74
Ex. 75
Ex. 76
Ex. 77
Ex. 78
Ex. 79
























HFO-1132(E)
Mass %
40.0
45.0
50.0
10.0
15.0
20.0
25.0
30.0


HFO-1123
Mass %
12.9
7.9
2.9
37.9
32.9
27.9
22.9
17.9


R1234yf
Mass %
40.0
40.0
40.0
45.0
45.0
45.0
45.0
45.0


R32
Mass %
7.1
7.1
7.1
7.1
7.1
7.1
7.1
7.1


GWP

50
50
50
50
50
50
50
50


COP ratio
% (relative
98.8
99.2
99.6
97.4
97.7
98.0
98.3
98.7



to R410A)


Refrigerating
% (relative
85.5
84.9
84.2
84.9
84.6
84.3
83.9
83.5


capacity ratio
to R410A)




















TABLE 62







Comp.
Comp.
Comp.


Item
Unit
Ex. 80
Ex. 81
Ex. 82



















HFO-1132(E)
Mass %
35.0
40.0
45.0


HFO-1123
Mass %
12.9
7.9
2.9


R1234yf
Mass %
45.0
45.0
45.0


R32
Mass %
7.1
7.1
7.1


GWP

50
50
50


COP ratio
% (relative
99.1
99.5
99.9



to R410A)


Refrigerating
% (relative
82.9
82.3
81.7


capacity ratio
to R410A)

























TABLE 63







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
89
90
91
92
93
94
95
96
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0


HFO-1123
Mass %
70.5
65.5
60.5
55.5
50.5
45.5
40.5
35.5


R1234yf
Mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

99
99
99
99
99
99
99
99


COP ratio
% (relative
93.7
93.9
94.1
94.4
94.7
95.0
95.4
95.8



to R410A)


Refrigerating
% (relative
110.2
110.0
109.7
109.3
108.9
108.4
107.9
107.3


capacity ratio
to R410A)

























TABLE 64







Ex.
Comp.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
97
Ex. 83
98
99
100
101
102
103
























HFO-1132(E)
Mass %
50.0
55.0
10.0
15.0
20.0
25.0
30.0
35.0


HFO-1123
Mass %
30.5
25.5
65.5
60.5
55.5
50.5
45.5
40.5


R1234yf
Mass %
5.0
5.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

99
99
99
99
99
99
99
99


COP ratio
% (relative
96.2
96.6
94.2
94.4
94.6
94.9
95.2
95.5



to R410A)


Refrigerating
% (relative
106.6
106.0
107.5
107.3
107.0
106.6
106.1
105.6


capacity ratio
to R410A)

























TABLE 65







Ex.
Ex.
Ex.
Comp.
Ex.
Ex.
Ex.
Ex.


Item
Unit
104
105
106
Ex. 84
107
108
109
110
























HFO-1132(E)
Mass %
40.0
45.0
50.0
55.0
10.0
15.0
20.0
25.0


HFO-1123
Mass %
35.5
30.5
25.5
20.5
60.5
55.5
50.5
45.5


R1234yf
Mass %
10.0
10.0
10.0
10.0
15.0
15.0
15.0
15.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

99
99
99
99
99
99
99
99


COP ratio
% (relative
95.9
96.3
96.7
97.1
94.6
94.8
95.1
95.4



to R410A)


Refrigerating
% (relative
105.1
104.5
103.8
103.1
104.7
104.5
104.1
103.7


capacity ratio
to R410A)

























TABLE 66







Ex.
Ex.
Ex.
Ex.
Ex.
Comp.
Ex.
Ex.


Item
Unit
111
112
113
114
115
Ex. 85
116
117
























HFO-1132(E)
Mass %
30.0
35.0
40.0
45.0
50.0
55.0
10.0
15.0


HFO-1123
Mass %
40.5
35.5
30.5
25.5
20.5
15.5
55.5
50.5


R1234yf
Mass %
15.0
15.0
15.0
15.0
15.0
15.0
20.0
20.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

99
99
99
99
99
99
99
99


COP ratio
% (relative
95.7
96.0
96.4
96.8
97.2
97.6
95.1
95.3



to R410A)


Refrigerating
% (relative
103.3
102.8
102.2
101.6
101.0
100.3
101.8
101.6


capacity ratio
to R410A)

























TABLE 67







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Comp.


Item
Unit
118
119
120
121
122
123
124
Ex. 86
























HFO-1132(E)
Mass %
20.0
25.0
30.0
35.0
40.0
45.0
50.0
55.0


HFO-1123
Mass %
45.5
40.5
35.5
30.5
25.5
20.5
15.5
10.5


R1234yf
Mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
20.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

99
99
99
99
99
99
99
99


COP ratio
% (relative
95.6
95.9
96.2
96.5
96.9
97.3
97.7
98.2



to R410A)


Refrigerating
% (relative
101.2
100.8
100.4
99.9
99.3
98.7
98.0
97.3


capacity ratio
to R410A)

























TABLE 68







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
125
126
127
128
129
130
131
132
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0


HFO-1123
Mass %
50.5
45.5
40.5
35.5
30.5
25.5
20.5
15.5


R1234yf
Mass %
25.0
25.0
25.0
25.0
25.0
25.0
25.0
25.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

99
99
99
99
99
99
99
99


COP ratio
% (relative
95.6
95.9
96.1
96.4
96.7
97.1
97.5
97.9



to R410A)


Refrigerating
% (relative to
98.9
98.6
98.3
97.9
97.4
96.9
96.3
95.7


capacity ratio
R410A)

























TABLE 69







Ex.
Comp.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
133
Ex. 87
134
135
136
137
138
139
























HFO-1132(E)
Mass %
50.0
55.0
10.0
15.0
20.0
25.0
30.0
35.0


HFO-1123
Mass %
10.5
5.5
45.5
40.5
35.5
30.5
25.5
20.5


R1234yf
Mass %
25.0
25.0
30.0
30.0
30.0
30.0
30.0
30.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

99
99
100
100
100
100
100
100


COP ratio
% (relative
98.3
98.7
96.2
96.4
96.7
97.0
97.3
97.7



to R410A)


Refrigerating
% (relative
95.0
94.3
95.8
95.6
95.2
94.8
94.4
93.8


capacity ratio
to R410A)

























TABLE 70







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
140
141
142
143
144
145
146
147
























HFO-1132(E)
Mass %
40.0
45.0
50.0
10.0
15.0
20.0
25.0
30.0


HFO-1123
Mass %
15.5
10.5
5.5
40.5
35.5
30.5
25.5
20.5


R1234yf
Mass %
30.0
30.0
30.0
35.0
35.0
35.0
35.0
35.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

100
100
100
100
100
100
100
100


COP ratio
% (relative
98.1
98.5
98.9
96.8
97.0
97.3
97.6
97.9



to R410A)


Refrigerating
% (relative
93.3
92.6
92.0
92.8
92.5
92.2
91.8
91.3


capacity ratio
to R410A)

























TABLE 71







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
148
149
150
151
152
153
154
155
























HFO-1132(E)
Mass %
35.0
40.0
45.0
10.0
15.0
20.0
25.0
30.0


HFO-1123
Mass %
15.5
10.5
5.5
35.5
30.5
25.5
20.5
15.5


R1234yf
Mass %
35.0
35.0
35.0
40.0
40.0
40.0
40.0
40.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

100
100
100
100
100
100
100
100


COP ratio
% (relative
98.3
98.7
99.1
97.4
97.7
98.0
98.3
98.6



to R410A)


Refrigerating
% (relative
90.8
90.2
89.6
89.6
89.4
89.0
88.6
88.2


capacity ratio
to R410A)

























TABLE 72







Ex.
Ex.
Ex.
Ex.
Ex.
Comp.
Comp.
Comp.


Item
Unit
156
157
158
159
160
Ex. 88
Ex. 89
Ex. 90
























HFO-1132(E)
Mass %
35.0
40.0
10.0
15.0
20.0
25.0
30.0
35.0


HFO-1123
Mass %
10.5
5.5
30.5
25.5
20.5
15.5
10.5
5.5


R1234yf
Mass %
40.0
40.0
45.0
45.0
45.0
45.0
45.0
45.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5
14.5
14.5
14.5


GWP

100
100
100
100
100
100
100
100


COP ratio
% (relative
98.9
99.3
98.1
98.4
98.7
98.9
99.3
99.6



to R410A)


Refrigerating
% (relative
87.6
87.1
86.5
86.2
85.9
85.5
85.0
84.5


capacity ratio
to R410A)






















TABLE 73







Comp.
Comp.
Comp.
Comp.
Comp.


Item
Unit
Ex. 91
Ex. 92
Ex. 93
Ex. 94
Ex. 95





















HFO-
Mass %
10.0
15.0
20.0
25.0
30.0


1132(E)


HFO-1123
Mass %
25.5
20.5
15.5
10.5
5.5


R1234yf
Mass %
50.0
50.0
50.0
50.0
50.0


R32
Mass %
14.5
14.5
14.5
14.5
14.5


GWP

100
100
100
100
100


COP ratio
%
98.9
99.1
99.4
99.7
100.0



(relative



to R410A)


Refrigerating
%
83.3
83.0
82.7
82.2
81.8


capacity
(relative


ratio
to R410A)

























TABLE 74







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
161
162
163
164
165
166
167
168
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0


HFO-1123
Mass %
63.1
58.1
53.1
48.1
43.1
38.1
33.1
28.1


R1234yf
Mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9
21.9
21.9


GWP

149
149
149
149
149
149
149
149


COP ratio
% (relative
94.8
95.0
95.2
95.4
95.7
95.9
96.2
96.6



to R410A)


Refrigerating
% (relative
111.5
111.2
110.9
110.5
110.0
109.5
108.9
108.3


capacity ratio
to R410A)

























TABLE 75







Comp.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
Ex. 96
169
170
171
172
173
174
175
























HFO-1132(E)
Mass %
50.0
10.0
15.0
20.0
25.0
30.0
35.0
40.0


HFO-1123
Mass %
23.1
58.1
53.1
48.1
43.1
38.1
33.1
28.1


R1234yf
Mass %
5.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9
21.9
21.9


GWP

149
149
149
149
149
149
149
149


COP ratio
% (relative
96.9
95.3
95.4
95.6
95.8
96.1
96.4
96.7



to R410A)


Refrigerating
% (relative
107.7
108.7
108.5
108.1
107.7
107.2
106.7
106.1


capacity ratio
to R410A)

























TABLE 76







Ex.
Comp.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
176
Ex. 97
177
178
179
180
181
182
























HFO-1132(E)
Mass %
45.0
50.0
10.0
15.0
20.0
25.0
30.0
35.0


HFO-1123
Mass %
23.1
18.1
53.1
48.1
43.1
38.1
33.1
28.1


R1234yf
Mass %
10.0
10.0
15.0
15.0
15.0
15.0
15.0
15.0


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9
21.9
21.9


GWP

149
149
149
149
149
149
149
149


COP ratio
% (relative
97.0
97.4
95.7
95.9
96.1
96.3
96.6
96.9



to R410A)


Refrigerating
% (relative
105.5
104.9
105.9
105.6
105.3
104.8
104.4
103.8


capacity ratio
to R410A)

























TABLE 77







Ex.
Ex.
Comp.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
183
184
Ex. 98
185
186
187
188
189
























HFO-1132(E)
Mass %
40.0
45.0
50.0
10.0
15.0
20.0
25.0
30.0


HFO-1123
Mass %
23.1
18.1
13.1
48.1
43.1
38.1
33.1
28.1


R1234yf
Mass %
15.0
15.0
15.0
20.0
20.0
20.0
20.0
20.0


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9
21.9
21.9


GWP

149
149
149
149
149
149
149
149


COP ratio
% (relative
97.2
97.5
97.9
96.1
96.3
96.5
96.8
97.1



to R410A)


Refrigerating
% (relative
103.3
102.6
102.0
103.0
102.7
102.3
101.9
101.4


capacity ratio
to R410A)

























TABLE 78







Ex.
Ex.
Ex.
Comp.
Ex.
Ex.
Ex.
Ex.


Item
Unit
190
191
192
Ex. 99
193
194
195
196
























HFO-1132(E)
Mass %
35.0
40.0
45.0
50.0
10.0
15.0
20.0
25.0


HFO-1123
Mass %
23.1
18.1
13.1
8.1
43.1
38.1
33.1
28.1


R1234yf
Mass %
20.0
20.0
20.0
20.0
25.0
25.0
25.0
25.0


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9
21.9
21.9


GWP

149
149
149
149
149
149
149
149


COP ratio
% (relative
97.4
97.7
98.0
98.4
96.6
96.8
97.0
97.3



to R410A)


Refrigerating
% (relative
100.9
100.3
99.7
99.1
100.0
99.7
99.4
98.9


capacity ratio
to R410A)

























TABLE 79







Ex.
Ex.
Ex.
Ex.
Comp.
Ex.
Ex.
Ex.


Item
Unit
197
198
199
200
Ex. 100
201
202
203
























HFO-1132(E)
Mass %
30.0
35.0
40.0
45.0
50.0
10.0
15.0
20.0


HFO-1123
Mass %
23.1
18.1
13.1
8.1
3.1
38.1
33.1
28.1


R1234yf
Mass %
25.0
25.0
25.0
25.0
25.0
30.0
30.0
30.0


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9
21.9
21.9


GWP

149
149
149
149
149
150
150
150


COP ratio
% (relative
97.6
97.9
98.2
98.5
98.9
97.1
97.3
97.6



to R410A)


Refrigerating
% (relative
98.5
97.9
97.4
96.8
96.1
97.0
96.7
96.3


capacity ratio
to R410A)

























TABLE 80







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
204
205
206
207
208
209
210
211
























HFO-1132(E)
Mass %
25.0
30.0
35.0
40.0
45.0
10.0
15.0
20.0


HFO-1123
Mass %
23.1
18.1
13.1
8.1
3.1
33.1
28.1
23.1


R1234yf
Mass %
30.0
30.0
30.0
30.0
30.0
35.0
35.0
35.0


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9
21.9
21.9


GWP

150
150
150
150
150
150
150
150


COP ratio
% (relative
97.8
98.1
98.4
98.7
99.1
97.7
97.9
98.1



to R410A)


Refrigerating
% (relative
95.9
95.4
94.9
94.4
93.8
93.9
93.6
93.3


capacity ratio
to R410A)

























TABLE 81







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
212
213
214
215
216
217
218
219
























HFO-1132(E)
Mass %
25.0
30.0
35.0
40.0
10.0
15.0
20.0
25.0


HFO-1123
Mass %
18.1
13.1
8.1
3.1
28.1
23.1
18.1
13.1


R1234yf
Mass %
35.0
35.0
35.0
35.0
40.0
40.0
40.0
40.0


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9
21.9
21.9


GWP

150
150
150
150
150
150
150
150


COP ratio
% (relative
98.4
98.7
99.0
99.3
98.3
98.5
98.7
99.0



to R410A)


Refrigerating
% (relative
92.9
92.4
91.9
91.3
90.8
90.5
90.2
89.7


capacity ratio
to R410A)

























TABLE 82







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Comp.


Item
Unit
220
221
222
223
224
225
226
Ex. 101
























HFO-1132(E)
Mass %
30.0
35.0
10.0
15.0
20.0
25.0
30.0
10.0


HFO-1123
Mass %
8.1
3.1
23.1
18.1
13.1
8.1
3.1
18.1


R1234yf
Mass %
40.0
40.0
45.0
45.0
45.0
45.0
45.0
50.0


R32
Mass %
21.9
21.9
21.9
21.9
21.9
21.9
21.9
21.9


GWP

150
150
150
150
150
150
150
150


COP ratio
% (relative
99.3
99.6
98.9
99.1
99.3
99.6
99.9
99.6



to R410A)


Refrigerating
% (relative
89.3
88.8
87.6
87.3
87.0
86.6
86.2
84.4


capacity ratio
to R410A)




















TABLE 83







Comp.
Comp.
Comp.


Item
Unit
Ex. 102
Ex. 103
Ex. 104



















HFO-1132(E)
Mass %
15.0
20.0
25.0


HFO-1123
Mass %
13.1
8.1
3.1


R1234yf
Mass %
50.0
50.0
50.0


R32
Mass %
21.9
21.9
21.9


GWP

150
150
150


COP ratio
% (relative
99.8
100.0
100.2



to R410A)


Refrigerating
% (relative
84.1
83.8
83.4


capacity ratio
to R410A)

























TABLE 84







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Comp.


Item
Unit
227
228
229
230
231
232
233
Ex. 105
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0


HFO-1123
Mass %
55.7
50.7
45.7
40.7
35.7
30.7
25.7
20.7


R1234yf
Mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


R32
Mass %
29.3
29.3
29.3
29.3
29.3
29.3
29.3
29.3


GWP

199
199
199
199
199
199
199
199



% (relative


COP ratio
to R410A)
95.9
96.0
96.2
96.3
96.6
96.8
97.1
97.3


Refrigerating
% (relative


capacity ratio
to R410A)
112.2
111.9
111.6
111.2
110.7
110.2
109.6
109.0

























TABLE 85







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Comp.


Item
Unit
234
235
236
237
238
239
240
Ex. 106
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0


HFO-1123
Mass %
50.7
45.7
40.7
35.7
30.7
25.7
20.7
15.7


R1234yf
Mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
Mass %
29.3
29.3
29.3
29.3
29.3
29.3
29.3
29.3


GWP

199
199
199
199
199
199
199
199



% (relative


COP ratio
to R410A)
96.3
96.4
96.6
96.8
97.0
97.2
97.5
97.8


Refrigerating
% (relative


capacity ratio
to R410A)
109.4
109.2
108.8
108.4
107.9
107.4
106.8
106.2

























TABLE 86







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Comp.


Item
Unit
241
242
243
244
245
246
247
Ex. 107
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0


HFO-1123
Mass %
45.7
40.7
35.7
30.7
25.7
20.7
15.7
10.7


R1234yf
Mass %
15.0
15.0
15.0
15.0
15.0
15.0
15.0
15.0


R32
Mass %
29.3
29.3
29.3
29.3
29.3
29.3
29.3
29.3


GWP

199
199
199
199
199
199
199
199


COP ratio
% (relative
96.7
96.8
97.0
97.2
97.4
97.7
97.9
98.2



to R410A)


Refrigerating
% (relative
106.6
106.3
106.0
105.5
105.1
104.5
104.0
103.4


capacity ratio
to R410A)

























TABLE 87







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Comp.


Item
Unit
248
249
250
251
252
253
254
Ex. 108
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0


HFO-1123
Mass %
40.7
35.7
30.7
25.7
20.7
15.7
10.7
5.7


R1234yf
Mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
20.0


R32
Mass %
29.3
29.3
29.3
29.3
29.3
29.3
29.3
29.3


GWP

199
199
199
199
199
199
199
199


COP ratio
% (relative
97.1
97.3
97.5
97.7
97.9
98.1
98.4
98.7



to R410A)


Refrigerating
% (relative
103.7
103.4
103.0
102.6
102.2
101.6
101.1
100.5


capacity ratio
to R410A)

























TABLE 88







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
255
256
257
258
259
260
261
262
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
40.0
10.0


HFO-1123
Mass %
35.7
30.7
25.7
20.7
15.7
10.7
5.7
30.7


R1234yf
Mass %
25.0
25.0
25.0
25.0
25.0
25.0
25.0
30.0


R32
Mass %
29.3
29.3
29.3
29.3
29.3
29.3
29.3
29.3


GWP

199
199
199
199
199
199
199
199


COP ratio
% (relative
97.6
97.7
97.9
98.1
98.4
98.6
98.9
98.1



to R410A)


Refrigerating
% (relative
100.7
100.4
100.1
99.7
99.2
98.7
98.2
97.7


capacity ratio
to R410A)

























TABLE 89







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
263
264
265
266
267
268
269
270
























HFO-1132(E)
Mass %
15.0
20.0
25.0
30.0
35.0
10.0
15.0
20.0


HFO-1123
Mass %
25.7
20.7
15.7
10.7
5.7
25.7
20.7
15.7


R1234yf
Mass %
30.0
30.0
30.0
30.0
30.0
35.0
35.0
35.0


R32
Mass %
29.3
29.3
29.3
29.3
29.3
29.3
29.3
29.3


GWP

199
199
199
199
199
200
200
200


COP ratio
% (relative
98.2
98.4
98.6
98.9
99.1
98.6
98.7
98.9



to R410A)


Refrigerating
% (relative
97.4
97.1
96.7
96.2
95.7
94.7
94.4
94.0


capacity ratio
to R410A)

























TABLE 90







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
271
272
273
274
275
276
277
278
























HFO-1132(E)
Mass %
25.0
30.0
10.0
15.0
20.0
25.0
10.0
15.0


HFO-1123
Mass %
10.7
5.7
20.7
15.7
10.7
5.7
15.7
10.7


R1234yf
Mass %
35.0
35.0
40.0
40.0
40.0
40.0
45.0
45.0


R32
Mass %
29.3
29.3
29.3
29.3
29.3
29.3
29.3
29.3


GWP

200
200
200
200
200
200
200
200


COP ratio
% (relative
99.2
99.4
99.1
99.3
99.5
99.7
99.7
99.8



to R410A)


Refrigerating
% (relative
93.6
93.2
91.5
91.3
90.9
90.6
88.4
88.1


capacity ratio
to R410A)





















TABLE 91









Comp.
Comp.


Item
Unit
Ex. 279
Ex. 280
Ex. 109
Ex. 110




















HFO-1132(E)
Mass %
20.0
10.0
15.0
10.0


HFO-1123
Mass %
5.7
10.7
5.7
5.7


R1234yf
Mass %
45.0
50.0
50.0
55.0


R32
Mass %
29.3
29.3
29.3
29.3


GWP

200
200
200
200


COP ratio
% (relative
100.0
100.3
100.4
100.9



to R410A)


Refrigerating
% (relative
87.8
85.2
85.0
82.0


capacity ratio
to R410A)

























TABLE 92







Ex.
Ex.
Ex.
Ex.
Ex.
Comp. Ex.
Ex.
Ex.


Item
Unit
281
282
283
284
285
111
286
287
























HFO-1132(E)
Mass %
10.0
15.0
20.0
25.0
30.0
35.0
10.0
15.0


HFO-1123
Mass %
40.9
35.9
30.9
25.9
20.9
15.9
35.9
30.9


R1234yf
Mass %
5.0
5.0
5.0
5.0
5.0
5.0
10.0
10.0


R32
Mass %
44.1
44.1
44.1
44.1
44.1
44.1
44.1
44.1


GWP

298
298
298
298
298
298
299
299


COP ratio
% (relative
97.8
97.9
97.9
98.1
98.2
98.4
98.2
98.2



to R410A)


Refrigerating
% (relative
112.5
112.3
111.9
111.6
111.2
110.7
109.8
109.5


capacity ratio
to R410A)

























TABLE 93







Ex.
Ex.
Ex.
Comp. Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
288
289
290
112
291
292
293
294
























HFO-1132(E)
Mass %
20.0
25.0
30.0
35.0
10.0
15.0
20.0
25.0


HFO-1123
Mass %
25.9
20.9
15.9
10.9
30.9
25.9
20.9
15.9


R1234yf
Mass %
10.0
10.0
10.0
10.0
15.0
15.0
15.0
15.0


R32
Mass %
44.1
44.1
44.1
44.1
44.1
44.1
44.1
44.1


GWP

299
299
299
299
299
299
299
299


COP ratio
% (relative
98.3
98.5
98.6
98.8
98.6
98.6
98.7
98.9



to R410A)


Refrigerating
% (relative
109.2
108.8
108.4
108.0
107.0
106.7
106.4
106.0


capacity ratio
to R410A)

























TABLE 94







Ex.
Comp. Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
295
113
296
297
298
299
300
301
























HFO-1132(E)
Mass %
30.0
35.0
10.0
15.0
20.0
25.0
30.0
10.0


HFO-1123
Mass %
10.9
5.9
25.9
20.9
15.9
10.9
5.9
20.9


R1234yf
Mass %
15.0
15.0
20.0
20.0
20.0
20.0
20.0
25.0


R32
Mass %
44.1
44.1
44.1
44.1
44.1
44.1
44.1
44.1


GWP

299
299
299
299
299
299
299
299


COP ratio
% (relative
99.0
99.2
99.0
99.0
99.2
99.3
99.4
99.4



to R410A)


Refrigerating
% (relative
105.6
105.2
104.1
103.9
103.6
103.2
102.8
101.2


capacity ratio
to R410A)

























TABLE 95







Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.
Ex.


