REFRIGERANT CYCLE APPARATUS

Information

  • Patent Application
  • 20240174905
  • Publication Number
    20240174905
  • Date Filed
    February 02, 2024
    10 months ago
  • Date Published
    May 30, 2024
    6 months ago
Abstract
A showcase includes a refrigerant circuit and a refrigerant enclosed in the refrigerant circuit. The refrigerant circuit includes a compressor (121), a radiator (122), an expansion valve (123), and an evaporator (124). The refrigerant is a low-GWP refrigerant.
Description
TECHNICAL FIELD

It relates to a refrigerant cycle apparatus for freezing or cold storage.


BACKGROUND ART

Hitherto, heat cycle systems such as apparatuses for freezing or cold storage frequently use R410A or R404A as a refrigerant. R410A is a two-component mixed refrigerant of (CH2F2; HFC-32 or R32) and pentafluoroethane (C2HF5; HFC-125 or R125), and is a pseudo-azeotropic composition. R404A is a three-component mixed refrigerant of R125, R134a, and R143a, and is a pseudo-azeotropic composition.


However, the global warming potential (GWP) of R410A is 2088, and the global warming potential (GWP) of R404A is 3920. In recent years, a refrigerant having a low GWP tends to be used due to an increasing concern about global warming.


Due to this, for example, PTL 1 (International Publication No. 2015/141678) suggests a low-GWP mixed refrigerant alternative to R410A. Moreover, PTL 2 (Japanese Unexamined Patent Application Publication No. 2018-184597) suggests various low-GWP mixed refrigerants alternative to R404A.


SUMMARY OF INVENTION
Technical Problem

Hitherto, no study has been made which refrigerant among refrigerants with low GWPs should be used for a refrigerant cycle apparatus for freezing or cold storage.


Solution to Problem

A refrigerant cycle apparatus for freezing or cold storage according to a first aspect includes a refrigerant circuit and a refrigerant enclosed in the refrigerant circuit. The refrigerant circuit includes a compressor, a radiator, a decompressing portion, and a heat absorber. The refrigerant contains at least 1,2-difluoroethylene.


A refrigerant cycle apparatus for freezing or cold storage according to a sixteenth aspect is the refrigerant cycle for freezing or cold storage according to the first aspect, wherein the refrigerant contains CO2, trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (R1234yf);

    • wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,
      • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100−w) mass % are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B″D and straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point L (51.7, 28.9, 19.4-w)
    • point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2−3.75w+49.5)
    • point D (−2.9167w+40.317, 0.0, 1.9167w+59.683)
    • point C (0.0, −4.9167w+58.317, 3.9167w+41.683);
      • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding the points on straight line B″D and straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point L (51.7, 28.9, 19.4-w)
    • point B″ (51.6, 0.0, 48.4-w)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and
      • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B″D and straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point L (51.7, 28.9, 19.4-w)
    • point B″ (51.6, 0.0, 48.4-w)
    • point D (−2.8w+40.1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7),
    • and
      • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28-w),
      • curve JK is represented by coordinates (x, 0.0095x2−1.2222x+67.676, −0.0095x2+0.2222x+32.324-w), and
      • curve KL is represented by coordinates (x, 0.0049x2−0.8842x+61.488, −0.0049x2−0.1158x+38.512).


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

    • wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z,
      • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass % are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997)
    • point C (0.0, −4.9167w+58.317, 3.9167w+41.683);
      • if 1.2<w≤1.3, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point F (36.6, −3w+3.9, 2w+59.5)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553);
      • if 1.3<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point B′ (36.6, 0.0, −w+63.4)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and
      • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point B′ (36.6, 0.0, −w+63.4)
    • point D (−2.8w+40.1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7),
    • and
      • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28-w), and
      • curve JK is represented by coordinates (x, 0.0095x2−1.2222x+67.676, −0.0095x2+0.2222x+32.324-w).


A refrigerant cycle apparatus for freezing or cold storage according to a thirty-seventh aspect includes a refrigerant circuit and a refrigerant enclosed in the refrigerant circuit. The refrigerant circuit includes a compressor, a radiator, a decompressing portion, and a heat absorber. The refrigerant comprises HFO-1132(E) and HFO-1234yf. A content rate of HFO-1132(E) is 31.1 to 39.8 mass % and a content rate of HFO-1234yf is 68.9 to 60.2 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.


A refrigerant cycle apparatus for freezing or cold storage according to a thirty-eighth aspect is the refrigerant cycle for freezing or cold storage according to the thirty-seventh aspect, wherein a content rate of HFO-1132(E) is 31.1 to 37.9 mass % and a content rate of HFO-1234yf is 68.9 to 62.1 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.


A refrigerant cycle apparatus for freezing or cold storage according to a forty-first aspect includes a refrigerant circuit and a refrigerant enclosed in the refrigerant circuit. The refrigerant circuit includes a compressor, a radiator, a decompressing portion, and a heat absorber. The refrigerant comprises HFO-1132(E) and HFO-1234yf. A content rate of HFO-1132(E) is 21.0 to 28.4 mass % and a content rate of HFO-1234yf is 79.0 to 71.6 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.


A refrigerant cycle apparatus for freezing or cold storage according to a forty-third aspect includes a refrigerant circuit and a refrigerant enclosed in the refrigerant circuit. The refrigerant circuit includes a compressor, a radiator, a decompressing portion, and a heat absorber. The refrigerant comprises HFO-1132(E) and HFO-1234yf,

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





BRIEF DESCRIPTION OF DRAWINGS


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



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



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



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



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



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



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



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



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



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



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



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



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



FIG. 1N is a ternary composition diagram in which the sum of the concentrations of R32, HFO-1132(E), and R1234yf is 98.8 mass % (CO2 content is 1.2 mass %), the diagram showing points and line segments defining the refrigerant according to the present disclosure.



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



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



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



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



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



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



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



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



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



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



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



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



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



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


FIG. 2I1 is a schematic view illustrating one aspect of a refrigerant circuit in a refrigerator of the present disclosure.


FIG. 2I2 is a schematic view illustrating a variant of the refrigerant circuit in FIG. 2I1.


FIG. 2I3 is a schematic view illustrating a variant of the refrigerant circuit in FIG. 2I2.


FIG. 2I4 is a schematic view illustrating a variant of the refrigerant circuit in FIG. 2I2.


FIG. 2I5 is a schematic view for explaining an off-cycle defrost.


FIG. 2I6 is a schematic view for explaining a heating defrost.


FIG. 2I7 is a schematic view for explaining a reverse cycle hot gas defrost.


FIG. 2I8 is a schematic view for explaining a normal cycle hot gas defrost.



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



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



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



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



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



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



FIG. 3 is a vertically sectioned side view of a built-in type open showcase.



FIG. 4 is a schematic view of a separate-installation type showcase cooling apparatus.



FIG. 5 is a refrigerant circuit diagram of the showcase cooling apparatus.



FIG. 6 is a refrigerant circuit diagram of a showcase having a function of intermediate injection.



FIG. 7 is a refrigerant circuit diagram of a showcase that adjusts capacity using a bypass circuit.



FIG. 8 is a refrigerant circuit diagram of a showcase having a function of suction injection.



FIG. 9 is a refrigerant circuit diagram of a showcase having a function of intermediate injection and a function of subcooling.



FIG. 10A is a refrigerant circuit diagram of two-stage compression and single-stage expansion.



FIG. 10B is a Mollier diagram of the two-stage compression and single-stage expansion.



FIG. 11A is a refrigerant circuit diagram of two-stage compression and two-stage expansion.



FIG. 11B is a Mollier diagram of the two-stage compression and two-stage expansion.



FIG. 12 is a refrigerant circuit diagram having a hot-gas defrosting function.





DESCRIPTION OF EMBODIMENTS

(1)


(1-1) Definition of Terms

The term “refrigerant” herein includes at least any compound prescribed in ISO817 (International Organization for Standardization) and marked by a refrigerant number (ASHRAE number) representing the type of a refrigerant with R at the beginning, and further includes one having properties equivalent to those of such a refrigerant even if such one is not marked by any refrigerant number. Refrigerants are roughly classified to “fluorocarbon-based compounds” and “non-fluorocarbon-based compounds” in terms of the structure of such compounds. Such “fluorocarbon-based compounds” include chlorofluorocarbon (CFC), hydrochlorofluorocarbon (HCFC) and hydrofluorocarbon (HFC). Such “non-fluorocarbon-based compounds” include propane (R290), propylene (R1270), butane (R600), isobutene (R600a), carbon dioxide (R744) and ammonia (R717).


The term “composition including a refrigerant” herein includes at least (1) a refrigerant itself (including a mixture of refrigerants), (2) a composition that further includes other component and that can be mixed with at least a refrigerator oil and thus used to obtain a working fluid for a refrigerator, and (3) a working fluid for a refrigerator, containing a refrigerator oil. The composition (2) among such three aspects is herein designated as a “refrigerant composition” so as to be distinguished from the refrigerant itself (including a mixture of refrigerants). The working fluid (3) for a refrigerator is designated as a “refrigerator oil-containing working fluid” so as to be distinguished from the “refrigerant composition”.


A first type of the term “alternative” herein means that, in a case where the term is used in the context indicating that a second refrigerant corresponds to an “alternative” of a first refrigerant, the second refrigerant can be used for operating under optimal conditions, if necessary, by undergoing only the change of a few parts (at least one of a refrigerator oil, a gasket, a packing, an expansion valve, a dryer and other parts) in any equipment designed for operating with the first refrigerant, and adjustment of the equipment. That is, this type means that the same equipment is operated with such an “alternative” of the refrigerant. An aspect of the “alternative” in this type can be any of “drop in alternative”, “nearly drop in alternative” and “retrofit”, in which the degree of the change or the adjustment necessary for replacement with the second refrigerant is lower in the listed order.


A second type of the term “alternative” includes use of any equipment designed for operating with the second refrigerant, in which the second refrigerant is mounted, for the same application as the existing application of the first refrigerant. This type means that the same application, with such an “alternative” of the refrigerant, is provided.


The term “refrigerator” herein means a general apparatus that draws heat from an object or space to thereby allow such an object or space to be at a temperature lower than the temperature of a surrounding atmosphere and is kept at such a low temperature. In other words, the refrigerator refers to a conversion apparatus that gains energy from the outside and works for energy conversion in order to transfer heat from any place at a lower temperature to any place at a higher temperature.


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


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


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


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


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


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


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


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


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


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


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


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


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


(1-2) Refrigerant

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


(1-3) Refrigerant Composition

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


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


(1-3-1) Water

The refrigerant composition according to the present disclosure may contain a small amount of water. The water content of the refrigerant composition is preferably 0.1 mass % or less based on the entire refrigerant. 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.


(1-3-2) Tracer

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


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


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


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


The following compounds are preferable as the tracer.

    • FC-14 (tetrafluoromethane, CF4)
    • HCC-40 (chloromethane, CH3Cl)
    • HFC-23 (trifluoromethane, CHF3)
    • HFC-41 (fluoromethane, CH3Cl)
    • HFC-125 (pentafluoroethane, CF3CHF2)
    • HFC-134a (1,1,1,2-tetrafluoroethane, CF3CH2F)
    • HFC-134 (1,1,2,2-tetrafluoroethane, CHF2CHF2)
    • HFC-143a (1,1,1-trifluoroethane, CF3CH3)
    • HFC-143 (1,1,2-trifluoroethane, CHF2CH2F)
    • HFC-152a (1,1-difluoroethane, CHF2CH3)
    • HFC-152 (1,2-difluoroethane, CH2FCH2F)
    • HFC-161 (fluoroethane, CH3CH2F)
    • HFC-245fa (1,1,1,3,3-pentafluoropropane, CF3CH2CHF2)
    • HFC-236fa (1,1,1,3,3,3-hexafluoropropane, CF3CH2CF3)
    • HFC-236ea (1,1,1,2,3,3-hexafluoropropane, CF3CHFCHF2)
    • HFC-227ea (1,1,1,2,3,3,3-heptafluoropropane, CF3CHFCF3)
    • HCFC-22 (chlorodifluoromethane, CHClF2)
    • HCFC-31 (chlorofluoromethane, CH2ClF)
    • CFC-1113 (chlorotrifluoroethylene, CF2═CClF)
    • HFE-125 (trifluoromethyl-difluoromethyl ether, CF3OCHF2)
    • HFE-134a (trifluoromethyl-fluoromethyl ether, CF3OCH2F)
    • HFE-143a (trifluoromethyl-methyl ether, CF3OCH3)
    • HFE-227ea (trifluoromethyl-tetrafluoroethyl ether, CF3OCHFCF3)
    • HFE-236fa (trifluoromethyl-trifluoroethyl ether, CF3OCH2CF3)


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


(1-3-3) Ultraviolet Fluorescent Dye

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


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


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


(1-3-4) Stabilizer

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


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


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


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


Examples of ethers include 1,4-dioxane.


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


Examples of stabilizers also include butylhydroxyxylene and benzotriazole.


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


(1-3-5) Polymerization Inhibitor

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


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


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


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


(1-4) Refrigeration Oil-Containing Working Fluid

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


(1-4-1) Refrigeration Oil

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


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


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


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


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


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


(1-4-2) 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.


(1-5) Various Refrigerants 1

Refrigerant 1E used in the present disclosure are described below in detail.


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


Refrigerant 1E according to the present disclosure has various properties that are desirable as an R410A-alternative refrigerant, i.e., a refrigerating capacity equivalent to that of R410A, a sufficiently low GWP, and lower flammability.


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

    • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass % are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B″D and straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point L (51.7, 28.9, 19.4-w)
    • point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2−3.75w+49.5)
    • point D (−2.9167w+40.317, 0.0, 1.9167w+59.683)
    • point C (0.0, −4.9167w+58.317, 3.9167w+41.683);
      • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding the points on straight line B″D and straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point L (51.7, 28.9, 19.4-w)
    • point B″ (51.6, 0.0, 48.4-w)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and
      • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B″D and straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point L (51.7, 28.9, 19.4-w)
    • point B″ (51.6, 0.0, 48.4-w)
    • point D (−2.8w+40.1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7),
    •  and
      • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28-w),
      • curve JK is represented by coordinates (x, 0.0095x2−1.2222x+67.676, −0.0095x2+0.2222x+32.324-w), and
      • curve KL is represented by coordinates (x, 0.0049x2−0.8842x+61.488, −0.0049x2−0.1158x+38.512).


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


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

    • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass % are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997)
    • point C (0.0, −4.9167w+58.317, 3.9167w+41.683);
      • if 1.2<w≤1.3, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point F (36.6, −3w+3.9, 2w+59.5)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553);
      • if 1.3<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point B′(36.6, 0.0, −w+63.4)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and
      • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point K (36.8, 35.6, 27.6-w)
    • point B′ (36.6, 0.0, −w+63.4)
    • point D (−2.8w+40.1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7),
    •  and
      • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28-w), and
      • curve JK is represented by coordinates (x, 0.0095x2−1.2222x+67.676, −0.0095x2+0.2222x+32.324-w).


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


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

    • if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass % are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 4 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point E (18.2, −1.1111w2−3.1667w+31.9, 1.1111w2+2.1667w+49.9)
    • point C (0.0, −4.9167w+58.317, 3.9167w+41.683);
      • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 4 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point E (−0.0365w+18.26, 0.0623w2−4.5381w+31.856, −0.0623w2+3.5746w+49.884)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553); and
      • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 4 points or on these line segments (excluding points on straight line CI):
    • point I (0.0, 72.0, 28.0-w)
    • point J (18.3, 48.5, 33.2-w)
    • point E (18.1, 0.0444w2−4.3556w+31.411, −0.0444w2+3.3556w+50.489)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7),
    •  and
      • curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28-w).


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


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

    • if 0<w≤0.6, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass % are within the range of a figure surrounded by curve GO, curve OP, straight line PB″, straight line B″D, and straight line DG that connect the following 5 points or on these line segments (excluding points on straight line B″D):
    • point G (−5.8333w2−3.1667w+22.2, 7.0833w2+1.4167w+26.2, −1.25w2+0.75w+51.6)
    • point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)
    • point P (51.7, 1.1111w2+20.5, −1.1111w2−w+27.8)
    • point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2−3.75w+49.5)
    • point D (−2.9167w+40.317, 0.0, 1.9167w+59.683);
    •  and
      • if 0.6<w≤1.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve GN, curve NO, curve OP, straight line PB″, straight line B″D, and straight line DG that connect the following 6 points or on these line segments (excluding the points on straight line B″D):
    • point G (−5.8333w2−3.1667w+22.2, 7.0833w2+1.4167w+26.2, −1.25w2+0.75w+51.6)
    • point N (18.2, 0.2778w2+3w+27.7, −0.2778w2−4w+54.1)
    • point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)
    • point P (51.7, 1.1111w2+20.5, −1.1111w2−w+27.8)
    • point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2−3.75w+49.5)
    • point D (−2.9167w+40.317, 0.0, 1.9167w+59.683); and
      • when 0<w≤0.6, curve GO is represented by coordinates (x, (0.00487w2-0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100-w-x-y);
      • when 0.6<w≤1.2, curve GN is represented by coordinates (x, (0.0122w2-0.0113w+0.0313)x2+(−0.3582w2+0.1624w−1.4551)x+2.7889w2+3.7417w+43.824, 100-w-x-y);
      • when 0.6<w≤1.2, curve NO is represented by coordinates (x, (0.00487w2-0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100-w-x-y); and
      • when 0<w≤1.2, curve OP is represented by coordinates (x, (0.0074w2-0.0133w+0.0064)x2+(−0.5839w2+1.0268w−0.7103)x+11.472w2−17.455w+40.07, 100-w-x-Y);
      • if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, curve OP, straight line PB″, straight line B″D, straight line DC, and straight line CM that connect the following 8 points or on these line segments (excluding points on straight line B″D and straight line CM):
    • point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)
    • point W (10.0, −0.3645w2+3.5024w+44.422, 0.3645w2−4.5024w+55.57)
    • point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)
    • point O (36.8, −0.1392w2+1.4381w+24.475, 0.1392w2−2.4381w+38.725)
    • point P (51.7, −0.2381w2+1.881w+20.186, 0.2381w2−2.881w+28.114)
    • point B″ (51.6, 0.0, −w+48.4)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553),
    •  and
      • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100-w-x-y),
      • curve WN is represented by coordinates (x, (0.0055w2-0.0326w+0.0665)x2+(−0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100-w-x-Y),
      • curve NO is represented by coordinates (x, (−0.00062w2+0.0036w+0.0037)x2+(0.0375w2−0.239w−0.4977)x−0.8575w2+6.4941w+36.078, 100-w-x-y), and
      • curve OP is represented by coordinates (x, (−0.000463w2+0.0024w−0.0011)x2+(0.0457w2−0.2581w−0.075)x−1.355w2+8.749w+27.096, 100-w-x-y); and
      • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, curve OP, straight line PB″, straight line B″D, straight line DC, and straight line CM that connect the following 8 points or on these line segments (excluding points on straight line B″D and straight line CM):
    • point M (0.0, −0.0667w2+0.8333w+58.133, 0.0667w2−1.8333w+41.867)
    • point W (10.0, −0.0667w2+1.1w+39.267, 0.0667w2−2.1w+50.733)
    • point N (18.2, −0.0889w2+1.3778w+31.411, 0.0889w2−2.3778w+50.389)
    • point O (36.8, −0.0444w2+0.6889w+25.956, 0.0444w2−1.6889w+37.244)
    • point P (51.7, −0.0667w2+0.8333w+21.633, 0.0667w2−1.8333w+26.667)
    • point B″ (51.6, 0.0, −w+48.4)
    • point D (−2.8w+40.1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and
      • curve MW is represented by coordinates (x, (0.00357w2-0.0391w+0.1756)x2+(−0.0356w2+0.4178w−3.6422)x−0.0667w2+0.8333w+58.103, 100-w-x-y),
      • curve WN is represented by coordinates (x, (−0.002061w2+0.0218w−0.0301)x2+(0.0556w2−0.5821w−0.1108)x−0.4158w2+4.7352w+43.383, 100-w-x-y),
      • curve NO is represented by coordinates (x, 0.0082x2+(0.0022w2−0.0345w−0.7521)x−0.1307w2+2.0247w+42.327, 100-w-x-y), and
      • curve OP is represented by coordinates (x, (−0.0006258w2+0.0066w−0.0153)x2+(0.0516w2−0.5478w+0.9894)x−1.074w2+11.651w+10.992, 100-w-x-y).