Item
Unit
302
303
304
305
306
307
308
309
























HFO-1132(E)
Mass %
15.0
20.0
25.0
10.0
15.0
20.0
10.0
15.0


HFO-1123
Mass %
15.9
10.9
5.9
15.9
10.9
5.9
10.9
5.9


R1234yf
Mass %
25.0
25.0
25.0
30.0
30.0
30.0
35.0
35.0


R32
Mass %
44.1
44.1
44.1
44.1
44.1
44.1
44.1
44.1


GWP

299
299
299
299
299
299
299
299


COP ratio
% (relative
99.5
99.6
99.7
99.8
99.9
100.0
100.3
100.4



to R410A)


Refrigerating
% (relative
101.0
100.7
100.3
98.3
98.0
97.8
95.3
95.1


capacity ratio
to R410A)




















TABLE 96







Item
Unit
Ex. 400




















HFO-1132(E)
Mass %
10.0



HFO-1123
Mass %
5.9



R1234yf
Mass %
40.0



R32
Mass %
44.1



GWP

299



COP ratio
% (relative
100.7




to R410A)



Refrigerating
% (relative
92.3



capacity ratio
to R410A)










The above results indicate that the refrigerating capacity ratio relative to R410A is 85% or more in the following cases:


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, in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is (100−a) mass %, a straight line connecting a point (0.0, 100.0−a, 0.0) and a point (0.0, 0.0, 100.0−a) is the base, and the point (0.0, 100.0−a, 0.0) is on the left side, if 0<a≤11.1, coordinates (x,y,z) in the ternary composition diagram are on, or on the left side of, a straight line AB that connects point A (0.0134a2−1.9681a+68.6, 0.0, −0.0134a2+0.9681a+31.4) and point B (0.0, 0.0144a2-1.6377a+58.7, −0.0144a2+0.6377a+41.3);


if 11.1<a≤18.2, coordinates (x,y,z) in the ternary composition diagram are on, or on the left side of, a straight line AB that connects point A (0.0112a2−1.9337a+68.484, 0.0, −0.0112a2+0.9337a+31.516) and point B (0.0, 0.0075a2−1.5156a+58.199, −0.0075a2+0.5156a+41.801);


if 18.2a<a≤26.7, coordinates (x,y,z) in the ternary composition diagram are on, or on the left side of, a straight line AB that connects point A (0.0107a2−1.9142a+68.305, 0.0, −0.0107a2+0.9142a+31.695) and point B (0.0, 0.009a2−1.6045a+59.318, −0.009a2+0.6045a+40.682);


if 26.7<a≤36.7, coordinates (x,y,z) in the ternary composition diagram are on, or on the left side of, a straight line AB that connects point A (0.0103a2−1.9225a+68.793, 0.0, −0.0103a2+0.9225a+31.207) and point B (0.0, 0.0046a2−1.41a+57.286, −0.0046a2+0.41a+42.714); and


if 36.7<a≤46.7, coordinates (x,y,z) in the ternary composition diagram are on, or on the left side of, a straight line AB that connects point A (0.0085a2−1.8102a+67.1, 0.0, −0.0085a2+0.8102a+32.9) and point B (0.0, 0.0012a2−1.1659a+52.95, −0.0012a2+0.1659a+47.05).


Actual points having a refrigerating capacity ratio of 85% or more form a curved line that connects point A and point B in FIG. 3, and that extends toward the 1234yf side. Accordingly, when coordinates are on, or on the left side of, the straight line AB, the refrigerating capacity ratio relative to R410A is 85% or more.


Similarly, it was also found that in the ternary composition diagram, if 0<a≤11.1, when coordinates (x,y,z) are on, or on the left side of, a straight line D′C that connects point D′ (0.0, 0.0224a2+0.968a+75.4, −0.0224a2−1.968a+24.6) and point C (−0.2304a2−0.4062a+32.9, 0.2304a2−0.5938a+67.1, 0.0); or if 11.1<a≤46.7, when coordinates are in the entire region, the COP ratio relative to that of R410A is 92.5% or more.


In FIG. 3, the COP ratio of 92.5% or more forms a curved line CD. In FIG. 3, an approximate line formed by connecting three points: point C (32.9, 67.1, 0.0) and points (26.6, 68.4, 5) (19.5, 70.5, 10) where the COP ratio is 92.5% when the concentration of R1234yf is 5 mass % and 10 mass was obtained, and a straight line that connects point C and point D′ (0, 75.4, 24.6), which is the intersection of the approximate line and a point where the concentration of HFO-1132(E) is 0.0 mass % was defined as a line segment D′C. In FIG. 4, point D′(0, 83.4, 9.5) was similarly obtained from an approximate curve formed by connecting point C (18.4, 74.5, 0) and points (13.9, 76.5, 2.5) (8.7, 79.2, 5) where the COP ratio is 92.5%, and a straight line that connects point C and point D′ was defined as the straight line D′C.


The composition of each mixture was defined as WCF. A leak simulation was performed using NIST Standard Reference Database REFLEAK Version 4.0 under the conditions of Equipment, Storage, Shipping, Leak, and Recharge according to the ASHRAE Standard 34-2013. The most flammable fraction was defined as WCFF.


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


A burning velocity test was performed using the apparatus shown in FIG. 1 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.


The results are shown in Tables 97 to 104.















TABLE 97






Comp.
Comp.
Comp.
Comp.
Comp.
Comp.


Item
Ex. 6
Ex. 13
Ex. 19
Ex. 24
Ex. 29
Ex. 34























WCF
HFO-1132(E)
Mass %
72.0
60.9
55.8
52.1
48.6
45.4



HFO-1123
Mass %
28.0
32.0
33.1
33.4
33.2
32.7



R1234yf
Mass %
0.0
0.0
0.0
0
0
0



R32
Mass %
0.0
7.1
11.1
14.5
18.2
21.9














Burning velocity (WCF)
cm/s
10
10
10
10
10
10





















TABLE 98






Comp.
Comp.
Comp.
Comp.
Comp.


Item
Ex. 39
Ex. 45
Ex. 51
Ex. 57
Ex. 62






















WCF
HFO-1132(E)
Mass %
41.8
40
35.7
32
30.4



HFO-1123
Mass %
31.5
30.7
23.6
23.9
21.8



R1234yf
Mass %
0
0
0
0
0



R32
Mass %
26.7
29.3
36.7
44.1
47.8













Burning velocity (WCF)
cm/s
10
10
10
10
10






















TABLE 99






Comp.
Comp.
Comp.
Comp.
Comp.
Comp.


Item
Ex. 7
Ex. 14
Ex. 20
Ex. 25
Ex. 30
Ex. 35























WCF
HFO-1132(E)
Mass %
72.0
60.9
55.8
52.1
48.6
45.4



HFO-1123
Mass %
0.0
0.0
0.0
0
0
0



R1234yf
Mass %
28.0
32.0
33.1
33.4
33.2
32.7



R32
Mass %
0.0
7.1
11.1
14.5
18.2
21.9














Burning velocity (WCF)
cm/s
10
10
10
10
10
10





















TABLE 100






Comp.
Comp.
Comp.
Comp.
Comp.


Item
Ex. 40
Ex. 46
Ex. 52
Ex. 58
Ex. 63






















WCF
HFO-1132(E)
Mass %
41.8
40
35.7
32
30.4



HFO-1123
Mass %
0
0
0
0
0



R1234yf
Mass %
31.5
30.7
23.6
23.9
21.8



R32
Mass %
26.7
29.3
36.7
44.1
47.8













Burning velocity (WCF)
cm/s
10
10
10
10
10






















TABLE 101





Item
Comp. Ex. 8
Comp. Ex. 15
Comp. Ex. 21
Comp. Ex. 26
Comp. Ex. 31
Comp. Ex. 36























WCF
HFO-1132 (E)
Mass %
47.1
40.5
37.0
34.3
32.0
30.3



HFO-1123
Mass %
52.9
52.4
51.9
51.2
49.8
47.8



R1234yf
Mass %
0.0
0.0
0.0
0.0
0.0
0.0



R32
Mass %
0.0
7.1
11.1
14.5
18.2
21.9













Leak condition that
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/


results in WCFF
Shipping −40° C.,
Shipping −40° C.,
Shipping −40° C.,
Shipping −40° C.,
Shipping −40° C.,
Shipping −40° C.,


















92% release,
92% release,
92% release,
92% release,
92% release,
92% release,





liquid phase
liquid phase
liquid phase
liquid phase
liquid phase
liquid phase





side
side
side
side
side
side


WCFF
HFO-1132 (E)
Mass %
72.0
62.4
56.2
50.6
45.1
40.0



HFO-1123
Mass %
28.0
31.6
33.0
33.4
32.5
30.5



R1234yf
Mass %
0.0
0.0
0.0
20.4
0.0
0.0



R32
Mass %
0.0
50.9
10.8
16.0
22.4
29.5














Burning velocity
cm/s
8 or less
8 or less
8 or less
8 or less
8 or less
8 or less


(WCF)


Burning velocity
cm/s
10
10
10
10
10
10


(WCFF)





















TABLE 102






Comp.
Comp.
Comp.
Comp.
Comp.


Item
Ex. 41
Ex. 47
Ex. 53
Ex. 59
Ex. 64






















WCF
HFO-1132(E)
Mass %
29.1
28.8
29.3
29.4
28.9



HFO-1123
Mass %
44.2
41.9
34.0
26.5
23.3



R1234yf
Mass %
0.0
0.0
0.0
0.0
0.0



R32
Mass %
26.7
29.3
36.7
44.1
47.8












Leak condition that
Storage/
Storage/
Storage/
Storage/
Storage/


results in WCFF
Shipping −40°
Shipping −40°
Shipping −40°
Shipping −40°
Shipping −40°



C., 92% release,
C., 92% release,
C., 92% release,
C., 90% release,
C., 86% release,



liquid phase
liquid phase
liquid phase
gas phase
gas phase



side
side
side
side
side














WCFF
HFO-1132(E)
Mass %
34.6
32.2
27.7
28.3
27.5



HFO-1123
Mass %
26.5
23.9
17.5
18.2
16.7



R1234yf
Mass %
0.0
0.0
0.0
0.0
0.0



R32
Mass %
38.9
43.9
54.8
53.5
55.8













Burning velocity
cm/s
8 or less
8 or less
8.3
9.3
9.6


(WCF)


Burning velocity
cm/s
10
10
10
10
10


(WCFF)






















TABLE 103






Comp.
Comp.
Comp.
Comp.
Comp.
Comp.


Item
Ex. 9
Ex. 16
Ex. 22
Ex. 27
Ex. 32
Ex. 37























WCF
HFO-1132(E)
Mass %
61.7
47.0
41.0
36.5
32.5
28.8



HFO-1123
Mass %
5.9
7.2
6.5
5.6
4.0
2.4



R1234yf
Mass %
32.4
38.7
41.4
43.4
45.3
46.9



R32
Mass %
0.0
7.1
11.1
14.5
18.2
21.9













Leak condition that
Storage/
Storage/
Storage/
Storage/
Storage/
Storage/


results in WCFF
Shipping −40°
Shipping −40°
Shipping −40°
Shipping −40°
Shipping −40°
Shipping −40°



C., 0% release,
C., 0% release,
C., 0% release,
C., 92% release,
C., 0% release,
C., 0% release,



gas phase
gas phase
gas phase
liquid
gas phase
gas phase



side
side
side
phase side
side
side















WCFF
HFO-1132(E)
Mass %
72.0
56.2
50.4
46.0
42.4
39.1



HFO-1123
Mass %
10.5
12.6
11.4
10.1
7.4
4.4



R1234yf
Mass %
17.5
20.4
21.8
22.9
24.3
25.7



R32
Mass %
0.0
10.8
16.3
21.0
25.9
30.8














Burning velocity
cm/s
8 or less
8 or less
8 or less
8 or less
8 or less
8 or less


(WCF)


Burning velocity
cm/s
10
10
10
10
10
10


(WCFF)





















TABLE 104






Comp.
Comp.
Comp.
Comp.
Comp.


Item
Ex. 42
Ex. 48
Ex. 54
Ex. 60
Ex. 65






















WCF
HFO-1132(E)
Mass %
24.8
24.3
22.5
21.1
20.4



HFO-1123
Mass %
0.0
0.0
0.0
0.0
0.0



R1234yf
Mass %
48.5
46.4
40.8
34.8
31.8



R32
Mass %
26.7
29.3
36.7
44.1
47.8












Leak conditions that
Storage/
Storage/
Storage/
Storage/
Storage/


results in WCFF
Shipping −40°
Shipping −40°
Shipping −40°
Shipping −40°
Shipping −40°



C., 0% release,
C., 0% release,
C., 0% release,
C., 0% release,
C., 0% release,



gas phase
gas phase
gas phase
gas phase
gas phase



side
side
side
side
side














WCFF
HFO-1132(E)
Mass %
35.3
34.3
31.3
29.1
28.1



HFO-1123
Mass %
0.0
0.0
0.0
0.0
0.0



R1234yf
Mass %
27.4
26.2
23.1
19.8
18.2



R32
Mass %
37.3
39.6
45.6
51.1
53.7













Burning velocity
cm/s
8 or less
8 or less
8 or less
8 or less
8 or less


(WCF)


Burning velocity
cm/s
10
10
10
10
10


(WCFF)









The results in Tables 97 to 100 indicate that the refrigerant has a WCF lower flammability in the following cases:


When the mass % of HFO-1132(E), HFO-1123, R1234yf, and R32 based on their sum in the mixed refrigerant of HFO-1132(E), HFO-1123, R1234yf, and R32 is respectively represented by x, y, z, and a, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is (100−a) mass % and a straight line connecting a point (0.0, 100.0−a, 0.0) and a point (0.0, 0.0, 100.0−a) is the base, if 0<a≤11.1, coordinates (x,y,z) in the ternary composition diagram are on or below a straight line GI that connects point G (0.026a2−1.7478a+72.0, −0.026a2+0.7478a+28.0, 0.0) and point I (0.026a2−1.7478a+72.0, 0.0, −0.026a2+0.7478a+28.0);


if 11.1<a≤18.2, coordinates (x,y,z) in the ternary composition diagram are on or below a straight line GI that connects point G (0.02a2−1.6013a+71.105, −0.02a2+0.6013a+28.895, 0.0) and point I (0.02a2−1.6013a+71.105, 0.0, −0.02a2+0.6013a+28.895); if 18.2<a≤26.7, coordinates (x,y,z) in the ternary composition diagram are on or below a straight line GI that connects point G (0.0135a2−1.4068a+69.727, −0.0135a2+0.4068a+30.273, 0.0) and point I (0.0135a2−1.4068a+69.727, 0.0, −0.0135a2+0.4068a+30.273); if 26.7<a≤36.7, coordinates (x,y,z) in the ternary composition diagram are on or below a straight line GI that connects point G (0.0111a2−1.3152a+68.986, −0.0111a2+0.3152a+31.014, 0.0) and point I (0.0111a2−1.3152a+68.986, 0.0, −0.0111a2+0.3152a+31.014); and if 36.7<a≤46.7, coordinates (x,y,z) in the ternary composition diagram are on or below a straight line GI that connects point G (0.0061a2−0.9918a+63.902, −0.0061a2−0.0082a+36.098, 0.0) and point I (0.0061a2−0.9918a+63.902, 0.0, −0.0061a2−0.0082a+36.098).


Three points corresponding to point G (Table 105) and point I (Table 106) were individually obtained in each of the following five ranges by calculation, and their approximate expressions were obtained.












TABLE 105







Item
11.1 ≥ R32 > 0
18.2 ≥ R32 ≥ 11.1
26.7 ≥ R32 ≥ 18.2



















R32
0
7.1
11.1
11.1
14.5
18.2
18.2
21.9
26.7


HFO-1132(E)
72.0
60.9
55.8
55.8
52.1
48.6
48.6
45.4
41.8


HFO-1123
28.0
32.0
33.1
33.1
33.4
33.2
33.2
32.7
31.5


R1234yf
0
0
0
0
0
0
0
0
0










R32
a
a
a


HFO-1132(E)
 0.026a2 − 1.7478a + 72.0
 0.02a2 − 1.6013a + 71.105
 0.0135a2 − 1.4068a + 69.727


Approximate


expression


HFO-1123
−0.026a2 + 0.7478a + 28.0
−0.02a2 + 0.6013a + 28.895
−0.0135a2 + 0.4068a + 30.273


Approximate


expression


R1234yf
0
0
0


Approximate


expression














Item
36.7 ≥ R32 ≥ 26.7
46.7 ≥ R32 ≥ 36.7



















R32
26.7
29.3
36.7
36.7
44.1
47.8



HFO-1132(E)
41.8
40.0
35.7
35.7
32.0
30.4



HFO-1123
31.5
30.7
27.6
27.6
23.9
21.8



R1234yf
0
0
0
0
0
0











R32
a
a



HFO-1132(E)
 0.0111a2 − 1.3152a + 68.986
 0.0061a2 − 0.9918a + 63.902



Approximate



expression



HFO-1123
−0.0111a2 + 0.3152a + 31.014
−0.0061a2 − 0.0082a + 36.098



Approximate



expression



R1234yf
0
0



Approximate



expression




















TABLE 106







Item
11.1 ≥ R32 > 0
18.2 ≥ R32 ≥ 11.1
26.7 ≥ R32 ≥ 18.2



















R32
0
7.1
11.1
11.1
14.5
18.2
18.2
21.9
26.7


HFO-1132(E)
72.0
60.9
55.8
55.8
52.1
48.6
48.6
45.4
41.8


HFO-1123
0
0
0
0
0
0
0
0
0


R1234yf
28.0
32.0
33.1
33.1
33.4
33.2
33.2
32.7
31.5










R32
a
a
a


HFO-1132(E)
 0.026a2 − 1.7478a + 72.0
 0.02a2 − 1.6013a + 71.105
 0.0135a2 − 1.4068a + 69.727


Approximate


expression


HFO-1123
0
0
0


Approximate


expression


R1234yf
−0.026a2 + 0.7478a + 28.0
−0.02a2 + 0.6013a + 28.895
−0.0135a2 + 0.4068a + 30.273


Approximate


expression














Item
36.7 ≥ R32 ≥ 26.7
46.7 ≥ R32 ≥ 36.7



















R32
26.7
29.3
36.7
36.7
44.1
47.8



HFO-1132(E)
41.8
40.0
35.7
35.7
32.0
30.4



HFO-1123
0
0
0
0
0
0



R1234yf
31.5
30.7
23.6
23.6
23.5
21.8











R32
x
x



HFO-1132(E)
 0.0111a2 − 1.3152a + 68.986
 0.0061a2 − 0.9918a + 63.902



Approximate



expression



HFO-1123
0
0



Approximate



expression



R1234yf
−0.0111a2 + 0.3152a + 31.014
−0.0061a2 − 0.0082a + 36.098



Approximate



expression










The results in Tables 101 to 104 indicate that the refrigerant is determined to have a WCFF lower flammability, and the flammability classification according to the ASHRAE Standard is “2L (flammability)” in the following cases:


When the mass % of HFO-1132(E), HFO-1123, R1234yf, and R32 based on their sum in the mixed refrigerant of HFO-1132(E), HFO-1123, R1234yf, and R32 is respectively represented by x, y, z, and a, in a ternary composition diagram in which the sum of HFO-1132(E), HFO-1123, and R1234yf is (100−a) mass % and a straight line connecting a point (0.0, 100.0−a, 0.0) and a point (0.0, 0.0, 100.0−a) is the base, if 0<a≤11.1, coordinates (x,y,z) in the ternary composition diagram are on or below a straight line JK′ that connects point J (0.0049a2−0.9645a+47.1, −0.0049a2−0.0355a+52.9, 0.0) and point K′(0.0514a2-2.4353a+61.7, −0.0323a2+0.4122a+5.9, −0.0191a2+1.0231a+32.4); if 11.1<a≤18.2, coordinates are on a straight line JK′ that connects point J (0.0243a2−1.4161a+49.725, −0.0243a2+0.4161a+50.275, 0.0) and point K′(0.0341a2−2.1977a+61.187, −0.0236a2+0.34a+5.636, −0.0105a2+0.8577a+33.177); if 18.2<a≤26.7, coordinates are on or below a straight line JK′ that connects point J (0.0246a2−1.4476a+50.184, −0.0246a2+0.4476a+49.816, 0.0) and point K′ (0.0196a2−1.7863a+58.515, −0.0079a2-0.1136a+8.702, −0.0117a2+0.8999a+32.783); if 26.7<a≤36.7, coordinates are on or below a straight line JK′ that connects point J (0.0183a2−1.1399a+46.493, −0.0183a2+0.1399a+53.507, 0.0) and point K′ (−0.0051a2+0.0929a+25.95, 0.0, 0.0051a2−1.0929a+74.05); and if 36.7<a≤46.7, coordinates are on or below a straight line JK′ that connects point J (−0.0134a2+1.0956a+7.13, 0.0134a2−2.0956a+92.87, 0.0) and point K′(−1.892a+29.443, 0.0, 0.892a+70.557).


Actual points having a WCFF lower flammability form a curved line that connects point J and point K′ (on the straight line AB) in FIG. 3 and extends toward the HFO-1132(E) side. Accordingly, when coordinates are on or below the straight line JK′, WCFF lower flammability is achieved.


Three points corresponding to point J (Table 107) and point K′ (Table 108) were individually obtained in each of the following five ranges by calculation, and their approximate expressions were obtained.












TABLE 107







Item
11.1 ≥ R32 > 0
18.2 ≥ R32 ≥ 11.1
26.7 ≥ R32 ≥ 18.2



















R32
0
7.1
11.1
11.1
14.5
18.2
18.2
21.9
26.7


HFO-1132(E)
47.1
40.5
37
37.0
34.3
32.0
32.0
30.3
29.1


HFO-1123
52.9
52.4
51.9
51.9
51.2
49.8
49.8
47.8
44.2


R1234yf
0
0
0
0
0
0
0
0
0










R32
a
a
a


HFO-1132(E)
 0.0049a2 − 0.9645a + 47.1
 0.0243a2 − 1.4161a + 49.725
 0.0246a2 − 1.4476a + 50.184


Approximate


expression


HFO-1123
−0.0049a2 − 0.0355a + 52.9
−0.0243a2 + 0.4161a + 50.275
−0.0246a2 + 0.4476a + 49.816


Approximate


expression


R1234yf
0
0
0


Approximate


expression














Item
36.7 ≥ R32 ≥ 26.7
47.8 ≥ R32 ≥ 36.7



















R32
26.7
29.3
36.7
36.7
44.1
47.8



HFO-1132(E)
29.1
28.8
29.3
29.3
29.4
28.9



HFO-1123
44.2
41.9
34.0
34.0
26.5
23.3



R1234yf
0
0
0
0
0
0











R32
a
a



HFO-1132(E)
 0.0183a2 − 1.1399a + 46.493
−0.0134a2 + 1.0956a + 7.13 



Approximate



expression



HFO-1123
−0.0183a2 + 0.1399a + 53.507
 0.0134a2 − 2.0956a + 92.87



Approximate



expression



R1234yf
0
0



Approximate



expression




















TABLE 108







Item
11.1 ≥ R32 > 0
18.2 ≥ R32 ≥ 11.1
26.7 ≥ R32 ≥ 18.2



















R32
0
7.1
11.1
11.1
14.5
18.2
18.2
21.9
26.7


HFO-1132(E)
61.7
47.0
41.0
41.0
36.5
32.5
32.5
28.8
24.8


HFO-1123
5.9
7.2
6.5
6.5
5.6
4.0
4.0
2.4
0


R1234yf
32.4
38.7
41.4
41.4
43.4
45.3
45.3
46.9
48.5










R32
x
x
x


HFO-1132(E)
 0.0514a2 − 2.4353a + 61.7
 0.0341a2 − 2.1977a + 61.187
 0.0196a2 − 1.7863a + 58.515


Approximate


expression


HFO-1123
−0.0323a2 + 0.4122a + 5.9 
−0.0236a2 + 0.34a + 5.636 
−0.0079a2 − 0.1136a + 8.702 


Approximate


expression


R1234yf
−0.0191a2 + 1.0231a + 32.4
−0.0105a2 + 0.8577a + 33.177
−0.0117a2 + 0.8999a + 32.783


Approximate


expression














Item
36.7 ≥ R32 ≥ 26.7
46.7 ≥ R32 ≥ 36.7



















R32
26.7
29.3
36.7
36.7
44.1
47.8



HFO-1132(E)
24.8
24.3
22.5
22.5
21.1
20.4



HFO-1123
0
0
0
0
0
0



R1234yf
48.5
46.4
40.8
40.8
34.8
31.8











R32
x
x



HFO-1132(E)
−0.0051a2 + 0.0929a + 25.95
−1.892a + 29.443



Approximate



expression



HFO-1123
0
0



Approximate



expression



R1234yf
 0.0051a2 − 1.0929a + 74.05
 0.892a + 70.557



Approximate



expression











FIGS. 3 to 13 show compositions whose R32 content a (mass %) is 0 mass %, 7.1 mass %, 11.1 mass %, 14.5 mass %, 18.2 mass %, 21.9 mass %, 26.7 mass %, 29.3 mass %, 36.7 mass %, 44.1 mass %, and 47.8 mass %, respectively.


Points A, B, C, and D′ were obtained in the following manner according to approximate calculation.


Point A is a point where the content of HFO-1123 is 0 mass %, and a refrigerating capacity ratio of 85% relative to that of R410A is achieved. Three points corresponding to point A were obtained in each of the following five ranges by calculation, and their approximate expressions were obtained (Table 109).