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


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

    • if 0<w≤0.6, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass % are within the range of a figure surrounded by curve GO, straight line OF, and straight line FG that connect the following 3 points or on these line segments:
    • point G (−5.8333w2−3.1667w+22.2, 7.0833w2−1.4167w+26.2, −1.25w2+3.5834w+51.6)
    • point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)
    • point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997), and
      • curve GO is represented by coordinates (x, (0.00487w2-0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100-w-x-y);
      • if 0.6<w≤1.2, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve GN, curve NO, straight line OF, and straight line FG that connect the following 4 points or on these line segments:
    • point G (−5.8333w2−3.1667w+22.2, 7.0833w2−1.4167w+26.2, −1.25w2+3.5834w+51.6)
    • point N (18.2, 0.2778w2+3.0w+27.7, −0.2.778w2−4.0w+54.1)
    • point O (36.8, 0.8333w2+1.8333w+22.6, −0.8333w2−2.8333w+40.6)
    • point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997), and
      • when 0.6<w≤1.2, curve GN is represented by coordinates (x, (0.0122w2-0.0113w+0.0313)x2+(−0.3582w2+0.1624w−1.4551)x+2.7889w2+3.7417w+43.824, 100-w-x-y), and
      • when 0.6<w≤1.2, curve NO is represented by coordinates (x, (0.00487w2-0.0059w+0.0072)x2+(−0.279w2+0.2844w−0.6701)x+3.7639w2−0.2467w+37.512, 100-w-x-y); and
      • if 1.2<w≤1.3, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, straight line OF, straight line FC, and straight line CM that connect the following 6 points or on these line segments (excluding points on straight line CM):
    • point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)
    • point W (10.0, −0.3645w2+3.5024w34.422, 0.3645w2−4.5024w+55.578)
    • point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)
    • point O (36.8, −0.1392w2+1.4381w+24.475, 0.1392w2−2.4381w+38.725)
    • point F (36.6, −3w+3.9, 2w+59.5)
    • point C (0.1081w2−5.169w+58.447, 0.0, −0.1081w2+4.169w+41.553),
    •  and
      • curve MW is represented by coordinates (x, (0.0043w2-0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100-w-x-y),
      • curve WN is represented by coordinates (x, (0.0055w2-0.0326w+0.0665)x2+(−0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100-w-x-y), and
      • curve NO is represented by coordinates (x, (−0.00062w2+0.0036w+0.0037)x2+(0.0375w2−0.239w−0.4977)x−0.8575w2+6.4941w+36.078, 100-w-x-y);
      • if 1.3<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, straight line OB′, straight line B′D, straight line DC, and straight line CM that connect the following 7 points or on these line segments (excluding points on straight line CM):
    • point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)
    • point W (10.0, −0.3645w2+3.5024w+34.422, 0.3645w2−4.5024w+55.578)
    • point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)
    • point O (36.8, −0.1392w2+1.4381w+24.475, 0.1392w2−2.4381w+38.725)
    • point B′(36.6, 0.0, −w+63.4)
    • point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553),
    •  and
      • curve MW is represented by coordinates (x, (0.0043w2−0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100-w-x-y),
      • curve WN is represented by coordinates (x, (0.0055w2-0.0326w+0.0665)x2+(−0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100-w-x-y), and
      • curve NO is represented by coordinates (x, (−0.00062w2+0.0036w+0.0037)x2+(0.0457w2−0.2581w−0.075)x−1.355w2+8.749w+27.096, 100-w-x-y); and
      • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, curve NO, straight line OB′, straight line B′D, straight line DC, and straight line CM that connect the following 7 points or on these line segments (excluding points on straight line CM):
    • point M (0.0, −0.0667w2+0.8333w58.133, 0.0667w2−1.8333w+41.867)
    • point W (10.0, −0.0667w2+1.1w+39.267, 0.0667w2−2.1w+50.733)
    • point N (18.2, −0.0889w2+1.3778w+31.411, 0.0889w2−2.3778w+50.389)
    • point O (36.8, −0.0444w2+0.6889w+25.956, 0.0444w2−1.6889w+37.244)
    • point B′ (36.6, 0.0, −w+63.4)
    • point D (−2.8w+40. 1, 0.0, 1.8w+59.9)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and
      • curve MW is represented by coordinates (x, (0.00357w2-0.0391w+0.1756)x2+(−0.0356w2+0.4178w−3.6422)x−0.0667w2+0.8333w+58.103, 100-w-x-y),
      • curve WN is represented by coordinates (x, (−0.002061w2+0.0218w−0.0301)x2+(0.0556w2−0.5821w−0.1108)x−0.4158w2+4.7352w+43.383, 100-w-x-y), and
      • curve NO is represented by coordinates (x, (0.0082x2+(0.0022w2−0.0345w−0.7521)x−0.1307w2+2.0247w+42.327, 100-w-x-y).


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


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

    • if 1.2<w≤4.0, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass % are within the range of a figure surrounded by curve MW, curve WN, straight line NE, straight line EC, and straight line CM that connect the following 5 points or on these line segments (excluding points on straight line CM):
    • point M (0.0, −0.3004w2+2.419w+55.53, 0.3004w2−3.419w+44.47)
    • point W (10.0, −0.3645w2+3.5024w+34.422, 0.3645w2−4.5024w+55.578)
    • point N (18.2, −0.3773w2+3.319w+28.26, 0.3773w2−4.319w+53.54)
    • point E (−0.0365w+18.26, 0.0623w2−4.5381w+31.856, −0.0623w2+3.5746w+49.884)
    • point C (0.0, 0.1081w2−5.169w+58.447, −0.1081w2+4.169w+41.553),
    •  and
      • curve MW is represented by coordinates (x, (0.0043w2-0.0359w+0.1509)x2+(−0.0493w2+0.4669w−3.6193)x−0.3004w2+2.419w+55.53, 100-w-x-y), and
      • curve WN is represented by coordinates (x, (0.0055w2-0.0326w+0.0665)x2+(−0.1571w2+0.8981w−2.6274)x+0.6555w2−2.2153w+54.044, 100-w-x-y); and
      • if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve MW, curve WN, straight line NE, straight line EC, and straight line CM that connect the following 5 points or on these line segments (excluding points on straight line CM):
    • point M (0.0, −0.0667w2+0.8333w+58.133, 0.0667w2−1.8333w+41.867)
    • point W (10.0, −0.0667w2+1.1w+39.267, 0.0667w2−2.1w+50.733)
    • point N (18.2, −0.0889w2+1.3778w+31.411, 0.0889w2−2.3778w+50.389)
    • point E (18.1, 0.0444w2−4.3556w+31.411, −0.0444w2+3.3556w+50.489)
    • point C (0.0, 0.0667w2−4.9667w+58.3, −0.0667w2+3.9667w+41.7), and
      • curve MW is represented by coordinates (x, (0.00357w2-0.0391w+0.1756)x2+(−0.0356w2+0.4178w−3.6422)x−0.0667w2+0.8333w+58.103, 100-w-x-y), and
      • curve WN is represented by coordinates (x, (−0.002061w2+0.0218w−0.0301)x2+(0.0556w2−0.5821w−0.1108)x−0.4158w2+4.7352w+43.383, 100-w-x-y). When the requirements above are satisfied, Refrigerant 1E according to the present disclosure has a refrigerating capacity ratio of 80% or more relative to R410A, a GWP of 125 or less, and a lower ASHRAE flammability.


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


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


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


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


Examples of Refrigerant 1E

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


The burning velocity of each of the mixed refrigerants of CO2, R32, HFO-1132(E), and R1234yf was measured in accordance with the ANSI/ASHRAE Standard 34-2013. While changing the concentration of CO2, a formulation that shows a burning velocity of 10 cm/s was found. Tables 1 to 3 show the formulations found.


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


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









TABLE 1







0% CO2

















Comp.

Comp.

Comp.

Comp.




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


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





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


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
28.0
32.8
33.2
31.2
27.6
23.8
19.4


CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Burning
cm/s
10
10
10
10
10
10
10


velocity










(WCF)










0.6% CO2

















Example 3

Example 5

Example 7

Example 9


Item
Unit
I
Example 4
J
Example 6
K
Example 8
L





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


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
27.4
32.6
32.6
30.6
27.0
23.3
10.8


CO2
mass %
0.6
0.6
0.6
0.6
0.6
0.6
0.6


Burning
cm/s
10
10
10
10
10
10
10


velocity










(WCF)










1.2% CO2

















Comp.










Ex. 48

Example 18

Example 20

Example 22


Item
Unit
I
Example 17
J
Example 19
K
Example 21
L





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


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
26.8
31.6
32.0
30.0
26.4
22.7
18.2


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2


Burning
cm/s
10
10
10
10
10
10
10


velocity










(WCF)










1.3% CO2

















Comp.










Ex. 59

Example 30

Example 32

Example 34


Item
Unit
I
Example 29
J
Example 31
K
Example 33
L





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


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
26.7
31.5
31.9
29.9
26.3
22.6
18.1


CO2
mass %
1.3
1.3
1.3
1.3
1.3
1.3
1.3


Burning
cm/s
10
10
10
10
10
10
10


velocity










(WCF)










2.5% CO2

















Comp.










Ex. 69

Example 45

Example 47

Example 49


Item
Unit
I
Example 44
J
Example 46
K
Example 48
L





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


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
25.5
30.3
30.7
28.7
25.1
21.3
16.9


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5


Burning
cm/s
10
10
10
10
10
10
10


velocity










(WCF)










4.0 CO2

















Comp.










Ex. 79

Example 60

Example 62

Example 64


Item
Unit
I
Example 59
J
Example 61
K
Example 63
L





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


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
24.0
28.8
29.2
27.2
23.6
19.8
15.4


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0


Burning
cm/s
10
10
10
10
10
10
10


velocity










(WCF)










5.5 CO2

















Comp.










Ex. 89

Example 75

Example 77

Example 79


Item
Unit
I
Example 74
J
Example 76
K
Example 78
L





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


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
22.5
27.3
27.7
25.7
22.1
183
13.9


CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5


Burning
cm/s
10
10
10
10
10
10
10


velocity










(WCF)










7.0 CO2

















Comp.










Ex. 99

Example 90

Example 92

Example 94


Item
Unit
I
Example 89
J
Example 91
K
Example 93
L





HFO-1132(E)
mass %
72.0
57.2
48.5
412
35.6
32.0
28.9


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
21.0
25.8
26.2
24.2
20.6
16.8
12.4


CO2
mass %
7.0
7.0
7.0
7.0
7.0
7.0
7.0


Burning
cm/s
10
10
10
10
10
10
10


velocity










(WCF)
















TABLE 2







0% CO2













Comp.

Comp.

Comp.



Ex. 20
Comp.
Ex. 22
Comp.
Ex. 24


Item
M
Ex. 21
W
Ex. 23
N

















WCF
HFO-1132(E)
mass %
52.6
39.2
32.4
29.3
27.7



R32
mass %
0.0
5.0
10.0
14.5
18.2



R1234yf
mass %
47.4
55.8
57.6
56.2
54.1



CO2
mass %
0.0
0.0
0.0
0.0
0.0












Leak conditions to make
Storage/
Storage/
Storage/
Storage/
Storage/


WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,



0%, at release,
0%, at release,
0%, at release,
0%, at release,
0%, at release,



gas phase
gas phase
gas phase
gas phase
gas phase



side
side
side
side
side














WCFF
HFO-1132(E)
mass %
72.0
57.8
48.7
43.6
40.6



R32
mass %
0.0
9.5
17.9
24.2
28.7



R1234yf
mass %
28.0
32.7
33.4
32.2
30.7



CO2
mass %
0.0
0.0
0.0
0.0
0.0













Burning velocity
cm/s
≤8
≤8
≤8
≤8
≤8


(WCF)








Burning velocity
cm/s
10
10
10
10
10


(WCFR)










0% CO2













Comp.

Comp.



Comp.
Ex. 26
Comp.
Ex. 28













Item
Ex. 25
O
Ex. 27
P


















WCF
HFO-1132(E)
mass %
24.5
22.6
21.2
20.5




R32
mass %
27.6
36.8
44.2
51.7




R1234yf
mass %
47.9
40.6
34.6
27.8




CO2
mass %
0.0
0.0
0.0
0.0













Leak conditions to make
Storage/
Storage/
Storage/
Storage/



WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,




0%, at release,
0%, at release,
0%, at release,
0%, at release,




gas phase
gas phase
gas phase
gas phase




side
side
side
side















WCFF
HFO-1132(E)
mass %
34.9
31.4
292
27.1




R32
mass %
38.1
45.7
51.1
56.4




R1234yf
mass %
27.0
23.0
19.7
16.5




CO2
mass %
0.0
0.0
0.0
0.0














Burning velocity
cm/s
≤8
≤8
≤8
≤8



(WCF)








Burning velocity
cm/s
10
10
10
10



(WCFR)










0.6% CO2













Comp.

Comp.





Ex. 35
Comp.
Ex. 38
Comp.
Example 1


Item
C = M
Ex. 37
W
Ex. 39
N(=E = G)

















WCF
HFO-1132(E)
mass %
55.4
42.4
35.1
31.6
29.6



R32
mass %
0.0
5.0
10.0
14.5
18.2



R1234yf
mass %
44.0
52.0
54.3
53.3
51.6



CO2
mass %
0.6
0.6
0.6
0.6
0.6












Leak conditions to make WCFF
Storage/
Storage/
Storage/
Storage/
Storage/



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



0%, at release,
0%, at release,
0%, at release,
0%, at release,
0%, at release,



gas phase
gas phase
liquid phase
liquid phase
gas phase



side
side
side
side
side














WCFF
HFO-1132(E)
mass %
72.0
58.6
49.7
44.5
41.3



R32
mass %
0.0
8.9
16.9
23.0
27.4



R1234yf
mass %
2.7
29.1
30.2
29.4
28.3



CO2
mass %
3.3
3.4
3.2
3.1
3.0













Burning velocity (WCF)
cm/s
≤8
≤8
≤8
≤8
≤8


Burning velocity (WCFF)
cm/s
10
10
10
10
10










0.6% CO2











Example 11

Example 13













Item
Example 10
O
Example 12
P


















WCF
HFO-1132(E)
mass %
26.3
24.0
22.4
20.9




R32
mass %
27.6
36.8
44.0
51.7




R1234yf
mass %
45.5
38.6
33.0
26.8




CO2
mass %
0.6
0.6
0.6
0.6













Leak conditions to make WCFF
Storage/
Storage/
Storage/
Storage/




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




0%, at release,
0%, at release,
0%, at release,
0%, at release,




gas phase
liquid phase
liquid phase
liquid phase




side
side
side
side















WCFF
HFO-1132(E)
mass %
35.8
32.1
29.8
27.8




R32
mass %
36.6
44.1
49.4
54.7




R1234yf
mass %
24.8
21.1
18.2
14.9




CO2
mass %
2.8
2.7
2.6
2.6














Burning velocity (WCF)
cm/s
≤8
≤8
≤8
≤8



Burning velocity (WCFF)
cm/s
10
10
10
10










1.2% CO2













Comp.







Ex. 49
Comp.
Example 16

Example 24


Item
M
Ex. 50
G = W
Example 23
N

















WCF
HFO-1132(E)
mass %
58.0
45.2
38.1
34.0
31.7



R32
mass %
0.0
5.0
10.0
14.4
18.2



R1234yf
mass %
40.8
48.6
50.7
48.9
48.9



CO2
mass %
1.2
1.2
1.2
1.2
1.2












Leak conditions to make
Storage/
Storage/
Storage/
Storage/
Storage/


WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,



0%, at release,
6%, at release,
6%, at release,
4%, at release,
4%, at release,



gas phase
gas phase
liquid phase
liquid phase
liquid phase



side
side
side
side
side














WCFF
HFO-1132(E)
mass %
72.0
59.3
50.9
45.6
42.2



R32
mass %
0.0
8.3
15.8
21.7
26.2



R1234yf
mass %
24.8
28.0
28.5
27.7
26.7



CO2
mass %
3.2
4.4
4.8
5.0
4.9













Burning velocity
cm/s
≤8
≤8
≤8
≤8
≤8


(WCF)








Burning velocity
cm/s
10
10
10
10
10


(WCFF)










1.2% CO2











Example 26

Example 28













Item
Example 25
O
Example 27
P


















WCF
HFO-1132(E)
mass %
27.9
25.4
23.7
22.1




R32
mass %
27.6
36.8
44.0
51.7




R1234yf
mass %
43.3
36.0
31.1
25.0




CO2
mass %
1.2
1.2
1.2
1.2













Leak conditions to make
Storage/
Storage/
Storage/
Storage/



WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,




4%, at release,
4%, at release,
4%, at release,
4%, at release,




liquid phase
liquid phase
liquid phase
liquid phase




side
side
side
side















WCFF
HFO-1132(E)
mass %
36.4
32.7
30.3
28.3




R32
mass %
35.3
42.8
48.1
53.4




R1234yf
mass %
23.6
20.0
17.1
13.9




CO2
mass %
4.7
4.5
45
4.4














Burning velocity
cm/s
≤8
≤8
≤8
≤8



(WCF)








Burning velocity
cm/s
10
10
10
10



(WCFF)










1.3% CO2













Comp.







Ex. 60

Example 36

Example 38


Item
M
Example 35
W
Example 37
N

















WCF
HFO-1132(E)
mass %
58.2
45.5
38.4
34.3
31.9



R32
mass %
0.0
5.0
10.0
14.4
18.2



R1234yf
mass %
40.5
48.2
50.3
50.0
48.6



CO2
mass %
1.3
1.3
1.3
1.3
1.3












Leak conditions to make
Storage/
Storage/
Storage/
Storage/
Storage/


WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,



0%, at release,
8%, at release,
6%, at release,
6%, at release,
6%, at release,



gas phase
gas phase
liquid phase
liquid phase
liquid phase



side
side
side
side
side














WCFF
HFO-1132(E)
mass %
72.0
59.4
51.0
45.7
42.2



R32
mass %
0.0
8.2
15.8
21.5
26.0



R1234yf
mass %
25.0
27.6
28.1
27.8
26.9



CO2
mass %
3.0
4.8
5.1
5.0
4.9













Burning velocity
cm/s
≤8
≤8
≤8
≤8
≤8


(WCF)








Burning velocity
cm/s
10
10
10
10
10


(WCFF)










1.3% CO2











Example 40

Example 42













Item
Example 39
O
Example 41
P


















WCF
HFO-1132(E)
mass %
28.1
25.6
23.9
22.3




R32
mass %
27.6
36.8
44.0
51.7




R1234yf
mass %
43.0
36.3
30.8
24.7




CO2
mass %
1.3
1.3
1.3
1.3













Leak conditions to make
Storage/
Storage/
Storage/
Storage/



WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,




4%, at release,
4%, at release,
4%, at release,
4%, at release,




liquid phase
liquid phase
liquid phase
liquid phase




side
side
side
side















WCFF
HFO-1132(E)
mass %
36.5
32.8
30.4
28.4




R32
mass %
35.1
42.6
47.9
53.2




R1234yf
mass %
26.3
19.7
16.9
13.6




CO2
mass %
5.1
4.9
4.8
4.8














Burning velocity
cm/s
≤8
≤8
≤8
≤8



(WCF)








Burning velocity
cm/s
10
10
10
10



(WCFF)
















TABLE 3







2.5% CO2













Comp.







Ex. 70

Example 51

Example 53


Item
M
Example 50
W
Example 52
N

















WCF
HFO-1132(E)
mass %
59.7
48.1
40.9
36.9
34.2



R32
mass %
0.0
5.0
10.0
14.4
18.2



R1234yf
mass %
37.8
44.4
46.6
46.2
45.1



CO2
mass %
2.5
2.5
2.5
2.5
2.5












Leak conditions to make
Storage/
Storage/
Storage/
Storage/
Storage/


WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,



26%, at release,
20%, at release,
20%, at release,
20%, at release,
18%, at release,



gas phase
gas phase
gas phase
gas phase
liquid phase



side
side
side
side
side














WCFF
HFO-1132(E)
mass %
72.0
60.3
52.1
46.9
43.2



R32
mass %
0.0
7.5
14.6
20.2
24.7



R1234yf
mass %
24.9
27.4
28.4
28.0
26.7



CO2
mass %
3.1
4.8
4.9
4.9
5.4













Burning
cm/s
≤8
≤8
≤8
≤8
≤8


velocity (WCF)








Burning
cm/s
10
10
10
10
10


velocity (WCFF)










2.5% CO2











Example 55

Example 57













Item
Example 54
O
Example 56
P


















WCF
HFO-1132(E)
mass %
29.9
27.2
25.2
23.4




R32
mass %
27.6
36.8
44.0
51.7




R1234yf
mass %
40.0
33.5
28.1
22.4




CO2
mass %
2.5
2.5
2.5
2.5













Leak conditions to make
Storage/
Storage/
Storage/
Storage/



WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,




18%, at release,
18%, at release,
20%, at release,
22%, at release,




liquid phase
liquid phase
gas phase
gas phase




side
side
side
side















WCFF
HFO-1132(E)
mass %
37.1
33.2
30.6
28.3




R32
mass %
34.1
41.8
47.6
53.4




R1234yf
mass %
23.4
19.7
16.9
13.8




CO2
mass %
5.4
5.4
4.9
4.5














Burning
cm/s
≤8
≤8
≤8
≤8



velocity (WCF)








Burning
cm/s
10
10
10
10



velocity (WCFF)










4.0% CO2













Comp.







Ex. 80

Example 66

Example 68


Item
M
Example 65
W
Example 67
N

















WCF
HFO-1132(E)
mass %
60.4
49.6
42.6
38.3
35.5



R32
mass %
0.0
5.0
10.0
14.4
18.2



R1234yf
mass %
35.6
41.4
43.4
43.3
42.3



CO2
mass %
4.0
4.0
4.0
4.0
4.0












Leak conditions to make WCFF
Storage/
Storage/
Storage/
Storage/
Storage/



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



32%, at release,
28%, at release,
28%, at release,
28%, at release,
28%, at release,



gas phase
gas phase
gas phase
gas phase
gas phase



side
side
side
side
side














WCFF
HFO-1132(E)
mass %
72.0
60.9
52.9
47.5
43.8



R32
mass %
0.0
7.1
13.9
19.4
23.9



R1234yf
mass %
24.5
27.0
28.0
27.8
26.9



CO2
mass %
3.5
5.0
5.2
5.3
5.4













Burning velocity
cm/s
≤8
≤8
≤8
≤8
≤8


(WCF)








Burning velocity
cm/s
10
10
10
10
10


(WCFF)










4.0% CO2











Example 70

Example 72













Item
Example 69
O
Example 71
P


















WCF
HFO-1132(E)
mass %
31.0
28.0
25.9
23.9




R32
mass %
27.6
36.8
44.0
51.7




R1234yf
mass %
37.4
31.2
26.1
20.4




CO2
mass %
4.0
4.0
4.0
4.0













Leak conditions to make WCFF
Storage/
Storage/
Storage/
Storage/




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




28%, at release,
32%, at release,
32%, at release,
32%, at release,




gas phase
gas phase
gas phase
gas phase




side
side
side
side















WCFF
HFO-1132(E)
mass %
37.4
33.1
30.5
28.1




R32
mass %
33.5
41.7
47.6
53.6




R1234yf
mass %
23.6
20.5
17.2
13.5




CO2
mass %
5.5
4.7
4.7
4.8














Burning velocity
cm/s
≤8
≤8
≤8
≤8



(WCF)








Burning velocity
cm/s
10
10
10
10



(WCFF)










5.5% CO2













Comp.