TABLE 109







Item
11.1 ≥ R32 > 0
18.2 ≥ R32 ≥ 11.1
26.7 ≥ R32 ≥ 18.2



















R32
0
7.1
11.1
11.1
14.5
18.2
18.2
21.9
26.7


HFO-1132(E)
68.6
55.3
48.4
48.4
42.8
37
37
31.5
24.8


HFO-1123
0
0
0
0
0
0
0
0
0


R1234yf
31.4
37.6
40.5
40.5
42.7
44.8
44.8
46.6
48.5










R32
a
a
a


HFO-1132(E)
 0.0134a2 − 1.9681a + 68.6
 0.0112a2 − 1.9337a + 68.484
 0.0107a2 − 1.9142a + 68.305


Approximate


expression


HFO-1123
0
0
0


Approximate


expression


R1234yf
−0.0134a2 + 0.9681a + 31.4
−0.0112a2 + 0.9337a + 31.516
−0.0107a2 + 0.9142a + 31.695


Approximate


expression














Item
36.7 ≥ R32 ≥ 26.7
46.7 ≥ R32 ≥ 36.7



















R32
26.7
29.3
36.7
36.7
44.1
47.8



HFO-1132(E)
24.8
21.3
12.1
12.1
3.8
0



HFO-1123
0
0
0
0
0
0



R1234yf
48.5
49.4
51.2
51.2
52.1
52.2











R32
a
a



HFO-1132(E)
 0.0103a2 − 1.9225a + 68.793
 0.0085a2 − 1.8102a + 67.1



Approximate



expression



HFO-1123
0
0



Approximate



expression



R1234yf
−0.0103a2 + 0.9225a + 31.207
−0.0085a2 + 0.8102a + 32.9



Approximate



expression










Point B is a point where the content of HFO-1132(E) is 0 mass %, and a refrigerating capacity ratio of 85% relative to that of R410A is achieved.


Three points corresponding to point B were obtained in each of the following five ranges by calculation, and their approximate expressions were obtained (Table 110).












TABLE 110







Item
11.1 ≥ R32 > 0
18.2 ≥ R32 ≥ 11.1
26.7 ≥ R32 ≥ 18.2



















R32
0
7.1
11.1
11.1
14.5
18.2
18.2
21.9
26.7


HFO-1132(E)
0
0
0
0
0
0
0
0
0


HFO-1123
58.7
47.8
42.3
42.3
37.8
33.1
33.1
28.5
22.9


R1234yf
41.3
45.1
46.6
46.6
47.7
48.7
48.7
49.6
50.4










R32
a
a
a


HFO-1132(E)
0
0
0


Approximate


expression


HFO-1123
 0.0144a2 − 1.6377a + 58.7
 0.0075a2 − 1.5156a + 58.199
 0.009a2 − 1.6045a + 59.318


Approximate


expression


R1234yf
−0.0144a2 + 0.6377a + 41.3
−0.0075a2 + 0.5156a + 41.801
−0.009a2 + 0.6045a + 40.682


Approximate


expression














Item
36.7 ≥ R32 ≥ 26.7
46.7 ≥ R32 ≥ 36.7



















R32
26.7
29.3
36.7
36.7
44.1
47.8



HFO-1132(E)
0
0
0
0
0
0



HFO-1123
22.9
19.9
11.7
11.8
3.9
0



R1234yf
50.4
50.8
51.6
51.5
52.0
52.2











R32
a
a



HFO-1132(E)
0
0



Approximate



expression



HFO-1123
 0.0046a2 − 1.41a + 57.286
 0.0012a2 − 1.1659a + 52.95



Approximate



expression



R1234yf
−0.0046a2 + 0.41a + 42.714
−0.0012a2 + 0.1659a + 47.05



Approximate



expression










Point D′ is a point where the content of HFO-1132(E) is 0 mass %, and a COP ratio of 95.5% relative to that of R410A is achieved.


Three points corresponding to point D′ were obtained in each of the following by calculation, and their approximate expressions were obtained (Table 111).












TABLE 111







Item
11.1 ≥ R32 > 0





















R32
0
7.1
11.1



HFO-1132(E)
0
0
0



HFO-1123
75.4
83.4
88.9



R1234yf
24.6
9.5
0










R32
a



HFO-1132(E)
0



Approximate



expression



HFO-1123
 0.0224a2 + 0.968a + 75.4



Approximate



expression



R1234yf
−0.0224a2 − 1.968a + 24.6



Approximate



expression










Point C is a point where the content of R1234yf is 0 mass %, and a COP ratio of 95.5% relative to that of R410A is achieved.


Three points corresponding to point C were obtained in each of the following by calculation, and their approximate expressions were obtained (Table 112).












TABLE 112







Item
11.1 ≥ R32 > 0





















R32
0
7.1
11.1



HFO-1132(E)
32.9
18.4
0



HFO-1123
67.1
74.5
88.9



R1234yf
0
0
0










R32
a



HFO-1132(E)
−0.2304a2 − 0.4062a + 32.9



Approximate



expression



HFO-1123
 0.2304a2 − 0.5938a + 67.1



Approximate



expression



R1234yf
0



Approximate



expression











(5-4) Refrigerant D


The refrigerant D according to the present disclosure is a mixed refrigerant comprising trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (R1234yf).


The refrigerant D 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 D 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 IJ, JN, NE, and EI that connect the following 4 points:


point I (72.0, 0.0, 28.0),


point J (48.5, 18.3, 33.2),


point N (27.7, 18.2, 54.1), and


point E (58.3, 0.0, 41.7),


or on these line segments (excluding the points on the line segment EI);


the line segment U is represented by coordinates (0.0236y2−1.7616y+72.0, y, −0.0236y2+0.7616y+28.0);


the line segment NE is represented by coordinates (0.012y2−1.9003y+58.3, y, −0.012y2+0.9003y+41.7); and


the line segments JN and EI are straight lines. When the requirements above are satisfied, the refrigerant 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 WCF lower flammability.


The refrigerant D 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 MM′, M′N, NV, VG, and GM that connect the following 5 points:


point M (52.6, 0.0, 47.4),


point M′ (39.2, 5.0, 55.8),


point N (27.7, 18.2, 54.1),


point V (11.0, 18.1, 70.9), and


point G (39.6, 0.0, 60.4),


or on these line segments (excluding the points on the line segment GM);


the line segment MM′ is represented by coordinates (0.132y2−3.34y+52.6, y, −0.132y2+2.34y+47.4);


the line segment MN is represented by coordinates (0.0596y2−2.2541y+48.98, y, −0.0596y2+1.2541y+51.02);


the line segment VG is represented by coordinates (0.0123y2−1.8033y+39.6, y, −0.0123y2+0.8033y+60.4); and


the line segments NV and GM are straight lines. When the requirements above are satisfied, the refrigerant according to the present disclosure has a refrigerating capacity ratio of 70% or more relative to R410A, a GWP of 125 or less, and an ASHRAE lower flammability.


The refrigerant D 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 ON, NU, and UO that connect the following 3 points:


point O (22.6, 36.8, 40.6),


point N (27.7, 18.2, 54.1), and


point U (3.9, 36.7, 59.4),


or on these line segments;


the line segment ON is represented by coordinates (0.0072y2−0.6701y+37.512, y, −0.0072y2−0.3299y+62.488);


the line segment NU is represented by coordinates (0.0083y2−1.7403y+56.635, y, −0.0083y2+0.7403y+43.365); and


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


The refrigerant D 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 QR, RT, TL, LK, and KQ that connect the following 5 points:


point Q (44.6, 23.0, 32.4),


point R (25.5, 36.8, 37.7),


point T (8.6, 51.6, 39.8),


point L (28.9, 51.7, 19.4), and


point K (35.6, 36.8, 27.6),


or on these line segments;


the line segment QR is represented by coordinates (0.0099y2−1.975y+84.765, y, −0.0099y2+0.975y+15.235);


the line segment RT is represented by coordinates (0.0082y2−1.8683y+83.126, y, −0.0082y2+0.8683y+16.874);


the line segment LK is represented by coordinates (0.0049y2−0.8842y+61.488, y, −0.0049y2−0.1158y+38.512);


the line segment KQ is represented by coordinates (0.0095y2−1.2222y+67.676, y, −0.0095y2+0.2222y+32.324); and


the line segment TL is a straight line. When the requirements above are satisfied, the refrigerant according to the present disclosure has a refrigerating capacity ratio of 92.5% or more relative to R410A, a GWP of 350 or less, and a WCF lower flammability.


The refrigerant D 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 PS, ST, and TP that connect the following 3 points:


point P (20.5, 51.7, 27.8),


point S (21.9, 39.7, 38.4), and


point T (8.6, 51.6, 39.8),


or on these line segments;


the line segment PS is represented by coordinates (0.0064y2−0.7103y+40.1, y, −0.0064y2−0.2897y+59.9);


the line segment ST is represented by coordinates (0.0082y2−1.8683y+83.126, y, −0.0082y2+0.8683y+16.874); and


the line segment TP is a straight line. When the requirements above are satisfied, the refrigerant according to the present disclosure has a refrigerating capacity ratio of 92.5% or more relative to R410A, a GWP of 350 or less, and an ASHRAE lower flammability.


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


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


The refrigerant D 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 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 according to the present disclosure has a refrigerating capacity ratio of 95% or more relative to 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 D 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 according to the present disclosure has a refrigerating capacity ratio of 95% or more relative to 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 D 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 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.


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.


(Examples of Refrigerant D)


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


The composition of each mixed refrigerant of HFO-1132(E), R32, and R1234yf was defined as WCF. A leak simulation was performed using the NIST Standard Reference Database REFLEAK Version 4.0 under the conditions of Equipment, Storage, Shipping, Leak, and Recharge according to the ASHRAE Standard 34-2013. The most flammable fraction was defined as WCFF.


A burning velocity test was performed using the apparatus shown in FIG. 1 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. Tables 113 to 115 show the results.

















TABLE 113







Comparative

Example

Example

Example




Example 13
Example
12
Example
14
Example
16


Item
Unit
I
11
J
13
K
15
L
























WCF
HFO-1132 (E)
Mass %
72
57.2
48.5
41.2
35.6
32
28.9



R32
Mass %
0
10
18.3
27.6
36.8
44.2
51.7



R1234yf
Mass %
28
32.8
33.2
31.2
27.6
23.8
19.4















Burning Velocity
cm/s
10
10
10
10
10
10
10


(WCF)























TABLE 114







Comparative

Example

Example





Example 14
Example
19
Example
21
Example


Item
Unit
M
18
W
20
N
22























WCF
HFO-1132 (E)
Mass %
52.6
39.2
32.4
29.3
27.7
24.6



R32
Mass %
0.0
5.0
10.0
14.5
18.2
27.6



R1234yf
Mass %
47.4
55.8
57.6
56.2
54.1
47.8













Leak condition that results
Storage,
Storage,
Storage,
Storage,
Storage,
Storage,


in WCFF
Shipping, −40°
Shipping, −40°
Shipping, −40°
Shipping, −40°
Shipping, −40°
Shipping, −40°



C., 0% release,
C., 0% release,
C., 0% release,
C., 0% release,
C., 0% release,
C., 0% release,



on the gas
on the gas
on the gas
on the gas
on the gas
on the gas



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















WCF
HFO-1132 (E)
Mass %
72.0
57.8
48.7
43.6
40.6
34.9



R32
Mass %
0.0
9.5
17.9
24.2
28.7
38.1



R1234yf
Mass %
28.0
32.7
33.4
32.2
30.7
27.0














Burning Velocity
cm/s
8 or less
8 or less
8 or less
8 or less
8 or less
8 or less


(WCF)


Burning Velocity
cm/s
10
10
10  
10  
10  
10  


(WCFF)




















TABLE 115







Example

Example




23
Example
25


Item
Unit
O
24
P




















WCF
HFO-1132 (E)
Mass %
22.6
21.2
20.5



HFO-1123
Mass %
36.8
44.2
51.7



R1234yf
Mass %
40.6
34.6
27.8










Leak condition that
Storage,
Storage,
Storage,


results in WCFF
Shipping, −40° C.,
Shipping, −40° C.,
Shipping, −40° C.,















0% release,
0% release,
0% release,





on the gas
on the gas
on the gas





phase side
phase side
phase side


WCFF
HFO-1132 (E)
Mass %
31.4
29.2
27.1



HFO-1123
Mass %
45.7
51.1
56.4



R1234yf
Mass %
23.0
19.7
16.5











Burning Velocity
cm/s
8 or less
8 or less
8 or less


(WCF)


Burning Velocity
cm/s
10  
10  
10  


(WCFF)









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. 14 in which the sum of HFO-1132(E), R32, and R1234yf is 100 mass % are on the line segment that connects point I, point J, point K, and point L, or below these line segments, the refrigerant has a WCF lower flammability.


The results also indicate that when coordinates (x,y,z) in the ternary composition diagram shown in FIG. 14 are on the line segments that connect point M, point M′, point W, point J, point N, and point P, or below these line segments, the refrigerant has an ASHRAE lower flammability.


Mixed refrigerants were prepared by mixing HFO-1132(E), R32, and R1234yf in amounts (mass %) shown in Tables 116 to 144 based on the sum of HFO-1132(E), R32, and R1234yf. The coefficient of performance (COP) ratio and the refrigerating capacity ratio relative to R410 of the mixed refrigerants shown in Tables 116 to 144 were determined. The conditions for calculation were as described below.


Evaporating temperature: 5° C.


Condensation temperature: 45° C.


Degree of superheating: 5 K


Degree of subcooling: 5 K


Compressor efficiency: 70%


Tables 116 to 144 show these values together with the GWP of each mixed refrigerant.

















TABLE 116








Comparative
Comparative
Comparative
Comparative
Comparative
Comparative




Comparative
Example 2
Example 3
Example 4
Example 5
Example 6
Example 7


Item
Unit
Example 1
A
B
A′
B′
A″
B″























HFO-1132(E)
Mass %

81.6
0.0
63.1
0.0
48.2
0.0


R32
Mass %
R410A
18.4
18.1
36.9
36.7
51.8
51.5


R1234yf
Mass %

0.0
81.9
0.0
63.3
0.0
48.5


GWP

2088
125
125
250
250
350
350


COP Ratio
% (relative
100
98.7
103.6
98.7
102.3
99.2
102.2



to R410A)


Refrigerating
% (relative
100
105.3
62.5
109.9
77.5
112.1
87.3


Capacity Ratio
to R410A)
























TABLE 117







Comparative

Comparative

Example

Example




Example 8
Comparative
Example 10
Example
2
Example
4


Item
Unit
C
Example 9
C′
1
R
3
T























HFO-1132(E)
Mass %
85.5
66.1
52.1
37.8
25.5
16.6
8.6


R32
Mass %
0.0
10.0
18.2
27.6
36.8
44.2
51.6


R1234yf
Mass %
14.5
23.9
29.7
34.6
37.7
39.2
39.8


GWP

1
69
125
188
250
300
350


COP Ratio
% (relative
99.8
99.3
99.3
99.6
100.2
100.8
101.4



to R410A)


Refrigerating
% (relative
92.5
92.5
92.5
92.5
92.5
92.5
92.5


Capacity Ratio
to R410A)

























TABLE 118







Comparative

Example

Example
Comparative

Example




Example 11
Example
6
Example
8
Example 12
Example
10


Item
Unit
E
5
N
7
U
G
9
V
























HFO-1132(E)
Mass %
58.3
40.5
27.7
14.9
3.9
39.6
22.8
11.0


R32
Mass %
0.0
10.0
18.2
27.6
36.7
0.0
10.0
18.1


R1234yf
Mass %
41.7
49.5
54.1
57.5
59.4
60.4
67.2
70.9


GWP

2
70
125
189
250
3
70
125


COP Ratio
% (relative
100.3
100.3
100.7
101.2
101.9
101.4
101.8
102.3



to R410A)


Refrigerating
% (relative
80.0
80.0
80.0
80.0
80.0
70.0
70.0
70.0


Capacity Ratio
to R410A)

























TABLE 119







Comparative

Example

Example

Example
Example




Example 13
Example
12
Example
14
Example
16
17


Item
Unit
I
11
J
13
K
15
L
Q
























HFO-1132(E)
Mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9
44.6


R32
Mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7
23.0


R1234yf
Mass %
28.0
32.8
33.2
31.2
27.6
23.8
19.4
32.4


GWP

2
69
125
188
250
300
350
157


COP Ratio
% (relative
99.9
99.5
99.4
99.5
99.6
99.8
100.1
99.4



to R410A)


Refrigerating
% (relative
86.6
88.4
90.9
94.2
97.7
100.5
103.3
92.5


Capacity Ratio
to R410A)























TABLE 120







Comparative

Example

Example





Example 14
Example
19
Example
21
Example


Item
Unit
M
18
W
20
N
22






















HFO-1132(E)
Mass %
52.6
39.2
32.4
29.3
27.7
24.5


R32
Mass %
0.0
5.0
10.0
14.5
18.2
27.6


R1234yf
Mass %
47.4
55.8
57.6
56.2
54.1
47.9


GWP

2
36
70
100
125
188


COP Ratio
% (relative
100.5
100.9
100.9
100.8
100.7
100.4



to R410A)


Refrigerating
% (relative
77.1
74.8
75.6
77.8
80.0
85.5


Capacity Ratio
to R410A)





















TABLE 121







Example

Example
Example




23
Example
25
26


Item
Unit
O
24
P
S




















HFO-
Mass %
22.6
21.2
20.5
21.9


1132(E)


R32
Mass %
36.8
44.2
51.7
39.7


R1234yf
Mass %
40.6
34.6
27.8
38.4


GWP

250
300
350
270


COP Ratio
%
100.4
100.5
100.6
100.4



(relative



to R410A)


Refrigerating
%
91.0
95.0
99.1
92.5


Capacity
(relative


Ratio
to R410A)

























TABLE 122







Comparative
Comparative
Comparative
Comparative
Example
Example
Comparative
Comparative


Item
Unit
Example 15
Example 16
Example 17
Example 18
27
28
Example 19
Example 20
























HFO-1132(E)
Mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


R32
Mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


R1234yf
Mass %
85.0
75.0
65.0
55.0
45.0
35.0
25.0
15.0


GWP

37
37
37
36
36
36
35
35


COP Ratio
% (relative
103.4
102.6
101.6
100.8
100.2
99.8
99.6
99.4



to R410A)


Refrigerating
% (relative
56.4
63.3
69.5
75.2
80.5
85.4
90.1
94.4


Capacity Ratio
to R410A)

























TABLE 123







Comparative
Comparative
Example
Comparative
Example
Comparative
Comparative
Comparative


Item
Unit
Example 21
Example 22
29
Example 23
30
Example 24
Example 25
Example 26
























HFO-1132(E)
Mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


R32
Mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R1234yf
Mass %
80.0
70.0
60.0
50.0
40.0
30.0
20.0
10.0


GWP

71
71
70
70
70
69
69
69


COP Ratio
% (relative
103.1
102.1
101.1
100.4
99.8
99.5
99.2
99.1



to R410A)


Refrigerating
% (relative
61.8
68.3
74.3
79.7
84.9
89.7
94.2
98.4


Capacity Ratio
to R410A)

























TABLE 124







Comparative
Example
Comparative
Example
Example
Comparative
Comparative
Comparative


Item
Unit
Example 27
31
Example 28
32
33
Example 29
Example 30
Example 31
























HFO-1132(E)
Mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


R32
Mass %
15.0
15.0
15.0
15.0
15.0
15.0
15.0
15.0


R1234yf
Mass %
75.0
65.0
55.0
45.0
35.0
25.0
15.0
5.0


GWP

104
104
104
103
103
103
103
102


COP Ratio
% (relative
102.7
101.6
100.7
100.0
99.5
99.2
99.0
98.9



to R410A)


Refrigerating
% (relative
66.6
72.9
78.6
84.0
89.0
93.7
98.1
102.2


Capacity Ratio
to R410A)

























TABLE 125







Comparative
Comparative
Comparative
Comparative
Comparative
Comparative
Comparative
Comparative


Item
Unit
Example 32
Example 33
Example 34
Example 35
Example 36
Example 37
Example 38
Example 39
























HFO-1132(E)
Mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
10.0


R32
Mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
25.0


R1234yf
Mass %
70.0
60.0
50.0
40.0
30.0
20.0
10.0
65.0


GWP

138
138
137
137
137
136
136
171


COP Ratio
% (relative
102.3
101.2
100.4
99.7
99.3
99.0
98.8
101.9



to R410A)


Refrigerating
% (relative
71.0
77.1
82.7
88.0
92.9
97.5
101.7
75.0


Capacity Ratio
to R410A)

























TABLE 126







Example
Comparative
Comparative
Comparative
Comparative
Comparative
Comparative
Example


Item
Unit
34
Example 40
Example 41
Example 42
Example 43
Example 44
Example 45
35
























HFO-1132(E)
Mass %
20.0
30.0
40.0
50.0
60.0
70.0
10.0
20.0


R32
Mass %
25.0
25.0
25.0
25.0
25.0
25.0
30.0
30.0


R1234yf
Mass %
55.0
45.0
35.0
25.0
15.0
5.0
60.0
50.0


GWP

171
171
171
170
170
170
205
205


COP Ratio
% (relative
100.9
100.1
99.6
99.2
98.9
98.7
101.6
100.7



to R410A)


Refrigerating
% (relative
81.0
86.6
91.7
96.5
101.0
105.2
78.9
84.8


Capacity Ratio
to R410A)

























TABLE 127







Comparative
Comparative
Comparative
Comparative
Example
Example
Example
Comparative


Item
Unit
Example 46
Example 47
Example 48
Example 49
36
37
38
Example 50
























HFO-1132(E)
Mass %
30.0
40.0
50.0
60.0
10.0
20.0
30.0
40.0


R32
Mass %
30.0
30.0
30.0
30.0
35.0
35.0
35.0
35.0


R1234yf
Mass %
40.0
30.0
20.0
10.0
55.0
45.0
35.0
25.0


GWP

204
204
204
204
239
238
238
238


COP Ratio
% (relative
100.0
99.5
99.1
98.8
101.4
100.6
99.9
99.4



to R410A)


Refrigerating
% (relative
90.2
95.3
100.0
104.4
82.5
88.3
93.7
98.6


Capacity Ratio
to R410A)

























TABLE 128







Comparative
Comparative
Comparative
Comparative
Example
Comparative
Comparative
Comparative


Item
Unit
Example 51
Example 52
Example 53
Example 54
39
Example 55
Example 56
Example 57
























HFO-1132(E)
Mass %
50.0
60.0
10.0
20.0
30.0
40.0
50.0
10.0


R32
Mass %
35.0
35.0
40.0
40.0
40.0
40.0
40.0
45.0


R1234yf
Mass %
15.0
5.0
50.0
40.0
30.0
20.0
10.0
45.0


GWP

237
237
272
272
272
271
271
306


COP Ratio
% (relative
99.0
98.8
101.3
100.6
99.9
99.4
99.0
101.3



to R410A)


Refrigerating
% (relative
103.2
107.5
86.0
91.7
96.9
101.8
106.3
89.3


Capacity Ratio
to R410A)

























TABLE 129







Example
Example
Comparative
Comparative
Comparative
Example
Comparative
Comparative


Item
Unit
40
41
Example 58
Example 59
Example 60
42
Example 61
Example 62
























HFO-1132(E)
Mass %
20.0
30.0
40.0
50.0
10.0
20.0
30.0
40.0


R32
Mass %
45.0
45.0
45.0
45.0
50.0
50.0
50.0
50.0


R1234yf
Mass %
35.0
25.0
15.0
5.0
40.0
30.0
20.0
10.0


GWP

305
305
305
304
339
339
339
338


COP Ratio
% (relative
100.6
100.0
99.5
99.1
101.3
100.6
100.0
99.5



to R410A)


Refrigerating
% (relative
94.9
100.0
104.7
109.2
92.4
97.8
102.9
107.5


Capacity Ratio
to R410A)

























TABLE 130







Comparative
Comparative
Comparative
Comparative
Example
Example
Example
Example


Item
Unit
Example 63
Example 64
Example 65
Example 66
43
44
45
46
























HFO-1132(E)
Mass %
10.0
20.0
30.0
40.0
56.0
59.0
62.0
65.0


R32
Mass %
55.0
55.0
55.0
55.0
3.0
3.0
3.0
3.0


R1234yf
Mass %
35.0
25.0
15.0
5.0
41.0
38.0
35.0
32.0


GWP

373
372
372
372
22
22
22
22


COP Ratio
% (relative
101.4
100.7
100.1
99.6
100.1
100.0
99.9
99.8



to R410A)


Refrigerating
% (relative
95.3
100.6
105.6
110.2
81.7
83.2
84.6
86.0


Capacity Ratio
to R410A)

























TABLE 131







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
47
48
49
50
51
52
53
54
























HFO-1132(E)
Mass %
49.0
52.0
55.0
58.0
61.0
43.0
46.0
49.0


R32
Mass %
6.0
6.0
6.0
6.0
6.0
9.0
9.0
9.0


R1234yf
Mass %
45.0
42.0
39.0
36.0
33.0
48.0
45.0
42.0


GWP

43
43
43
43
42
63
63
63


COP Ratio
% (relative
100.2
100.0
99.9
99.8
99.7
100.3
100.1
99.9



to R410A)


Refrigerating
% (relative
80.9
82.4
83.9
85.4
86.8
80.4
82.0
83.5


Capacity Ratio
to R410A)

