Ex. 90

Example 81

Example 83


Item
M
Example 80
W
Example 82
N

















WCF
HFO-1132(E)
mass %
60.7
50.3
43.3
39.0
36.3



R32
mass %
0.0
5.0
10.0
14.4
18.2



R1234yf
mass %
33.8
39.2
41.2
41.1
40.0



CO2
mass %
5.5
5.5
5.5
5.5
5.5












Leak conditions to make
Storage/
Storage/
Storage/
Storage/
Storage/


WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,



36%, at release,
34%, at release,
34%, at release,
32%, at release,
34%, at release,



gas phase
gas phase
gas phase
gas phase
gas phase



side
side
side
side
side














WCFF
HFO-1132(E)
mass %
72.0
61.2
53.2
47.8
44.2



R32
mass %
0.0
6.8
13.5
19.0
23.4



R1234yf
mass %
24.5
27.0
28.1
27.7
26.8



CO2
mass %
3.5
5.0
5.2
5.5
5.6













Burning
cm/s
≤8
≤8
≤8
≤8
≤8


velocity (WCF)








Burning
cm/s
10
10
10
10
10


velocity (WCFF)










5.5% CO2











Example 85

Example 87













Item
Example 84
O
Example 86
P


















WCF
HFO-1132(E)
mass %
31.6
28.4
26.2
24.2




R32
mass %
27.6
36.8
44.0
51.7




R1234yf
mass %
35.3
29.3
24.3
18.6




CO2
mass %
5.5
5.5
5.5
5.5













Leak conditions to make
Storage/
Storage/
Storage/
Storage/



WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,




36%, at release,
38%, at release,
40%, at release,
40%, at release,




gas phase
gas phase
gas phase
gas phase




side
side
side
side















WCFF
HFO-1132(E)
mass %
37.6
33.2
30.3
27.9




R32
mass %
33.2
41.7
47.9
54.2




R1234yf
mass %
23.9
20.2
17.3
13.3




CO2
mass %
5.3
4.9
4.5
4.6














Burning
cm/s
≤8
≤8
≤8
≤8



velocity (WCF)








Burning
cm/s
10
10
10
10



velocity (WCFF)










7.0% CO2













Comp.







Ex. 100

Example 96

Example 98


Item
M
Example 95
W
Example 97
N

















WCF
HFO-1132(E)
mass %
60.7
50.3
43.7
39.5
36.7



R32
mass %
0.0
5.0
10.0
14.4
18.2



R1234yf
mass %
32.3
37.7
39.3
39.1
38.1



CO2
mass %
7.0
7.0
7.0
7.0
7.0












Leak conditions to make
Storage/
Storage/
Storage/
Storage/
Storage/


WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,



42%, at release,
34%, at release,
38%, at release,
40%, at release,
40%, at release,



gas phase
gas phase
gas phase
gas phase
gas phase



side
side
side
side
side














WCF
HFO-1132(E)
mass %
72.0
61.2
53.4
48.1
44.4



R32
mass %
0.0
6.8
13.3
18.7
23.2



R1234yf
mass %
24.4
27.0
27.8
28.1
27.1



CO2
mass %
3.6
5.0
5.5
5.1
5.3













Burning velocity
cm/s
≤8
≤8
≤8
≤8
≤8


(WCF)








Burning velocity
cm/s
10
10
10
10
10


(WCFF)










7.0% CO2











Example 100

Example 102













Item
Example 99
O
Example 101
P


















WCF
HFO-1132(E)
mass %
31.9
28.6
26.4
24.2




R32
mass %
27.6
36.8
44.0
51.7




R1234yf
mass %
33.5
27.6
22.6
17.1




CO2
mass %
7.0
7.0
7.0
7.0













Leak conditions to make
Storage/
Storage/
Storage/
Storage/



WCFF
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,
transport, −40° C.,




42%, at release,
42%, at release,
42%, at release,
44%, at release,




gas phase
gas phase
gas phase
gas phase




side
side
side
side















WCF
HFO-1132(E)
mass %
37.7
33.2
30.4
27.8




R32
mass %
33.1
41.7
47.9
54.6




R1234yf
mass %
24.1
19.8
16.3
12.7




CO2
mass %
5.1
5.3
5.4
4.9














Burning velocity
cm/s
≤8
≤8
≤8
≤8



(WCF)








Burning velocity
cm/s
10
10
10
10



(WCFF)









These results indicate that when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum is respectively represented by w, x, y, and z, the mixed refrigerant has a lower WCF flammability when coordinates (x,y,z) in the ternary composition diagram shown in FIGS. 1B to 11, in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass %, are on the line segments that connect point I, point J, point K, and point L, or below these line segments.


The results further indicate that the refrigerant has a lower ASHRAE flammability when coordinates (x,y,z) in the ternary composition diagram shown in FIG. 1B are on the line segments that connect point M, point N, point O, and point P, or below these line segments.


Mixed refrigerants were prepared by mixing R32, HFO-1132(E), and R1234yf in amounts in terms of mass % shown in Tables 4 to 14, based on their sum. The coefficient of performance (COP) ratio and the refrigerating capacity ratio of the mixed refrigerants shown in Tables 4 to 11 relative to those of R410 were determined.


The GWP of compositions comprising a mixture of R410A (R32=50%/R125=50%) and R1234yf was evaluated based on the value stated in the Intergovernmental Panel on Climate Change (IPCC), fourth report. The GWP of HFO-1132(E), which is not stated in the report, was assumed to be 1 from HFO-1132a (GWP=1 or less) and HFO-1123 (GWP=0.3, described in PTL 1). The refrigerating capacity of R410A and that of compositions comprising a mixture of HFO-1132(E), HFO-1123, and R1234yf were determined by performing theoretical refrigeration cycle calculations for mixed refrigerants using the National Institute of Science and Technology (NIST) Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0) under the following conditions.

    • Evaporating temperature: 5° C.
    • Condensation temperature: 45° C.
    • Superheating temperature: 1 K
    • Supercooling temperature: 5 K
    • Ecomp (compressive modulus): 0.7 kWh
    • Tables 4 to 11 show these values together with the GWP of each mixed refrigerant. Tables 4 to 11 show cases at a CO2 concentration of 0 mass %, 0.6 mass %, 1.2 mass %, 1.3 mass %, 2.5 mass %, 4 mass %, 5.5 mass %, and 7 mass %, respectively.









TABLE 4







0% CO2




















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




Comp.
Ex. 2
Ex. 3
Ex. 4
Ex. 5
Ex. 6
Ex. 7
Ex. 8
Ex. 9


Item
Unit
Ex. 1
A
B
A′
B′
A″
B″
C
D





HFO-1132(E)
mass %
R410A
81.6
0.0
63.1
0.0
48.2
0.0
58.3
0.0


R32
mass %

18.4
18.1
36.9
36.7
51.8
51.5
0.0
40.3


R1234yf
mass %

0.0
81.9
0.0
63.3
0.0
49.5
41.7
59.7


CO2
mass %

0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

2088
125
125
250
250
350
350
2
274


COP ratio
% (relative
100
98.7
103.6
98.7
102.3
99.2
102.1
100.3
102.2



to R410A)











Refrigerating
% (relative
100
105.3
62.5
109.9
77.5
112.1
87.0
80.0
80.0


capacity ratio
to R410A)











Condensation
° C.
0.1
0.3
6.8
0.1
4.5
0.0
2.7
2.9
4.0


glide







Comp.
Comp.
Comp.
Comp.

Comp.

Comp.





Ex. 10
Ex. 11
Ex. 12
Ex. 13
Comp.
Ex. 15
Comp.
Ex. 17
Comp.


Item
Unit
E
F
G
I
Ex. 14
J
Ex. 16
K
Ex. 18





HFO-1132(E)
mass %
31.9
5.2
26.2
72.0
57.2
48.5
41.2
35.6
32.0


R32
mass %
18.2
36.7
22.2
0.0
10.0
18.3
27.6
36.8
44.2


R1234yf
mass %
49.9
58.1
51.6
28.0
32.8
33.2
31.2
27.6
23.8


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


GWP

125
250
152
2
69
125
188
250
300


COP ratio
% (relative
100.3
101.8
100.5
99.9
99.5
99.4
99.5
99.6
99.8



to R410A)











Refrigerating
% (relative
82.3
80.8
82.4
86.6
88.4
90.9
94.2
97.7
100.5


capacity ratio
to R410A)











Condensation
° C.
4.4
4.3
4.5
1.7
2.6
2.7
2.4
1.9
1.6


glide























Comp.
Comp.

Comp.

Comp.

Comp.

Comp.




Ex. 19
Ex. 20
Comp.
Ex. 22
Comp.
Ex. 24
Comp.
Ex. 26
Comp.
Ex. 28


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





HFO-1132(E)
mass %
28.9
52.6
39.2
32.4
29.3
27.7
24.5
22.6
21.2
20.5


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


R1234yf
mass %
19.4
47.4
55.8
57.6
56.2
54.1
47.9
40.6
34.6
27.8


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


GWP

350
2
36
70
100
12.5
188
250
300
350


COP ratio
% (relative
100.1
100.5
100.9
100.9
100.8
100.7
100.4
100.4
100.5
100.6



to R410A)












Refrigerating
% (relative
103.3
77.1
74.8
75.6
77.8
80.0
85.5
91.0
95.0
99.1


capacity ratio
to R410A)












Condensation
° C.
1.2
3.4
4.7
5.2
5.1
4.9
4.0
3.0
2.3
1.7


glide
















TABLE 5







0.6% CO2



















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





Ex. 29
Ex. 30
Ex. 31
Ex. 32
Ex. 33
Ex. 34
Ex. 35
Ex. 36
Example 1


Item
Unit
A
B
A′
B′
A″
B″
C = M
D
E = G = N





HFO-1132(E)
mass %
81.0
0.0
62.5
0.0
47.6
0.0
55.4
0.0
29.6


R32
mass %
18.4
18.1
36.9
36.7
51.8
51.6
0.0
38.6
18.2


R1234yf
mass %
0.0
81.3
0.0
62.7
0.0
47.8
44.0
60.8
51.6


CO2
mass %
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6


GWP

125
125
250
250
350
350
2
263
125


COP ratio
% (relative
98.4
103.4
98.4
102.1
99.0
102.0
100.1
102.1
100.2



to R410A)











Refrigerating
% (relative
106.5
63.7
111.1
78.7
113.1
88.6
80.0
80.0
82.4


capacity ratio
to R410A)











Condensation
° C.
0.7
75
0.4
4.9
0.3
3.0
3.9
4.7
5.2


glide






















Example 2
Example 3

Example 5

Example 7

Example 9
Comp.


Item
Unit
F
I
Example 4
J
Example 6
K
Example 8
L
Ex. 37





HFO-1132(E)
mass %
2.7
72.0
57.2
48.5
41.2
35.6
32.0
28.9
42.4


R32
mass %
36.7
0.0
10.0
18.3
27.6
36.8
44.2
51.7
5.0


R1234yf
mass %
60.0
27.4
32.6
32.6
30.6
27.0
23.3
10.8
52.0


CO2
mass %
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6


GWP

250
2
69
125
188
250
300
350
36


COP ratio
% (relative
101.8
99.5
99.2
99.1
99.2
99.4
99.6
99.7
100.3



to R410A)











Refrigerating
% (relative to
80.4
88.1
89.7
92.3
95.5
99.0
101.7
108.2
77.9


capacity ratio
R410A)











Condensation
° C.
4.8
5.2
2.4
3.2
3.1
2.8
2.3
1.9
3.9


glide



















Comp.









Ex. 38
Comp.

Example 11

Example 13


Item
Unit
W
Ex. 39
Example 10
O
Example 12
P





HFO-1132(E)
mass %
35.1
31.6
26.3
24.0
22.4
20.9


R32
mass %
10.0
14.5
27.6
36.8
44.0
51.7


R1234yf
mass %
54.3
53.3
45.5
38.6
33.0
26.8


CO2
mass %
0.6
0.6
0.6
0.6
0.6
0.6


GWP

70
100
188
250
299
350


COP ratio
% (relative
100.4
100.3
100.1
100.1
100.2
100.4



to R410A)








Refrigerating
% (relative
78.5
80.4
87.8
93.0
96.8
100.5


capacity ratio
to R410A)








Condensation
° C.
5.1
5.5
5.4
5.1
4.2
3.2


glide
















TABLE 6





1.2% CO2



























Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example




40
41
42
43
44
45
46
47
14


Item
Unit
A
B
A′
B′
A″
B″
C
D
E





HFO-1132(E)
mass %
80.4
0.0
61.9
0.0
47.0
0.0
52.4
0.0
26.5


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
36.8
18.2


R1234yf
mass %
0.0
80.7
0.0
62.2
0.0
46.9
46.4
62.0
54.1


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

125
125
250
250
350
350
2
251
125


COP ratio
%
98.1
103.2
98.2
101.9
98.7
101.7
99.9
101.9
100.2



(relative to












R410A)











Refrigerating
%
107.7
65.0
112.2
79.8
114.2
89.9
80.0
80.0
82.0


capacity ratio
(relative to












R410A)











Condensation
° C.
1.2
8.1
0.8
5.4
0.6
3.4
4.9
5.3
6.0


glide







Example
Example
Comp. Ex.

Example

Example

Example




15
16
48
Example
18
Example
20
Example
22


Item
Unit
F
G = W
I
17
J
19
K
21
L





HFO-1132(E)
mass %
0.3
38.1
72.0
57.2
48.5
41.2
35.6
32.0
28.9


R32
mass %
36.6
10.0
0.0
10.0
18.3
27.6
36.8
44.2
51.7


R1234yf
mass %
61.3
50.7
26.8
31.6
32.0
30.0
26.4
22.7
18.2


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

250
70
2
69
125
188
250
300
350


COP ratio
%
101.9
99.9
99.2
98.9
98.8
98.9
99.1
99.4
99.6



(relative to












R410A)











Refrigerating
%
80.0
81.6
89.7
91.3
93.7
96.9
100.3
103.0
105.8


capacity ratio
(relative to












R410A)











Condensation
° C.
5.4
5.7
3.1
3.6
3.6
3.2
2.6
2.2
1.8


glide





















Comp. Ex.


Example

Example

Example




49
Comp. Ex.
Example
24
Example
26
Example
28


Item
Unit
M
50
23
N
25
O
27
P





HFO-1132(E)
mass %
58.0
45.2
34.0
31.7
27.9
25.4
23.7
22.1


R32
mass %
0.0
5.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
40.8
48.6
48.9
48.9
43.3
36.0
31.1
25.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

2
36
100
125
188
250
298
350


COP ratio
%
99.6
99.8
99.8
99.8
99.7
99.7
99.9
100.0



(relative to











R410A)










Refrigerating
%
82.9
80.9
83.6
84.9
90.0
95.3
98.7
102.4


capacity ratio
(relative to











R410A)










Condensation
° C.
4.3
5.4
5.6
5.4
4.4
3.4
2.8
2.2


glide
















TABLE 7





1.3% CO2



























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




51
52
53
54
55
56
57
58
59


Item
Unit
A
B
A′
B′ = D = F
A″
B″
C
E
I





HFO-1132(E)
mass %
803
0.0
61.8
0.0
46.9
0.0
51.9
26.1
72.0


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
18.2
0.0


R1234yf
mass %
0.0
80.6
0.0
62.1
0.0
47.1
46.8
54.4
26.7


CO2
mass %
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3


GWP

125
125
250
250
350
350
2
125
2


COP ratio
%
98.0
103.2
98.1
101.9
98.7
101.7
99.8
100.2
99.1



(relative to












R410A)











Refrigerating
%
107.9
65.2
112.3
80.0
114.3
90.0
80.0
82.0
89.9


capacity ratio
(relative to












R410A)











Condensation
° C.
1.2
8.2
0.8
5.4
0.7
3.4
5.1
6.1
3.2


glide























Example

Example

Example
Comp. Ex.

Example




Example
30
Example
32
Example
34
60
Example
36


Item
Unit
29
J
31
K
33
L
M
35
W





HFO-1132(E)
mass %
57.2
48.5
41.2
35.6
32.0
28.9
58.2
45.5
38.4


R32
mass %
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0
10.0


R1234yf
mass %
31.5
31.9
29.9
26.3
22.6
18.1
40.5
48.2
50.3


CO2
mass %
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3
1.3


GWP

69
125
188
250
300
350
2
36
70


COP ratio
%
98.9
98.8
98.9
99.1
99.3
99.6
99.5
99.8
99.8



(relative to












R410A)











Refrigerating
%
91.5
93.9
97.1
100.5
103.2
106.0
83.3
81.3
82.0


capacity ratio
(relative to












R410A)











Condensation
° C.
3.7
3.6
3.2
2.7
2.3
1.8
4.4
5.4
5.8


glide




















Example

Example

Example




Example
38
Example
40
Example
42


Item
Unit
37
N
39
O
41
P





HFO-1132(E)
mass %
34.3
31.9
28.1
25.6
23.9
22.3


R32
mass %
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
50.0
48.6
43.0
36.3
30.8
24.7


CO2
mass %
1.3
1.3
1.3
1.3
1.3
1.3


GWP

100
125
188
250
298
350


COP ratio
%
99.8
99.8
99.6
99.7
99.8
100.0



(relative to









R410A)








Refrigerating
%
83.5
85.2
90.3
95.4
99.0
102.7


capacity ratio
(relative to









R410A)








Condensation
° C.
6
5.4
4.5
3.5
2.9
2.3


glide
















TABLE 8





2.5% CO2



























Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example




61
62
63
64
65
66
67
68
43


Item
Unit
A
B
A′
B′
A″
B″
C
D
E





HFO-1132(E)
mass %
79.1
0.0
60.6
0.0
45.7
0.0
46.2
0.0
20.9


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
33.2
18.2


R1234yf
mass %
0.0
79.4
0.0
60.9
0.0
45.9
51.3
64.3
58.4


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

125
125
250
250
350
350
3
227
125


COP ratio
%
97.4
102.7
97.6
101.5
98.3
101.3
99.6
101.6
100.2



(relative to












R410A)











Refrigerating
%
110.3
67.8
114.5
82.5
116.4
92.5
80.0
80.0
81.7


capacity ratio
(relative to












R410A)











Condensation
° C.
2.0
9.5
1.5
6.3
1.3
4.1
7.1
6.9
7.6


glide







Comp. Ex.

Example

Example

Example
Comp. Ex.





69
Example
45
Example
47
Example
49
70
Example


Item
Unit
I
44
J
46
K
48
L
M
50





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9
59.7
48.1


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0


R1234yf
mass %
25.5
30.3
30.7
28.7
25.1
21.3
16.9
37.8
44.4


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

2
69
125
188
250
300
350
2
36


COP ratio
%
98.4
98.2
98.2
98.4
98.6
98.9
99.1
98.8
99.0



(relative to












R410A)











Refrigerating
%
93.1
94.5
96.7
99.8
103.1
105.9
108.6
87.1
85.7


capacity ratio
(relative to












R410A)











Condensation
° C.
4.4
4.7
4.5
3.9
3.3
2.8
2.4
5.6
6.3


glide




















Example

Example

Example

Example




51
Example
53
Example
55
Example
57


Item
Unit
W
52
N
54
O
56
P





HFO-1132(E)
mass %
40.9
36.9
34.2
29.9
27.2
25.2
23.4


R32
mass %
10.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
46.6
46.2
45.1
40.0
33.5
28.1
22.4


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

70
99
125
188
250
298
350


COP ratio
%
99.1
99.1
99.1
99.0
99.1
99.3
99.5



(relative to










R410A)









Refrigerating
%
86.2
87.7
89.2
94.0
98.8
102.4
105.8


capacity ratio
(relative to










R410A)









Condensation
° C.
6
6.3
6.0
5.0
4.0
3.4
2.8


glide
















TABLE 9





4% CO2



























Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example




71
72
73
74
75
76
77
78
58


Item
Unit
A
B
A′
B′
A″
B″
C
D
E





HFO-1132(E)
mass %
77.6
0.0
59.1
0.0
44.2
0.0
39.5
0.0
14.7


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
28.9
18.1


R1234yf
mass %
0.0
77.9
0.0
59.4
0.0
44.4
56.5
67.1
63.2


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

125
125
250
249
350
350
3
198
125


COP ratio
%
96.7
102.2
97.0
101.0
97.7
100.8
99.4
101.3
100.4



(relative to












R410A)











Refrigerating
%
113.3
71.2
117.3
85.7
118.9
95.6
80.0
80.0
81.2


capacity ratio
(relative to












R410A)











Condensation
° C.
3.0
10.9
2.2
7.2
2.0
5.0
9.6
8.7
9.6


glide







Comp. Ex.

Example

Example

Example
Comp. Ex.





79
Example
60
Example
62
Example
64
80
Example


Item
Unit
I
59
J
61
K
63
L
M
65





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9
60.4
49.6


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0


R1234yf
mass %
24.0
28.8
29.2
27.2
23.6
19.8
15.4
35.6
41.4


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

2
69
125
188
250
300
350
2
36


COP ratio
%
97.6
97.5
97.5
97.7
98.0
98.3
98.6
98.0
98.2



(relative to












R410A)











Refrigerating
%
97.0
98.1
100.2
103.2
106.5
109.1
111.8
91.3
90.2


capacity ratio
(relative to












R410A)











Condensation
° C.
5.8
5.8
5.4
4.7
4.0
3.5
3.1
6.9
7.4


glide




















Example

Example

Example

Example




66
Example
68
Example
70
Example
72


Item
Unit
W
67
N
69
O
71
P





HFO-1132(E)
mass %
42.6
38.3
35.5
31.0
28.0
25.9
23.9


R32
mass %
10.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
43.4
43.3
42.3
37.4
31.2
26.1
20.4


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

70
99
125
188
250
298
350


COP ratio
%
98.3
98.3
98.3
98.3
98.5
98.7
98.9



(relative to










R410A)









Refrigerating
%
90.7
92.0
93.4
97.9
102.5
105.9
109.3


capacity ratio
(relative to










R410A)









Condensation
° C.
7
7.2
6.9
5.8
4.7
4.0
3.4


glide
















TABLE 10





5.5% CO2



























Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example




81
82
83
84
85
86
87
88
73


Item
Unit
A
B
A′
B′
A″
B″
C
D
E





HFO-1132(E)
mass %
76.1
0.0
57.6
0.0
42.7
0.0
33.0
0.0
8.8


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
24.7
18.1


R1234yf
mass %
0.0
76.4
0.0
57.9
0.0
42.9
61.5
69.8
67.6


CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

125
125
250
249
350
350
3
170
125


COP ratio
%
96.0
101.8
96.4
100.5
97.2
100.3
99.4
101.2
100.6



(relative to












R410A)











Refrigerating
%
116.2
74.6
119.9
88.9
121.5
98.7
80.0
80.0
80.8


capacity ratio
(relative to












R410A)











Condensation
° C.
3.7
12.3
2.9
8.2
2.6
5.8
12.1
10.8
11.5


glide







Comp. Ex.