TABLE 132







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
55
56
57
58
59
60
61
62
























HFO-1132(E)
Mass %
52.0
55.0
58.0
38.0
41.0
44.0
47.0
50.0


R32
Mass %
9.0
9.0
9.0
12.0
12.0
12.0
12.0
12.0


R1234yf
Mass %
39.0
36.0
33.0
50.0
47.0
44.0
41.0
38.0


GWP

63
63
63
83
83
83
83
83


COP Ratio
% (relative
99.8
99.7
99.6
100.3
100.1
100.0
99.8
99.7



to R410A)


Refrigerating
% (relative
85.0
86.5
87.9
80.4
82.0
83.5
85.1
86.6


Capacity Ratio
to R410A)

























TABLE 133







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
63
64
65
66
67
68
69
70
























HFO-1132(E)
Mass %
53.0
33.0
36.0
39.0
42.0
45.0
48.0
51.0


R32
Mass %
12.0
15.0
15.0
15.0
15.0
15.0
15.0
15.0


R1234yf
Mass %
35.0
52.0
49.0
46.0
43.0
40.0
37.0
34.0


GWP

83
104
104
103
103
103
103
103


COP Ratio
% (relative
99.6
100.5
100.3
100.1
99.9
99.7
99.6
99.5



to R410A)


Refrigerating
% (relative
88.0
80.3
81.9
83.5
85.0
86.5
88.0
89.5


Capacity Ratio
to R410A)

























TABLE 134







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
71
72
73
74
75
76
77
78
























HFO-1132(E)
Mass %
29.0
32.0
35.0
38.0
41.0
44.0
47.0
36.0


R32
Mass %
18.0
18.0
18.0
18.0
18.0
18.0
18.0
3.0


R1234yf
Mass %
53.0
50.0
47.0
44.0
41.0
38.0
35.0
61.0


GWP

124
124
124
124
124
123
123
23


COP Ratio
% (relative
100.6
100.3
100.1
99.9
99.8
99.6
99.5
101.3



to R410A)


Refrigerating
% (relative
80.6
82.2
83.8
85.4
86.9
88.4
89.9
71.0


Capacity Ratio
to R410A)

























TABLE 135







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
79
80
81
82
83
84
85
86
























HFO-1132(E)
Mass %
39.0
42.0
30.0
33.0
36.0
26.0
29.0
32.0


R32
Mass %
3.0
3.0
6.0
6.0
6.0
9.0
9.0
9.0


R1234yf
Mass %
58.0
55.0
64.0
61.0
58.0
65.0
62.0
59.0


GWP

23
23
43
43
43
64
64
63


COP Ratio
% (relative
101.1
100.9
101.5
101.3
101.0
101.6
101.3
101.1



to R410A)


Refrigerating
% (relative
72.7
74.4
70.5
72.2
73.9
71.0
72.8
74.5


Capacity Ratio
to R410A)

























TABLE 136







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
87
88
89
90
91
92
93
94
























HFO-1132(E)
Mass %
21.0
24.0
27.0
30.0
16.0
19.0
22.0
25.0


R32
Mass %
12.0
12.0
12.0
12.0
15.0
15.0
15.0
15.0


R1234yf
Mass %
67.0
64.0
61.0
58.0
69.0
66.0
63.0
60.0


GWP

84
84
84
84
104
104
104
104


COP Ratio
% (relative
101.8
101.5
101.2
101.0
102.1
101.8
101.4
101.2



to R410A)


Refrigerating
% (relative
70.8
72.6
74.3
76.0
70.4
72.3
74.0
75.8


Capacity Ratio
to R410A)

























TABLE 137







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
95
96
97
98
99
100
101
102
























HFO-1132(E)
Mass %
28.0
12.0
15.0
18.0
21.0
24.0
27.0
25.0


R32
Mass %
15.0
18.0
18.0
18.0
18.0
18.0
18.0
21.0


R1234yf
Mass %
57.0
70.0
67.0
64.0
61.0
58.0
55.0
54.0


GWP

104
124
124
124
124
124
124
144


COP Ratio
% (relative
100.9
102.2
101.9
101.6
101.3
101.0
100.7
100.7



to R410A)


Refrigerating
% (relative
77.5
70.5
72.4
74.2
76.0
77.7
79.4
80.7


Capacity Ratio
to R410A)

























TABLE 138







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
103
104
105
106
107
108
109
110
























HFO-1132(E)
Mass %
21.0
24.0
17.0
20.0
23.0
13.0
16.0
19.0


R32
Mass %
24.0
24.0
27.0
27.0
27.0
30.0
30.0
30.0


R1234yf
Mass %
55.0
52.0
56.0
53.0
50.0
57.0
54.0
51.0


GWP

164
164
185
185
184
205
205
205


COP Ratio
% (relative
100.9
100.6
101.1
100.8
100.6
101.3
101.0
100.8



to R410A)


Refrigerating
% (relative
80.8
82.5
80.8
82.5
84.2
80.7
82.5
84.2


Capacity Ratio
to R410A)

























TABLE 139







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
111
112
113
114
115
116
117
118
























HFO-1132(E)
Mass %
22.0
9.0
12.0
15.0
18.0
21.0
8.0
12.0


R32
Mass %
30.0
33.0
33.0
33.0
33.0
33.0
36.0
36.0


R1234yf
Mass %
48.0
58.0
55.0
52.0
49.0
46.0
56.0
52.0


GWP

205
225
225
225
225
225
245
245


COP Ratio
% (relative
100.5
101.6
101.3
101.0
100.8
100.5
101.6
101.2



to R410A)


Refrigerating
% (relative
85.9
80.5
82.3
84.1
85.8
87.5
82.0
84.4


Capacity Ratio
to R410A)

























TABLE 140







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
119
120
121
122
123
124
125
126
























HFO-1132(E)
Mass %
15.0
18.0
21.0
42.0
39.0
34.0
37.0
30.0


R32
Mass %
36.0
36.0
36.0
25.0
28.0
31.0
31.0
34.0


R1234yf
Mass %
49.0
46.0
43.0
33.0
33.0
35.0
32.0
36.0


GWP

245
245
245
170
191
211
211
231


COP Ratio
% (relative
101.0
100.7
100.5
99.5
99.5
99.8
99.6
99.9



to R410A)


Refrigerating
% (relative
86.2
87.9
89.6
92.7
93.4
93.0
94.5
93.0


Capacity Ratio
to R410A)

























TABLE 141







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
127
128
129
130
131
132
133
134
























HFO-1132(E)
Mass %
33.0
36.0
24.0
27.0
30.0
33.0
23.0
26.0


R32
Mass %
34.0
34.0
37.0
37.0
37.0
37.0
40.0
40.0


R1234yf
Mass %
33.0
30.0
39.0
36.0
33.0
30.0
37.0
34.0


GWP

231
231
252
251
251
251
272
272


COP Ratio
% (relative
99.8
99.6
100.3
100.1
99.9
99.8
100.4
100.2



to R410A)


Refrigerating
% (relative
94.5
96.0
91.9
93.4
95.0
96.5
93.3
94.9


Capacity Ratio
to R410A)

























TABLE 142







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
135
136
137
138
139
140
141
142
























HFO-1132(E)
Mass %
29.0
32.0
19.0
22.0
25.0
28.0
31.0
18.0


R32
Mass %
40.0
40.0
43.0
43.0
43.0
43.0
43.0
46.0


R1234yf
Mass %
31.0
28.0
38.0
35.0
32.0
29.0
26.0
36.0


GWP

272
271
292
292
292
292
292
312


COP Ratio
% (relative
100.0
99.8
100.6
100.4
100.2
100.1
99.9
100.7



to R410A)


Refrigerating
% (relative
96.4
97.9
93.1
94.7
96.2
97.8
99.3
94.4


Capacity Ratio
to R410A)

























TABLE 143







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
143
144
145
146
147
148
149
150
























HFO-1132(E)
Mass %
21.0
23.0
26.0
29.0
13.0
16.0
19.0
22.0


R32
Mass %
46.0
46.0
46.0
46.0
49.0
49.0
49.0
49.0


R1234yf
Mass %
33.0
31.0
28.0
25.0
38.0
35.0
32.0
29.0


GWP

312
312
312
312
332
332
332
332


COP Ratio
% (relative
100.5
100.4
100.2
100.0
101.1
100.9
100.7
100.5



to R410A)


Refrigerating
% (relative
96.0
97.0
98.6
100.1
93.5
95.1
96.7
98.3


Capacity Ratio
to R410A)





















TABLE 144









Example
Example



Item
Unit
151
152





















HFO-1132(E)
Mass %
25.0
28.0



R32
Mass %
49.0
49.0



R1234yf
Mass %
26.0
23.0



GWP

332
332



COP Ratio
% (relative
100.3
100.1




to R410A)



Refrigerating
% (relative
99.8
101.3



Capacity Ratio
to R410A)










The results also 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 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 IJ, JN, NE, and EI that connect the following 4 points:


point I (72.0, 0.0, 28.0),


point J (48.5, 18.3, 33.2),


point N (27.7, 18.2, 54.1), and


point E (58.3, 0.0, 41.7),


or on these line segments (excluding the points on the line segment EI),


the line segment U is represented by coordinates (0.0236y2−1.7616y+72.0, y, −0.0236y2+0.7616y+28.0),


the line segment NE is represented by coordinates (0.012y2−1.9003y+58.3, y, −0.012y2+0.9003y+41.7), and


the line segments JN and EI are straight lines, the refrigerant D has a refrigerating capacity ratio of 80% or more relative to R410A, a GWP of 125 or less, and a WCF lower flammability.


The results also 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 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 MM′, M′N, NV, VG, and GM that connect the following 5 points:


point M (52.6, 0.0, 47.4),


point M′ (39.2, 5.0, 55.8),


point N (27.7, 18.2, 54.1),


point V (11.0, 18.1, 70.9), and


point G (39.6, 0.0, 60.4),


or on these line segments (excluding the points on the line segment GM),


the line segment MM′ is represented by coordinates (0.132y2−3.34y+52.6, y, −0.132y2+2.34y+47.4),


the line segment M′N is represented by coordinates (0.0596y2−2.2541y+48.98, y, −0.0596y2+1.2541y+51.02),


the line segment VG is represented by coordinates (0.0123y2−1.8033y+39.6, y, −0.0123y2+0.8033y+60.4), and


the line segments NV and GM are straight lines, the refrigerant D according to the present disclosure has a refrigerating capacity ratio of 70% or more relative to R410A, a GWP of 125 or less, and an ASHRAE lower flammability.


The results also 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 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 ON, NU, and UO that connect the following 3 points:


point O (22.6, 36.8, 40.6),


point N (27.7, 18.2, 54.1), and


point U (3.9, 36.7, 59.4),


or on these line segments,


the line segment ON is represented by coordinates (0.0072y2−0.6701y+37.512, y, −0.0072y2−0.3299y+62.488),


the line segment NU is represented by coordinates (0.0083y2−1.7403y+56.635, y, −0.0083y2+0.7403y+43.365), and


the line segment UO is a straight line, the refrigerant D according to the present disclosure has a refrigerating capacity ratio of 80% or more relative to R410A, a GWP of 250 or less, and an ASHRAE lower flammability.


The results also 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 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 QR, RT, TL, LK, and KQ that connect the following 5 points:


point Q (44.6, 23.0, 32.4),


point R (25.5, 36.8, 37.7),


point T (8.6, 51.6, 39.8),


point L (28.9, 51.7, 19.4), and


point K (35.6, 36.8, 27.6),


or on these line segments,


the line segment QR is represented by coordinates (0.0099y2−1.975y+84.765, y, −0.0099y2+0.975y+15.235),


the line segment RT is represented by coordinates (0.0082y2−1.8683y+83.126, y, −0.0082y2+0.8683y+16.874),


the line segment LK is represented by coordinates (0.0049y2−0.8842y+61.488, y, −0.0049y2−0.1158y+38.512),


the line segment KQ is represented by coordinates (0.0095y2−1.2222y+67.676, y, −0.0095y2+0.2222y+32.324), and


the line segment TL is a straight line, the refrigerant D according to the present disclosure has a refrigerating capacity ratio of 92.5% or more relative to R410A, a GWP of 350 or less, and a WCF lower flammability.


The results further 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 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 PS, ST, and TP that connect the following 3 points:


point P (20.5, 51.7, 27.8),


point S (21.9, 39.7, 38.4), and


point T (8.6, 51.6, 39.8),


or on these line segments,


the line segment PS is represented by coordinates (0.0064y2−0.7103y+40.1, y, −0.0064y2−0.2897y+59.9),


the line segment ST is represented by coordinates (0.0082y2−1.8683y+83.126, y, −0.0082y2+0.8683y+16.874), and


the line segment TP is a straight line, the refrigerant D according to the present disclosure has a refrigerating capacity ratio of 92.5% or more relative to R410A, a GWP of 350 or less, and an ASHRAE lower flammability.


(5-5) Refrigerant E


The refrigerant E according to the present disclosure is a mixed refrigerant comprising trans-1,2-difluoroethylene (HFO-1132(E)), trifluoroethylene (HFO-1123), and difluoromethane (R32).


The refrigerant E 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 E 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 IK, KB′, B′H, HR, RG, and GI that connect the following 6 points:


point I (72.0, 28.0, 0.0),


point K (48.4, 33.2, 18.4),


point B′ (0.0, 81.6, 18.4),


point H (0.0, 84.2, 15.8),


point R (23.1, 67.4, 9.5), and


point G (38.5, 61.5, 0.0),


or on these line segments (excluding the points on the line segments B′H and GI);


the line segment IK is represented by coordinates (0.025z2−1.7429z+72.00, −0.025z2+0.7429z+28.0, z),


the line segment HR is represented by coordinates (−0.3123z2+4.234z+11.06, 0.3123z2−5.234z+88.94, z),


the line segment RG is represented by coordinates (−0.0491z2−1.1544z+38.5, 0.0491z2+0.1544z+61.5, z), and


the line segments KB′ and GI are straight lines. When the requirements above are satisfied, the refrigerant according to the present disclosure has WCF lower flammability, a COP ratio of 93% or more relative to that of R410A, and a GWP of 125 or less.


The refrigerant E 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 IJ, JR, RG, and GI that connect the following 4 points:


point I (72.0, 28.0, 0.0),


point J (57.7, 32.8, 9.5),


point R (23.1, 67.4, 9.5), and


point G (38.5, 61.5, 0.0),


or on these line segments (excluding the points on the line segment GI);


the line segment U is represented by coordinates (0.025z2−1.7429z+72.0, −0.025z2+0.7429z+28.0, z),


the line segment RG is represented by coordinates (−0.0491z2−1.1544z+38.5, 0.0491z2+0.1544z+61.5, z), and


the line segments JR and GI are straight lines. When the requirements above are satisfied, the refrigerant according to the present disclosure has WCF lower flammability, a COP ratio of 93% or more relative to that of R410A, and a GWP of 125 or less.


The refrigerant E 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 MP, PB′, B′H, HR, RG, and GM that connect the following 6 points:


point M (47.1, 52.9, 0.0),


point P (31.8, 49.8, 18.4),


point B′ (0.0, 81.6, 18.4),


point H (0.0, 84.2, 15.8),


point R (23.1, 67.4, 9.5), and


point G (38.5, 61.5, 0.0),


or on these line segments (excluding the points on the line segments B′H and GM);


the line segment MP is represented by coordinates (0.0083z2−0.984z+47.1, −0.0083z2−0.016z+52.9, z),


the line segment HR is represented by coordinates (−0.3123z2+4.234z+11.06, 0.3123z2−5.234z+88.94, z),


the line segment RG is represented by coordinates (−0.0491z2−1.1544z+38.5, 0.0491z2+0.1544z+61.5, z), and


the line segments PB′ and GM are straight lines. When the requirements above are satisfied, the refrigerant according to the present disclosure has ASHRAE lower flammability, a COP ratio of 93% or more relative to that of R410A, and a GWP of 125 or less.


The refrigerant E 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 MN, NR, RG, and GM that connect the following 4 points:


point M (47.1, 52.9, 0.0),


point N (38.5, 52.1, 9.5),


point R (23.1, 67.4, 9.5), and


point G (38.5, 61.5, 0.0),


or on these line segments (excluding the points on the line segment GM);


the line segment MN is represented by coordinates (0.0083z2−0.984z+47.1, −0.0083z2−0.016z+52.9, z),


the line segment RG is represented by coordinates (−0.0491z2−1.1544z+38.5, 0.0491z2+0.1544z+61.5, z),


the line segments NR and GM are straight lines. When the requirements above are satisfied, the refrigerant according to the present disclosure has ASHRAE lower flammability, a COP ratio of 93% or more relative to that of R410A, and a GWP of 65 or less.


The refrigerant E 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 PS, ST, and TP that connect the following 3 points:


point P (31.8, 49.8, 18.4),


point S (25.4, 56.2, 18.4), and


point T (34.8, 51.0, 14.2),


or on these line segments;


the line segment ST is represented by coordinates (−0.0982z2+0.9622z+40.931, 0.0982z2−1.9622z+59.069, z),


the line segment TP is represented by coordinates (0.0083z2−0.984z+47.1, −0.0083z2−0.016z+52.9, z), and


the line segment PS is a straight line. When the requirements above are satisfied, the refrigerant according to the present disclosure has ASHRAE lower flammability, a COP ratio of 94.5% or more relative to that of R410A, and a GWP of 125 or less.


The refrigerant E 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 QB″, B″D, DU, and UQ that connect the following 4 points:


point Q (28.6, 34.4, 37.0),


point B″ (0.0, 63.0, 37.0),


point D (0.0, 67.0, 33.0), and


point U (28.7, 41.2, 30.1),


or on these line segments (excluding the points on the line segment B″D);


the line segment DU is represented by coordinates (−3.4962z2+210.71z−3146.1, 3.4962z2−211.71z+3246.1, z),


the line segment UQ is represented by coordinates (0.0135z2−0.9181z+44.133, −0.0135z2−0.0819z+55.867, z), and


the line segments QB″ and B″D are straight lines. When the requirements above are satisfied, the refrigerant according to the present disclosure has ASHRAE lower flammability, a COP ratio of 96% or more relative to that of R410A, and a GWP of 250 or less.


The refrigerant E 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 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 E 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 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 E 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 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), 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 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 E 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 a (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 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 E 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 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.


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.


(Examples of Refrigerant E)


The present disclosure is described in more detail below with reference to Examples of refrigerant E. However, the refrigerant E 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 145 and 146.


The composition of each mixture was defined as WCF. A leak simulation was performed using National Institute of Science and Technology (NIST) Standard Reference Data Base Refleak Version 4.0 under the conditions for equipment, storage, shipping, leak, and recharge according to the ASHRAE Standard 34-2013. The most flammable fraction was defined as WCFF.


For each mixed refrigerant, the burning velocity was measured according to the ANSI/ASHRAE Standard 34-2013. When the burning velocities of the WCF composition and the WCFF composition are 10 cm/s or less, the flammability of such a refrigerant is classified as Class 2L (lower flammability) in the ASHRAE flammability classification.


A burning velocity test was performed using the apparatus shown in FIG. 1 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.


Tables 145 and 146 show the results.














TABLE 145





Item
Unit
I
J
K
L





















WCF
HFO-1132(E)
mass %
72.0
57.7
48.4
35.5



HFO-1123
mass %
28.0
32.8
33.2
27.5



R32
mass %
0.0
9.5
18.4
37.0












Burning velocity
cm/s
10
10
10
10


(WCF)























TABLE 146





Item
Unit
M
N
T
P
U
Q























WCF
HFO-1132(E)
mass %
47.1
38.5
34.8
31.8
28.7
28.6



HFO-1123
mass %
52.9
52.1
51.0
49.8
41.2
34.4



R32
mass %
0.0
9.5
14.2
18.4
30.1
37.0













Leak condition that
Storage,
Storage,
Storage,
Storage,
Storage,
Storage,


results in WCFF
Shipping, −40°
Shipping, −40°
Shipping, −40°
Shipping, −40°
Shipping, −40°
Shipping, −40°



C., 92%, release,
C., 92%, release,
C., 92%, release,
C., 92%, release,
C., 92%, release,
C., 92%, release,



on the liquid
on the liquid
on the liquid
on the liquid
on the liquid
on the liquid



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















WCFF
HFO-1132(E)
mass %
72.0
58.9
51.5
44.6
31.4
27.1



HFO-1123
mass %
28.0
32.4
33.1
32.6
23.2
18.3



R32
mass %
0.0
8.7
15.4
22.8
45.4
54.6














Burning velocity
cm/s
8 or less
8 or less
8 or less
8 or less
8 or less
8 or less


(WCF)


Burning velocity
cm/s
10
10
10  
10  
10  
10  


(WCFF)









The results in Table 1 indicate that in a ternary composition diagram of a mixed refrigerant of HFO-1132(E), HFO-1123, and R32 in which their sum is 100 mass %, a line segment connecting a point (0.0, 100.0, 0.0) and a point (0.0, 0.0, 100.0) is the base, the point (0.0, 100.0, 0.0) is on the left side, and the point (0.0, 0.0, 100.0) is on the right side, when coordinates (x,y,z) are on or below line segments IK and KL that connect the following 3 points:


point I (72.0, 28.0, 0.0),


point K (48.4, 33.2, 18.4), and


point L (35.5, 27.5, 37.0);


the line segment IK is represented by coordinates (0.025z2−1.7429z+72.00, −0.025z2+0.7429z+28.00, z), and


the line segment KL is represented by coordinates (0.0098z2−1.238z+67.852, −0.0098z2+0.238z+32.148, z),


it can be determined that the refrigerant has WCF lower flammability.


For the points on the line segment IK, an approximate curve (x=0.025z2−1.7429z+72.00) was obtained from three points, i.e., I (72.0, 28.0, 0.0), J (57.7, 32.8, 9.5), and K (48.4, 33.2, 18.4) by using the least-square method to determine coordinates (x=0.025z2−1.7429z+72.00, y=100−z−x=−0.00922z2+0.2114z+32.443, z).


Likewise, for the points on the line segment KL, an approximate curve was determined from three points, i.e., K (48.4, 33.2, 18.4), Example 10 (41.1, 31.2, 27.7), and L (35.5, 27.5, 37.0) by using the least-square method to determine coordinates.


The results in Table 146 indicate that in a ternary composition diagram of a mixed refrigerant of HFO-1132(E), HFO-1123, and R32 in which their sum is 100 mass %, a line segment connecting a point (0.0, 100.0, 0.0) and a point (0.0, 0.0, 100.0) is the base, the point (0.0, 100.0, 0.0) is on the left side, and the point (0.0, 0.0, 100.0) is on the right side, when coordinates (x,y,z) are on or below line segments MP and PQ that connect the following 3 points:


point M (47.1, 52.9, 0.0),


point P (31.8, 49.8, 18.4), and


point Q (28.6, 34.4, 37.0),


it can be determined that the refrigerant has ASHRAE lower flammability.


In the above, the line segment MP is represented by coordinates (0.0083z2−0.984z+47.1, −0.0083z2−0.016z+52.9, z), and the line segment PQ is represented by coordinates


(0.0135z2−0.9181z+44.133, −0.0135z2−0.0819z+55.867, z).


For the points on the line segment MP, an approximate curve was obtained from three points, i.e., points M, N, and P, by using the least-square method to determine coordinates. For the points on the line segment PQ, an approximate curve was obtained from three points, i.e., points P, U, and Q, by using the least-square method to determine coordinates.


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 Patent Literature 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.


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: 5K


Degree of subcooling: 5K


Compressor efficiency: 70%


Tables 147 to 166 show these values together with the GWP of each mixed refrigerant.

















TABLE 147








Comparative
Comparative
Comparative
Comparative
Comparative
Comparative




Comparative
Example 2
Example 3
Example 4
Example 5
Example 6
Example 7


Item
Unit
Example 1
A
B
A′
B′
A″
B″























HFO-1132(E)
mass %
R410A
90.5
0.0
81.6
0.0
63.0
0.0


HFO-1123
mass %

0.0
90.5
0.0
81.6
0.0
63.0


R32
mass %

9.5
9.5
18.4
18.4
37.0
37.0


GWP

2088
65
65
125
125
250
250


COP ratio
% (relative
100
99.1
92.0
98.7
93.4
98.7
96.1



to R410A)


Refrigerating
% (relative
100
102.2
111.6
105.3
113.7
110.0
115.4


capacity ratio
to R410A)























TABLE 148







Comparative
Comparative

Example

Comparative




Example 8
Example 9
Comparative
1
Example
Example 11


Item
Unit
O
C
Example 10
U
2
D






















HFO-1132(E)
mass %
100.0
50.0
41.1
28.7
15.2
0.0


HFO-1123
mass %
0.0
31.6
34.6
41.2
52.7
67.0


R32
mass %
0.0
18.4
24.3
30.1
32.1
33.0


GWP

1
125
165
204
217
228


COP ratio
% (relative
99.7
96.0
96.0
96.0
96.0
96.0



to R410A)


Refrigerating
% (relative
98.3
109.9
111.7
113.5
114.8
115.4


capacity ratio
to R410A)






















TABLE 149







Comparative

Example
Example
Comparative




Example 12
Comparative
3
4
Example 14


Item
Unit
E
Example 13
T
S
F





















HFO-1132(E)
mass %
53.4
43.4
34.8
25.4
0.0


HFO-1123
mass %
46.6
47.1
51.0
56.2
74.1


R32
mass %
0.0
9.5
14.2
18.4
25.9


GWP

1
65
97
125
176


COP ratio
% (relative
94.5
94.5
94.5
94.5
94.5



to R410A)


Refrigerating
% (relative
105.6
109.2
110.8
112.3
114.8


capacity ratio
to R410A)






















TABLE 150







Comparative

Example

Comparative




Example 15
Example
6
Example
Example 16


Item
Unit
G
5
R
7
H





















HFO-1132(E)
mass %
38.5
31.5
23.1
16.9
0.0


HFO-1123
mass %
61.5
63.5
67.4
71.1
84.2


R32
mass %
0.0
5.0
9.5
12.0
15.8


GWP

1
35
65
82
107


COP ratio
% (relative
93.0
93.0
93.0
93.0
93.0



to R410A)


Refrigerating
% (relative
107.0
109.1
110.9
111.9
113.2


capacity ratio
to R410A)






















TABLE 151







Comparative
Example
Example

Comparative




Example 17
8
9
Comparative
Example 19


Item
Unit
I
J
K
Example 18
L





















HFO-1132(E)
mass %
72.0
57.7
48.4
41.1
35.5


HFO-1123
mass %
28.0
32.8
33.2
31.2
27.5


R32
mass %
0.0
9.5
18.4
27.7
37.0


GWP

1
65
125
188
250


COP ratio
% (relative
96.6
95.8
95.9
96.4
97.1



to R410A)


Refrigerating
% (relative
103.1
107.4
110.1
112.1
113.2


capacity ratio
to R410A)





















TABLE 152







Compar-







ative
Example
Example
Example




Example 20
10
11
12


Item
Unit
M
N
P
Q




















HFO-
mass %
47.1
38.5
31.8
28.6


1132(E)


HFO-1123
mass %
52.9
52.1
49.8
34.4


R32
mass %
0.0
9.5
18.4
37.0


GWP

1
65
125
250


COP ratio
%
93.9
94.1
94.7
96.9



(relative



to R410A)


Refrig-
%
106.2
109.7
112.0
114.1


erating
(relative


capacity
to R410A)


ratio

























TABLE 153







Comparative
Comparative
Comparative
Example
Example
Example
Comparative
Comparative


Item
Unit
Example 22
Example 23
Example 24
14
15
16
Example 25
Example 26
























HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


HFO-1123
mass %
85.0
75.0
65.0
55.0
45.0
35.0
25.0
15.0


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
91.7
92.2
92.9
93.7
94.6
95.6
96.7
97.7



to R410A)


Refrigerating
% (relative
110.1
109.8
109.2
108.4
107.4
106.1
104.7
103.1


capacity ratio
to R410A)

























TABLE 154







Comparative
Comparative
Comparative
Example
Example
Example
Comparative
Comparative


Item
Unit
Example 27
Example 28
Example 29
17
18
19
Example 30
Example 31
























HFO-1132(E)
mass %
90.0
10.0
20.0
30.0
40.0
50.0
60.0
70.0


HFO-1123
mass %
5.0
80.0
70.0
60.0
50.0
40.0
30.0
20.0


R32
mass %
5.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


GWP

35
68
68
68
68
68
68
68


COP ratio
% (relative
98.8
92.4
92.9
93.5
94.3
95.1
96.1
97.0



to R410A)


Refrigerating
% (relative
101.4
111.7
111.3
110.6
109.6
108.5
107.2
105.7


capacity ratio
to R410A)

























TABLE 155







Comparative
Example
Example
Example
Example
Example
Comparative
Comparative


Item
Unit
Example 32
20
21
22
23
24
Example 33
Example 34
























HFO-1132(E)
mass %
80.0
10.0
20.0
30.0
40.0
50.0
60.0
70.0


HFO-1123
mass %
10.0
75.0
65.0
55.0
45.0
35.0
25.0
15.0


R32
mass %
10.0
15.0
15.0
15.0
15.0
15.0
15.0
15.0


GWP

68
102
102
102
102
102
102
102


COP ratio
% (relative
98.0
93.1
93.6
94.2
94.9
95.6
96.5
97.4



to R410A)


Refrigerating
% (relative
104.1
112.9
112.4
111.6
110.6
109.4
108.1
106.6


capacity ratio
to R410A)

























TABLE 156







Comparative
Comparative
Comparative
Comparative
Comparative
Comparative
Comparative
Comparative


Item
Unit
Example 35
Example 36
Example 37
Example 38
Example 39
Example 40
Example 41
Example 42
























HFO-1132(E)
mass %
80.0
10.0
20.0
30.0
40.0
50.0
60.0
70.0


HFO-1123
mass %
5.0
70.0
60.0
50.0
40.0
30.0
20.0
10.0


R32
mass %
15.0
20.0
20.0
20.0
20.0
20.0
20.0
20.0


GWP

102
136
136
136
136
136
136
136


COP ratio
% (relative
98.3
93.9
94.3
94.8
95.4
96.2
97.0
97.8



to R410A)


Refrigerating
% (relative
105.0
113.8
113.2
112.4
111.4
110.2
108.8
107.3


capacity ratio
to R410A)

























TABLE 157







Comparative
Comparative
Comparative
Comparative
Comparative
Comparative
Comparative
Comparative


Item
Unit
Example 43
Example 44
Example 45
Example 46
Example 47
Example 48
Example 49
Example 50
























HFO-1132(E)
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
10.0


HFO-1123
mass %
65.0
55.0
45.0
35.0
25.0
15.0
5.0
60.0


R32
mass %
25.0
25.0
25.0
25.0
25.0
25.0
25.0
30.0


GWP

170
170
170
170
170
170
170
203


COP ratio
% (relative
94.6
94.9
95.4
96.0
96.7
97.4
98.2
95.3



to R410A)


Refrigerating
% (relative
114.4
113.8
113.0
111.9
110.7
109.4
107.9
114.8


capacity ratio
to R410A)

























TABLE 158







Comparative
Comparative
Comparative
Comparative
Comparative
Example
Example
Comparative


Item
Unit
Example 51
Example 52
Example 53
Example 54
Example 55
25
26
Example 56
























HFO-1132(E)
mass %
20.0
30.0
40.0
50.0
60.0
10.0
20.0
30.0


HFO-1123
mass %
50.0
40.0
30.0
20.0
10.0
55.0
45.0
35.0


R32
mass %
30.0
30.0
30.0
30.0
30.0
35.0
35.0
35.0


GWP

203
203
203
203
203
237
237
237


COP ratio
% (relative
95.6
96.0
96.6
97.2
97.9
96.0
96.3
96.6



to R410A)


Refrigerating
% (relative
114.2
113.4
112.4
111.2
109.8
115.1
114.5
113.6


capacity ratio
to R410A)

























TABLE 159







Comparative
Comparative
Comparative
Comparative
Comparative
Comparative
Comparative
Comparative


Item
Unit
Example 57
Example 58
Example 59
Example 60
Example 61
Example 62
Example 63
Example 64
























HFO-1132(E)
mass %
40.0
50.0
60.0
10.0
20.0
30.0
40.0
50.0


HFO-1123
mass %
25.0
15.0
5.0
50.0
40.0
30.0
20.0
10.0


R32
mass %
35.0
35.0
35.0
40.0
40.0
40.0
40.0
40.0


GWP

237
237
237
271
271
271
271
271


COP ratio
% (relative
97.1
97.7
98.3
96.6
96.9
97.2
97.7
98.2



to R410A)


Refrigerating
% (relative
112.6
111.5
110.2
115.1
114.6
113.8
112.8
111.7


capacity ratio
to R410A)

























TABLE 160







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
27
28
29
30
31
32
33
34
























HFO-1132(E)
mass %
38.0
40.0
42.0
44.0
35.0
37.0
39.0
41.0


HFO-1123
mass %
60.0
58.0
56.0
54.0
61.0
59.0
57.0
55.0


R32
mass %
2.0
2.0
2.0
2.0
4.0
4.0
4.0
4.0


GWP

14
14
14
14
28
28
28
28


COP ratio
% (relative
93.2
93.4
93.6
93.7
93.2
93.3
93.5
93.7



to R410A)


Refrigerating
% (relative
107.7
107.5
107.3
107.2
108.6
108.4
108.2
108.0


capacity ratio
to R410A)

























TABLE 161







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
35
36
37
38
39
40
41
42
























HFO-1132(E)
mass %
43.0
31.0
33.0
35.0
37.0
39.0
41.0
27.0


HFO-1123
mass %
53.0
63.0
61.0
59.0
57.0
55.0
53.0
65.0


R32
mass %
4.0
6.0
6.0
6.0
6.0
6.0
6.0
8.0


GWP

28
41
41
41
41
41
41
55


COP ratio
% (relative
93.9
93.1
93.2
93.4
93.6
93.7
93.9
93.0



to R410A)


Refrigerating
% (relative
107.8
109.5
109.3
109.1
109.0
108.8
108.6
110.3


capacity ratio
to R410A)

























TABLE 162







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
43
44
45
46
47
48
49
50
























HFO-1132(E)
mass %
29.0
31.0
33.0
35.0
37.0
39.0
32.0
32.0


HFO-1123
mass %
63.0
61.0
59.0
57.0
55.0
53.0
51.0
50.0


R32
mass %
8.0
8.0
8.0
8.0
8.0
8.0
17.0
18.0


GWP

55
55
55
55
55
55
116
122


COP ratio
% (relative
93.2
93.3
93.5
93.6
93.8
94.0
94.5
94.7



to R410A)


Refrigerating
% (relative
110.1
110.0
109.8
109.6
109.5
109.3
111.8
111.9


capacity ratio
to R410A)

























TABLE 163







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
51
52
53
54
55
56
57
58
























HFO-1132(E)
mass %
30.0
27.0
21.0
23.0
25.0
27.0
11.0
13.0


HFO-1123
mass %
52.0
42.0
46.0
44.0
42.0
40.0
54.0
52.0


R32
mass %
18.0
31.0
33.0
33.0
33.0
33.0
35.0
35.0


GWP

122
210
223
223
223
223
237
237


COP ratio
% (relative
94.5
96.0
96.0
96.1
96.2
96.3
96.0
96.0



to R410A)


Refrigerating
% (relative
112.1
113.7
114.3
114.2
114.0
113.8
115.0
114.9


capacity ratio
to R410A)

























TABLE 164







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
59
60
61
62
63
64
65
66
























HFO-1132(E)
mass %
15.0
17.0
19.0
21.0
23.0
25.0
27.0
11.0


HFO-1123
mass %
50.0
48.0
46.0
44.0
42.0
40.0
38.0
52.0


R32
mass %
35.0
35.0
35.0
35.0
35.0
35.0
35.0
37.0


GWP

237
237
237
237
237
237
237
250


COP ratio
% (relative
96.1
96.2
96.2
96.3
96.4
96.4
96.5
96.2



to R410A)


Refrigerating
% (relative
114.8
114.7
114.5
114.4
114.2
114.1
113.9
115.1


capacity ratio
to R410A)

























TABLE 165







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
67
68
69
70
71
72
73
74
























HFO-1132(E)
mass %
13.0
15.0
17.0
15.0
17.0
19.0
21.0
23.0


HFO-1123
mass %
50.0
48.0
46.0
50.0
48.0
46.0
44.0
42.0


R32
mass %
37.0
37.0
37.0
0.0
0.0
0.0
0.0
0.0


GWP

250
250
250
237
237
237
237
237


COP ratio
% (relative
96.3
96.4
96.4
96.1
96.2
96.2
96.3
96.4



to R410A)


Refrigerating
% (relative
115.0
114.9
114.7
114.8
114.7
114.5
114.4
114.2


capacity ratio
to R410A)

























TABLE 166







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
75
76
77
78
79
80
81
82
























HFO-1132(E)
mass %
25.0
27.0
11.0
19.0
21.0
23.0
25.0
27.0


HFO-1123
mass %
40.0
38.0
52.0
44.0
42.0
40.0
38.0
36.0


R32
mass %
0.0
0.0
0.0
37.0
37.0
37.0
37.0
37.0


GWP

237
237
250
250
250
250
250
250


COP ratio
% (relative
96.4
96.5
96.2
96.5
96.5
96.6
96.7
96.8



to R410A)


Refrigerating
% (relative
114.1
113.9
115.1
114.6
114.5
114.3
114.1
114.0


capacity ratio
to R410A)









The above 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 %, a line segment connecting a point (0.0, 100.0, 0.0) and a point (0.0, 0.0, 100.0) is the base, and the point (0.0, 100.0, 0.0) is on the left side are within the range of a figure surrounded by line segments that connect the following 4 points:


point O (100.0, 0.0, 0.0),


point A″ (63.0, 0.0, 37.0),


point B″ (0.0, 63.0, 37.0), and


point (0.0, 100.0, 0.0),


or on these line segments,


the refrigerant has a GWP of 250 or less.


The results also indicate that when coordinates (x,y,z) are within the range of a figure surrounded by line segments that connect the following 4 points:


point O (100.0, 0.0, 0.0),


point A′ (81.6, 0.0, 18.4),


point B′ (0.0, 81.6, 18.4), and


point (0.0, 100.0, 0.0),


or on these line segments,


the refrigerant has a GWP of 125 or less.


The results also indicate that when coordinates (x,y,z) are within the range of a figure surrounded by line segments that connect the following 4 points:


point O (100.0, 0.0, 0.0),


point A (90.5, 0.0, 9.5),


point B (0.0, 90.5, 9.5), and


point (0.0, 100.0, 0.0),


or on these line segments,


the refrigerant has a GWP of 65 or less.


The results also indicate that when coordinates (x,y,z) are on the left side of line segments that connect the following 3 points:


point C (50.0, 31.6, 18.4),


point U (28.7, 41.2, 30.1), and


point D (52.2, 38.3, 9.5),


or on these line segments,


the refrigerant has a COP ratio of 96% or more relative to that of R410A.


In the above, the line segment CU is represented by coordinates (−0.0538z2+0.7888z+53.701, 0.0538z2−1.7888z+46.299, z), and the line segment UD is represented by coordinates


(−3.4962z2+210.71z−3146.1, 3.4962z2−211.71z+3246.1, z).


The points on the line segment CU are determined from three points, i.e., point C, Comparative Example 10, and point U, by using the least-square method.


The points on the line segment UD are determined from three points, i.e., point U, Example 2, and point D, by using the least-square method.


The results also indicate that when coordinates (x,y,z) are on the left side of line segments that connect the following 3 points:


point E (55.2, 44.8, 0.0),


point T (34.8, 51.0, 14.2), and


point F (0.0, 76.7, 23.3),


or on these line segments,


the refrigerant has a COP ratio of 94.5% or more relative to that of R410A.


In the above, the line segment ET is represented by coordinates (−0.0547z2−0.5327z+53.4, 0.0547z2−0.4673z+46.6, z), and the line segment TF is represented by coordinates


(−0.0982z2+0.9622z+40.931, 0.0982z2−1.9622z+59.069, z).


The points on the line segment ET are determined from three points, i.e., point E, Example 2, and point T, by using the least-square method.


The points on the line segment TF are determined from three points, i.e., points T, S, and F, by using the least-square method.


The results also indicate that when coordinates (x,y,z) are on the left side of line segments that connect the following 3 points:


point G (0.0, 76.7, 23.3),


point R (21.0, 69.5, 9.5), and


point H (0.0, 85.9, 14.1),


or on these line segments,


the refrigerant has a COP ratio of 93% or more relative to that of R410A.


In the above, the line segment GR is represented by coordinates (−0.0491z2−1.1544z+38.5, 0.0491z2+0.1544z+61.5, z), and the line segment RH is represented by coordinates


(−0.3123z2+4.234z+11.06, 0.3123z2−5.234z+88.94, z).


The points on the line segment GR are determined from three points, i.e., point G, Example 5, and point R, by using the least-square method.


The points on the line segment RH are determined from three points, i.e., point R, Example 7, and point H, by using the least-square method.


In contrast, as shown in, for example, Comparative Examples 8, 9, 13, 15, 17, and 18, 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.


(6) First Embodiment

An air conditioning apparatus 1 serving as a refrigeration cycle apparatus according to a first embodiment, is described with reference to FIG. 16, which is a schematic structural view of a refrigerant circuit, and FIG. 17, which is a schematic control block structural view.


The air conditioning apparatus 1 is a apparatus that air-conditions a target space by performing a vapor compression refrigeration cycle.


The air conditioning apparatus 1 primarily includes an outdoor unit 20, a first indoor unit 30, a second indoor unit 35, a liquid-side refrigerant connection pipe 6 and a gas-side refrigerant connection pipe 5 that connect the first indoor unit 30 and the second indoor unit 35 in parallel with respect to the outdoor unit 20, a remote controller (not shown) that serves as an input device and an output device, and a controller 7 that controls the operation of the air conditioning apparatus 1.


The air conditioning apparatus 1 performs a refrigeration cycle in which the refrigerant sealed in a refrigerant circuit 10 is compressed, cooled or condensed, decompressed, and heated or evaporated, and is then compressed again. In the present embodiment, the refrigerant circuit 10 is filled with a refrigerant for performing the vapor compression refrigeration cycle. The refrigerant is a mixed refrigerant containing 1,2-difluoroethylene, and any one of the refrigerants A to E above may be used. The refrigerant circuit 10 is filled with refrigerating-machine oil along with the mixed refrigerant.


(6-1) Outdoor Unit 20


The outdoor unit 20 is connected to the indoor unit 30 via the liquid-side refrigerant connection pipe 6 and the gas-side refrigerant connection pipe 5, and constitutes a part of the refrigerant circuit 10. The outdoor unit 20 primarily includes a compressor 21, a four-way switching valve 22, an outdoor heat exchanger 23, a subcooling heat exchanger 47, a suction injection pipe 40, a subcooling expansion valve 48, an outdoor expansion valve 24, an outdoor fan 25, a low-pressure receiver 41, a liquid-side shutoff valve 29, and a gas-side shutoff valve 28.


The compressor 21 is equipment that compresses a low-pressure refrigerant in the refrigeration cycle into a high-pressure refrigerant. Here, as the compressor 21, a compressor having a hermetic structure in which a displacement compression element (not shown) of, for example, a rotary type or scroll type is rotationally driven by a compressor motor is used. The compressor motor is a motor for changing capacity, and an operation frequency can be controlled by an inverter. An attachment accumulator (not shown) is provided on a suction side of the compressor 21 (the internal volume of the attachment accumulator is less than, and is desirably less than or equal to half of, the internal volume of refrigerant containers, such as low-pressure receivers, intermediate-pressure receivers, and high-pressure receivers).


The four-way switching valve 22 can be switched between a cooling operation connection state and a heating operation connection state by switching a connection state, the cooling operation connection state being a state in which the four-way switching valve 22 connects the suction side of the compressor 21 and the gas-side shutoff valve 28 to each other while connecting a discharge side of the compressor 21 and the outdoor heat exchanger 23, the heating operation connection state being a state in which the four-way switching valve 22 connects the suction side of the compressor 21 and the outdoor heat exchanger 23 to each other while connecting the discharge side of the compressor 21 and the gas-side shutoff valve 28.


The outdoor heat exchanger 23 is a heat exchanger that functions as a condenser for a high-pressure refrigerant in the refrigeration cycle during the cooling operation and that functions as an evaporator for a low-pressure refrigerant in the refrigeration cycle during the heating operation.


The outdoor expansion valve 24 is provided between a liquid-side outlet of the outdoor heat exchanger 23 and the liquid-side shutoff valve 29 in the refrigerant circuit 10. The outdoor expansion valve 24 is an electric expansion valve whose valve opening degree is adjustable.


The suction injection pipe 40 branches off from a branching portion between the outdoor expansion valve 24 and the liquid-side shutoff valve 29 in a main circuit of the refrigerant circuit 10, and is provided so as to merge at a merging portion between the low-pressure receiver 41 and one connection port of the four-way switching valve 22. The subcooling expansion valve 48 is provided at the suction injection pipe 40. The subcooling expansion valve 48 is an electric expansion valve whose valve opening degree is adjustable.


The subcooling heat exchanger 47 is a heat exchanger that causes heat to be exchanged between a refrigerant that flows along a portion of the refrigerant circuit 10 between the outdoor expansion valve 24 and the liquid-side shutoff valve 29 and a refrigerant that flows on a side of the merging portion of the subcooling expansion valve 48 in the suction injection pipe 40. In the present embodiment, the subcooling heat exchanger 47 is a portion between the outdoor expansion valve 24 and the liquid-side shutoff valve 29, and is provided closer than the branching portion of the suction injection pipe 40 to the liquid-side shutoff valve 29.


The outdoor fan 25 sucks outdoor air into the outdoor unit 20 and causes heat to be exchanged with a refrigerant in the outdoor heat exchanger 23, and then causes an air flow for discharge to the outside to be generated. The outdoor fan 25 is rotationally driven by an outdoor fan motor.


The low-pressure receiver 41 is provided between the suction side of the compressor 21 and the one connection port of the four-way switching valve 22, and is a refrigerant container that is capable of storing an excess refrigerant as a liquid refrigerant in the refrigerant circuit 10. The compressor 21 is provided with the attachment accumulator (not shown), and the low-pressure receiver 41 is connected on a downstream side of the attachment accumulator.


The liquid-side shutoff valve 29 is a manual valve disposed at a portion of the outdoor unit 20 that is connected to the liquid-side refrigerant connection pipe 6.


The gas-side shutoff valve 28 is a manual valve disposed at a portion of the outdoor unit 20 that is connected to the gas-side refrigerant connection pipe 5.


The outdoor unit 20 includes an outdoor unit control unit 27 that controls the operation of each portion that constitutes the outdoor unit 20. The outdoor unit control unit 27 includes a microcomputer including, for example, a CPU and a memory. The outdoor unit control unit 27 is connected to an indoor unit control units 34 and 39 of each indoor unit 30 and 35 via a communication line, and sends and receives, for example, control signals.


The outdoor unit 20 is provided with, for example, a discharge pressure sensor 61, a discharge temperature sensor 62, a suction pressure sensor 63, a suction temperature sensor 64, an outdoor heat-exchange temperature sensor 65, an outside air temperature sensor 66, and a subcooling temperature sensor 67. Each of these sensors is electrically connected to the outdoor unit control unit 27 and sends a detection signal to the outdoor unit control unit 27. The discharge pressure sensor 61 detects the pressure of a refrigerant that flows through a discharge tube that connects the discharge side of the compressor 21 and one connection port of the four-way switching valve 22. The discharge temperature sensor 62 detects the temperature of the refrigerant that flows through the discharge tube. The suction pressure sensor 63 detects the pressure of a refrigerant that flows through a suction tube that connects the suction side of the compressor 21 and the low-pressure receiver 41. The suction temperature sensor 64 detects the temperature of the refrigerant that flows through the suction tube. The outdoor heat-exchange temperature sensor 65 detects the temperature of a refrigerant that flows through the liquid-side outlet of the outdoor heat exchanger 23 on a side opposite to a side where the four-way switching valve 22 is connected. The outside air temperature sensor 66 detects the temperature of outdoor air that is air before passing through the outdoor heat exchanger 23. The subcooling temperature sensor 67 detects the temperature of a refrigerant that flows between the subcooling heat exchanger 47 and a second outdoor expansion valve 24 in the main circuit of the refrigerant circuit 10.


(6-2) First Indoor Unit 30 and Second Indoor Unit 35


The first indoor unit 30 and the second indoor unit 35 are installed on, for example, a ceiling or wall surfaces in a room corresponding to the same target space or different target spaces. The first indoor unit 30 and the second indoor unit 35 are connected to the outdoor unit 20 via the liquid-side refrigerant connection pipe 6 and the gas-side refrigerant connection pipe 5, and constitute a part of the refrigerant circuit 10.


The first indoor unit 30 includes a first indoor heat exchanger 31, a first indoor expansion valve 33, and a first indoor fan 32.


A liquid side of the first indoor heat exchanger 31 is connected to the liquid-side refrigerant connection pipe 6, and a gas side end of the first indoor heat exchanger 31 is connected to the gas-side refrigerant connection pipe 5. The first indoor heat exchanger 31 is a heat exchanger that functions as an evaporator for a low-pressure refrigerant in the refrigeration cycle during the cooling operation, and that functions as a condenser for a high-pressure refrigerant in the refrigeration cycle during the heating operation.


The first indoor expansion valve 33 is an electric expansion valve that is provided at a refrigerant pipe on a liquid refrigerant side of the first indoor heat exchanger 31 and whose valve opening degree is adjustable.


The first indoor fan 32 sucks indoor air into the first indoor unit 30 and causes heat to be exchanged with a refrigerant in the first indoor heat exchanger 31, and then causes an air flow for discharge to the outside to be generated. The first indoor fan 32 is rotationally driven by an indoor fan motor.


The first indoor unit 30 includes the first indoor unit control unit 34 that controls the operation of each portion that constitutes the first indoor unit 30. The first indoor unit control unit 34 includes a microcomputer including, for example, a CPU and a memory. The first indoor unit control unit 34 is connected to a second indoor unit control unit 39 and the outdoor unit control unit 27 via the communication line, and sends and receives, for example, control signals.