Example

Example

Example
Comp. Ex.





89
Example
75
Example
77
Example
79
90
Example


Item
Unit
I
74
J
76
K
78
L
M
80





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9
60.7
50.3


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0


R1234yf
mass %
22.5
27.3
27.7
25.7
22.1
18.3
13.9
33.8
39.2


CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

2
69
125
188
250
299
350
2
36


COP ratio
%
96.8
96.8
96.9
97.1
97.4
97.7
98.0
97.2
97.4



(relative to












R410A)











Refrigerating
%
100.9
101.8
103.8
106.6
109.8
112.4
115.0
95.4
94.3


capacity ratio
(relative to












R410A)











Condensation
° C.
6.9
6.7
6.2
5.4
4.7
4.1
3.7
8.1
8.5


glide




















Example

Example

Example

Example




81
Example
83
Example
85
Example
87


Item
Unit
W
82
N
84
O
86
P





HFO-1132(E)
mass %
43.3
39.0
36.3
31.6
28.4
26.2
24.2


R32
mass %
10.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
41.2
41.1
40.0
35.3
29.3
24.3
18.6


CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

70
99
125
188
250
298
350


COP ratio
%
97.5
97.6
97.6
97.7
97.9
98.1
98.3



(relative to










R410A)









Refrigerating
%
94.7
95.9
97.4
101.6
106.1
109.3
112.6


capacity ratio
(relative to










R410A)









Condensation
° C.
8
8.1
7.6
6.5
5.4
4.7
4.0


glide
















TABLE 11





7% CO2



























Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example




91
92
93
94
95
96
97
98
88


Item
Unit
A
B
A′
B′
A″
B″
C
D
E





HFO-1132(E)
mass %
74.6
0.0
56.1
0.0
41.2
0.0
26.8
0.0
3.1


R32
mass %
18.4
18.1
36.9
36.6
51.8
51.6
0.0
20.5
18.1


R1234yf
mass %
0.0
74.9
0.0
56.4
0.0
41.4
66.2
72.5
71.8


CO2
mass %
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0


GWP

125
125
250
249
350
350
3
141
125


COP ratio
%
95.3
101.3
95.8
100.0
96.7
99.8
99.5
101.1
100.9



(relative to












R410A)











Refrigerating
%
119.0
78.0
122.6
92.2
124.0
101.9
80.0
80.0
80.3


capacity ratio
(relative to












R410A)











Condensation
° C.
4.4
13.6
3.4
9.0
3.1
6.5
14.6
13.0
13.3


glide







Comp. Ex.

Example

Example

Example
Comp. Ex.





99
Example
90
Example
92
Example
94
100
Example


Item
Unit
I
89
J
91
K
93
L
M
95





HFO-1132(E)
mass %
72.0
57.2
48.5
41.2
35.6
32.0
28.9
60.7
50.3


R32
mass %
0.0
10.0
18.3
27.6
36.8
44.2
51.7
0.0
5.0


R1234yf
mass %
21.0
25.8
26.2
24.2
20.6
16.8
12.4
32.3
37.7


CO2
mass %
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0
7.0


GWP

2
69
125
188
250
299
350
2
36


COP ratio
%
96.0
96.1
96.2
96.5
96.8
97.1
97.5
96.5
96.7



(relative to












R410A)











Refrigerating
%
104.7
105.5
107.3
110.0
113.1
115.6
118.2
99.2
98.0


capacity ratio
(relative to












R410A)











Condensation
° C.
7.9
7.5
6.9
6.0
5.3
4.7
4.2
9.2
9.4


glide




















Example

Example

Example

Example




96
Example
98
Example
100
Example
102


Item
Unit
W
97
N
99
O
101
P





HFO-1132(E)
mass %
43.7
39.5
36.7
31.9
28.6
26.4
24.2


R32
mass %
10.0
14.4
18.2
27.6
36.8
44.0
51.7


R1234yf
mass %
39.3
39.1
38.1
33.5
27.6
22.6
17.1


CO2
mass %
7.0
7.0
7.0
7.0
7.0
7.0
7.0


GWP

70
99
125
188
250
298
350


COP ratio
%
96.9
96.9
97.0
97.1
97.3
97.5
97.8



(relative to










R410A)









Refrigerating
%
98.6
99.7
101.1
105.2
109.5
112.7
115.8


capacity ratio
(relative to










R410A)









Condensation
° C.
9
8.8
8.4
7.1
6.0
5.2
4.6


glide

























TABLE 12









Comp. Ex.
Comp. Ex.
Comp. Ex.
Example
Example
Comp. Ex.
Comp. Ex.
Comp. Ex.


Item
Unit
101
102
103
103
104
104
105
106





HFO-1132(E)
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
mass %
78.8
68.8
58.8
48.8
38.8
28.8
18.8
8.8


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

532
465
398
331
264
197
130
63


COP ratio
%
101.3
101.2
101.1
101.0
101.0
101.3
102.0
102.8



(relative to











R410A)










Refrigerating
%
108.5
104.1
99.2
93.6
87.2
80.1
72.2
63.1


capacity ratio
(relative to











R410A)










Condensation
° C.
1.1
1.6
2.2
3.1
4.3
5.8
7.4
8.4


glide







Comp. Ex.
Comp. Ex.
Example
Example
Example
Comp. Ex.
Comp. Ex.
Comp. Ex.


Item
Unit
107
108
105
106
107
109
110
111





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
30.0


R32
mass %
68.8
58.8
48.8
38.8
28.8
18.8
8.8
58.3


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
10.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

465
398
331
264
197
130
62
398


COP ratio
%
100.6
100.5
100.4
100.3
100.4
100.9
101.8
100.0



(relative to











R410A)










Refrigerating
%
108.6
103.9
98.6
92.6
85.8
78.2
69.6
108.3


capacity ratio
(relative to











R410A)










Condensation
° C.
1.1
1.7
2.5
3.5
4.8
6.4
7.7
1.2


glide







Example
Example
Example
Example
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example


Item
Unit
108
109
110
111
112
113
114
112





HFO-1132(E)
mass %
30.0
30.0
30.0
30.0
30.0
40.0
40.0
40.0


R32
mass %
48.8
38.8
28.8
18.8
8.8
48.8
38.8
28.8


R1234yf
mass %
20.0
30.0
40.0
50.0
60.0
10.0
20.0
30.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

331
263
196
129
62
330
263
196


COP ratio
%
99.9
99.8
99.8
100.1
100.8
99.4
99.3
99.3



(relative to











R410A)










Refrigerating
%
103.2
97.5
91.0
83.7
75.6
107.5
102.0
95.8


capacity ratio
(relative to











R410A)










Condensation
° C.
1.8
2.7
3.8
5.2
6.6
1.3
2.0
2.9


glide







Example
Example
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example
Comp. Ex.
Comp. Ex.


Item
Unit
113
114
115
116
117
115
118
119





HFO-1132(E)
mass %
40.0
40.0
50.0
50.0
50.0
50.0
60.0
60.0


R32
mass %
18.8
8.8
38.8
28.8
18.8
8.8
28.8
18.8


R1234yf
mass %
40.0
50.0
10.0
20.0
30.0
40.0
10.0
20.0


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

129
62
263
196
129
62
195
128


COP ratio
%
99.5
100.0
99.0
98.9
99.0
99.4
98.7
98.7



(relative to











R410A)










Refrigerating
%
88.9
81.1
106.2
100.3
93.7
86.2
104.5
98.2


capacity ratio
(relative to











R410A)










Condensation
° C.
4.1
5.4
1.4
2.2
3.2
4.3
1.5
2.4


glide







Comp. Ex.
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example
Example
Example
Example


Item
Unit
120
121
122
123
116
117
118
119





HFO-1132(E)
mass %
60.0
70.0
70.0
80.0
15.0
15.0
15.0
15.0


R32
mass %
8.8
18.8
8.8
8.8
48.8
46.3
43.8
41.3


R1234yf
mass %
30.0
10.0
20.0
10.0
35.0
37.5
40.0
42.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

61
128
61
61
331
314
297
281


COP ratio
%
99.0
98.5
98.8
98.6
100.7
100.7
100.6
100.6



(relative to











R410A)










Refrigerating
%
91.0
102.4
95.5
99.7
96.1
94.7
93.1
91.6


capacity ratio
(relative to











R410A)










Condensation
° C.
3.3
1.7
2.5
1.9
2.8
3.0
3.3
3.6


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
120
121
122
123
124
125
126
127





HFO-1132(E)
mass %
15.0
15.0
15.0
15.0
15.0
17.5
17.5
17.5


R32
mass %
38.8
36.3
33.8
31.3
28.8
48.8
46.3
43.8


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
32.5
35.0
37.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

264
247
230
214
197
331
314
297


COP ratio
%
100.6
100.7
100.7
100.7
100.8
100.5
100.5
100.5



(relative to











R410A)










Refrigerating
%
89.9
88.3
86.6
84.8
83.0
97.4
95.9
94.4


capacity ratio
(relative to











R410A)










Condensation
° C.
3.9
4.2
4.6
4.9
5.3
2.6
2.9
3.1


glide

























TABLE 13









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
128
129
130
131
132
133
134
135





HFO-1132(E)
mass %
17.5
17.5
17.5
17.5
17.5
17.5
17.5
20.0


R32
mass %
41.3
38.8
36.3
33.8
31.3
28.8
26.3
46.3


R1234yf
mass %
40.0
42.5
45.0
47.5
50.0
52.5
55.0
32.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

281
264
247
230
213
197
180
314


COP ratio
%
100.5
100.5
100.5
100.5
100.6
100.6
100.7
100.4



(relative to











R410A)










Refrigerating
%
92.9
91.3
89.6
87.9
86.2
84.4
82.6
97.1


capacity ratio
(relative to











R410A)










Condensation
° C.
3.4
3.7
4.0
4.3
4.7
5.1
5.4
2.7


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
136
137
138
139
140
141
142
143





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
22.5
22.5


R32
mass %
43.8
41.3
36.3
33.8
31.3
26.3
46.3
43.8


R1234yf
mass %
35.0
37.5
42.5
45.0
47.5
52.5
30.0
32.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

297
280
247
230
213
180
314
297


COP ratio
%
100.3
100.3
100.3
100.3
100.4
100.5
100.2
100.2



(relative to











R410A)










Refrigerating
%
95.7
94.1
90.9
89.3
87.5
84.0
98.4
96.9


capacity ratio
(relative to











R410A)










Condensation
° C.
2.9
3.2
3.8
4.1
4.4
5.2
2.5
2.7


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
144
145
146
147
148
149
150
151





HFO-1132(E)
mass %
22.5
22.5
22.5
22.5
22.5
22.5
22.5
22.5


R32
mass %
41.3
38.8
36.3
33.8
31.3
28.8
26.3
23.8


R1234yf
mass %
35.0
37.5
40.0
42.5
45.0
47.5
50.0
52.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

280
264
247
230
213
197
180
163


COP ratio
%
100.2
100.2
100.2
100.2
100.2
100.3
100.3
100.4



(relative to











R410A)










Refrigerating
%
95.4
93.8
92.2
90.6
88.9
87.1
85.3
83.5


capacity ratio
(relative to











R410A)










Condensation
° C.
3.0
3.3
3.6
3.9
4.2
4.5
4.9
5.3


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
152
153
154
155
156
157
158
159





HFO-1132(E)
mass %
25.0
25.0
25.0
25.0
25.0
25.0
27.5
27.5


R32
mass %
33.8
31.3
28.8
26.3
23.8
21.3
21.9
21.9


R1234yf
mass %
40.0
42.5
45.0
47.5
50.0
52.5
45.0
47.5


CO2
mass %
1.2
1.2
1.2
1.2
1.2
1.2
1.2
1.2


GWP

230
213
196
180
163
146
150
150


COP ratio
%
100.0
100.0
100.1
100.1
100.2
100.3
100.0
100.1



(relative to











410A)










Refrigerating
%
91.8
90.2
88.4
86.7
84.8
83.0
86.3
85.4


capacity ratio
(relative to











410A)










Condensation
° C.
3.6
4.0
4.3
4.7
5.0
5.4
4.8
4.9


glide




















Example
Example
Example
Example
Example



Item
Unit
160
161
162
163
164






HFO-1132(E)
mass %
27.5
27.5
30.0
32.0
34.0



R32
mass %
21.9
21.9
21.9
21.9
13.8



R1234yf
mass %
50.0
52.5
52.5
51.0
51.0



CO2
mass %
1.2
1.2
1.2
1.2
1.2



GWP

150
150
150
150
96



COP ratio
%
100.1
100.2
100.1
100.0
100.1




(relative to









R410A)








Refrigerating
%
84.5
83.7
84.2
85.1
82.0



capacity ratio
(relative to









R410A)








Condensation
° C.
5.1
5.2
5.0
4.9
5.5



glide

























TABLE 14









Comp. Ex.
Comp. Ex
Comp. Ex.
Example
Example
Example
Comp. Ex.
Comp. Ex.


Item
Unit
125
126
127
166
167
168
128
129





HFO-1132(E)
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
mass %
77.5
67.5
57.5
47.5
37.5
275
17.5
7.5


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

524
457
389
322
255
188
121
54


COP ratio
%
100.9
100.8
100.6
100.5
100.5
100.9
101.6
102.4



(relative to











R410A)










Refrigerating
%
110.6
106.2
101.2
95.5
89.1
81.9
74.0
64.8


capacity ratio
(relative to











R410A)










Condensation
° C.
1.8
2.3
3.0
4.0
5.3
7.0
8.8
10.1


glide







Comp. Ex.
Comp. Ex.
Example
Example
Example
Comp. Ex.
Comp. Ex.
Comp. Ex.


Item
Unit
130
131
169
170
171
132
133
134





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
30.0


R32
mass %
67.5
57.5
47.5
37.5
27.5
17.5
7.5
57.5


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
10.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

456
389
322
255
188
121
54
389


COP ratio
%
100.1
100.0
99.9
99.8
100.0
100.5
101.3
99.5



(relative to











R410A)










Refrigerating
%
110.7
106.0
100.6
94.5
87.7
80.1
71.5
110.4


capacity ratio
(relative to











R410A)










Condensation
° C.
1.8
2.5
3.3
4.4
5.9
7.7
9.3
1.9


glide







Example
Example
Example
Example
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example


Item
Unit
172
173
174
175
135
136
137
176





HFO-1132(E)
mass %
30.0
30.0
30.0
30.0
30.0
40.0
40.0
40.0


R32
mass %
47.5
37.5
27.5
17.5
7.5
47.5
37.5
27.5


R1234yf
mass %
20.0
30.0
40.0
50.0
60.0
10.0
20.0
30.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

322
255
188
120
53
321
254
187


COP ratio
%
99.3
99.2
99.3
99.6
100.3
98.9
98.8
98.7



(relative to











R410A)










Refrigerating
%
105.3
99.5
93.0
85.7
77.5
109.6
104.1
97.9


capacity ratio
(relative to











R410A)










Condensation
° C.
2.6
3.6
4.8
6.4
8.1
2.0
2.8
3.9


glide







Example
Example
Comp. Ex
Comp. Ex.
Comp. Ex.
Example
Comp. Ex.
Comp. Ex.


Item
Unit
177
178
138
139
140
179
141
142





HFO-1132(E)
mass %
40.0
40.0
50.0
50.0
50.0
50.0
60.0
60.0


R32
mass %
17.5
7.5
37.5
27.5
17.5
7.5
27.5
17.5


R1234yf
mass %
40.0
50.0
10.0
20.0
30.0
40.0
10.0
20.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

120
53
254
187
120
53
187
120


COP ratio
%
98.9
99.4
98.4
98.3
98.4
98.8
98.0
98.1



(relative to











R410A)










Refrigerating
%
91.0
83.1
108.4
102.5
95.9
88.4
106.8
100.4


capacity ratio
(relative to











R410A)










Condensation
° C.
5.3
6.8
2.2
3.1
4.3
5.6
2.4
3.4


glide







Example
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example
Example
Example
Example


Item
Unit
180
143
144
145
181
182
183
184





HFO-1132 (E)
mass %
60.0
70.0
70.0
80.0
15.0
15.0
15.0
15.0


R32
mass %
7.5
17.5
7.5
7.5
50.0
47.5
45.0
42.5


R1234yf
mass %
30.0
10.0
20.0
10.0
32.5
35.0
37.5
40.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

52
119
52
52
339
322
305
289


COP ratio
%
98.4
97.9
98.1
98.0
100.2
100.2
100.2
100.2



(relative to











R410A)










Refrigerating
%
93.3
104.7
97.8
102.1
99.6
98.1
96.6
95.1


capacity ratio
(relative to











R410A)










Condensation
° C.
4.6
2.7
3.8
3.0
3.4
3.6
3.9
4.2


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
185
186
187
188
189
190
191
192





HFO-1132(E)
mass %
15.0
15.0
15.0
15.0
15.0
15.0
15.0
17.5


R32
mass %
40.0
37.5
35.0
32.5
30.0
27.5
25.0
50.0


R1234yf
mass %
42.5
45.0
47.5
50.0
52.5
55.0
57.5
30.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

272
255
238
222
205
188
171
339


COP ratio
%
100.2
100.2
100.2
100.2
100.3
100.4
100.5
100.1



(relative to











R410A)










Refrigerating
%
93.5
91.9
90.2
88.5
86.7
84.9
83.0
100.8


capacity ratio
(relative to











R410A)










Condensation
° C.
4.5
4.8
5.2
5.6
6.0
6.4
6.9
3.2


glide

























TABLE 15









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
193
194
195
196
197
198
199
200





HFO-1132(E)
mass %
17.5
17.5
17.5
17.5
17.5
17.5
17.5
17.5


R32
mass %
47.5
45.0
42.5
40.0
37.5
35.0
32.5
30.0


R1234yf
mass %
32.5
35.0
37.5
40.0
42.5
45.0
47.5
50.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

322
305
289
272
255
238
221
205


COP ratio
%
100.0
100.0
100.0
100.0
100.0
100.0
100.0
100.1



(relative to











R410A)










Refrigerating
%
99.4
97.9
96.4
94.8
93.2
91.5
89.8
88.1


capacity ratio
(relative to











R410A)










Condensation
° C.
3.5
3.7
4.0
4.3
4.6
5.0
5.3
5.7


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
201
202
203
204
205
206
207
208





HFO-1132(E)
mass %
17.5
17.5
17.5
20.0
20.0
20.0
20.0
20.0


R32
mass %
27.5
25.0
22.5
50.0
45.0
42.5
40.0
35.0


R1234yf
mass %
52.5
55.0
57.5
27.5
32.5
35.0
37.5
42.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

188
171
154
339
305
289
272
238


COP ratio
%
100.2
100.3
100.4
99.9
99.9
99.8
99.8
99.8



(relative to











R410A)










Refrigerating
%
86.3
84.4
82.6
102.0
99.2
97.7
96.1
92.9


capacity ratio
(relative to











R410A)










Condensation
° C.
6.2
6.6
7.0
3.1
3.5
3.8
4.1
4.7


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
209
210
211
212
213
214
215
216





HFO1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
22.5
22.5
22.5


R32
mass %
32.5
30.0
25.0
22.5
20.0
50.0
47.5
45.0


R1234yf
mass %
45.0
47.5
52.5
55.0
57.5
25.0
27.5
30.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

221
205
171
154
138
339
322
305


COP ratio
%
99.8
99.9
100.0
100.2
100.3
99.8
99.7
99.7



(relative to











R410A)










Refrigerating
%
91.2
89.5
85.9
84.0
82.1
103.2
101.8
100.4


capacity ratio
(relative to











R410A)










Condensation
° C.
5.1
5.5
6.3
6.7
7.2
2.9
3.1
3.4


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
217
218
219
220
221
222
223
224





HFO-1132(E)
mass %
22.5
22.5
22.5
22.5
22.5
22.5
22.5
22.5


R32
mass %
42.5
40.0
37.5
35.0
32.5
30.0
27.5
25.0


R1234yf
mass %
32.5
35.0
37.5
40.0
42.5
45.0
47.5
50.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

288
272
255
238
221
205
188
171


COP ratio
%
99.7
99.7
99.7
99.7
99.7
99.7
99.8
99.8



(relative to











R410A)










Refrigerating
%
98.9
97.4
95.8
94.2
92.5
90.8
89.0
87.2


capacity ratio
(relative to











R410A)










Condensation
° C.
3.6
3.9
4.2
4.5
4.9
5.2
5.6
6.0


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
225
226
227
228
229
230
231
232





HFO-1132(E)
mass %
22.5
22.5
22.5
25.0
25.0
25.0
25.0
25.0


R32
mass %
22.5
20.0
17.5
40.0
37.5
35.0
32.5
30.0


R1234yf
mass %
52.5
55.0
57.5
32.5
35.0
37.5
40.0
42.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

154
137
121
272
255
238
221
204


COP ratio
%
99.9
100.1
100.2
99.5
99.5
99.5
99.5
99.5



(relative to











R410A)










Refrigerating
%
85.4
83.5
81.5
98.6
97.1
95.5
93.8
92.1


capacity ratio
(relative to











R410A)










Condensation
° C.
6.5
6.9
7.3
3.7
4.0
4.3
4.6
5.0


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
233
234
235
236
237
238
239
240





HFO-1132(E)
mass %
25.0
25.0
25.0
25.0
25.0
27.5
27.5
27.5


R32
mass %
27.5
25.0
22.5
20.0
17.5
32.5
30.0
27.5


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
37.5
40.0
42.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