The first indoor unit 30 is provided with, for example, a first indoor liquid-side heat-exchange sensor 71, a first indoor air temperature sensor 72, and a first indoor gas-side heat-exchange temperature sensor 73. Each of these sensors is electrically connected to the first indoor unit control unit 34 and sends a detection signal to the indoor unit control unit 34. The first indoor liquid-side heat-exchange sensor 71 detects the temperature of a refrigerant that flows through a liquid-refrigerant-side outlet of the first indoor heat exchanger 31. The first indoor air temperature sensor 72 detects the temperature of indoor air that is air before passing through the first indoor heat exchanger 31. The first indoor gas-side heat-exchange temperature sensor 73 detects the temperature of a refrigerant that flows through a gas-refrigerant-side outlet of the first indoor heat exchanger 31.


The second indoor unit 35 is provided with a second indoor heat exchanger 36, a second indoor expansion valve 38, and a second indoor fan 37.


A liquid side of the second indoor heat exchanger 36 is connected to the liquid-side refrigerant connection pipe 6, and a gas side end of the second indoor heat exchanger 36 is connected to the gas-side refrigerant connection pipe 5. The second indoor heat exchanger 36 is a heat exchanger that functions as an evaporator for a low-pressure refrigerant in the refrigeration cycle during the cooling operation, and that functions as a condenser for a high-pressure refrigerant in the refrigeration cycle during the heating operation.


The second indoor expansion valve 38 is an electric expansion valve that is provided at a refrigerant pipe on a liquid refrigerant side of the second indoor heat exchanger 36 and whose valve opening degree is adjustable.


The second indoor fan 37 sucks indoor air into the second indoor unit 35 and causes heat to be exchanged with a refrigerant in the second indoor heat exchanger 36, and then causes an air flow for discharge to the outside to be generated. The second indoor fan 37 is rotationally driven by an indoor fan motor.


The second indoor unit 35 includes the second indoor unit control unit 39 that controls the operation of each portion that constitutes the second indoor unit 35. The second indoor unit control unit 39 includes a microcomputer including, for example, a CPU and a memory. The second indoor unit control unit 39 is connected to the first indoor unit control unit 34 and the outdoor unit control unit 27 via a communication line, and sends and receives, for example, control signals.


The second indoor unit 35 is provided with, for example, a second indoor liquid-side heat-exchange sensor 75, a second indoor air temperature sensor 76, and a second indoor gas-side heat-exchange temperature sensor 77. Each of these sensors is electrically connected to the second indoor unit control unit 39 and sends a detection signal to the second indoor unit control unit 39. The second indoor liquid-side heat-exchange sensor 75 detects the temperature of a refrigerant that flows through a liquid-refrigerant-side outlet of the second indoor heat exchanger 36. The second indoor air temperature sensor 76 detects the temperature of indoor air that is air before passing through the second indoor heat exchanger 36. The second indoor gas-side heat-exchange temperature sensor 77 detects the temperature of a refrigerant that flows through a gas-refrigerant-side outlet of the second indoor heat exchanger 36.


(6-3) Details of Controller 7


In the air conditioning apparatus 1, by connecting the outdoor unit control unit 27, the first indoor unit control unit 34, and the second indoor unit control unit 39 to each other via the communication lines, the controller 7 that controls the operation of the air conditioning apparatus 1 is formed.


The controller 7 primarily includes a CPU (central processing unit) and a memory, such as ROM or RAM. Various processing operations and control that are performed by the controller 7 are realized as a result of each portion included in the outdoor unit control unit 27 and/or the first indoor unit control unit 34 and/or the second indoor unit control unit 39 functioning together.


(6-4) Operation Modes


Operation modes are described below.


As the operation modes, a cooling operation mode and a heating operation mode are provided.


On the basis of an instruction received from, for example, a remote controller, the controller 7 determines whether or not a mode is the cooling operation mode or the heating operation mode, and executes the mode.


(6-4-1) Cooling Operation Mode


In the air conditioning apparatus 1, in the cooling operation mode, the compressor 21 is such that an operation frequency is capacity-controlled to cause the evaporation temperature of a refrigerant in the refrigerant circuit 10 to become a target evaporation temperature. Here, it is desirable that the target evaporation temperature be determined in accordance with the indoor unit 30 or 35 whichever has the largest difference between a set temperature and an indoor temperature (the indoor unit having the largest load).


A gas refrigerant discharged from the compressor 21 is condensed at the outdoor heat exchanger 23 via the four-way switching valve 22. The refrigerant that has flowed through the outdoor heat exchanger 23 passes through the outdoor expansion valve 24. In this case, the outdoor expansion valve 24 is controlled so as to be in a fully open state.


A portion of the refrigerant that has passed through the outdoor expansion valve 24 flows toward the liquid-side shutoff valve 29 and the other portion thereof flows into the branching portion of the suction injection pipe 40. The refrigerant that has flowed through the branching portion of the suction injection pipe 40 is decompressed at the subcooling expansion valve 48. At the subcooling heat exchanger 47, the refrigerant that flows toward the liquid-side shutoff valve 29 from the outdoor expansion valve 24 and the refrigerant that is decompressed at the subcooling expansion valve 48 and that flows in the suction injection pipe 40 exchange heat. After the refrigerant that flows in the suction injection pipe 40 has finished exchanging heat at the subcooling heat exchanger 47, the refrigerant flows so as to merge at the merging portion between the low-pressure receiver 41 and the one connection port of the four-way switching valve 22. The valve opening degree of the subcooling expansion valve 48 is controlled so as to satisfy predetermined conditions such as the subcooling degree of the refrigerant that has passed though the sub cooling heat exchanger 47 in the refrigerant circuit 10 becoming a predetermined target value.


After the refrigerant that flows toward the liquid-side shutoff valve 29 from the outdoor expansion valve 24 has finished exchanging heat at the subcooling heat exchanger 47, the refrigerant flows through the liquid-side refrigerant connection pipe 6 via the liquid-side shutoff valve 29, and is sent to the first indoor unit 30 and the second indoor unit 35.


Here, in the first indoor unit 30, the valve opening degree of the first indoor expansion valve 33 is controlled so as to satisfy predetermined conditions such as the superheating degree of a refrigerant that flows through a gas-side outlet of the first indoor heat exchanger 31 becoming a predetermined target value. Similarly to the first indoor expansion valve 33, the valve opening degree of the second indoor expansion valve 38 of the second indoor unit 35 is controlled so as to satisfy predetermined conditions such as the superheating degree of a refrigerant that flows through a gas-side outlet of the second indoor heat exchanger 36 becoming a predetermined target value. The valve opening degree of the first indoor expansion valve 33 and the valve opening degree of the second indoor expansion valve 38 may be controlled so as to satisfy predetermined conditions such as the superheating degree of the refrigerant that is obtained by subtracting the saturation temperature of the refrigerant that is equivalent to a detected pressure of the suction pressure sensor 63 from a detected temperature of the suction temperature sensor 64 becoming a target value. Further, the method of controlling the valve opening degree of the first indoor expansion valve 33 and the valve opening degree of the second indoor expansion valve 38 are not limited, so that, for example, the valve opening degrees may be controlled to cause the discharge temperature of the refrigerant that is discharged from the compressor 21 to become a predetermined temperature, or the superheating degree of the refrigerant that is discharged from the compressor 21 to satisfy a predetermined condition. The refrigerant decompressed at the first indoor expansion valve 33 evaporates at the first indoor heat exchanger 31, the refrigerant decompressed at the second indoor expansion valve 38 evaporates at the second indoor heat exchanger 36, and the refrigerants merge, after which the refrigerant flows to the gas-side refrigerant connection pipe 5. The refrigerant that has flowed through the gas-side refrigerant connection pipe 5 merges with the refrigerant that has flowed through the suction injection pipe 40 via the gas-side shutoff valve 28 and the four-way switching valve 22. The merged refrigerant is sucked into the compressor 21 again via the low-pressure receiver 41. Liquid refrigerants that could not be evaporated at the first indoor heat exchanger 31, the second indoor heat exchanger 36, and the subcooling heat exchanger 47 are stored as excess refrigerants in the low-pressure receiver 41.


(6-4-2) Heating Operation Mode


In the air conditioning apparatus 1, in the heating operation mode, the compressor 21 is such that an operation frequency is subjected to capacity control to cause the condensation temperature of a refrigerant in the refrigerant circuit 10 to become a target condensation temperature. Here, it is desirable that the target condensation temperature be determined in accordance with the indoor unit 30 or 35 whichever has the largest difference between a set temperature and an indoor temperature (the indoor unit having the largest load).


After a gas refrigerant discharged from the compressor 21 has flowed through the four-way switching valve 22 and the gas-side refrigerant connection pipe 5, a portion of the refrigerant flows into a gas-side end of the first indoor heat exchanger 31 of the first indoor unit 30 and is condensed at the first indoor heat exchanger 31, and the other portion of the refrigerant flows into a gas-side end of the second indoor heat exchanger 36 of the second indoor unit 35 and is condensed at the second indoor heat exchanger 36.


The valve opening degree of the first indoor expansion valve 33 of the first indoor unit 30 is controlled so as to satisfy predetermined conditions, such as the subcooling degree of a refrigerant that flows along the liquid side of the first indoor heat exchanger 31 becoming a predetermined target value. Similarly, the valve opening degree of the second indoor expansion valve 38 of the second indoor unit 35 is controlled so as to satisfy predetermined conditions, such as the subcooling degree of a refrigerant that flows along the liquid side of the second indoor heat exchanger 36 becoming a predetermined target value.


After the refrigerant decompressed at the first indoor expansion valve 33 and the refrigerant decompressed at the second indoor expansion valve 38 have merged, the refrigerant flows through the liquid-side refrigerant connection pipe 6 and flows into the outdoor unit 20.


After the refrigerant that has passed through the liquid-side shutoff valve 29 of the outdoor unit 20 has flowed through the subcooling heat exchanger 47, the refrigerant is decompressed at the outdoor expansion valve 24. Here, the valve opening degree of the outdoor expansion valve 24 is controlled so as to satisfy predetermined conditions, such as the superheating degree of a refrigerant that flows along the suction side of the compressor 21 becoming a target value. The method of controlling the valve opening degree of the outdoor expansion valve 24 is not limited, so that, for example, the valve opening degrees may be controlled to cause the discharge temperature of the refrigerant that is discharged from the compressor 21 to become a predetermined temperature, or the superheating degree of the refrigerant that is discharged from the compressor 21 to satisfy a predetermined condition.


In the heating operation mode, since the subcooling expansion valve 48 that is provided at the suction injection pipe 40 is controlled so as to be in a fully closed state, the refrigerant does not flow through the suction injection pipe 40 and heat is also not exchanged at the subcooling heat exchanger 47.


The refrigerant decompressed at the outdoor expansion valve 24 is evaporated at the outdoor heat exchanger 23, flows through the four-way switching valve 22 and the low-pressure receiver 41, and is sucked into the compressor 21 again. A liquid refrigerant that could not be evaporated at the outdoor heat exchanger 23 is stored as an excess refrigerant in the low-pressure receiver 41.


(6-5) Features of the First Embodiment


Since the air conditioning apparatus 1 above uses a refrigerant containing 1,2-difluoroethylene, the air conditioning apparatus 1 can sufficiently reduce GWP.


Since the temperature of the refrigerant that is sucked into the compressor 21 can be reduced by the suction injection pipe 40, the air conditioning apparatus 1 can improve the operation efficiency in the refrigeration cycle.


(6-6) Modification a of the First Embodiment


Although, in the first embodiment, the air conditioning apparatus 1 is described by using as an example an air conditioning apparatus including a plurality of indoor units that are connected in parallel, an air conditioning apparatus including one indoor unit that is connected in series may be used as the air conditioning apparatus.


(6-7) Modification B of the First Embodiment


In the first embodiment, the air conditioning apparatus 1 including the suction injection pipe 40 that allows a refrigerant to be sent to the suction side of the compressor 21 after the refrigerant has flowed through the subcooling heat exchanger 47 is described as an example.


In contrast, as an air conditioning apparatus, for example, as shown in FIG. 18, an air conditioning apparatus 1a including an economizer injection pipe 40a that sends a refrigerant to a region of intermediate pressure of a compressor 21a after the refrigerant has flowed through an economizer heat exchanger 47a may be used.


The economizer injection pipe 40a is a pipe that branches off from a portion of a main circuit of a refrigerant circuit 10 between the outdoor expansion valve 24 and the liquid-side shutoff valve 29 and extends up to the region of intermediate pressure of the compressor 21a. An economizer expansion valve 48a whose valve opening degree can be controlled is provided at the economizer injection pipe 40a.


The economizer heat exchanger 47a is a heat exchanger that causes heat to be exchanged between a refrigerant that flows into a portion branching off from the main circuit of the refrigerant circuit 10, that flows in the economizer injection pipe 40a, and that has been decompressed at the economizer expansion valve 48a and a refrigerant that flows between the outdoor expansion valve 24 and the liquid-side shutoff valve 29 in the main circuit of the refrigerant circuit 10.


The compressor 21a is not limited, and, for example, a scroll compressor as that shown in FIG. 19 can be used.


The compressor 21a includes a casing 80, a scroll compression mechanism 81 including a fixed scroll 82, a driving motor 91, a crank shaft 94, and a lower bearing 98.


The casing 80 includes a circular cylindrical member 80a that is substantially circularly cylindrical and that has an open top and an open bottom, and an upper cover 80b and a lower cover 80c that are provided on an upper end and a lower end, respectively, of the circular cylindrical member 80a. The circular cylindrical member 80a and the upper cover 80b and the lower cover 80c are fixed to each other by welding so as to be kept air-tight. Pieces of structural equipment of the compressor 21a including the scroll compression mechanism 81, the driving motor 91, the crank shaft 94, and the lower bearing 98 are accommodated in the casing 80. An oil-storage space So is formed in a lower portion of the casing 80. A refrigerating-machine oil O for lubricating, for example, the scroll compression mechanism 81 can be stored in the oil-storage space So. A suction tube 19 that allows a low-pressure gas refrigerant in a refrigeration cycle of the refrigerant circuit 10 to be sucked and that allows a gas refrigerant to be supplied to the scroll compression mechanism 81 is provided at an upper portion of the casing 80 so as to extend through the upper cover 80b. A lower end of the suction tube 19 is connected to the fixed scroll 82 of the scroll compression mechanism 81. The suction tube 19 communicates with a compression chamber Sc of the scroll compression mechanism 81 described below. An intermediate portion of the circular cylindrical member 80a of the casing 80 is provided with a discharge tube 18 through which a refrigerant that is discharged to the outside of the casing 80 passes. The discharge tube 18 is disposed so that an end portion of the discharge tube 18 inside the casing 80 protrudes into a high-pressure space Sh formed below a housing 88 of the scroll compression mechanism 81. A high-pressure refrigerant in the refrigeration cycle that has been compressed by the scroll compression mechanism 81 flows through the discharge tube 18. A side surface of the upper cover 80b of the casing 80 has an injection connection port, and the economizer injection pipe 40a is connected in the injection connection port.


The scroll compression mechanism 81 primarily includes the housing 88, the fixed scroll 82 that is disposed above the housing 88, and a movable scroll 84 that forms the compression chamber Sc by being assembled to the fixed scroll 82.


The fixed scroll 82 includes a plate-shaped fixed-side end plate 82a, a spiral fixed-side lap 82b that protrudes from a front surface of the fixed-side end plate 82a, and an outer edge portion 82c that surrounds the fixed-side lap 82b. Anon-circular discharge port 82d that communicates with the compression chamber Sc of the scroll compression mechanism 81 is formed in a central portion of the fixed-side end plate 82a so as to extend through the fixed-side end plate 82a in a thickness direction thereof. A refrigerant compressed in the compression chamber Sc is discharged from the discharge port 82d, passes through a refrigerant passage (not shown) formed in the fixed scroll 82 and the housing 88, and flows into the high-pressure space Sh. The fixed-side end plate 82a has a supply passage 82e that opens in a side of the fixed-side end plate 82a and that communicates with the compression chamber Sc. The supply passage 82e allows an intermediate-pressure refrigerant that has flowed through the economizer injection pipe 40a to be supplied to the compression chamber Sc. The supply passage 82e has a horizontal passage portion 82f that extends in a horizontal direction from the opening in the side of the fixed-side end plate 82a toward the center of the fixed-side end plate 82a. The supply passage 82e has an injection port 82g that extends toward the compression chamber Sc from a portion of the horizontal passage portion 82f on a center side of the fixed-side end plate 82a (near an end portion of the horizontal passage portion 82f on the center side of the fixed-side end plate 82a) and that directly communicates with the compression chamber Sc. The injection port 82g is a circular hole.


The movable scroll 84 includes a plate-shaped movable-side end plate 84a, a spiral movable-side lap 84b that protrudes from a front surface of the movable-side end plate 84a, and a circular cylindrical boss portion 84c that protrudes from a rear surface of the movable-side end plate 84a. The fixed-side lap 82b of the fixed scroll 82 and the movable-side lap 84b of the movable scroll 84 are assembled to each other in a state in which a lower surface of the fixed-side end plate 82a and an upper surface of the movable-side end plate 84a face each other. The compression chamber Sc is formed between the fixed-side lap 82b and the movable-side lap 84b that are adjacent to each other. Due to the movable scroll 84 revolving with respect to the fixed scroll 82 as described below, the volume of the compression chamber Sc changes periodically, and a refrigerant is sucked, compressed, and discharged in the scroll compression mechanism 81. The boss portion 84c is a circular cylindrical portion whose upper end is closed. Due to a decentered portion 95 of the crank shaft 94 (described below) being inserted into a hollow portion of the boss portion 84c, the movable scroll 84 and the crank shaft 94 are coupled to each other. The boss portion 84c is disposed in a decentered-portion space 89 that is formed between the movable scroll 84 and the housing 88. The decentered-portion space 89 communicates with the high-pressure space Sh via, for example, an oil-supply path 97 of the crank shaft 94 (described below), and a high pressure acts in the decentered-portion space 89. This pressure causes a lower surface of the movable-side end plate 84a in the decentered-portion space 89 to be pushed upward toward the fixed scroll 82. This force causes the movable scroll 84 to closely contact the fixed scroll 82. The movable scroll 84 is supported by the housing 88 via an Oldham ring disposed in an “Oldham ring space Sr”. The Oldham ring is a member that prevents the movable scroll 84 from rotating and that causes the movable scroll 84 to revolve. By using the Oldham ring, when the crank shaft 94 rotates, the movable scroll 84 connected to the crank shaft 94 at the boss portion 84c revolves without rotating with respect to the fixed scroll 82, and a refrigerant in the compression chamber Sc is compressed.


The housing 88 is press-fitted to the circular cylindrical member 80a, and an outer peripheral surface of the housing 88 is fixed to the circular cylindrical member 80a in its entirety in a peripheral direction. The housing 88 and the fixed scroll 82 are fixed to each other with, for example, a bolt (not shown) so that an upper end surface of the housing 88 is in close contact with a lower surface of the outer edge portion 82c of the fixed scroll 82. The housing 88 includes a concave portion 88a disposed so as to be recessed in a central portion of an upper surface of the housing 88 and a bearing portion 88b disposed below the concave portion 88a. The concave portion 88a surrounds a side surface forming the decentered-portion space 89 where the boss portion 84c of the movable scroll 84 is disposed. A bearing 90 that supports a main shaft 96 of the crank shaft 94 is disposed in the bearing portion 88b. The bearing 90 rotatably supports the main shaft 96 inserted in the bearing 90. The housing 88 has the Oldham ring space Sr where the Oldham ring is disposed.


The driving motor 91 includes a ring-shaped stator 92 fixed to an inner wall surface of the circular cylindrical member 80a and a rotor 93 rotatably accommodated on an inner side of the stator 92 with a slight gap (air gap passage) therebetween. The rotor 93 is connected to the movable scroll 84 via the crank shaft 94 disposed so as to extend in an up-down direction along an axial center of the circular cylindrical member 80a. Due to the rotation of the rotor 93, the movable scroll 84 revolves with respect to the fixed scroll 82.


The crank shaft 94 transmits driving force of the driving motor 91 to the movable scroll 84. The crank shaft 94 is disposed so as to extend in the up-down direction along the axial center of the circular cylindrical member 80a, and connects the rotor 93 of the driving motor 91 and the movable scroll 84 of the scroll compression mechanism 81 to each other. The crank shaft 94 includes the main shaft 96 whose center axis coincides with the axial center of the circular cylindrical member 80a and the decentered portion 95 that is decentered with respect to the axial center of the circular cylindrical member 80a. The decentered portion 95 is inserted into the boss portion 84c of the movable scroll 84 as described above. The main shaft 96 is rotatably supported by the bearing 90 at the bearing portion 88b of the housing 88 and the lower bearing 98 described below. The main shaft 96 is connected to the rotor 93 of the driving motor 91 at a location between the bearing portion 88b and the lower bearing 98. The oil-supply path 97 for supplying the refrigerating-machine oil O to, for example, the scroll compression mechanism 81 is formed in the crank shaft 94. A lower end of the main shaft 96 is positioned in the oil-storage space So formed in the lower portion of the casing 80, and the refrigerating-machine oil O in the oil-storage space So is supplied to, for example, the scroll compression mechanism 81 via the oil-supply path 97.


The lower bearing 98 is disposed below the driving motor 91. The lower bearing 98 is fixed to the circular cylindrical member 80a. The lower bearing 98 constitutes a bearing on a lower end side of the crank shaft 94, and rotatably supports the main shaft 96 of the crank shaft 94.


Next, an operation of the compressor 21a is described.


When the driving motor 91 starts up, the rotor 93 rotates with respect to the stator 92, and the crank shaft 94 fixed to the rotor 93 rotates. When the crank shaft 94 rotates, the movable scroll 84 connected to the crank shaft 94 revolves with respect to the fixed scroll 82. A low-pressure gas refrigerant in a refrigeration cycle passes through the suction tube 19 and is sucked into the compression chamber Sc from a peripheral edge side of the compression chamber Sc. As the movable scroll 84 revolves, the suction tube 19 and the compression chamber Sc no longer communicate with each other. As the volume of the compression chamber Sc is reduced, the pressure in the compression chamber Sc starts to increase.


An intermediate-pressure refrigerant that has flowed through the economizer injection pipe 40a is supplied to the compression chamber Sc during compression via the horizontal passage portion 82f and the injection port 82g.


As the compression of the refrigerant progresses, the compression chamber Sc no longer communicates with the injection port 82g. The refrigerant in the compression chamber Sc is compressed as the volume of the compression chamber Sc is reduced, and finally becomes a high-pressure gas refrigerant. The high-pressure gas refrigerant is discharged from the discharge port 82d that is positioned near the center of the fixed-side end plate 82a. Thereafter, the high-pressure gas refrigerant passes through the refrigerant passage (not shown) formed in the fixed scroll 82 and the housing 88, and flows into the high-pressure space Sh. The high-pressure gas refrigerant in the refrigeration cycle that has flowed into the high-pressure space Sh and that has been compressed by the scroll compression mechanism 81 is discharged from the discharge tube 18.


In the air conditioning apparatus 1a, due to the refrigerant that has flowed through the economizer injection pipe 40a merging in the region of intermediate pressure of the compressor 21a, the temperature of the refrigerant having intermediate pressure in the compressor 21a can be reduced, so that it is possible to increase the operation efficiency in the refrigeration cycle.


(6-8) Modification C of the First Embodiment


In the Modification B of the first embodiment, a scroll compressor is used as an example of the compressor to describe the compressor.


In contrast, as the compressor that is used in the first embodiment, a compressor 21b, which is a rotary compressor in a second embodiment described below, may be used.


(7) Second Embodiment

With reference to FIG. 20, which is a schematic structural view of a refrigerant circuit, and FIG. 21, which is schematic control block structural view, an air conditioning apparatus 1b serving as a refrigeration cycle apparatus according to the second embodiment is described below.


The air conditioning apparatus 1b of the second embodiment is described below primarily by focusing on portions that differ from those of the air conditioning apparatus 1 of the first embodiment.


Even in the air conditioning apparatus 1b, a refrigerant circuit 10 is filled with a refrigerant that is a mixed refrigerant containing 1,2-difluoroethylene as a refrigerant for performing a vapor compression refrigeration cycle, and is filled with any one of the refrigerants A to E above. The refrigerant circuit 10 is filled with refrigerating-machine oil along with the refrigerant.


(7-1) Outdoor Unit 20


An outdoor unit 20 of the air conditioning apparatus 1b of the second embodiment includes the compressor 21b, a high-pressure receiver 42, an intermediate injection pipe 46, and an intermediate injection expansion valve 49 instead of the compressor 21, the low-pressure receiver 41, the suction injection pipe 40, the subcooling expansion valve 48, the subcooling heat exchanger 47, and the subcooling temperature sensor 67 of the outdoor unit 20 in the first embodiment.


The high-pressure receiver 42 is provided between an outdoor expansion valve 24 and a liquid-side shutoff valve 29 in a main flow path of the refrigerant circuit 10. The high-pressure receiver 42 has an internal space having positioned therein both an end portion of a pipe that extends from a side of the outdoor expansion valve 24 and an end portion of a pipe that extends from a side of the liquid-side shutoff valve 29, and is a container that is capable of storing a refrigerant.