188
171
154
137
121
221
204
188


COP ratio
%
99.6
99.6
99.7
99.9
100.0
99.4
99.4
99.4



(relative to











R410A)










Refrigerating
%
90.4
88.6
86.8
84.9
83.0
95.1
93.4
91.7


capacity ratio
(relative to











R410A)










Condensation
° C.
5.4
5.7
6.2
6.6
7.0
4.4
4.7
5.1


glide

























TABLE 16









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
241
242
243
244
245
246
247
248





HFO-1132(E)
mass %
27.5
27.5
27.5
27.5
27.5
30.0
30.0
30.0


R32
mass %
25.0
22.5
20.0
17.5
15.0
25.0
22.5
20.0


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
42.5
45.0
47.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

171
154
137
121
104
171
154
137


COP ratio
%
99.5
99.5
99.6
99.8
99.9
99.3
99.4
99.5



(relative to











R410A)










Refrigerating
%
89.9
88.1
86.3
84.3
82.4
91.3
89.5
87.6


capacity ratio
(relative to











R410A)










Condensation
° C.
5.5
5.9
6.3
6.7
7.2
5.2
5.6
6.0


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
249
250
251
252
253
254
255
256





HFO-1132(E)
mass %
30.0
30.0
32.5
32.5
32.5
32.5
35.0
35.0


R32
mass %
15.0
12.5
20.0
17.5
15.0
12.5
15.0
12.5


R1234yf
mass %
52.5
55.0
45.0
47.5
50.0
52.5
47.5
50.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

104
87
137
120
104
87
104
87


COP ratio
%
99.7
99.9
99.3
99.4
99.5
99.7
99.3
99.5



(relative to











R410A)










Refrigerating
%
83.8
81.8
88.9
87.1
85.1
83.1
86.5
84.5


capacity ratio
(relative to











R410A)










Condensation
° C.
6.8
7.3
5.7
6.1
6.5
7.0
6.2
6.6


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
257
258
259
260
261
262
263
264





HFO-1132(E)
mass %
35.0
37.5
37.5
37.5
40.0
40.0
42.5
42.5


R32
mass %
10.0
12.5
10.0
7.5
10.0
5.0
7.5
5.0


R1234yf
mass %
52.5
47.5
50.0
52.5
47.5
52.5
47.5
50.0


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

70
87
70
53
70
36
53
36


COP ratio
%
99.6
99.3
99.4
99.6
99.3
99.6
99.3
99.4



(relative to











R410A)










Refrigerating
%
82.5
85.8
83.8
81.8
85.2
81.0
845
82.4


capacity ratio
(relative to











R410A)










Condensation
° C.
7.1
6.3
6.7
7.1
6.4
7.2
6.5
6.9


glide




















Example
Example
Example
Example
Example
Example
Example


Item
Unit
265
266
267
268
269
270
271





HFO-1132(E)
mass %
45.0
45.0
47.5
47.5
50.0
52.5
55.0


R32
mass %
5.0
2.5
4.0
1.5
2.5
1.5
1.0


R1234yf
mass %
47.5
50.0
46.0
48.5
45.0
43.5
41.5


CO2
mass %
2.5
2.5
2.5
2.5
2.5
2.5
2.5


GWP

36
19
29
13
19
12
9


COP ratio
%
99.3
99.4
99.2
99.3
99.1
99.1
99.0



(relative to










R410A)









Refrigerating
%
83.7
81.6
84.2
82.0
84.2
84.7
85.6


capacity ratio
(relative to










R410A)









Condensation
° C.
6.6
6.9
6.4
6.7
6.3
6.2
5.9


glide

























TABLE 17









Comp. Ex.
Comp. Ex.
Comp. Ex.
Example
Example
Example
Comp. Ex.
Comp. Ex.


Item
Unit
146
147
148
272
273
274
149
150





HFO-1132(E)
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R32
mass %
76.0
66.0
56.0
46.0
36.0
26.0
16.0
6.0


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

514
446
379
312
245
178
111
44


COP ratio
%
100.3
100.2
100.1
100.0
100.0
100.4
101.2
102.0



(relative to











R410A)










Refrigerating
%
113.0
108.6
103.5
97.8
91.3
84.1
76.1
66.8


capacity ratio
(relative to











R410A)










Condensation
° C.
2.5
3.1
3.9
5.0
6.4
8.3
10.4
12.2


glide







Comp. Ex.
Comp. Ex.
Example
Example
Example
Example
Comp. Ex.
Comp. Ex.


Item
Unit
146
147
275
276
277
278
153
154





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
30.0


R32
mass %
66.0
56.0
46.0
36.0
26.0
16.0
6.0
56.0


R1234yf
mass %
10.0
20.0
30.0
40.0
50.0
60.0
70.0
10.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

446
379
312
245
178
111
44
379


COP ratio
%
99.6
99.5
99.3
99.2
99.4
100.0
100.9
98.9



(relative to











R410A)










Refrigerating
%
113.1
108.4
103.0
96.8
89.9
82.3
73.7
112.9


capacity ratio
(relative to











R410A)










Condensation
° C.
2.6
3.3
4.2
5.5
7.1
9.2
11.2
2.7


glide







Example
Example
Example
Example
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example


Item
Unit
279
280
281
282
155
156
157
283





HFO-1132(E)
mass %
30.0
30.0
30.0
30.0
30.0
40.0
40.0
40.0


R32
mass %
46.0
36.0
26.0
16.0
6.0
46.0
36.0
26.0


R1234yf
mass %
20.0
30.0
40.0
50.0
60.0
10.0
20.0
30.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

312
245
177
110
43
311
244
177


COP ratio
%
98.7
98.6
98.7
99.0
99.8
98.3
98.1
98.1



(relative to











R410A)










Refrigerating
%
107.7
101.9
95.4
88.0
79.9
112.1
106.6
100.4


capacity ratio
(relative to











R410A)










Condensation
° C.
3.5
4.6
6.0
7.8
9.8
2.8
3.8
5.0


glide







Example
Example
Comp. Ex.
Comp. Ex.
Example
Example
Comp. Ex.
Comp. Ex.


Item
Unit
284
285
158
159
286
287
160
161





HFO-1132(E)
mass %
40.0
40.0
50.0
50.0
50.0
50.0
60.0
60.0


R32
mass %
16.0
6.0
36.0
26.0
16.0
6.0
26.0
16.0


R1234yf
mass %
40.0
50.0
10.0
20.0
30.0
40.0
10.0
20.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

110
43
244
177
110
43
177
109


COP ratio
%
98.3
98.8
97.7
97.7
97.8
98.2
97.3
97.4



(relative to











R410A)










Refrigerating
%
93.4
85.6
110.9
105.0
98.4
90.9
109.3
103.0


capacity ratio
(relative to











R410A)










Condensation
° C.
6.6
8.4
3.1
4.1
5.5
7.1
3.4
4.6


glide







Example
Comp. Ex.
Comp. Ex.
Comp. Ex.
Example
Example
Example
Example


Item
Unit
288
162
163
164
289
290
291
292





HFO-1132(E)
mass %
60.0
70.0
70.0
80.0
15.0
15.0
15.0
15.0


R32
mass %
6.0
16.0
6.0
6.0
48.5
46.0
43.5
41.0


R1234yf
mass %
30.0
10.0
20.0
10.0
32.5
35.0
37.5
40.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

42
109
42
42
329
312
295
279


COP ratio
%
97.7
97.2
97.4
97.2
99.7
99.6
99.6
99.6



(relative to











R410A)










Refrigerating
%
95.9
107.3
100.5
104.9
101.9
100.4
98.9
97.4


capacity ratio
(relative to











R410A)










Condensation
° C.
6.0
3.8
5.1
4.3
4.3
4.6
4.9
5.2


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
293
294
295
296
297
298
299
300





HFO-1132(E)
mass %
15.0
15.0
15.0
15.0
15.0
15.0
15.0
15.0


R32
mass %
38.5
36.0
33.5
31.0
28.5
26.0
23.5
21.0


R1234yf
mass %
42.5
45.0
47.5
50.0
52.5
55.0
57.5
60.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

262
245
228
211
195
178
161
144


COP ratio
%
99.6
99.6
99.6
99.7
99.8
99.9
100.0
100.2



(relative to











R410A)










Refrigerating
%
95.8
94.1
92.4
90.7
88.9
87.1
85.2
83.3


capacity ratio
(relative to











R410A)










Condensation
° C.
5.6
5.9
6.3
6.8
7.2
7.7
8.2
8.7


glide

























TABLE 18









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
301
302
303
304
305
306
307
308





HFO-1132(E)
mass %
15.0
17.5
17.5
17.5
17.5
17.5
17.5
17.5


R32
mass %
18.5
48.5
46.0
43.5
41.0
38.5
36.0
33.5


R1234yf
mass %
62.5
30.0
32.5
35.0
37.5
40.0
42.5
45.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

128
329
312
295
278
262
245
228


COP ratio
%
100.4
99.5
99.5
99.4
99.4
99.4
99.4
99.4



(relative to











R410A)










Refrigerating
%
81.3
103.1
101.7
100.2
98.7
97.1
95.5
93.8


capacity ratio
(relative to











R410A)










Condensation
° C.
9.3
4.1
4.4
4.7
5.0
5.3
5.7
6.1


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
309
310
311
312
313
314
315
316





HFO-1132(E)
mass %
17.5
17.5
17.5
17.5
17.5
17.5
20.0
20.0


R32
mass %
31.0
28.5
26.0
23.5
21.0
18.5
48.5
43.5


R1234yf
mass %
47.5
50.0
52.5
55.0
57.5
60.0
27.5
32.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

211
195
178
161
144
127
329
295


COP ratio
%
99.5
99.5
99.6
99.8
99.9
100.1
99.3
99.3



(relative to











R410A)










Refrigerating
%
92.1
90.3
88.5
86.7
84.8
82.8
104.4
101.5


capacity ratio
(relative to











R410A)










Condensation
° C.
6.5
7.0
7.4
7.9
8.4
9.0
4.0
4.5


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
317
318
319
320
321
322
323
324





HFO-1132(E)
mass %
20.0
20.0
20.0
20.0
20.0
20.0
20.0
20.0


R32
mass %
41.0
38.5
33.5
31.0
28.5
23.5
21.0
18.5


R1234yf
mass %
35.0
37.5
42.5
45.0
47.5
52.5
55.0
57.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

278
262
228
211
195
161
144
127


COP ratio
%
99.3
99.2
99.3
99.3
99.3
99.5
99.6
99.8



(relative to











R410A)










Refrigerating
%
100.0
98.4
95.2
93.5
91.7
88.1
86.2
84.3


capacity ratio
(relative to











R410A)










Condensation
° C.
4.8
5.1
5.8
6.2
6.7
7.6
8.1
8.6


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
325
326
327
328
329
330
331
332





HFO-1132(E)
mass %
22.5
22.5
22.5
22.5
22.5
22.5
22.5
22.5


R32
mass %
48.5
46.0
43.5
41.0
38.5
36.0
33.5
31.0


R1234yf
mass %
25.0
27.5
30.0
32.5
35.0
37.5
40.0
42.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

329
312
295
278
262
245
228
211


COP ratio
%
99.2
99.2
99.1
99.1
99.1
99.1
99.1
99.1



(relative to











R410A)










Refrigerating
%
105.6
104.2
102.7
101.3
99.7
98.1
96.5
94.8


capacity ratio
(relative to











R410A)










Condensation
° C.
3.8
4.0
4.3
4.6
4.3
5.2
5.6
6.0


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
333
334
335
336
337
338
339
340





HFO-1132(E)
mass %
22.5
22.5
22.5
22.5
22.5
22.5
22.5
25.0


R32
mass %
28.5
26.0
23.5
21.0
18.5
16.0
13.5
43.5


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
57.5
60.0
27.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

194
178
161
144
127
111
94
295


COP ratio
%
99.1
99.2
99.3
99.4
99.5
99.7
99.9
99.0



(relative to











R410A)










Refrigerating
%
93.1
91.3
89.5
87.7
85.8
83.8
81.8
104.0


capacity ratio
(relative to











R410A)










Condensation
° C.
6.4
6.8
7.3
7.8
8.3
8.8
9.3
4.1


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
341
342
343
344
345
346
347
348





HFO-1132(E)
mass %
25.0
25.0
25.0
25.0
25.0
25.0
25.0
25.0


R32
mass %
41.0
38.5
36.0
33.5
31.0
28.5
26.0
23.5


R1234yf
mass %
30.0
32.5
35.0
37.5
40.0
42.5
45.0
47.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

278
261
245
228
211
194
178
161


COP ratio
%
98.9
98.9
98.9
98.9
98.9
99.0
99.0
99.1



(relative to











R410A)










Refrigerating
%
102.5
101.0
99.4
97.8
96.1
94.4
92.7
90.9


capacity ratio
(relative to











R410A)










Condensation
° C.
4.4
4.7
5.0
5.4
5.7
6.1
6.5
7.0


glide

























TABLE 19









Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
349
350
351
352
353
354
355
356





HFO-1132(E)
mass %
25.0
25.0
25.0
25.0
27.5
27.5
27.5
27.5


R32
mass %
21.0
18.5
16.0
13.5
35.0
31.0
28.5
26.0


R1234yf
mass %
50.0
52.5
55.0
57.5
35.0
37.5
40.0
42.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

144
127
110
94
238
211
194
178


COP ratio
% (relative
99.2
99.3
99.5
99.7
98.8
98.8
98.3
98.8



to R410A)










Refrigerating
% (relative
89.1
87.2
85.2
83.2
99.4
97.4
95.8
94.0


capacity ratio
to R410A)










Condensation
° C.
7.5
8.0
8.5
9.0
5.0
5.5
5.9
6.3


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
357
358
359
360
361
362
363
364





HFO-1132(E)
mass %
27.5
27.5
27.5
27.5
27.5
27.5
30.0
30.0


R32
mass %
23.5
21.0
18.5
16.0
13.5
11.0
23.5
21.0


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
57.5
42.5
45.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

161
144
127
110
94
77
161
144


COP ratio
% (relative
98.9
99.0
99.1
99.2
99.4
99.6
98.7
98.8



to R410A)










Refrigerating
% (relative
92.3
90.4
88.6
86.7
84.7
82.6
93.6
91.8


capacity ratio
to R410A)










Condensation
° C.
6.7
7.2
7.6
8.1
8.7
9.2
6.4
6.9


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
365
366
367
368
369
400
401
402





HFO-1132(E)
mass %
30.0
30.0
30.0
30.0
32.5
32.5
32.5
32.5


R32
mass %
18.5
13.5
11.0
8.5
21.0
18.5
16.0
35.0


R1234yf
mass %
47.5
52.5
55.0
57.5
42.5
45.0
47.5
50.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

127
94
77
60
144
127
110
239


COP ratio
% (relative
98.9
99.2
99.3
99.5
98.6
98.7
98.8
99.1



to R410A)










Refrigerating
% (relative
89.9
86.1
84.1
82.0
93.1
91.3
89.4
94.0


capacity ratio
to R410A)










Condensation
° C.
7.3
8.3
8.8
9.3
6.6
7.0
7.5
5.5


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
403
404
405
406
407
408
409
410





HFO-1132(E)
mass %
32.5
32.5
32.5
35.0
35.0
35.0
35.0
35.0


R32
mass %
11.0
8.5
6.0
16.0
13.5
11.0
8.5
6.0


R1234yf
mass %
52.5
55.0
57.5
45.0
47.5
50.0
52.5
55.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

77
60
43
110
93
77
60
43


COP ratio
% (relative
99.1
99.3
99.5
98.6
98.7
98.9
99.1
99.3



to R410A)










Refrigerating
% (relative
85.5
83.4
81.3
90.8
88.8
86.9
84.8
82.8


capacity ratio
to R410A)










Condensation
° C.
8.5
9.0
9.5
7.2
7.6
8.1
8.6
9.1


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
411
412
413
414
415
416
417
418





HFO-1132(E)
mass %
37.5
37.5
37.5
37.5
37.5
40.0
40.0
40.0


R32
mass %
13.5
11.0
8.5
6.0
3.5
11.0
8.5
3.5


R1234yf
mass %
45.0
47.5
50.0
52.5
55.0
45.0
47.5
52.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

93
77
60
43
26
76
60
26


COP ratio
% (relative
98.6
98.7
98.9
99.0
99.2
98.5
98.7
99.0



to R410A)










Refrigerating
% (relative
90.2
88.2
86.2
84.2
82.0
89.6
87.6
83.4


capacity ratio
to R410A)










Condensation
° C.
7.3
7.8
8.3
8.8
9.2
7.5
7.9
8.9


glide







Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
419
420
421
422
423
424
425
426





HFO-1132(E)
mass %
40.0
42.5
42.5
42.5
42.5
45.0
45.0
45.0


R32
mass %
1.0
8.5
35.0
3.5
1.0
6.0
3.5
1.0


R1234yf
mass %
55.0
45.0
47.5
50.0
52.5
45.0
47.5
50.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

9
60
239
26
9
43
26
9


COP ratio
% (relative
99.2
98.5
98.8
98.8
99.0
98.5
98.6
98.8



to R410A)










Refrigerating
% (relative
81.2
88.9
95.6
84.8
82.6
88.3
86.2
84.0


capacity ratio
to R410A)










Condensation
° C.
9.3
7.6
5.0
8.5
9.0
7.8
8.2
8.7


glide























TABLE 20







Example
Example
Example
Example
Example
Example


Item
Unit
427
428
429
430
431
432






















HFO-1132(E)
mass %
47.5
47.5
50.0
50.0
52.5
55.0


R32
mass %
4.5
2.0
3.5
1.0
2.0
1.0


R1234yf
mass %
44.0
46.5
42.5
45.0
41.5
40.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0


GWP

33
16
26
9
16
9


COP ratio
% (relative
98.4
98.6
98.3
98.5
98.3
98.2



to R410A)








Refrigerating
% (relative
88.4
86.3
88.9
86.8
88.9
89.4


capacity ratio
to R410A)








Condensation
° C.
7.7
8.1
7.6
8.0
7.5
7.4


glide









These results indicate that when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum is respectively represented by w, x, y, and z, the mixed refrigerant has a GWP of 350 when coordinates (x,y,z) are on straight line A″B″ in the ternary composition diagrams shown in FIGS. 1B to 11, in which the sum of R32, and R1234yf, and HFO-1132(E) is (100-w) mass %, and the mixed refrigerant has a GWP of less than 350 when coordinates (x,y,z) in the ternary composition diagrams are located to the right of straight line A″B″. The results further indicate that the mixed refrigerant has a GWP of 250 when coordinates (x,y,z) are on straight line A′B′ in the ternary composition diagrams shown in FIGS. 1B to 11, and the mixed refrigerant has a GWP of less than 125 when coordinates (x,y,z) in the ternary composition diagrams are located to the right of straight line A′B′. The results further show that the mixed refrigerant has a GWP of 125 when coordinates (x,y,z) are on straight line segment AB in the ternary composition diagrams shown in FIGS. 1B to 11, and the mixed refrigerant has a GWP of less than 125 when coordinates (x,y,z) in the ternary composition diagrams are located to the right of straight line segment AB.


The straight line that connects point D and point C is found to be roughly located slightly to the left of the curve that connect points where the mixed refrigerant has a refrigerating capacity ratio of 80% relative to R410A. Accordingly, the results show that when coordinates (x, y, z) are located on the left side of the straight line that connects point D and point C, the mixed refrigerant has a refrigerating capacity ratio of 80% or more relative to R410A.


The coordinates of point A and point B, point A′ and point B′, and point A″ and point B″ were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, the calculation was performed as shown in Table 21 (point A and point B), Table 22 (point A′ and point B′), and Table 23 (point A″ and point B″).












TABLE 21





Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0















Point A
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
81.6
81.0
80.4
80.4
79.1
77.6
77.6
76.1
74.6


R32
18.4
18.4
18.4
18.4
18.4
18.4
18.4
18.4
18.4


R1234yf
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0










CO2
W
w
w


Approximate
−w + 81.6
−w + 81.6
−w + 81.6


formula of





HFO-1132 (E)





Approximate
18.4 
18.4 
18.4 


formula of R32





Approximate
0.0
0.0
0.0


formula of





R1234yf










Point B
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
18.1
18.1
18.1
18.1
18.1
18.1
18.1
18.1
18.1


R1234yf
81.9
81.3
80.7
80.7
79.4
77.9
77.9
76.4
74.9










CO2
w
w
W


Approximate
0.0
0.0
0.0


formula of





HFO-1132 (E)





Approximate
18.1 
18.1 
18.1 


formula of R32





Approximate
−w + 81.9
−w + 81.9
−w + 81.9


formula of





R1234yf



















TABLE 22





Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0















Point A′
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
63.1
62.5
61.9
61.9
60.6
59.1
59.1
57.6
56.1


R32
36.9
36.9
36.9
36.9
36.9
36.9
36.9
36.9
36.9


R1234yf
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0










CO2
w
w
w


Approximate
−w + 63.1
−w + 63.1
−w + 63.1


formula of





HFO-1132 (E)





Approximate
36.9 
36.9 
36.9 


formula of R32





Approximate
0.0
0.0
0.0


formula of





R1234yf










Point B′
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
36.7
36.7
36.6
36.6
36.6
36.6
36.6
36.6
36.6


R1234yf
63.3
62.7
62.2
62.2
60.9
59.4
59.4
57.9
56.4










CO2
w
w
w


Approximate
0  
0.0
0.0


formula of





HFO-1132 (E)





Approximate
100-R1234yf-CO2
36.6 
36.6 


formula of R32





Approximate
−0.9167w + 63.283
−w + 63.4
−w + 63.4


formula of





R1234yf



















TABLE 23





Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0















Point A″
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
48.2
47.6
47.0
47.0
45.7
44.2
44.2
42.7
41.2


R32
51.8
51.8
51.θ
51.8
51.8
51.8
51.8
51.8
51.8


R1234yf
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0










CO2
W
w
w


Approximate
−w + 48.2
−w + 48.2
−w + 48.2


formula of





HFO-1132 (E)





Approximate
51.8 
51.8 
51.8 


formula of R32





Approximate
0.0
0.0
0.0


formula of





R1234yf










Point B″
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
51.5
51.6
51.6
51.6
51.6
51.6
51.6
51.6
51.6


R1234yf
49.5
47.8
47.2
47.2
45.9
44.4
44.4
42.9
41.4










CO2
W
w
w


Approximate
0.0
0.0
0.0


formula of





HFO-1132 (E)





Approximate
100-R1234yf-CO2
51.6 
51.6 


formula of R32





Approximate
1.5278W2 − 3.75w + 49.5
−w + 48.4
−w + 48.4


formula of





R1234yf










The coordinates of points C to G were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, the calculation was performed as shown in Tables 24 and 25.












TABLE 24







Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0










Point C
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
58.3
55.4
52.4
52.4
46.2
39.5
39.5
33.0
26.8


R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R1234yf
41.7
44.0
46.4
46.4
51.3
56.5
56.5
61.5
66.2










CO2
w
w
w


Approximate
−4.9167w + 58.317
0.1081w2
0.0667w2


formula of

5.169w + 58.447
4.9667w + 58.3


HFO-1132 (E)





Approximate
0.0
0.0
0.0


formula of R32





Approximate
100-E-HFO-1132-CO2
100-E-HFO-1132-CO2
100-E-HFO-1132-CO2


formula of





R1234yf










Point D
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
40.3
38.6
36.8
36.8
33.2
28.9
28.9
24.7
20.5


R1234yf
59.7
60.8
62.0
62.0
64.3
67.1
67.1
69.8
72.5










CO2
w
W
w


Approximate
0.0
0.0
0.0


formula of





HFO-1132 (E)





Approximate
−2.9167w + 40.317
−2.8226w + 40.211
−2.8w + 40.1


formula of R32





Approximate
100-R32-CO2
100-R32-CO2
100-R32-CO2


formula of





R1234yf










Point E
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
31.9
29.6
26.5
26.5
20.9
14.7
14.7
8.8
3.1


R32
18.2
18.2
18.2
18.2
18.2
18.1
18.1
18.1
18.1


R1234yf
49.9
51.6
54.1
54.1
58.4
63.2
63.2
67.6
71.8










CO2
w
W
W


Approximate
−1.1111w2
0.0623w2
0.0444w2


formula of
3.1667w + 31.9
4.5381w + 31.856
4.3556w + 31.411


HFO-1132 (E)





Approximate
18.2 
−0.0365w + 18.26
18.1 


formula of R32





Approximate
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2


formula of





R1234yf












Item
1.2 ≥ CO2 > 0
1.3 ≥ CO2 > 1.2







Point F















CO2
0.0
0.6
1.2
1.2
1.3


E-HFO-1132
5.2
2.7
0.3
0.3
0


R32
36.7
36.7
36.6
36.6
36.6


R1234yf
58.1
60.0
61.9
61.9
62.1









CO2
W
w


Approximate
−4.0833w + 5.1833
−3w + 3.9


formula of




HFO-1132 (E)




Approximate
−0.0833w + 36.717
36.6


formula of R32




Approximate
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2


formula of




R1234yf













Item
1.2 ≥ CO2 ≥ 0







Point G















CO2
0.0
0.6
1.2



E-HFO-1132
26.2
29.6
38.1



R32
22.2
18.2
10.0



R1234yf
51.6
51.6
50.7










CO2
w



Approximate
7.0833w2 + l.4167w + 26.2



formula of




HFO-1132 (E)




Approximate
−5.8333w2



formula of R32
3.1667w + 22.2



Approximate
100-E-HFO-1132-R32-CO2



formula of




R1234yf



















TABLE 25





Item
1.2 ≥ CO2 > 0
4.0 ≥ CO2 ≥ 1.2
7.0 ≥ CO2 ≥ 4.0















Point M
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
52.6
55.4
58.0
58.0
59.7
60.4
0.0
33.0
26.8


R32
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R1234yf
47.4
44.0
40.8
40.8
37.8
35.6
56.5
61.5
66.2










CO2
w
w
w


Approximate
100-E-HFO-1132-
100-E-HFO-1132-
100-E-HFO-1132-


formula of
R1234yf-CO2
R1234yf-CO2
R1234yf-CO2


HFO-1132 (E)





Approximate
0.0
0.0
0.0


formula of R32





Approximate
0.2778w2
0.3004w2
0.0667w2


formula of
5.8333w + 47.4
3.419w + 44.47
1.8333w + 41.867


R1234yf










Point W
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
32.4
35.1
38.1
38.1
40.9
42.6
42.6
43.3
43.7


R32
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R1234yf
57.6
54.3
50.7
50.7
46.6
43.4
43.4
41.2
39.3










CO2
W
w
w


Approximate
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2


formula of





HFO-1132 (E)





Approximate
10.0 
10.0 
10.0 


formula of R32





Approximate
−0.4167w2
0.3645w2
0.0667w2


formula of
5.25w + 57.6
4.5024w + 55.578
2.1w + 50.733


R1234yf










Point N
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
27.7
29.6
31.7
31.7
34.2
35.5
35.5
36.3
36.7


R32
18.2
18.2
18.2
18.2
18.2
18.2
18.2
18.2
18.2


R1234yf
54.1
51.6
48.9
48.9
45.1
42.3
42.3
40.0
38.1










CO2
w
w
w


Approximate
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2


formula of





HFO-1132 (E)





Approximate
18.2 
18.2 
18.2 


formula of R32





Approximate
−0.2778w2
0.3773w2
0.0889w2


formula of
4w + 54.1
4.319w + 53.54
2.3778w + 50.389


R1234yf










Point O
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
22.6
24.0
25.4
25.4
27.2
28.0
28.0
28.4
28.6


R32
36.8
36.8
36.8
36.8
36.8
36.8
36.8
36.8
36.8


R1234yf
40.6
38.6
36.0
36.0
33.5
31.2
31.2
29.3
27.6










CO2
w
w
w


Approximate
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2


formula of





HFO-1132 (E)





Approximate
36.8 
36.8 
36.8 


formula of R32





Approximate
−0.8333w2
0.1392w2
0.0444w2


formula of
2.8333w + 40.6
2.4381w + 38.725
1.6889w + 37.244


R1234yf










Point P
















CO2
0.0
0.6
1.2
1.2
2.5
4.0
4.0
5.5
7.0


E-HFO-1132
20.5
20.9
22.1
22.1
23.4
23.9
23.9
24.2
24.2


R32
51.7
51.7
51.7
51.7
51.7
51.7
51.7
51.7
51.7


R1234yf
27.8
26.8
25.0
25.0
22.4
20.4
20.4
18.6
17.1










CO2
W
w
w


Approximate
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2
100-R32-R1234yf-CO2


formula of





HFO-1132 (E)





Approximate
51.7 
51.7 
51.7 


formula of R32





Approximate
−1.1111w2
0.2381w2
0.0667w2


formula of
w + 27.8
2.881w + 28.114
1.8333w + 26.667


R1234yf









The coordinates of points on curve IJ, curve JK, and curve KL were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, the calculation was performed as shown in Table 26.


















TABLE 26





Refrigerant type
I
Example
J
J
Example
K
K
Example
L

























CO2
R32
0.0
10.0
18.3
18.3
27.6
36.8
36.8
44.2
51.7


0.0
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
28.0
32.8
33.2
33.2
31.2
27.6
27.6
23.8
19.4


0.6
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
27.4
32.2
32.6
32.6
30.6
27.0
27.0
23.2
18.8


1.2
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
26.8
31.6
32.0
32.0
30.0
26.4
26.4
22.6
18.2


2.5
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
25.5
30.3
30.7
30.7
28.7
25.1
25.1
21.3
16.9


4.0
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
24.0
28.8
29.2
29.2
27.2
23.6
23.6
19.8
15.4


5.5
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
22.5
27.3
27.7
27.7
25.7
22.1
22..1
18.3
13.9


7.0
E-HFO-1132
72.0
57.2
48.5
48.5
41.2
35.6
35.6
32.0
28.9



R1234yf
21.0
25.8
26.2
26.2
24.2
20.6
20.6
16.8
12.4











w =
Approximate
0.0236x2
0.0095x2
0.0049x2


CO2
formula of
1.716x + 72
1.2222x + 67.676
0.8842x + 61.488



E-HFO-1132






when x = R32






R1234yf
100-E-HFO-1132-x-w
100-E-HFO-1132-x-w
100-E-HFO-1132-x-w









The coordinates of points on curve MW and curve WM were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, calculation was performed as shown in Table 27 (when 0 mass %<CO2 concentration ≤1.2 mass %), Table 28 (when 1.2 mass %<CO2 concentration ≤4.0 mass %), and Table 29 (4.0 mass %<CO2 concentration ≤7.0 mass %).









TABLE 27







1.2 ≥ CO2 > 0














M
Example
W
W
Example
N


Item
0.0
5.0
10.0
10.0
14.5
18.2





CO2 = 0 mass %
52.6
39.2
32.4
32.4
29.3
27.7









Approximate
0.132x2
0.0313x2


formula of
3.34x + 52.6
1.4551x + 43.824


E-HFO-1132




when x = R32















CO2 = 0.6 mass %
55.4
42.4
35.1
35.1
31.6
29.6









Approximate
0.114x2
0.0289x2


formula of
3.17x + 55.4
1.4866x + 47.073


E-HFO-1132




when x = R32















CO2 = 1.2 mass %
58.0
45.2
38.1
38.1
34.0
31.7









Approximate
0.114x2
0.0353x2


formula of
3.13x + 58.0
1.776x + 52.330


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.025w2
0.0122w2


formula of
0.045w + 0.132
0.0113w + 0.0313


coefficient a




Approximate
−0.1806w2 +
−0.3582w2 +


formula of
0.3917w − 3.34
0.1624w − 1.4551


coefficient b




Approximate
−0.2778w2 +
2.7889w2 +


formula of
4.8333w + 52.6
3.7417w + 43.824


coefficient c




Approximate
(0.025w2 − 0.045w +
(0.0122w2 − 0.0113w +


formula of
0.132)x2 + (−0.1806w2 +
0.0313)x2 + (−0.3582w2 +


E-HFO-1132
0.3917w − 3.34)x + (−0.2778w2 +
0.1624w − 1.4551)x + (2.7889w2 +


when x = R32,
4.8333w + 52.6)
3.7417w + 43.824)


w = CO2, and




1.2 ≥ w > 0




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
















TABLE 28







4.0 ≥ CO2 ≥ 1.2














M
Example
W
W
Example
N


Item
0.0
5.0
10.0
10.0
14.5
18.2





CO2 = 1.2 mass %
58  
45.2
38.1
38.1
34  
31.7









Approximate
0.114x2
0.0353x2


formula of
3.13x + 58.0
1.776x + 52.330


E-HFO-1132




when x = R32















CO2 = 2.5 mass %
59.7 
48.1
40.9
40.9
36.9 
34.2









Approximate
0.088x2
0.0194x2


formula of
2.76x + 59.7
1.3644x + 52.603


E-HFO-1132




when x = R32















CO2 = 4.0 mass %
60.4 
49.6
42.6
42.6
38.3 
35.5









Approximate
0.076x2
0.0242x2


formula of
2.54x + 60.4
1.5495x + 55.671


E-HFO-1132




when x = R32









In the approximate formula of E-HFO-1132 ax2 + bx + c, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.0043w2
0.0055w2


formula of
0.0359w + 0.1509
0.0326w + 0.0665


coefficient a




Approximate
−0.0493w2 +
−0.1571w2 +


formula of
0.4669w − 3.6193
0.8981w − 2.6274


coefficient b




Approximate
−0.3004w2 +
0.6555w2


formula of
2.419w + 55.53
2.2153w + 54.044


coefficient c




Approximate
(0.0043w2 − 0.0359w +
(0.0055w2 − 0.0326w +


formula of
0.1509)x2 + (−0.0493w2 +
0.0665)x2 + (−0.1571w2 +


E-HFO-1132
0.4669w − 3.6193)x + (−0.3004w2 +
0.8981w − 2.6274)x + (0.6555w2 −


when x = R32,
2.419w + 55.53)
2.2153w + 54.044)


w = CO2, and




4.0 ≥ w ≥ 1.2




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
















TABLE 29







7.0 ≥ CO2 ≥ 4.0














M
Example
W
W
Example
N


Item
0.0
5.0
10.0
10.0
14.5
18.2





CO2 = 4.0 mass %
60.4
49.6
42.6
42.6
38.3 
35.5









Approximate
0.076x2
0.0242x2


formula of
2.54x + 60.4
1.5495x + 55.671


E-HFO-1132




when x = R32















CO2 = 5.5 mass %
60.7
50.3
43.3
43.3
39  
36.3









Approximate
0.068x2
0.0275x2


formula of
2.42x + 60.7
1.6303x + 56.849


E-HFO-1132




when x = R32















CO2 = 7.0 mass %
60.7
50.3
43.7
43.7
39.5 
36.7









Approximate
0.076x2
0.0215x2


formula of
2.46x + 60.7
1.4609x + 56.156


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.00357w2
−0.002061w2 +


formula of
0.0391w + 0.1756
0.0218w − 0.0301


coefficient a




Approximate
−0.0356w2 +
0.0556w2


formula of
0.4178w − 3.6422
0.5821w − 0.1108


coefficient b




Approximate
−0.0667w2 +
− 0.4158w2 +


formula of
0.8333w + 58.103
4.7352w + 43.383


coefficient c




Approximate
(0.00357w2 − 0.0391w +
(−0.002061w2 + 0.0218w −


formula of
0.1756)x2 + (−0.0356w2 +
0.0301)x2 + (0.0556w2


E-HFO-1132
0.4178w − 3.6422)x +
0.5821w − 0.1108)x +


when x = R32,
(−0.0667w2 + 0.8333w + 58.103)
(−0.4158w2 + 4.7352w + 43.383)


w = CO2, and




7.0 ≥ w ≥ 4.0




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2









The coordinates of points on curve NO and curve OP were determined by obtaining approximate formulas based on the points shown in the above table. Specifically, calculation was performed as shown in Table 30 (when 0 mass %<CO2 concentration ≤1.2 mass %), Table 31 (when 1.2 mass %<CO2 concentration ≤4.0 mass %), and Table 32 (4.0 mass %<CO2 concentration ≤7.0 mass %).









TABLE 30







1.2 ≥ CO2 > 0














N
Example
O
O
Example
P


Item
18.2
27.6
36.8
36.8
44.2
51.7





CO2 = 0 mass %
27.7
24.5
22.6 
22.6 
21.2
20.5









Approximate
0.0072x2
0.0064x2


formula of
0.6701x + 37.512
0.7103x + 40.07


E-HFO-1132




when x = R32















CO2 = 0.6 mass %
29.6
26.3
24  
24  
22.4
20.9









Approximate
0.0054x2
0.0011x2


formula of
0.5999x + 38.719
0.3044x + 33.727


E-HFO-1132




when x = R32















CO2 = 1.2 mass %
31.7
27.9
25.4 
25.4 
23.7
22.1









Approximate
0.0071x2
0.0011x2


formula of
0.7306x + 42.636
0.3189x + 35.644


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.00487w2
0.0074w2


formula of
0.0059w + 0.0072
0.0133w + 0.0064


coefficient a




Approximate
−0.279w2 +
−0.5839w2 +


formula of
0.2844w − 0.6701
1.0268w − 0.7103


coefficient b




Approximate
3.7639w2
11.472w2


formula of
0.2467w + 37.512
17.455w + 40.07


coefficient c




Approximate
(0.00487w2 − 0.0059w +
(0.0074w2 − 0.0133w +


formula of
0.0072)x2 + (−0.279w2 +
0.0064)x2 + (−0.5839w2 +


E-HFO-1132
0.2844w − 0.6701)x + (3.7639w2
1.0268w − 0.7103)x + (11.472w2


when x = R32,
0.2467w + 37.512)
17.455w + 40.07)


w = CO2, and




1.2 ≥ w > 0




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
















TABLE 57







4.0 ≥ CO2 ≥ 1.2














N
Example
O
O
Example
P


Item
18.2
27.6
36.8
36.8
44.2
51.7
















CO2 = 1.2 mass %
31.7
27.9
25.4
25.4
23.7
22.1









Approximate
0.0071x2
0.0011x2


formula of
0.7306x + 42.636
0.3189x + 35.644


E-HFO-1132




when x = R32















CO2 = 2.5 mass %
34.2
29.9
27.2
27.2
25.2
23.4









Approximate
0.0088x2
0.002x2


formula of
0.8612x + 46.954
0.4348x + 40.5 


E-HFO-1132




when x = R32















CO2 = 4.0 mass %
35.5
31
28
28
25.9
23.9









Approximate
0.0082x2
0.0011x2


formula of
0.8546x + 48.335
0.3768x + 40.412


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
−0.00062w2 +
−0.000463w2 +


formula of
0.0036w + 0.0037
0.0024w − 0.0011


coefficient a




Approximate
0.0375w2
0.0457w2


formula of
0.239w − 0.4977
0.2581w − 0.075


coefficient b




Approximate
−0.8575w2 +
−1.355w2 +


formula of
6.4941w + 36.078
8.749w + 27.096


coefficient c




Approximate
(−0.00062w2 + 0.0036w +
(−0.000463w2 + 0.0024w −


formula of
0.0037)x2 + (0.0375w2
0.0011)x2 + (0.0457w2 −


E-HFO-1132
0.239w − 0.4977)x + (−0.8575w2 +
0.2581w − 0.075)x + (−1.355w2 +


when x = R32,
6.4941w + 36.078)
8.749w + 27.096)


w = CO2, and




4.0 ≥ w ≥ 1.2




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2
















TABLE 58







7.0 ≥ CO2 ≥ 4.0














N
Example
O
O
Example
P


Item
18.2
27.6
36.8
36.8
44.2
51.7
















CO2 = 4.0 mass %
35.5
31.0
28.0
28.0
25.9
23.9









Approximate
0.0082x2
0.0011x2


formula of
0.8546x + 48.335
0.3768x + 40.412


E-HFO-1132




when x = R32















CO2 = 5.5 mass %
36.3
31.6
28.4
28.4
26.2
24.2









Approximate
0.0082x2
0.0021x2


formula of
0.8747x + 49.51 
0.4638x + 42.584


E-HFO-1132




when x = R32















CO2 = 7.0 mass %
36.7
31.9
28.6
28.6
26.4
24.2









Approximate
0.0082x2
0.0003x2


formula of
0.8848x + 50.097
0.3188x + 39.923


E-HFO-1132




when x = R32









In ax2 + bx + c, which is the approximate formula of E-HFO-1132, approximate


formulas of coefficients a, b, and c when w = CO2 concentration









Approximate
0.0082
−0.0006258w2 + 0.0066w −


formula of

0.0153


coefficient a




Approximate
0.0022w2
0.0516w2


formula of
0.0345w − 0.7521
0.5478w + 0.9894


coefficient b




Approximate
−0.1307w2 +
−1.074w2 +


formula of
2.0247w + 42.327
11.651w + 10.992


coefficient c




Approximate
0.0082x2 + (0.0022w2
(−0.0006258w2 + 0.0066w −


formula of
0.0345w − 0.7521)x + (−0.1307w2 +
0.0153)x2 + (0.0516w2 −


E-HFO-1132
2.0247w + 42.327)
0.5478w + 0.9894)x + (−1.074w2 +


when x = R32,

11.651w + 10.992)


w = CO2, and




7.0 ≥ w ≥ 4.0




R1234yf
100-E-HFO-1132-R32-CO2
100-E-HFO-1132-R32-CO2









(1-6) Various Refrigerants 2

Hereinafter, the refrigerant 2C that are each the refrigerant for use in the present disclosure will be described in detail.


The refrigerant 2C includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 35.0 to 65.0 mass % and the content rate of HFO-1234yf is 65.0 to 35.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C1”.


(1-6-3-1) Refrigerant 2C1

The refrigerant 2C1, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP equivalent to or more than that of R404A, and (3) a refrigerating capacity equivalent to or more than that of R404A.


The content rate of HFO-1132(E) is 35.0 mass % or more based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1, thereby allowing the refrigerating capacity equivalent to or more than that of R404A to be obtained.


The content rate of HFO-1132(E) is 65.0 mass % or less based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1, thereby enabling the saturation pressure at a saturation temperature of 40° C., in the refrigeration cycle of the refrigerant 2C1, to be kept in a suitable range (in particular, 2.10 Mpa or less).


The refrigerating capacity relative to that of R404A, of the refrigerant 2C1, may be 95% or more, and is preferably 98% or more, more preferably 100% or more, further preferably 101% or more, particularly preferably 102% or more.


The refrigerant 2C1 has a GWP of 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The refrigerant 2C1 is preferably high in ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R404A, from the viewpoint of energy consumption efficiency, and specifically, the COP relative to that of R404A is preferably 98% or more, more preferably 100% or more, particularly preferably 102% or more.


Preferably, the content rate of HFO-1132(E) is 40.5 to 59.0 mass % and the content rate of HFO-1234yf is 59.5 to 41.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.75 MPa or more and 2.00 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


More preferably, the content rate of HFO-1132(E) is 41.3 to 59.0 mass % and the content rate of HFO-1234yf is 58.7 to 41.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99.5% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 2.00 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Further preferably, the content rate of HFO-1132(E) is 41.3 to 55.0 mass % and the content rate of HFO-1234yf is 58.7 to 45.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99.5% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.95 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Particularly preferably, the content rate of HFO-1132(E) is 41.3 to 53.5 mass % and the content rate of HFO-1234yf is 58.7 to 46.5 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.94 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Extremely preferably, the content rate of HFO-1132(E) is 41.3 to 51.0 mass % and the content rate of HFO-1234yf is 58.7 to 49.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.90 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Most preferably, the content rate of HFO-1132(E) is 41.3 to 49.2 mass % and the content rate of HFO-1234yf is 58.7 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C1. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The refrigerant 2C1 usually has a saturation pressure at a saturation temperature of 40° C., of 2.10 MPa or less, preferably 2.00 MPa or less, more preferably 1.95 MPa or less, further preferably 1.90 MPa or less, particularly preferably 1.88 MPa or less. The refrigerant 2C1, which has a saturation pressure at a saturation temperature of 40° C. within such a range, thus can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The refrigerant 2C1 usually has a saturation pressure at a saturation temperature of 40° C., of 1.70 MPa or more, preferably 1.73 MPa or more, more preferably 1.74 MPa or more, further preferably 1.75 MPa or more, particularly preferably 1.76 MPa or more. The refrigerant 2C1, which has a saturation pressure at a saturation temperature of 40° C. within such a range, thus can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 150° C. or less, more preferably 140° C. or less, further preferably 130° C. or less, particularly preferably 120° C. or less from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R404A is extended.