The intermediate injection pipe 46 extends from a gas region of the internal space of the high-pressure receiver 42, and is a pipe that is connected to a region of intermediate pressure of the compressor 21b. The intermediate injection expansion valve 49 is provided in the intermediate injection pipe 46, and has a controllable valve opening degree.


(7-2) Indoor Unit 30


Since a first indoor unit 30 and a second indoor unit 35 of the second embodiment are the same as those of the first embodiment, they are not described.


(7-3) Cooling Operation Mode and Heating Operation Mode


In the air conditioning apparatus 1b above, in a cooling operation mode, the outdoor expansion valve 24 is controlled so that, for example, the subcooling degree of a refrigerant that passes through a liquid-side outlet of an outdoor heat exchanger 23 satisfies a predetermined condition. The intermediate injection expansion valve 49 is controlled so that a refrigerant that flows from the high-pressure receiver 42 is reduced up to an intermediate pressure in the compressor 21b.


In a heating operation mode, the outdoor expansion valve 24 is controlled so that, for example, the superheating degree of a refrigerant that is sucked by the compressor 21b satisfies a predetermined condition. The intermediate injection expansion valve 49 is controlled so that the refrigerant that flows from the high-pressure receiver 42 is reduced up to the intermediate pressure in the compressor 21b.


(7-4) Compressor 21b


As shown in FIG. 22, the compressor 21b is a 1-cylinder rotary compressor including a casing 111 and a driving mechanism 120 and a compression mechanism 130 that are disposed in the casing 111. In the compressor 21b, the compression mechanism 130 is disposed on a lower side of the driving mechanism 120 in the casing 111.


(7-4-1) Driving Mechanism


The driving mechanism 120 is accommodated in an upper portion of an internal space of the casing 111 and drives the compression mechanism 130. The driving mechanism 120 includes a motor 121 that is a drive source and a crank shaft 122 that is a drive shaft mounted on the motor 121.


The motor 121 is a motor for rotationally driving the crank shaft 122 and primarily includes a rotor 123 and a stator 124. The rotor 123 has the crank shaft 122 fitted into its internal space and rotates together with the crank shaft 122. The rotor 123 is constituted by electromagnetic steel plates that are stacked, and a magnet that is embedded in a rotor main body. The stator 124 is disposed on an outer side of the rotor 123 in a radial direction with a predetermined space from the rotor 123. The stator 124 is constituted by electromagnetic steel plates that are stacked, and a coil wound around a stator main body. The motor 121 causes the rotor 123 to rotate together with the crank shaft 122 by electromagnetic force that is generated at the stator 124 by causing an electric current to flow through the coil.


The crank shaft 122 is fitted into the rotor 123 and rotates around a rotation axis as a center. As shown in FIG. 23, a crank pin 122a, which is a decentered portion of the crank shaft 122, is inserted into a roller 180 (described below) of a piston 131 of the compression mechanism 130, and is fitted to the roller 180 with rotation force from the rotor 123 being in a transmittable state. The crank shaft 122 rotates in accordance with rotation of the rotor 123, causes the crank pin 122a to rotate in a decentered manner, and causes the roller 180 of the piston 131 of the compression mechanism 130 to revolve. That is, the crank shaft 122 has the function of transmitting driving force of the motor 121 to the compression mechanism 130.


(7-4-2) Compression Mechanism


The compression mechanism 130 is accommodated on a lower portion side in the casing 111. The compression mechanism 130 compresses a refrigerant sucked via a suction tube 196. The compression mechanism 130 is a rotary compression mechanism and primarily includes a front head 140, a cylinder 150, the piston 131, and a rear head 160. A refrigerant compressed in a compression chamber S1 of the compression mechanism 130 flows from a front-head discharge hole 141a that is formed in the front head 140 to a muffler space S2 surrounded by the front head 140 and a muffler 170, and is discharged to a space where the motor 121 is disposed and a lower end of the discharge tube 125 is positioned.


(7-4-2-1) Cylinder


The cylinder 150 is a metallic cast member. The cylinder 150 includes a circular cylindrical central portion 150a, a first extending portion 150b that extends toward a side of an attachment accumulator 195 from the central portion 150a, and a second extending portion 150c that extends to a side opposite to the first extending portion 150b from the central portion 150a. The first extending portion 150b has a suction hole 151 into which a lower-pressure refrigerant in a refrigeration cycle is sucked. A columnar space on an inner side of an inner peripheral surface 150a1 of the central portion 150a is a cylinder chamber 152 into which the refrigerant that is sucked from the suction hole 151 flows. The suction hole 151 extends toward an outer peripheral surface of the first extending portion 150b from the cylinder chamber 152 and is open at the outer peripheral surface of the first extending portion 150b. An end portion of the suction tube 196 extending from the accumulator 195 is inserted into the suction hole 151. For example, the piston 131 for compressing the refrigerant that has flowed into the cylinder chamber 152 is accommodated in the cylinder chamber 152.


The cylinder chamber 152 that is formed by the circular cylindrical central portion 150a of the cylinder 150 is open at a first end, which is a lower end of the cylinder chamber 152, and is also open at a second end, which is an upper end of the cylinder chamber 152. A first end, which is a lower end, of the central portion 150a is closed by the rear head 160 described below. A second end, which is an upper end, of the central portion 150a is closed by the front head 140 described below.


The cylinder 150 has a blade swing space 153 where a bush 135 and a blade 190 (described below) are disposed. The blade swing space 153 is formed in both the central portion 150a and the first extending portion 150b, and the blade 190 of the piston 131 is swingably supported by the cylinder 150 via the bush 135. The blade swing space 153 is formed so as to, in a plane, extend toward an outer peripheral side from the cylinder chamber 152 in the vicinity of the suction hole 151.


(7-4-2-2) Front Head


As shown in FIG. 22, the front head 140 includes a front-head disk portion 141 that closes an opening at a second end, which is an upper end, of the cylinder 150, and a front-head boss portion 142 that extends upward from a peripheral edge of a front-head opening in the center of the front-head disk portion 141. The front-head boss portion 142 has a circular cylindrical shape, and functions as a bearing of the crank shaft 122.


In a planar position shown in FIG. 23, the front-head disk portion 141 has the front-head discharge hole 141a. A refrigerant compressed in the compression chamber S1 whose volume changes in the cylinder chamber 152 of the cylinder 150 is intermittently discharged from the front-head discharge hole 141a. The front-head disk portion 141 is provided with a discharge valve that opens and closes an outlet of the front-head discharge hole 141a. The discharge valve opens due to a pressure difference when the pressure of the compression chamber S1 becomes higher than the pressure of the muffler space S2, and discharges the refrigerant to the muffler space S2 from the front-head discharge hole 141a.


(7-4-2-3) Muffler


As shown in FIG. 22, the muffler 170 is mounted on an upper surface of a peripheral edge portion of the front-head disk portion 141 of the front head 140. The muffler 170 forms, along with an upper surface of the front-head disk portion 141 and an outer peripheral surface of the front-head boss portion 142, the muffler space S2 to reduce noise generated by the discharge of a refrigerant. As described above, the muffler space S2 and the compression chamber S1 communicate with each other via the front-head discharge hole 141a when the discharge valve is open.


The muffler 170 has a center muffler opening that allows the front-head boss portion 142 to extend therethrough and a muffler discharge hole in which a refrigerant flows toward an accommodation space of the motor 121, disposed above, from the muffler space S2.


For example, the muffler space S2, the accommodation space of the motor 121, a space above the motor 121 where the discharge tube 125 is positioned, and a space below the compression mechanism 130 where a lubricant is accumulated are all connected to each other, and form a high-pressure space having equal pressure.


(7-4-2-4) Rear Head


The rear head 160 includes a rear-head disk portion 161 that closes an opening at a first end, which is a lower end, of the cylinder 150, and a rear-head boss portion 162 that extends downward from a peripheral edge portion of a central opening of the rear-head disk portion 161 and serves as a bearing. As shown in FIG. 23, the front-head disk portion 141, the rear-head disk portion 161, and the central portion 150a of the cylinder 150 form the cylinder chamber 152. The front-head boss portion 142 and the rear-head boss portion 162 are each a circular cylindrical boss portion, and support the crank shaft 122.


A supply flow path 161a is formed in the rear-head disk portion 161. The supply flow path 161a is connected to an injection hole (not shown) that opens in the casing 111, and is connected to the intermediate injection pipe 46. The supply flow path 161a extends horizontally toward a rotation axis CA of the crank shaft 122 from the injection hole of the casing 111, bends upward, and opens in an upper surface of the rear-head disk portion 161. An outlet opening 161a1 of the supply flow path 161a opens at a planar position shown by an alternate long and two short dashed line in FIG. 23. That is, the outlet opening 161a1 of the supply flow path 161a opens into the cylinder chamber 152 on an inner side of the inner peripheral surface 150a1 of the central portion 150a of the cylinder 150. The supply flow path 161a has the role of, when the angle of revolution of the roller 180 of the piston 131 is in a certain range, allowing an intermediate-pressure refrigerant introduced from the outside of the compressor 21b to flow to the compression chamber S1 whose volume changes in the cylinder chamber 152. Therefore, when the angle of revolution of the roller 180 of the piston 131 is in a predetermined range other than the certain range above, the supply flow path is closed by a part of a lower end surface of the roller 180.


(7-4-2-5) Piston


The piston 131 is disposed in the cylinder chamber 152 and is mounted on the crank pin 122a, which is the decentered portion of the crank shaft 122. The piston 131 is a member including the roller 180 and the blade 190 that are integrated with each other. The blade 190 of the piston 131 is disposed in the blade swing space 153 that is formed in the cylinder 150 and, as described above, is swingably supported by the cylinder 150 via the bush 135. The blade 190 is slidable with respect to the bush 135, and, during operation, swings and repeatedly moves away from the crank shaft 122 and moves toward the crank shaft 122.


The roller 180 includes a first end portion 181, where a first end surface 181a that is a roller lower end surface is formed, a second end portion 182, where a second end surface 182a that is a roller upper end surface is formed, and a central portion 183 that is positioned between the first end portion 181 and the second end portion 182. As shown in FIG. 24, the central portion 183 is a circular cylindrical portion having an inside diameter D2 and an outside diameter D1. The first end portion 181 includes a circular cylindrical first main body portion 181b that has an inside diameter D3 and an outside diameter D1, and a first protruding portion 181c that protrudes inward from the first main body portion 181b. The outside diameter D1 of the first main body portion 181b is equal to the outside diameter D1 of the central portion 183. The inside diameter D3 of the first main body portion 181b is larger than the inside diameter D2 of the central portion 183. The second end portion 182 includes a circular cylindrical second main body portion 182b having an inside diameter D3 and an outside diameter D1 and a second protruding portion 182c that protrudes inward from the second main body portion 182b. Similarly to the outside diameter D1 of the first main body portion 181b, the outside diameter D1 of the second main body portion 182b is equal to the outside diameter D1 of the central portion 183. The inside diameter D3 of the second main body portion 182b is equal to the inside diameter D3 of the first main body portion 181b, and is larger than the inside diameter D2 of the central portion 183. An inner surface 181c1 of the first protruding portion 181c and an inner surface 182c1 of the second protruding portion 182c substantially overlap an inner peripheral surface 183a1 of the central portion 183 when viewed in a direction of the rotation axis of the crank shaft 122. In detail, in plan view, the inner surface 181c1 of the first protruding portion 181c and the inner surface 182c1 of the second protruding portion 182c are positioned slightly outward with respect to the inner peripheral surface 183a1 of the central portion 183. In this way, when the first protruding portion 181c and the second protruding portion 182c are excluded, the inside diameters D3 of the first main body portion 181b and the second main body portion 182b are larger than the inside diameter D2 of the central portion 183. Therefore, a first stepped surface 183a2 is formed at a height position of a boundary between the first end portion 181 and the central portion 183, and a second stepped surface 183a3 is formed at a height position of a boundary between the second end portion 182 and the central portion 183 (see FIG. 24).


The ring-shaped first end surface 181a of the first end portion 181 of the roller 180 is in contact with the upper surface of the rear-head disk portion 161, and slides along the upper surface of the rear-head disk portion 161. The first end surface 181a of the roller 180 includes a first wide surface 181a1 whose width in a radial direction is partly large. The first protruding portion 181c of the first end portion 181 and a part of the first main body portion 181b of the first end portion 181 positioned outward with respect to the first protruding portion 181c form the first wide surface 181a1 (see FIG. 24).


The ring-shaped second end surface 182a of the second end portion 182 of the roller 180 is in contact with a lower surface of the front-head disk portion 141, and slides along the lower surface of the front-head disk portion 141. The second end surface 182a of the roller 180 includes a second wide surface 182a1 whose width in a radial direction is partly large. The second wide surface 182a1 is positioned in correspondence with the position of the first wide surface 181a1 when viewed in the direction of the rotation axis of the crank shaft 122. The second protruding portion 182c of the second end portion 182 and a part of the second main body portion 182b of the second end portion 182 positioned outward with respect to the second protruding portion 182c form the second wide surface 182a1.


As shown in FIG. 23, the roller 180 and the blade 190 of the piston 131 form the compression chamber S1 whose volume changes due to the revolution of the piston 131 while partitioning the cylinder chamber 152. The compression chamber S1 is a space that is surrounded by the inner peripheral surface 150a1 of the central portion 150a of the cylinder 150, the upper surface of the rear-head disk portion 161, the lower surface of the front-head disk portion 141, and the piston 131. The volume of the compression chamber S1 changes in accordance with the revolution of the piston 131, a low-pressure refrigerant sucked from the suction hole 151 is compressed and becomes a high-pressure refrigerant, and the refrigerant is discharged to the muffler space S2 from the front-head discharge hole 141a.


(7-4-3) Operation


In the compressor 21b above, movement of the piston 131 of the compression mechanism 130 that revolves due to rotation of the crank pin 122a in a decentered manner causes the volume of the compression chamber S1 to change. Specifically, first, a low-pressure refrigerant from the suction hole 151 is sucked into the compression chamber S1 while the piston 131 revolves. When the compression chamber S1 facing the suction hole 151 is sucking the refrigerant, the volume of the compression chamber S1 gradually increases. When the piston 131 revolves further, the state of communication between the compression chamber S1 and the suction hole 151 is stopped, and compression of the refrigerant is started in the compression chamber S1. Thereafter, after an intermediate-pressure refrigerant has been injected into the compression chamber S1 from the outlet opening 161a1 of the supply flow path 161a, the volume of the compression chamber S1 in a state of communication with the front-head discharge hole 141a becomes considerably small, and the pressure of the refrigerant is increased. Here, the first wide surface 181a1 of the first end surface 181a of the roller 180 of the piston 131 closes the outlet opening 161a1 of the supply flow path 161a of the rear-head disk portion 161, and the intermediate-pressure refrigerant is no longer in a state of being injected to the compression chamber S1. Thereafter, due to further revolution of the piston 131, the refrigerant whose pressure has become high pushes and opens the discharge valve from the front-head discharge hole 141a, and is discharged to the muffler space S2. The refrigerant introduced into the muffler space S2 is discharged to a space above the muffler space S2 from the muffler discharge hole of the muffler 170. The refrigerant discharged to the outside of the muffler space S2 passes through a space between the rotor 123 and the stator 124 of the motor 121, cools the motor 121, and is then discharged from the discharge tube 125.


(7-5) Features of the Second Embodiment


Similarly to the air conditioning apparatus 1 according to the first embodiment, since even the air conditioning apparatus 1b according to the second embodiment uses a refrigerant containing 1,2-difluoroethylene, the air conditioning apparatus 1b can sufficiently reduce GWP.


Since the air conditioning apparatus 1b can reduce the temperature of an intermediate-pressure refrigerant in the compressor 21b by causing a refrigerant that has flowed through the intermediate injection pipe 46 to merge at the region of intermediate pressure of the compressor 21b, the air conditioning apparatus 1b can improve an operation efficiency in a refrigeration cycle.


(7-6) Modification a of the Second Embodiment


Although, in the second embodiment, the air conditioning apparatus 1b is described by using as an example an air conditioning apparatus including a plurality of indoor units that are connected in parallel, an air conditioning apparatus including one indoor unit that is connected in series may be used as the air conditioning apparatus.


(7-7) Modification B of the Second Embodiment


In the second embodiment, the compressor 21b is described by using a rotary compressor as an example.


In contrast, as the compressor that is used in the second embodiment, the compressor 21a, which is the scroll compressor that is described in the Modification B of the first embodiment, may be used.


(7-8) Modification C of the Second Embodiment


The second embodiment is described by using as an example a case in which a gas refrigerant in the high-pressure receiver 42 is caused to merge at the region of intermediate pressure of the compressor 21b by the intermediate injection pipe 46.


In contrast, the gas refrigerant in the high-pressure receiver 42 in the second embodiment may be caused to merge on a suction side instead of at the region of intermediate pressure of the compressor. In this case, by reducing the temperature of the refrigerant that is sucked into the compressor, it is possible to increase the operation efficiency in a refrigeration cycle.


Although the embodiments of the present disclosure are described above, it is to be understood that various changes may 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, 1a, 1b air conditioning apparatus (refrigeration cycle apparatus)


    • 10 refrigerant circuit


    • 19 suction tube (suction flow path)


    • 20 outdoor unit


    • 21, 21a, 21b compressor


    • 23 outdoor heat exchanger (condenser, evaporator)


    • 24 outdoor expansion valve (decompressor)


    • 30 indoor unit, first indoor unit


    • 31 indoor heat exchanger, first indoor heat exchanger (evaporator, condenser)


    • 35 second indoor unit


    • 36 second indoor heat exchanger (evaporator, condenser)


    • 40 suction injection pipe (suction injection flow path, branching flow path)


    • 40
      a economizer injection pipe (intermediate injection flow path, branching flow path)


    • 42 high-pressure receiver (refrigerant storage tank)


    • 46 intermediate injection pipe (intermediate injection flow path)


    • 47 subcooling heat exchanger (injection heat exchanger)


    • 47
      a economizer heat exchanger (injection heat exchanger)


    • 48 subcooling expansion valve (opening degree adjusting valve)


    • 48
      a economizer expansion valve (opening degree adjusting valve)


    • 82 fixed scroll


    • 84 movable scroll (swinging scroll)


    • 196 suction tube (suction flow path)