The refrigerant 2C1 is used for operating a refrigeration cycle at an evaporating temperature of −75 to −5° C., and thus, an advantage is that the refrigerating capacity equivalent to or more than that of R404A is obtained.


In a case where the evaporating temperature is more than −5° C. in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used, the compression ratio is less than 2.5 to cause the efficiency of the refrigeration cycle to be deteriorated. In a case where the evaporating temperature is less than −75° C. in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used, the evaporating pressure is less than 0.02 MPa to cause suction of the refrigerant into a compressor to be difficult. The compression ratio can be determined by the following expression.


Compression ratio=Condensation pressure (Mpa)/Evaporating pressure (Mpa) The evaporating temperature in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably −7.5° C. or less, more preferably −10° C. or less, further preferably −35° C. or less.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably −65° C. or more, more preferably −60° C. or more, further preferably −55° C. or more, particularly preferably −50° C. or more.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably −65° C. or more and −5° C. or less, more preferably −60° C. or more and −5° C. or less, further preferably −55° C. or more and −7.5° C. or less, particularly preferably −50° C. or more and −10° C. or less.


The evaporating pressure in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably 0.02 MPa or more, more preferably 0.03 MPa or more, further preferably 0.04 MPa or more, particularly preferably 0.05 MPa or more, from the viewpoint that suction of the refrigerant into a compressor is enhanced.


The compression ratio in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably 2.5 or more, more preferably 3.0 or more, further preferably 3.5 or more, particularly preferably 4.0 or more, from the viewpoint that the efficiency of the refrigeration cycle is enhanced. The compression ratio in the refrigeration cycle where the refrigerant 2C1 of the present disclosure is used is preferably 200 or less, more preferably 150 or less, further preferably 100 or less, particularly preferably 50 or less, from the viewpoint that the efficiency of the refrigeration cycle is enhanced.


The refrigerant 2C1 may usually include 99.5 mass % or more of HFO-1132(E) and HFO-1234yf in terms of the sum of the concentrations of these components. In the present disclosure, the total amount of HFO-1132(E) and HFO-1234yf in the entire refrigerant 2C1 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2C1 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C1 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C1.


The refrigerant 2C1 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C1 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C1.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 35.0 to 65.0 mass % and the content rate of HFO-1234yf is usually 65.0 to 35.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant 2C1, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP equivalent to or more than that of R404A, and (3) a refrigerating capacity equivalent to or more than that of R404A.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, preferably, the content rate of HFO-1132(E) is 40.5 to 59.0 mass % and the content rate of HFO-1234yf is 59.5 to 41.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99% or more.


Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.75 MPa or more and 2.00 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, more preferably, the content rate of HFO-1132(E) is 41.3 to 59.0 mass % and the content rate of HFO-1234yf is 58.7 to 41.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99.5% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 2.00 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 41.3 to 55.0 mass % and the content rate of HFO-1234yf is 58.7 to 45.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has a GWP of 100 or less, a COP relative to that of R404A of 101% or more, and a refrigerating capacity relative to that of R404A of 99.5% or more. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.95 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, particularly preferably, the content rate of HFO-1132(E) is 41.3 to 53.5 mass % and the content rate of HFO-1234yf is 58.7 to 46.5 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.94 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, extremely preferably, the content rate of HFO-1132(E) is 41.3 to 51.0 mass % and the content rate of HFO-1234yf is 58.7 to 49.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.90 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C1 consists only of HFO-1132(E) and HFO-1234yf, most preferably, the content rate of HFO-1132(E) is 41.3 to 49.2 mass % and the content rate of HFO-1234yf is 58.7 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C1 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more and a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C1 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


(1-6-3-2) Refrigerant 2C2

The refrigerant included in the composition of the present disclosure includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 40.5 to 49.2 mass % and the content rate of HFO-1234yf is 59.5 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C2”.


The refrigerant 2C2, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP equivalent to or more than that of R404A, (3) a refrigerating capacity equivalent to or more than that of R404A, and (4) lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.75 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The content rate of HFO-1132(E) is 40.5 mass % or more based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2, thereby allowing the refrigerating capacity equivalent to or more than that of R404A to be obtained.


The content rate of HFO-1132(E) is 49.2 mass % or less based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2, thereby enabling the saturation pressure at a saturation temperature of 40° C., in the refrigeration cycle of the refrigerant 2C2, to be kept in a suitable range (in particular, 2.10 Mpa or less).


The refrigerating capacity relative to that of R404A, of the refrigerant 2C2, may be 99% or more, and is preferably 100% or more, more preferably 101% or more, further preferably 102% or more, particularly preferably 103% or more.


The refrigerant 2C2 has a GWP of 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The refrigerant 2C2 is preferably high in ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R404A, from the viewpoint of energy consumption efficiency, and specifically, the COP relative to that of R404A is preferably 98% or more, more preferably 100% or more, further preferably 101% or more, particularly preferably 102% or more.


Preferably, the content rate of HFO-1132(E) is 41.3 to 49.2 mass % and the content rate of HFO-1234yf is 58.7 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


More preferably, the content rate of HFO-1132(E) is 43.0 to 49.2 mass % and the content rate of HFO-1234yf is 57.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 101% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.78 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Further preferably, the content rate of HFO-1132(E) is 44.0 to 49.2 mass % and the content rate of HFO-1234yf is 56.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 101% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.80 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Particularly preferably, the content rate of HFO-1132(E) is 45.0 to 49.2 mass % and the content rate of HFO-1234yf is 55.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 102% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Extremely preferably, the content rate of HFO-1132(E) is 45.0 to 48.0 mass % and the content rate of HFO-1234yf is 55.0 to 52.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102.5% or more, a refrigerating capacity relative to that of R404A of 102.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.87 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


Most preferably, the content rate of HFO-1132(E) is 45.0 to 47.0 mass % and the content rate of HFO-1234yf is 55.0 to 53.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C2. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102.5% or more, a refrigerating capacity relative to that of R404A of 102.5% or more, and lower flammability (Class 2L) according to ASRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.85 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The refrigerant 2C2 usually has a saturation pressure at a saturation temperature of 40° C., of 2.10 MPa or less, preferably 2.00 MPa or less, more preferably 1.95 MPa or less, further preferably 1.90 MPa or less, particularly preferably 1.88 MPa or less. The refrigerant 2C2, which has a saturation pressure at a saturation temperature of 40° C. within such a range, thus can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


The refrigerant 2C2 usually has a saturation pressure at a saturation temperature of 40° C., of 1.70 MPa or more, preferably 1.73 MPa or more, more preferably 1.74 MPa or more, further preferably 1.75 MPa or more, particularly preferably 1.76 MPa or more. The refrigerant 2C2, which has a saturation pressure at a saturation temperature of 40° C. within such a range, thus can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 150° C. or less, more preferably 140° C. or less, further preferably 130° C. or less, particularly preferably 120° C. or less from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R404A is extended.


The refrigerant 2C2 is preferably used for operating a refrigeration cycle at an evaporating temperature of −75 to 15° C. in the present disclosure, from the viewpoint that the refrigerating capacity equivalent to or more than that of R404A is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably 15° C. or less, more preferably 5° C. or less, further preferably 0° C. or less, particularly preferably −5° C. or less.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably −65° C. or more, more preferably −60° C. or more, further preferably −55° C. or more, particularly preferably −50° C. or more.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably −65° C. or more and 15° C. or less, more preferably −60° C. or more and 5° C. or less, further preferably −55° C. or more and 0° C. or less, particularly preferably −50° C. or more and −5° C. or less.


The evaporating pressure in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably 0.02 MPa or more, more preferably 0.03 MPa or more, further preferably 0.04 MPa or more, particularly preferably 0.05 MPa or more, from the viewpoint that suction of the refrigerant into a compressor is enhanced.


The compression ratio in the refrigeration cycle where the refrigerant 2C2 of the present disclosure is used is preferably 2.5 or more, more preferably 3.0 or more, further preferably 3.5 or more, particularly preferably 4.0 or more, from the viewpoint that the efficiency of the refrigeration cycle is enhanced.


The refrigerant 2C2 may usually include 99.5 mass % or more of HFO-1132(E) and HFO-1234yf in terms of the sum of the concentrations of these components. In the present disclosure, the total amount of HFO-1132(E) and HFO-1234yf in the entire refrigerant 2C2 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2C2 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C2 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C2.


The refrigerant 2C2 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C2 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C2.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 40.5 to 49.2 mass % and the content rate of HFO-1234yf is usually 59.5 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant 2C2, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP equivalent to or more than that of R404A, (3) a refrigerating capacity equivalent to or more than that of R404A, and (4) lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.75 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, preferably, the content rate of HFO-1132(E) is 41.3 to 49.2 mass % and the content rate of HFO-1234yf is 58.7 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 99.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard.


Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.76 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, more preferably, the content rate of HFO-1132(E) is 43.0 to 49.2 mass % and the content rate of HFO-1234yf is 57.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 101% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.78 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 44.0 to 49.2 mass % and the content rate of HFO-1234yf is 56.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 101% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.80 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, particularly preferably, the content rate of HFO-1132(E) is 45.0 to 49.2 mass % and the content rate of HFO-1234yf is 55.0 to 50.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102% or more, a refrigerating capacity relative to that of R404A of 102% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.88 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


In a case where the refrigerant 2C2 consists only of HFO-1132(E) and HFO-1234yf, extremely preferably, the content rate of HFO-1132(E) is 45.0 to 48.0 mass % and the content rate of HFO-1234yf is 55.0 to 52.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C2 has various characteristics of a GWP of 100 or less, a COP relative to that of R404A of 102.5% or more, a refrigerating capacity relative to that of R404A of 102.5% or more, and lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C2 has a saturation pressure at a saturation temperature of 40° C., of 1.81 MPa or more and 1.87 MPa or less, and can be applied to a commercially available refrigerating apparatus for R404A without any significant change in design.


(1-6-3-3) Refrigerant 2C3

The refrigerant included in the composition of the present disclosure includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 31.1 to 39.8 mass % and the content rate of HFO-1234yf is 68.9 to 60.2 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C3”.


The refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R134a, (3) a refrigerating capacity relative to that of R134a of 150% or more, and (4) a discharge temperature of 90° C. or less.


The content rate of HFO-1132(E) is 31.1 mass % or more based on the total amount of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3, thereby allowing a refrigerating capacity relative to that of R134a of 150% or more to be obtained.


The content rate of HFO-1132(E) is 39.8 mass % or less based on the total amount of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3, thereby enabling the discharge temperature in the refrigeration cycle of the refrigerant 2C3 to be kept at 90° C. or less, and enabling the life of any member of a refrigerating apparatus for R134a to be kept long.


The refrigerating capacity relative to that of R134a, of the refrigerant 2C3, may be 150% or more, and is preferably 151% or more, more preferably 152% or more, further preferably 153% or more, particularly preferably 154% or more.


The refrigerant 2C3 preferably has a discharge temperature in the refrigeration cycle of 90.0° C. or less, more preferably 89.7° C. or less, further preferably 89.4° C. or less, particularly preferably 89.0° C. or less.


The refrigerant 2C3 has a GWP of 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The refrigerant 2C3 is preferably high in ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R134a, from the viewpoint of energy consumption efficiency, and specifically, the COP relative to that of R134a is preferably 90% or more, more preferably 91% or more, further preferably 91.5% or more, particularly preferably 92% or more.


The content rate of HFO-1132(E) is usually 31.1 to 39.8 mass % and the content rate of HFO-1234yf is usually 68.9 to 60.2 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3.


The refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R134a, (3) a refrigerating capacity relative to that of R134a of 150% or more, and (4) a discharge temperature of 90.0° C. or less.


Preferably, the content rate of HFO-1132(E) is 31.1 to 37.9 mass % and the content rate of HFO-1234yf is 68.9 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 150% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


More preferably, the content rate of HFO-1132(E) is 32.0 to 37.9 mass % and the content rate of HFO-1234yf is 68.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 151% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


Still more preferably, the content rate of HFO-1132(E) is 33.0 to 37.9 mass % and the content rate of HFO-1234yf is 67.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 152% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


Further preferably, the content rate of HFO-1132(E) is 34.0 to 37.9 mass % and the content rate of HFO-1234yf is 66.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 153% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


Particularly preferably, the content rate of HFO-1132(E) is 35.0 to 37.9 mass % and the content rate of HFO-1234yf is 65.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C3. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 155% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 90.0° C. or less, more preferably 89.7° C. or less, further preferably 89.4° C. or less, particularly preferably 89.0° C. or less, from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R134a is extended.


In a case where the refrigerant 2C3 is used for operating the refrigeration cycle, in the present disclosure, a process of liquefaction (condensation) of the refrigerant is required in the refrigeration cycle, and thus the critical temperature is required to be remarkably higher than the temperature of cooling water or cooling air for liquefying the refrigerant. The critical temperature in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably 80° C. or more, more preferably 81° C. or more, further preferably 81.5° C. or more, in particular, 82° C. or more, from such a viewpoint.


The refrigerant 2C3 is usually used for operating a refrigeration cycle at an evaporating temperature of −75 to 15° C. in the present disclosure, from the viewpoint that a refrigerating capacity relative to that of R134a of 150% or more is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably 15° C. or less, more preferably 5° C. or less, further preferably 0° C. or less, particularly preferably −5° C. or less.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably −65° C. or more, more preferably −60° C. or more, further preferably −55° C. or more, particularly preferably −50° C. or more.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably −65° C. or more and 15° C. or less, more preferably −60° C. or more and 5° C. or less, further preferably −55° C. or more and 0° C. or less, particularly preferably −50° C. or more and −5° C. or less.


The critical temperature of the refrigerant in the refrigeration cycle where the refrigerant 2C3 of the present disclosure is used is preferably 80° C. or more, more preferably 81° C. or more, further preferably 81.5° C. or more, particularly preferably 82° C. or more, from the viewpoint of an enhancement in performance.


The refrigerant 2C3 may usually include 99.5 mass % or more of HFO-1132(E) and HFO-1234yf in terms of the sum of the concentrations of these components. In the present disclosure, the total amount of HFO-1132(E) and HFO-1234yf in the entire refrigerant 2C3 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2C3 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C3 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C3.


The refrigerant 2C3 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C3 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C3.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 31.1 to 39.8 mass % and the content rate of HFO-1234yf is usually 68.9 to 60.2 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R134a, (3) a refrigerating capacity relative to that of R134a of 150% or more, and (4) a discharge temperature of 90° C. or less.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, preferably, the content rate of HFO-1132(E) is 31.1 to 37.9 mass % and the content rate of HFO-1234yf is 68.9 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 150% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, more preferably, the content rate of HFO-1132(E) is 32.0 to 37.9 mass % and the content rate of HFO-1234yf is 68.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 151% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 33.0 to 37.9 mass % and the content rate of HFO-1234yf is 67.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 152% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 34.0 to 37.9 mass % and the content rate of HFO-1234yf is 66.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 153% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


In a case where the refrigerant 2C3 consists only of HFO-1132(E) and HFO-1234yf, further preferably, the content rate of HFO-1132(E) is 35.0 to 37.9 mass % and the content rate of HFO-1234yf is 65.0 to 62.1 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C3, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP relative to that of R134a of 92% or more, (3) a refrigerating capacity relative to that of R134a of 155% or more, (4) a discharge temperature of 90.0° C. or less, and (5) a critical temperature of 81° C. or more.


(1-6-3-4) Refrigerant 2C4

The refrigerant included in the composition of the present disclosure includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 21.0 to 28.4 mass % and the content rate of HFO-1234yf is 79.0 to 71.6 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C4”.


The refrigerant 2C4, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R1234yf, and (3) a refrigerating capacity relative to that of R1234yf of 140% or more, and (4) lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.380 MPa or more and 0.420 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is 21.0 mass % or more based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4, thereby allowing a refrigerating capacity relative to that of R1234yf of 140% or more to be obtained. The content rate of HFO-1132(E) is 28.4 mass % or less based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4, thereby allowing a critical temperature of 83.5° C. or more to be easily ensured.


The refrigerating capacity relative to that of R1234yf in the refrigerant 2C4 may be 140% or more, and is preferably 142% or more, more preferably 143% or more, further preferably 145% or more, particularly preferably 146% or more.


The refrigerant 2C4 has a GWP of 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The refrigerant 2C4 is preferably high in ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R1234yf, from the viewpoint of energy consumption efficiency, and specifically, the COP relative to that of R1234yf is preferably 95% or more, more preferably 96% or more, further preferably 97% or more, particularly preferably 98% or more.


The content rate of HFO-1132(E) is preferably 21.5 to 28.0 mass % and the content rate of HFO-1234yf is preferably 78.5 to 72.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 65.0° C. or less, and a critical temperature of 83.5° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.383 MPa or more and 0.418 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is more preferably 22.0 to 27.7 mass % and the content rate of HFO-1234yf is more preferably 78.0 to 72.3 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 65.0° C. or less, and a critical temperature of 83.5° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.385 MPa or more and 0.417 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is further preferably 22.5 to 27.5 mass % and the content rate of HFO-1234yf is further preferably 77.5 to 72.5 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.388 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is particularly preferably 23.0 to 27.2 mass % and the content rate of HFO-1234yf is particularly preferably 77.0 to 72.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 141% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.390 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is extremely preferably 23.5 to 27.0 mass % and the content rate of HFO-1234yf is extremely preferably 76.5 to 73.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 142% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.390 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The content rate of HFO-1132(E) is most preferably 24.0 to 26.7 mass % and the content rate of HFO-1234yf is most preferably 76.0 to 73.3 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C4. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 144% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.6° C. or less, and a critical temperature of 84.0° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.396 MPa or more and 0.411 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The refrigerant 2C4 usually has a saturation pressure at a saturation temperature of −10° C., of 0.420 MPa or less, preferably 0.418 MPa or less, more preferably 0.417 MPa or less, further preferably 0.415 MPa or less, particularly preferably 0.413 MPa or less. Such a range enables the refrigerant 2C4 to be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


The refrigerant 2C4 usually has a saturation pressure at a saturation temperature of −10° C., of 0.380 MPa or more, preferably 0.385 MPa or more, more preferably 0.390 MPa or more, further preferably 0.400 MPa or more, particularly preferably 0.410 MPa or more. In such a case, the refrigerant 2C4 can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 65° C. or less, more preferably 64.8° C. or less, further preferably 64.7° C. or less, particularly preferably 64.5° C. or less from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R1234yf is extended.


The refrigerant 2C4 is preferably used for operating a refrigeration cycle at an evaporating temperature of −75 to 5° C. in the present disclosure, from the viewpoint that a refrigerating capacity relative to that of R1234yf of 140% or more is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably 5° C. or less, more preferably 0° C. or less, further preferably −5° C. or less, particularly preferably −10° C. or less, from the viewpoint that a refrigerating capacity relative to that of R1234yf of 140% or more is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably −75° C. or more, more preferably −60° C. or more, further preferably −55° C. or more, particularly preferably −50° C. or more, from the viewpoint that a refrigerating capacity relative to that of R1234yf of 140% or more is obtained.


The evaporating temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably −65° C. or more and 0° C. or less, more preferably −60° C. or more and −5° C. or less, further preferably −55° C. or more and −7.5° C. or less, particularly preferably −50° C. or more and −10° C. or less, from the viewpoint that a refrigerating capacity relative to that of R1234yf of 140% or more is obtained.


The discharge temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably 65.0° C. or less, more preferably 64.9° C. or less, further preferably 64.8° C. or less, particularly preferably 64.7° C. or less, from the viewpoint that the life of any member of a commercially available refrigerating apparatus for R1234yf is extended.


In a case where the refrigerant 2C4 is used for operating the refrigeration cycle, in the present disclosure, a process of liquefaction (condensation) of the refrigerant is required in the refrigeration cycle, and thus the critical temperature is required to be remarkably higher than the temperature of cooling water or cooling air for liquefying the refrigerant. The critical temperature in the refrigeration cycle where the refrigerant 2C4 of the present disclosure is used is preferably 83.5° C. or more, more preferably 83.8° C. or more, further preferably 84.0° C. or more, particularly preferably 84.5° C. or more, from such a viewpoint.


The refrigerant 2C4 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C4 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C4.


The refrigerant 2C4 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C4 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C4.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 21.0 to 28.4 mass % and the content rate of HFO-1234yf is usually 79.0 to 71.6 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant 2C4, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R1234yf and (3) a refrigerating capacity relative to that of R1234yf of 140% or more, and (4) lower flammability (Class 2L) according to ASHRAE Standard. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.380 MPa or more and 0.420 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is preferably 21.5 to 28.0 mass % and the content rate of HFO-1234yf is preferably 78.5 to 72.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 65.0° C. or less, and a critical temperature of 83.5° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.383 MPa or more and 0.418 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is more preferably 22.0 to 27.7 mass % and the content rate of HFO-1234yf is more preferably 78.0 to 72.3 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 65.0° C. or less, and a critical temperature of 83.5° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.385 MPa or more and 0.417 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is further preferably 22.5 to 27.5 mass % and the content rate of HFO-1234yf is further preferably 77.5 to 72.5 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 140% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.388 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is particularly preferably 23.0 to 27.2 mass % and the content rate of HFO-1234yf is particularly preferably 77.0 to 72.8 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 141% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.390 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is extremely preferably 23.5 to 27.0 mass % and the content rate of HFO-1234yf is extremely preferably 76.5 to 73.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 142% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.8° C. or less, and a critical temperature of 83.8° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.390 MPa or more and 0.414 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


In a case where the refrigerant 2C4 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is most preferably 24.0 to 26.7 mass % and the content rate of HFO-1234yf is most preferably 76.0 to 73.3 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. In such a case, the refrigerant 2C4 has various characteristics of a GWP of 100 or less, a COP relative to that of R1234yf of 98% or more, a refrigerating capacity relative to that of R1234yf of 144% or more, lower flammability (Class 2L) according to ASHRAE Standard, a discharge temperature of 64.6° C. or less, and a critical temperature of 84.0° C. or more. Furthermore, in such a case, the refrigerant 2C4 has a saturation pressure at a saturation temperature of −10° C., of 0.396 MPa or more and 0.411 MPa or less, and can be applied to a commercially available refrigerating apparatus for R1234yf without any significant change in design.