    • Sc compression chamber





CITATION LIST
Patent Literature



  • [Patent Literature 1] International Publication No. 2015/141678


Claims
  • 1. A refrigeration cycle apparatus comprising: a compressor that sucks a refrigerant from a suction flow path, compresses the refrigerant, and discharges a high-pressure refrigerant, the refrigerant flowing through the suction flow path being a low-pressure refrigerant;a condenser that condenses the high-pressure refrigerant discharged from the compressor;a decompressor that decompresses the high-pressure refrigerant that has exited from the condenser;an evaporator that evaporates the refrigerant decompressed at the decompressor; andan injection flow path that is at least either one of an intermediate injection flow path and a suction injection flow path, the intermediate injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with an intermediate-pressure refrigerant in the compressor, the suction injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with the low-pressure refrigerant that is sucked by the compressor whereinthe refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (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 IJ, JN, NE, and EI that connect the following 4 points:point I (72.0, 0.0, 28.0),point J (48.5, 18.3, 33.2),point N (27.7, 18.2, 54.1), andpoint E (58.3, 0.0, 41.7),or on these line segments (excluding the points on the line segment EI; the line segment U is represented by coordinates (0.0236y2−1.7616y+72.0, y, −0.0236y2+0.7616y+28.0);the line segment NE is represented by coordinates (0.012y2-1.9003y+58.3, y, −0.012y2+0.9003y+41.7); andthe line segments JN and EI are straight lines.
  • 2. The refrigeration cycle apparatus according to claim 1, further comprising: a branching flow path that branches off from a main refrigerant flow path that connects the condenser and the evaporator to each other;an opening degree adjusting valve that is provided in the branching flow path; andan injection heat exchanger that causes the refrigerant that flows in the main refrigerant flow path and the refrigerant that flows on a downstream side with respect to the opening degree adjusting valve in the branching flow path to exchange heat,wherein the refrigerant that exits from the injection heat exchanger and flows in the branching flow path flows in the injection flow path.
  • 3. The refrigeration cycle apparatus according to claim 1, further comprising: a refrigerant storage tank that is provided in a main refrigerant flow path that connects the condenser and the evaporator to each other,wherein a gas component of the refrigerant that accumulates in the refrigerant storage tank flows in the injection flow path.
  • 4. The refrigeration cycle apparatus according to claim 1, wherein the compressor includes a fixed scroll and a swinging scroll, the fixed scroll including an end plate and a lap that stands spirally from the end plate, the swinging scroll forming a compression chamber (Sc) by engaging with the fixed scroll, andthe refrigerant that flows in the injection flow path merges at the compression chamber.
  • 5. A refrigeration cycle apparatus comprising: a compressor that sucks a refrigerant from a suction flow path, compresses the refrigerant, and discharges a high-pressure refrigerant, the refrigerant flowing through the suction flow path being a low-pressure refrigerant;a condenser that condenses the high-pressure refrigerant discharged from the compressor;a decompressor that decompresses the high-pressure refrigerant that has exited from the condenser;an evaporator that evaporates the refrigerant decompressed at the decompressor; andan injection flow path that is at least either one of an intermediate injection flow path and a suction injection flow path, the intermediate injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with an intermediate-pressure refrigerant in the compressor, the suction injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with the low-pressure refrigerant that is sucked by the compressor, whereinthe refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (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 MM′, M′N, NV, VG; and GM that connect the following 5 points:point M (52.6, 0.0, 47.4),point M′(39.2, 5.0, 55.8),point N (27.7, 18.2, 54.1),point V (11.0, 18.1, 70.9), andpoint G (39.6, 0.0, 60.4),or on these line segments (excluding the points on the line segment GM); the line segment MM′ is represented by coordinates (0.132y2−3.34y+52.6, y, −0.132y2+2.34y+47.4);the line segment MN is represented by coordinates (0.0596y2−2.2541y+48.98, y, −0.0596y2+1.2541y+51.02);the line segment VG is represented by coordinates (0.0123y2−1.8033y+39.6, y, −0.0123y2+0.8033y+60.4); andthe line segments NV and GM are straight lines.
  • 6. The refrigeration cycle apparatus according to claim 5, further comprising: a branching flow path that branches off from a main refrigerant flow path that connects the condenser and the evaporator to each other;an opening degree adjusting valve that is provided in the branching flow path; andan injection heat exchanger that causes the refrigerant that flows in the main refrigerant flow path and the refrigerant that flows on a downstream side with respect to the opening degree adjusting valve in the branching flow path to exchange heat,wherein the refrigerant that exits from the injection heat exchanger and flows in the branching flow path flows in the injection flow path.
  • 7. The refrigeration cycle apparatus according to claim 5, further comprising: a refrigerant storage tank that is provided in a main refrigerant flow path that connects the condenser and the evaporator to each other,wherein a gas component of the refrigerant that accumulates in the refrigerant storage tank flows in the injection flow path.
  • 8. The refrigeration cycle apparatus according to claim 5, wherein the compressor includes a fixed scroll and a swinging scroll, the fixed scroll including an end plate and a lap that stands spirally from the end plate, the swinging scroll forming a compression chamber (Sc) by engaging with the fixed scroll, andthe refrigerant that flows in the injection flow path merges at the compression chamber.
  • 9. A refrigeration cycle apparatus comprising: a compressor that sucks a refrigerant from a suction flow path, compresses the refrigerant, and discharges a high-pressure refrigerant, the refrigerant flowing through the suction flow path being a low-pressure refrigerant;a condenser that condenses the high-pressure refrigerant discharged from the compressor;a decompressor that decompresses the high-pressure refrigerant that has exited from the condenser;an evaporator that evaporates the refrigerant decompressed at the decompressor; andan injection flow path that is at least either one of an intermediate injection flow path and a suction injection flow path, the intermediate injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with an intermediate-pressure refrigerant in the compressor, the suction injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with the low-pressure refrigerant that is sucked by the compressor, whereinthe refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (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 ON, NU, and UO that connect the following 3 points:point O (22.6, 36.8, 40.6),point N (27.7, 18.2, 54.1), andpoint U (3.9, 36.7, 59.4),or on these line segments; the line segment ON is represented by coordinates (0.0072y2−0.6701y+37.512, y, −0.0072y2−0.3299y+62.488);the line segment NU is represented by coordinates (0.0083y2−1.7403y+56.635, y, −0.0083y2+0.7403y+43.365); andthe line segment UO is a straight line.
  • 10. The refrigeration cycle apparatus according to claim 9, further comprising: a branching flow path that branches off from a main refrigerant flow path that connects the condenser and the evaporator to each other;an opening degree adjusting valve that is provided in the branching flow path; andan injection heat exchanger that causes the refrigerant that flows in the main refrigerant flow path and the refrigerant that flows on a downstream side with respect to the opening degree adjusting valve in the branching flow path to exchange heat,wherein the refrigerant that exits from the injection heat exchanger and flows in the branching flow path flows in the injection flow path.
  • 11. The refrigeration cycle apparatus according to claim 9, further comprising: a refrigerant storage tank that is provided in a main refrigerant flow path that connects the condenser and the evaporator to each other,wherein a gas component of the refrigerant that accumulates in the refrigerant storage tank flows in the injection flow path.
  • 12. The refrigeration cycle apparatus according to claim 9, wherein the compressor includes a fixed scroll and a swinging scroll, the fixed scroll including an end plate and a lap that stands spirally from the end plate, the swinging scroll forming a compression chamber (Sc) by engaging with the fixed scroll, andthe refrigerant that flows in the injection flow path merges at the compression chamber.
  • 13. A refrigeration cycle apparatus comprising: a compressor that sucks a refrigerant from a suction flow path, compresses the refrigerant, and discharges a high-pressure refrigerant, the refrigerant flowing through the suction flow path being a low-pressure refrigerant;a condenser that condenses the high-pressure refrigerant discharged from the compressor;a decompressor that decompresses the high-pressure refrigerant that has exited from the condenser;an evaporator that evaporates the refrigerant decompressed at the decompressor; andan injection flow path that is at least either one of an intermediate injection flow path and a suction injection flow path, the intermediate injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with an intermediate-pressure refrigerant in the compressor, the suction injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with the low-pressure refrigerant that is sucked by the compressor, whereinthe refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (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 QR, RT, TL, LK, and KQ that connect the following 5 points:point Q (44.6, 23.0, 32.4),point R (25.5, 36.8, 37.7),point T (8.6, 51.6, 39.8),point L (28.9, 51.7, 19.4), andpoint K (35.6, 36.8, 27.6),or on these line segments; the line segment QR is represented by coordinates (0.0099y2−1.975y+84.765, y, −0.0099y2+0.975y+15.235);the line segment RT is represented by coordinates (0.0082y2−1.8683y+83.126, y, −0.0082y2+0.8683y+16.874);the line segment LK is represented by coordinates (0.0049y2-0.8842y+61.488, y, −0.0049y2−0.1158y+38.512);the line segment KQ is represented by coordinates (0.0095y2−1.2222y+67.676, y, −0.0095y2+0.2222y+32.324); andthe line segment TL is a straight line.
  • 14. The refrigeration cycle apparatus according to claim 13, further comprising: a branching flow path that branches off from a main refrigerant flow path that connects the condenser and the evaporator to each other;an opening degree adjusting valve that is provided in the branching flow path; andan injection heat exchanger that causes the refrigerant that flows in the main refrigerant flow path and the refrigerant that flows on a downstream side with respect to the opening degree adjusting valve in the branching flow path to exchange heat,wherein the refrigerant that exits from the injection heat exchanger and flows in the branching flow path flows in the injection flow path.
  • 15. The refrigeration cycle apparatus according to claim 13, further comprising: a refrigerant storage tank that is provided in a main refrigerant flow path that connects the condenser and the evaporator to each other,wherein a gas component of the refrigerant that accumulates in the refrigerant storage tank flows in the injection flow path.
  • 16. The refrigeration cycle apparatus according to claim 13, wherein the compressor includes a fixed scroll and a swinging scroll, the fixed scroll including an end plate and a lap that stands spirally from the end plate, the swinging scroll forming a compression chamber (Sc) by engaging with the fixed scroll, andthe refrigerant that flows in the injection flow path merges at the compression chamber.
  • 17. The refrigeration cycle apparatus according claim 1, A refrigeration cycle apparatus comprising: a compressor that sucks a refrigerant from a suction flow path, compresses the refrigerant, and discharges a high-pressure refrigerant, the refrigerant flowing through the suction flow path being a low-pressure refrigerant;a condenser that condenses the high-pressure refrigerant discharged from the compressor;a decompressor that decompresses the high-pressure refrigerant that has exited from the condenser;an evaporator that evaporates the refrigerant decompressed at the decompressor; andan injection flow path that is at least either one of an intermediate injection flow path and a suction injection flow path, the intermediate injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with an intermediate-pressure refrigerant in the compressor, the suction injection flow path allowing a part of the refrigerant that flows toward the evaporator from the condenser to merge with the low-pressure refrigerant that is sucked by the compressor, whereinthe refrigerant comprises trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (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 PS, ST, and TP that connect the following 3 points:point P (20.5, 51.7, 27.8),point S (21.9, 39.7, 38.4), andpoint T (8.6, 51.6, 39.8),or on these line segments; the line segment PS is represented by coordinates (0.0064y2−0.7103y+40.1, y, −0.0064y2−0.2897y+59.9);the line segment ST is represented by coordinates (0.0082y2−1.8683y+83.126, y, −0.0082y2+0.8683y+16.874); andthe line segment TP is a straight line.
  • 18. The refrigeration cycle apparatus according to claim 17, further comprising: a branching flow path that branches off from a main refrigerant flow path that connects the condenser and the evaporator to each other;an opening degree adjusting valve that is provided in the branching flow path; andan injection heat exchanger that causes the refrigerant that flows in the main refrigerant flow path and the refrigerant that flows on a downstream side with respect to the opening degree adjusting valve in the branching flow path to exchange heat,wherein the refrigerant that exits from the injection heat exchanger and flows in the branching flow path flows in the injection flow path.
  • 19. The refrigeration cycle apparatus according to claim 17, further comprising: a refrigerant storage tank that is provided in a main refrigerant flow path that connects the condenser and the evaporator to each other,wherein a gas component of the refrigerant that accumulates in the refrigerant storage tank flows in the injection flow path.
  • 20. The refrigeration cycle apparatus according to claim 17, wherein the compressor includes a fixed scroll and a swinging scroll, the fixed scroll including an end plate and a lap that stands spirally from the end plate, the swinging scroll forming a compression chamber (Sc) by engaging with the fixed scroll, andthe refrigerant that flows in the injection flow path merges at the compression chamber.
Priority Claims (9)
Number Date Country Kind
JP2017-242183 Dec 2017 JP national
JP2017-242185 Dec 2017 JP national
JP2017-242186 Dec 2017 JP national
JP2017-242187 Dec 2017 JP national
PCT/JP2018/037483 Oct 2018 WO international
PCT/JP2018/038746 Oct 2018 WO international
PCT/JP2018/038747 Oct 2018 WO international
PCT/JP2018/038748 Oct 2018 WO international
PCT/JP2018/038749 Oct 2018 WO international
US Referenced Citations (101)
Number Name Date Kind
5185092 Fukuda et al. Feb 1993 A
5344069 Narikiyo Sep 1994 A
5851968 Schnur Dec 1998 A
6591631 Taira Jul 2003 B1
6667285 Kawahara et al. Dec 2003 B1
8358040 Komuro et al. Jan 2013 B2
10131827 Fukushima et al. Nov 2018 B2
10883745 Higashiiue et al. Jan 2021 B2
20020140309 Yanashima et al. Oct 2002 A1
20020193262 Kaimai et al. Dec 2002 A1
20040011062 Taira Jan 2004 A1
20060000224 Matsuoka Jan 2006 A1
20070209373 Taira et al. Sep 2007 A1
20080184723 Sato et al. Aug 2008 A1
20080184731 Sienel et al. Aug 2008 A1
20080188173 Chen et al. Aug 2008 A1
20090260382 Takeichi et al. Oct 2009 A1
20100067264 Ohashi et al. Mar 2010 A1
20100082162 Mundy et al. Apr 2010 A1
20100122545 Minor et al. May 2010 A1
20110108756 Tsuchiya et al. May 2011 A1
20110167848 Wakashima et al. Jul 2011 A1
20120260679 Huerta-Ochoa Oct 2012 A1
20140070132 Fukushima Mar 2014 A1
20140077123 Fukushima Mar 2014 A1
20140291411 Tamaki et al. Oct 2014 A1
20140314606 Maeyama et al. Oct 2014 A1
20140373569 Tsuboe et al. Dec 2014 A1
20150001981 Hattori et al. Jan 2015 A1
20150075203 Mochizuki et al. Mar 2015 A1
20150096321 Kawano et al. Apr 2015 A1
20150143841 Kawano May 2015 A1
20150256038 Nigo et al. Sep 2015 A1
20150362199 Yumoto et al. Dec 2015 A1
20150376486 Hashimoto et al. Dec 2015 A1
20160018135 Yuzawa et al. Jan 2016 A1
20160075927 Fukushima Mar 2016 A1
20160131378 Hinokuma et al. May 2016 A1
20160276886 Baba et al. Sep 2016 A1
20160333241 Fukushima et al. Nov 2016 A1
20160333243 Fukushima et al. Nov 2016 A1
20160340565 Tasaka et al. Nov 2016 A1
20160348933 Takeuchi et al. Dec 2016 A1
20160355719 Fukushima et al. Dec 2016 A1
20170002245 Fukushima Jan 2017 A1
20170058172 Fukushima et al. Mar 2017 A1
20170058173 Fukushima Mar 2017 A1
20170058174 Fukushima et al. Mar 2017 A1
20170121581 Horiike et al. May 2017 A1
20170138642 Ueno May 2017 A1
20170166831 Matsumoto Jun 2017 A1
20170248328 Eskew et al. Aug 2017 A1
20170328586 Maeyama Nov 2017 A1
20170336085 Yasuo et al. Nov 2017 A1
20170338707 Shono et al. Nov 2017 A1
20180051198 Okamoto Feb 2018 A1
20180094844 Suzuki Apr 2018 A1
20180138763 Nakamura et al. May 2018 A1
20180156217 Sakima et al. Jun 2018 A1
20180156511 Chikami et al. Jun 2018 A1
20180254676 Nigo et al. Sep 2018 A1
20180299175 Hayamizu et al. Oct 2018 A1
20180320942 Hayamizu et al. Nov 2018 A1
20180331436 Hayamizu et al. Nov 2018 A1
20180358861 Hayamizu et al. Dec 2018 A1
20190063773 Nagahashi et al. Feb 2019 A1
20190068015 Yabe et al. Feb 2019 A1
20190309963 Zaki et al. Oct 2019 A1
20200079985 Okamoto et al. Mar 2020 A1
20200321816 Watanabe Oct 2020 A1
20200325375 Kumakura et al. Oct 2020 A1
20200325376 Kumakura et al. Oct 2020 A1
20200325377 Kumakura et al. Oct 2020 A1
20200326100 Ukibune et al. Oct 2020 A1
20200326101 Itano et al. Oct 2020 A1
20200326102 Kumakura et al. Oct 2020 A1
20200326103 Kumakura et al. Oct 2020 A1
20200326105 Kumakura et al. Oct 2020 A1
20200326109 Kumakura et al. Oct 2020 A1
20200326110 Asano et al. Oct 2020 A1
20200332164 Itano et al. Oct 2020 A1
20200332166 Kumakura et al. Oct 2020 A1
20200333041 Itano et al. Oct 2020 A1
20200333054 Asano et al. Oct 2020 A1
20200347283 Itano et al. Nov 2020 A1
20200363085 Itano et al. Nov 2020 A1
20200363105 Kumakura et al. Nov 2020 A1
20200363106 Itano et al. Nov 2020 A1
20200363112 Ohtsuka et al. Nov 2020 A1
20200369934 Itano et al. Nov 2020 A1
20200385620 Itano et al. Dec 2020 A1
20200385621 Itano et al. Dec 2020 A1
20200385622 Itano et al. Dec 2020 A1
20200392387 Ohtsuka et al. Dec 2020 A1
20200392388 Itano et al. Dec 2020 A1
20200393178 Kumakura et al. Dec 2020 A1
20210018191 Itano et al. Jan 2021 A1
20210135520 Shimokawa et al. May 2021 A1
20210189209 Yotdumoto et al. Jun 2021 A1
20210222040 Fukushima et al. Jul 2021 A1
20210355359 Ohkubo et al. Nov 2021 A1
Foreign Referenced Citations (244)
Number Date Country
2001284508 Mar 2002 AU
1288132 Mar 2001 CN
1447491 Oct 2003 CN
1455855 Nov 2003 CN
1723373 Jan 2006 CN
1987264 Jun 2007 CN
101235815 Aug 2008 CN
101441012 May 2009 CN
102401519 Apr 2012 CN
103562338 Feb 2014 CN
203704143 Jul 2014 CN
103975204 Aug 2014 CN
104094069 Oct 2014 CN
104456760 Mar 2015 CN
104578493 Apr 2015 CN
204534884 Aug 2015 CN
104903661 Sep 2015 CN
104937350 Sep 2015 CN
204648544 Sep 2015 CN
105102905 Nov 2015 CN
204943959 Jan 2016 CN
205261858 May 2016 CN
106029821 Oct 2016 CN
106030222 Oct 2016 CN
106062159 Oct 2016 CN
106085363 Nov 2016 CN
106103992 Nov 2016 CN
106133110 Nov 2016 CN
106414653 Feb 2017 CN
106414654 Feb 2017 CN
106415152 Feb 2017 CN
106574802 Apr 2017 CN
106661477 May 2017 CN
106839496 Jun 2017 CN
107110570 Aug 2017 CN
107112830 Aug 2017 CN
107429957 Dec 2017 CN
107614980 Jan 2018 CN
107925285 Apr 2018 CN
108139112 Jun 2018 CN
108431414 Aug 2018 CN
108469126 Aug 2018 CN
1 231 255 Aug 2002 EP
1 246 348 Oct 2002 EP
1 326 057 Jul 2003 EP
1 632 732 Mar 2006 EP
1 953 388 Aug 2008 EP
2 423 609 Feb 2012 EP
2 620 736 Jul 2013 EP
2 711 405 Mar 2014 EP
2 789 933 Oct 2014 EP
2 840 335 Feb 2015 EP
2 853 826 Apr 2015 EP
2 918 953 Sep 2015 EP
2 952 828 Dec 2015 EP
2 980 508 Feb 2016 EP
3 012 555 Apr 2016 EP
3 012 557 Apr 2016 EP
3 070 417 Sep 2016 EP
3 109 302 Dec 2016 EP
3 101082 Dec 2016 EP
3 115 716 Jan 2017 EP
3 121 242 Jan 2017 EP
3 128 259 Feb 2017 EP
3 147 595 Mar 2017 EP
3 153 559 Apr 2017 EP
3 153 561 Apr 2017 EP
3 170 881 May 2017 EP
3 222 934 Sep 2017 EP
3 249 309 Nov 2017 EP
3 299 731 Mar 2018 EP
3 358 272 Aug 2018 EP
3 358 278 Aug 2018 EP
3 399 189 Nov 2018 EP
2530915 Apr 2016 GB
51-90115 Jul 1976 JP
52-13025 Apr 1977 JP
57-198968 Dec 1982 JP
59-39790 Mar 1984 JP
62-69066 Mar 1987 JP
63-69066 Mar 1987 JP
2-4163 Jan 1990 JP
5-264070 Oct 1993 JP
5-272823 Oct 1993 JP
7-19627 Jan 1995 JP
7-190571 Jul 1995 JP
8-200273 Aug 1996 JP
08200273 Aug 1996 JP
10-46170 Feb 1998 JP
10-300292 Nov 1998 JP
10-309050 Nov 1998 JP
10-318564 Dec 1998 JP
11-206001 Jul 1999 JP
11-256358 Sep 1999 JP
2000-161805 Jun 2000 JP
2000-220877 Aug 2000 JP
2000-234767 Aug 2000 JP
2000-304302 Nov 2000 JP
2001-82755 Mar 2001 JP
2001-139972 May 2001 JP
2002-54888 Feb 2002 JP
2002-89978 Mar 2002 JP
2002-257366 Sep 2002 JP
2002-272043 Sep 2002 JP
2002-318028 Oct 2002 JP
2003-18776 Jan 2003 JP
2003-83614 Mar 2003 JP
2003-174794 Jun 2003 JP
2004-28035 Jan 2004 JP
2004-132647 Apr 2004 JP
2004-215406 Jul 2004 JP
2004-251535 Sep 2004 JP
2004-361036 Dec 2004 JP
2005-61711 Mar 2005 JP
2005-241045 Sep 2005 JP
2005-288502 Oct 2005 JP
2006-162197 Jun 2006 JP
2006-211824 Aug 2006 JP
2006-313027 Nov 2006 JP
2008-39305 Feb 2008 JP
2008-54488 Mar 2008 JP
2008-190377 Aug 2008 JP
2008-245384 Oct 2008 JP
2008-286422 Nov 2008 JP
2009-63216 Mar 2009 JP
2009-92274 Apr 2009 JP
2009-121654 Jun 2009 JP
2009-150620 Jul 2009 JP
2009-299975 Dec 2009 JP
2010-28985 Feb 2010 JP
2010-103346 May 2010 JP
2010-119190 May 2010 JP
2010-164222 Jul 2010 JP
2010-230242 Oct 2010 JP
2011-4449 Jan 2011 JP
2011-43304 Mar 2011 JP
2011-52884 Mar 2011 JP
2011-94841 May 2011 JP
2011-135638 Jul 2011 JP
2011-202738 Oct 2011 JP
2011-252636 Dec 2011 JP
2012-42169 Mar 2012 JP
2012-112617 Jun 2012 JP
2012-132637 Jul 2012 JP
2012-151969 Aug 2012 JP
2013-124848 Jun 2013 JP
2013-126281 Jun 2013 JP
2013-139990 Jul 2013 JP
2013-155892 Aug 2013 JP
2013-155921 Aug 2013 JP
2013-172615 Sep 2013 JP
2013-200090 Oct 2013 JP
2013-221671 Oct 2013 JP
2014-70840 Apr 2014 JP
2014-75971 Apr 2014 JP
2014-89004 May 2014 JP
2014-129543 Jul 2014 JP
2014-152999 Aug 2014 JP
2014-167381 Sep 2014 JP
2015-23721 Feb 2015 JP
2015-55455 Mar 2015 JP
2015-78789 Apr 2015 JP
2015-82875 Apr 2015 JP
2015-111012 Jun 2015 JP
2015-114082 Jun 2015 JP
2015-145765 Aug 2015 JP
2015-158282 Sep 2015 JP
2015-218909 Dec 2015 JP
2015-218912 Dec 2015 JP
2015-229767 Dec 2015 JP
2016-1062 Jan 2016 JP
2016-11423 Jan 2016 JP
2016-56340 Apr 2016 JP
2016-125808 Jul 2016 JP
2016-133256 Jul 2016 JP
2016-172869 Sep 2016 JP
2016-174461 Sep 2016 JP
2017-36861 Feb 2017 JP
2017-46430 Mar 2017 JP
2017-53285 Mar 2017 JP
2017-67373 Apr 2017 JP
2017-67428 Apr 2017 JP
2017-122549 Jul 2017 JP
2017-145975 Aug 2017 JP
2017-192190 Oct 2017 JP
2018-25377 Feb 2018 JP
2001-0029975 Apr 2001 KR
2003-0028838 Apr 2003 KR
10-0939609 Oct 2003 KR
10-2004-0075737 Aug 2004 KR
10-2005-0044931 May 2005 KR
10-2017-0034887 Mar 2017 KR
2013 156 380 Jun 2015 RU
20030103482 Feb 2003 TW
0136571 May 2001 WO
0223100 Mar 2002 WO
2009069679 Jun 2009 WO
2009093345 Jul 2009 WO
2012157764 Nov 2012 WO
2012157765 Nov 2012 WO
WO-2012157765 Nov 2012 WO
2013084301 Jun 2013 WO
2013146103 Oct 2013 WO
2013146208 Oct 2013 WO
2013151043 Oct 2013 WO
2014045400 Mar 2014 WO
2014118945 Aug 2014 WO
2014119149 Aug 2014 WO
2014156190 Oct 2014 WO
2014203353 Dec 2014 WO
2014203354 Dec 2014 WO
2015071967 May 2015 WO
2015115252 Aug 2015 WO
2015125763 Aug 2015 WO
2015125884 Aug 2015 WO
2015136981 Sep 2015 WO
2015140827 Sep 2015 WO
2015141678 Sep 2015 WO
2015186557 Dec 2015 WO
2015186670 Dec 2015 WO
2016009884 Jan 2016 WO
2016017460 Feb 2016 WO
2016103711 Jun 2016 WO
2016104418 Jun 2016 WO
2016117443 Jul 2016 WO
2016157538 Oct 2016 WO
2016182030 Nov 2016 WO
2016190232 Dec 2016 WO
2017038489 Mar 2017 WO
2017056789 Apr 2017 WO
2017057004 Apr 2017 WO
2017115636 Jul 2017 WO
2017122517 Jul 2017 WO
2017195248 Nov 2017 WO
2019123782 Jun 2019 WO
2019123804 Jun 2019 WO
2019123805 Jun 2019 WO
2019123806 Jun 2019 WO
2019123807 Jun 2019 WO
2019124400 Jun 2019 WO
2019124401 Jun 2019 WO
2019124402 Jun 2019 WO
2019124403 Jun 2019 WO
2019124404 Jun 2019 WO
Non-Patent Literature Citations (74)
Entry
International Search Report dated Mar. 19, 2019 in International Application No. PCT/JP2018/046531.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046531.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/045978.
International Search Report dated Mar. 19, 2019 in International Application No. PCT/JP2018/045978.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046532.
International Search Report dated Feb. 12, 2019 in International Application No. PCT/JP2018/046532.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/042027.
International Search Report dated Feb. 12, 2019 in International Application No. PCT/JP2018/042027.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/042032.
International Search Report dated Feb. 19, 2019 in International Application No. PCT/JP2018/042032.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046666.
International Search Report dated Apr. 2, 2019 in International Application No. PCT/JP2018/046666.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/045336.
International Search Report dated Feb. 19, 2019 in International Application No. PCT/JP2018/045336.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/045557.
International Search Report dated Mar. 12, 2019 in International Application No. PCT/JP2018/045557.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046426.
International Search Report dated Feb. 19, 2019 in International Application No. PCT/JP2018/046426
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046427.
International Search Report dated Feb. 19, 2019 in International Application No. PCT/JP2018/046427.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046428.
International Search Report dated Mar. 19, 2019 in International Application No. PCT/JP2018/046428.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046581.
International Search Report dated Mar. 5, 2019 in International Application No. PCT/JP2018/046581.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046630.
International Search Report dated Mar. 5, 2019 in International Application No. PCT/JP2018/046630.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046582.
International Search Report dated Mar. 5, 2019 in International Application No. PCT/JP2018/046582.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046631.
International Search Report dated Mar. 5, 2019 in International Application No. PCT/JP2018/046631.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046627.
International Search Report dated Mar. 19, 2019 in International Application No. PCT/JP2018/046627.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046628.
International Search Report dated Mar. 19, 2019 in International Application No. PCT/JP2018/046628.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/045979.
International Search Report dated Mar. 12, 2019 in International Application No. PCT/JP2018/045979
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046434.
International Search Report dated Feb. 19, 2019 in International Application No. PCT/JP2018/046434.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/045290.
International Search Report dated Jan. 22, 2019 in International Application No. PCT/JP2018/045290.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/045288.
International Search Report dated Jan. 22, 2019 in International Application No. PCT/JP2018/045288.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/045289.
International Search Report dated Jan. 22, 2019 in International Application No. PCT/JP2018/045289.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046639.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046642.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/038746.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046643.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/038748.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046640.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046644.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/038749.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/037483.
International Search Report dated Feb. 19, 2019 in International Application No. PCT/JP2018/045335
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/045335.
International Search Report dated Feb. 19, 2019 in International Application No. PCT/JP2018/046435.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046435.
International Search Report dated Mar. 19, 2019 in International (PCT) Application No. PCT/JP2018/046530.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046530.
International Search Report dated Feb. 12, 2019 in International (PCT) Application No. PCT/JP2018/046533.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/046533.
Hirahara et al., “Latest trend of alternative refrigerant: LCCP-analogy for HFO-1234yf Air Conditioners using a Simulation with R134a Properties”, Refrigeration, Jan. 15, 2010, vol. 85, No. 987, pp. 15-20, with partial translation.
International Preliminary Report on Patentability dated Jun. 23, 2020 in International Application No. PCT/JP2018/038747.
International Search Report dated Mar. 12, 2019 in International (PCT) Application No. PCT/JP2018/046639.
International Search Report dated Mar. 12, 2019 in International (PCT) Application No. PCT/JP2018/046642.
International Search Report dated Dec. 18, 2018 in International (PCT) Application No. PCT/JP2018/038746.
International Search Report dated Mar. 19, 2019 in International (PCT) Application No. PCT/JP2018/046643.
International Search Report dated Dec. 18, 2018 in International (PCT) Application No. PCT/JP2018/038748.
International Search Report dated Mar. 12, 2019 in International (PCT) Application No. PCT/JP2018/046640.
International Search Report dated Mar. 19, 2019 in International (PCT) Application No. PCT/JP2018/046644.
International Search Report dated Dec. 18, 2018 in International (PCT) Application No. PCT/JP2018/038749.
International Search Report dated Dec. 18, 2018 in International (PCT) Application No. PCT/JP2018/037483
International Search Report dated Dec. 18, 2018 in International (PCT) Application No. PCT/JP2018/038747.
Summary, Collection of Papers of the 2nd Symposium on New Technologies of Refrigeration and Air Conditioning, 2nd Edition, Ding Guoliang, Ed., published by Shanghai Jiatong University Press, 2003, with Concise Explanation.
Related Publications (1)
Number Date Country
20200326101 A1 Oct 2020 US
Continuation in Parts (1)
Number Date Country
Parent 16955222 US
Child 16912055 US