(1-6-3-5) Refrigerant 2C5

The refrigerant included in the composition of the present disclosure includes, in one aspect, HFO-1132(E) and HFO-1234yf, and the content rate of HFO-1132(E) is 12.1 to 72.0 mass % and the content rate of HFO-1234yf is 87.9 to 28.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf. The refrigerant is sometimes referred to as “refrigerant 2C5”.


In the present disclosure, the refrigerant 2C5 is used for in-car air conditioning equipment.


The refrigerant 2C5, which has such a configuration, thus has various characteristics of (1) a sufficiently low GWP (100 or less), (2) a COP comparable with that of R1234yf, (3) a refrigerating capacity relative to that of R1234yf of 128% or more, and (4) a flame velocity of less than 10.0 cm/s.


The content rate of HFO-1132(E) is 12.1 mass % or more based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5, and thus a boiling point of −40° C. or less can be ensured which is favorable in a case where heating is made by using a heat pump in an electric car. Herein, a boiling point of −40° C. or less means that the saturation pressure at −40° C. is equal to or more than atmospheric pressure, and such a lower boiling point of −40° C. or less is preferable in the above applications. The content rate of HFO-1132(E) is 72.0 mass % or less based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5, and thus a flame velocity of less than 10.0 cm/s can be ensured which contributes to safety in the case of use in in-car air conditioning equipment.


The refrigerating capacity relative to that of R1234yf in the refrigerant 2C5 may be 128% or more, and is preferably 130% or more, more preferably 140% or more, further preferably 150% or more, particularly preferably 160% or more.


The refrigerant 2C5 has a GWP of 5 or more and 100 or less, and thus can remarkably suppress the environmental load from the viewpoint of global warming as compared with other general-purpose refrigerants.


The ratio of the driving force consumed in the refrigeration cycle and the refrigerating capacity (coefficient of performance (COP)), relative to that of R1234yf, in the refrigerant 2C5 may be 100% or more from the viewpoint of energy consumption efficiency.


The refrigerant 2C5 is used in in-car air conditioning equipment, and thus an advantage is that heating can be made by a heat pump lower in consumption power as compared with an electric heater.


The air conditioning equipment with the refrigerant 2C5 is preferably for a gasoline-fueled car, a hybrid car, an electric car or a hydrogen-fueled car. In particular, the air conditioning equipment with the refrigerant 2C5 is particularly preferably for an electric car, from the viewpoint that not only heating in a vehicle interior is made by a heat pump, but also the travel distance of such a car is enhanced. That is, the refrigerant 2C5 is particularly preferably used in an electric car, in the present disclosure.


The refrigerant 2C5 is used in in-car air conditioning equipment, in the present disclosure. The refrigerant 2C5 is preferably used in air conditioning equipment of a gasoline-fueled car, air conditioning equipment of a hybrid car, air conditioning equipment of an electric car or air conditioning equipment of a hydrogen-fueled car, in the present disclosure. The refrigerant 2C5 is particularly preferably used in air conditioning equipment of an electric car, in the present disclosure.


Since a pressure equal to or more than atmospheric pressure at −40° C. is required in heating of a vehicle interior by a heat pump, the refrigerant 2C5 preferably has a boiling point of −51.2 to −40.0° C., more preferably −50.0 to −42.0° C., further preferably −48.0 to −44.0° C., in the present disclosure.


The content rate of HFO-1132(E) is preferably 15.0 to 65.0 mass % and the content rate of HFO-1234yf is preferably 85.0 to 35.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The content rate of HFO-1132(E) is more preferably 20.0 to 55.0 mass % and the content rate of HFO-1234yf is more preferably 80.0 to 45.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The content rate of HFO-1132(E) is further preferably 25.0 to 50.0 mass % and the content rate of HFO-1234yf is further preferably 75.0 to 50.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The content rate of HFO-1132(E) is particularly preferably 30.0 to 45.0 mass % and the content rate of HFO-1234yf is particularly preferably 70.0 to 55.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The content rate of HFO-1132(E) is most preferably 35.0 to 40.0 mass % and the content rate of HFO-1234yf is most preferably 65.0 to 60.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf in the refrigerant 2C5.


The refrigerant 2C5 preferably has a flame velocity of less than 10.0 cm/s, more preferably less than 5.0 cm/s, further preferably less than 3.0 cm/s, particularly preferably 2.0 cm/s, in the present disclosure.


The refrigerant 2C5 is preferably used for operating a refrigeration cycle at an evaporating temperature of −40 to 10° C. in the present disclosure, from the viewpoint that a refrigerating capacity equivalent to or more than that of R1234yf is obtained.


In a case where the refrigerant 2C5 is used for operating the refrigeration cycle, in the present disclosure, the discharge temperature is preferably 79° C. or less, more preferably 75° C. or less, further preferably 70° C. or less, particularly preferably 67° C. or less.


The refrigerant 2C5 may usually include 99.5 mass % or more of HFO-1132(E) and HFO-1234yf in terms of the sum of the concentrations of these components. In the present disclosure, the total amount of HFO-1132(E) and HFO-1234yf in the entire refrigerant 2C5 is preferably 99.7 mass % or more, more preferably 99.8 mass % or more, further preferably 99.9 mass % or more.


The refrigerant 2C5 can further include other refrigerant, in addition to HFO-1132(E) and HFO-1234yf, as long as the above characteristics are not impaired. In such a case, the content rate of such other refrigerant in the entire refrigerant 2C5 is preferably 0.5 mass % or less, more preferably 0.3 mass % or less, further preferably 0.2 mass % or less, particularly preferably 0.1 mass % or less. Such other refrigerant is not limited, and can be selected from a wide range of known refrigerants widely used in the art. Such other refrigerant may be included singly or in combinations of two or more kinds thereof in the refrigerant 2C5.


The refrigerant 2C5 particularly preferably consists only of HFO-1132(E) and HFO-1234yf. In other words, the refrigerant 2C5 particularly preferably includes HFO-1132(E) and HFO-1234yf at a total concentration of 100 mass % in the entire refrigerant 2C5.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is usually 12.1 to 72.0 mass % and the content rate of HFO-1234yf is usually 87.9 to 28.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is preferably 15.0 to 65.0 mass % and the content rate of HFO-1234yf is preferably 85.0 to 35.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is more preferably 20.0 to 55.0 mass % and the content rate of HFO-1234yf is more preferably 80.0 to 45.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is further preferably 25.0 to 50.0 mass % and the content rate of HFO-1234yf is further preferably 75.0 to 50.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is particularly preferably 30.0 to 45.0 mass % and the content rate of HFO-1234yf is particularly preferably 70.0 to 55.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


In a case where the refrigerant 2C5 consists only of HFO-1132(E) and HFO-1234yf, the content rate of HFO-1132(E) is most preferably 35.0 to 40.0 mass % and the content rate of HFO-1234yf is most preferably 65.0 to 60.0 mass % based on the total mass of HFO-1132(E) and HFO-1234yf.


[Examples of Refrigerant 2C]

Hereinafter, the refrigerant 2C will be described with reference to Examples in more detail. It is noted that the present disclosure is not limited to such Examples.


Test Example 1-1

The GWP of each mixed refrigerant represented in Examples 1-1 to 1-13, Comparative Examples 1-1 to 1-2 and Reference Example 1-1 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).



















Evaporating temperature
−35°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










An “evaporating temperature of −50° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is −50° C. A “condensation temperature of 40° C.” means that the condensation temperature of such each mixed refrigerant in a condenser included in a refrigerating apparatus is 40° C.


The results in Test Example 1-1 are shown in Table 33. Table 33 shows Examples and Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 33, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R404A.


In Table 33, the “Saturation pressure (40° C.)” represents the saturation pressure at a saturation temperature of 40° C. In Table 33, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant.


The coefficient of performance (COP) was determined according to the following expression.





COP=(Refrigerating capacity or heating capacity)/Power consumption


The compression ratio was determined by the following expression.





Compression ratio=Condensation pressure (Mpa)/Evaporating pressure (Mpa)


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. One having a flame velocity of 0 cm/s to 10 cm/s was rated as “Class 2L (lower flammability)”, one having a flame velocity of more than 10 cm/s was rated as “Class 2 (low flammability)”, and one causing no flame propagation was rated as “Class 1 (non-flammability)”. In Table 33, the “ASHRAE flammability classification” shows each result based on the criteria for determination.


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


The flammable range of the mixed refrigerant was measured by using an apparatus (see FIG. 1T) based on ASTM E681-09.


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>





    • Test container: spherical container of 280 mm in diameter (internal volume: 12 L)

    • Test temperature: 60° C.±3° C.

    • Pressure: 101.3 kPa±0.7 kPa

    • Water content: 0.0088 g±0.0005 g per gram of dry air (water content at a humidity of 50% at 23° C.)

    • Mixing ratio of refrigerant composition/air: ±0.2 vol. % by 1 vol. %

    • Mixing of refrigerant composition: ±0.1 mass %

    • Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer

    • Electrode interval: 6.4 mm (¼ inches)

    • Spark: 0.4 seconds±0.05 seconds





Criteria for Determination:





    • A case where any flame was spread at more than 90 degrees around the ignition point: flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)






















TABLE 33









Reference
Com-











Example
parative











1-1
Example
Example
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
1-1
1-1
1-2
1-3
14
1-5
1-6
1-7





















Composition
HFO-
mass %
  0
 30.0
 40.0
 40.5
 41.3
 43.0
 45.0
 47.0
 49.2


proportions
1132(E)













HFO-
mass %
  0
 70.0
 60.0
 59.5
 58.7
 57.0
 55.0
 53.0
 50.8



1234yf













HFC-134a
mass %
  4.0
 0
 0
 0
 0
 0
 0
 0
 0



HFC-143a
mass %
 52.0
 0
 0
 0
 0
 0
 0
 0
 0



HFC-125
mass %
 44.0
 0
 0
 0
 0
 0
 0
 0
 0

















GWP(AR4)

3922
 6
 6
 6
 6
 7
 7
 7
 7


Discharge temperature
° C.
 100.6
108.6
114.7
115.0
115.5
116.5
117.6
118.8
120.0


Saturationpressure (40° C.)
MPa
  1.822
 1.592
 1.745
 1.752
 1.764
 1.788
 1.817
 1.844
 1.874


Evaporating pressure
MPa
  0.082
 0.063
 0.072
 0.073
 0.074
 0.075
 0.077
 0.079
 0.081


Compression ratio

 22.2
 25.3
 24.1
 24.0
 23.9
 23.8
 23.6
 23.4
 23.1


COP ratio (relative to that of
%
100
106.2
106.2
106.2
106.2
106.2
106.2
106.2
106.2


R404A)












Refrigerating capacity ratio
%
100
 86.2
 98.5
 99.1
100
102.1
104.5
106.9
109.5


(relative to that of R404A)












ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification





























Com-






Exam-
Exam-
Exam-
Exam-
Exam-
Exam-
parative






ple
ple
ple
ple
ple
ple
Example




Item
Unit
1-8
1-9
1-10
1-11
1-12
1-13
1-2























Composition
HFO-
mass %
 51.0
 53.5
 55.0
 57.0
 59.0
 60.0
 70.0




proportions
1132(E)













HFO-
mass %
 49.0
 46.5
 45.0
 43.0
 41.0
 40.0
  30.0





1234yf













HFC-134a
mass %
 0
 0
 0
 0
 0
 0
 0





HFC-143a
mass %
 0
 0
 0
 0
 0
 0
 0





HFC-125
mass %
 0
 0
 0
 0
 0
 0
 0



















GWP(AR4)

 7
 7
 7
 7
 8
 8
 8




Discharge temperature
° C.
121.0
122.4
123.3
124.4
125.5
126.0
131.7




Saturationpressure (40° C.)
MPa
 1.898
 1.931
 1.950
 1.975
 2.000
 2.012
 2.128




Evaporating pressure
MPa
 0.083
 0.085
 0.086
 0.088
 0.090
 0.091
 0.099




Compression ratio

 23.0
 22.8
 22.6
 22.5
 22.3
 22.2
 21.6




COP ratio (relative to that of
%
106.3
106.3
106.3
106.3
106.4
106.4
106.7




R404A)












Refrigerating capacity ratio
%
111.7
114.6
116.4
118.7
121
122.2
133.3




(relative to that of R404A)












ASHRAE flammability

Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2




classification


















Test Example 1-2

The GWP of each mixed refrigerant represented in Examples 1-14 to 1-26, Comparative Examples 1-3 to 1-4 and Reference Example 1-2 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.



















Evaporating temperature
−35°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










The meaning of each of the above terms is the same as in Test Example 1-1.


The results in Test Example 1-2 are shown in Table 34. Table 34 shows Examples and Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 34, the meaning of each of the terms is the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 1-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 1-1. The flame velocity test was performed in the same manner as in Test Example 1-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 1-1.


















TABLE 34









Reference
Com-










Example
parative
Exam-
Exam-
Exam-
Exam-
Exam-
Exam-




1-2
Exam-
ple
ple
ple
ple
ple
ple


Item
Unit
(R404A)
ple 1-3
1-14
1-15
1-16
1-17
1-18
1-19




















Composition
HFO-1132(E)
mass %
  0
 30.0
 40.0
 40.5
 41.3
 43.0
 45.0
 47.0


proportions
HFO-1234yf
mass %
  0
 70.0
 60.0
 59.5
 58.7
 57.0
 55.0
 53.0



HFC-134a
mass %
  4.0
 0
 0
 0
 0
 0
 0
 0



HFC-143a
mass %
 52.0
 0
 0
 0
 0
 0
 0
 0



HFC-125
mass %
 44.0
 0
 0
 0
 0
 0
 0
 0
















GWP(AR4)

3922
 6
 6
 6
 6
 7
 7
 7


Discharge temperature
° C.
 89.1
 95.8
100.6
100.8
101.2
102.0
102.9
103.8


Saturation pressure
MPa
  1.822
 1.592
 1.745
 1.752
 1.764
 1.788
 1.817
 1.844


(40° C.)











Evaporating pressure
MPa
  0.165
 0.131
 0.148
 0.149
 0.151
 0.154
 0.157
 0.160


Compression ratio

 11.0
12.2
11.8
11.7
11.7
11.6
11.6
11.5


COP ratio (relative to that
%
 100
105.1
104.8
104.7
104.7
104.7
104.6
104.5


of R404A)











Refrigerating capacity ratio
%
 100
 87.7
 98.5
 99.0
 99.8
101.6
103.7
105.7


(relative to that of R404A)











ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification







Exam-
Exam-
Exam-
Exam-
Exam-
Exam-
Exam-
Com-




ple
ple
ple
ple
ple
ple
ple
parative


Item
Unit
1-20
1-21
1-22
1-23
1-24
1-25
1-26
Example 14




















Composition
HFO-1132(E)
mass %
 49.2
 51.0
 53.5
 55.0
 57.0
 59.0
 60.0
 70.0


proportions
HFO-1234yf
mass %
 50.8
 49.0
 46.5
 45.0
 43.0
 41.0
 40.0
 30.0



HFC-134a
mass %
  0
 0
 0
 0
 0
 0
 0
 0



HFC-143a
mass %
  0
 0
 0
 0
 0
 0
 0
 0



HFC-125
mass %
  0
 0
 0
 0
 0
 0
 0
 0
















GWP(AR4)

  7
 7
 7
 7
 7
 8
 8
 8


Discharge temperature
° C.
 104.7
105.5
106.6
107.3
108.1
109.0
109.5
113.9


Saturation pressure
MPa
  1.874
 1.898
 1.931
 1.950
 1.975
 2.000
 2.012
 2.128


(40° C.)











Evaporating pressure
MPa
  0.164
 0.167
 0.171
 0.174
 0.177
 0.180
 0.181
 0.196


Compression ratio

 11.4
 11.4
 11.3
 11.2
 11.2
 11.1
 11.1
 10.8


COP ratio (relative to that
%
 104.5
104.4
104.4
104.4
104.3
104.3
104.3
104.3


of R404A)











Refrigerating capacity ratio
%
 108.0
109.8
112.3
113.8
115.7
117.7
118.6
128.0


(relative to that of R404A)











ASHRAE flammability

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2


classification









Test Example 1-3

The GWP of each mixed refrigerant represented in Examples 1-27 to 1-39, Comparative Examples 1-5 to 1-6 and Reference Example 1-3 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.



















Evaporating temperature
−10°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










The meaning of each of the above terms is the same as in Test Example 1-1.


The results in Test Example 1-3 are shown in Table 35. Table 35 shows Examples and Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 35, the meaning of each of the terms is the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 1-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 1-1. The flame velocity test was performed in the same manner as in Test Example 1-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 1-1.


















TABLE 35









Reference











Example











1-3
Comparative
Example
Example
Example
Example
Example
Example


Item
Unit
(R404A)
Example 1-5
1-27
1-28
1-29
1-30
1-31
1-32




















Composition
HFO-
mass %
0
30.0
40.0
40.5
41.3
43.0
45.0
47.0


proportions
1132(E)












HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0
55.0
53.0



HFC-134a
mass %
4.0
0
0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0
0
0
















GWP(AR4)

3922
6
6
6
6
7
7
7


Discharge temperature
° C.
75.8
80.8
83.7
83.9
84.1
84.5
85.1
85.6


Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788
1.817
1.844


(40° C.)











Evaporating pressure
MPa
0.434
0.357
0.399
0.401
0.404
0.411
0.419
0.427


Compression ratio

4.2
4.5
4.4
4.4
4.4
4.3
4.3
4.3


COP ratio (relative to that
%
100
103.8
102.9
102.9
102.8
102.7
102.5
102.4


of R404A)











Refrigerating capacity ratio
%
100
89.8
98.7
99.1
99.8
101.2
102.8
104.5


(relative to that of R404A)











ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification























Example
Example
Example
Example
Example
Example
Example
Comparative



Item
Unit
1-33
1-34
1-35
1-36
1-37
1-38
1-39
Example 1-6






















Composition
HFO-
mass %
49.2
51.0
53.5
55.0
57.0
59.0
60.0
70.0




1132(E)












proportions
HFO-1234yf
mass %
50.8
49.0
46.5
45.0
43.0
41.0
40.0
30.0




HFC-134a
mass %
0
0
0
0
0
0
0
0




HFC-143a
mass %
0
0
0
0
0
0
0
0




HFC-125
mass %
0
0
0
0
0
0
0
0


















GWP(AR4)

7
7
7
7
7
8
8
8



Discharge temperature
° C.
86.2
86.6
87.3
87.7
88.2
88.7
88.9
91.5



Saturation pressure
MPa
1.874
1.898
1.931
1.950
1.975
2.000
2.012
2.128



(40° C.)












Evaporating pressure
MPa
0.436
0.443
0.452
0.457
0.465
0.472
0.475
0.509



Compression ratio

4.3
4.3
4.3
4.3
4.3
4.2
4.2
4.2



COP ratio (relative to that
%
102.2
102.1
102.0
101.9
101.8
101.7
101.6
101.3



of R404A)












Refrigerating capacity ratio
%
106.2
107.7
109.6
110.8
112.3
113.8
114.5
121.7



(relative to that of R404A)












ASHRAE flammability

Class 2L
Class 2L
Class 2L
Class 2
Class 2
Class 2
Class 2
Class 2



classification


















Test Example 1-4

The GWP of each mixed refrigerant represented in Comparative Examples 1-7 to 1-21 and Reference Example 1-4 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.



















Evaporating temperature
−80°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










The meaning of each of the above terms is the same as in Test Example 1-1.


The results in Test Example 1-4 are shown in Table 36. Table 36 shows Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 36, the meaning of each of the terms is the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 1-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 1-1. The flame velocity test was performed in the same manner as in Test Example 1-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 1-1.
















TABLE 36









Reference









Example 1-4
Comparative
Comparative
Comparative
Comparative
Comparative


Item
Unit
(R404A)
Example 1-7
Example 1-8
Example 1-9
Example 1-10
Example 1-11


















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0



HFC-134a
mass %
4.0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0














GWP (AR4)

3922
6
6
6
6
7


Discharge temperature
° C.
136.7
146.0
157.7
158.1
158.8
160.4


Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788


(40° C.)









Evaporating pressure
MPa
0.014
0.011
0.012
0.012
0.012
0.012


Compression ratio

134.6
149.1
150.8
150.2
149.3
147.2


COP ratio (relative to
%
100
112.6
110.3
110.3
110.4
110.6


that of R404A)









Refrigerating capacity
%
100
91.7
99.3
100.2
101.5
104.4


ratio (relative to









that of R404A)









ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification


















Comparative
Comparative
Comparative
Comparative
Comparative



Item
Example 1-12
Example 1-13
Example 1-14
Example 1-15
Example 1-16


















Composition
HFO-1132(E)
45.0
47.0
49.2
51.0
53.5



proportions
HFO-1234yf
55.0
53.0
50.8
49.0
46.5




HFC-134a
0
0
0
0
0




HFC-143a
0
0
0
0
0




HFC-125
0
0
0
0
0














GWP (AR4)
7
7
7
7
7



Discharge temperature
162.1
163.9
165.8
167.4
169.6



Saturation pressure
1.817
1.844
1.874
1.898
1.931



(40° C.)








Evaporating pressure
0.013
0.013
0.013
0.014
0.014



Compression ratio
145.0
142.8
140.5
138.7
136.3



COP ratio (relative to
110.8
111.0
111.3
111.4
111.7



that of R404A)








Refrigerating capacity
107.8
111.3
115.1
118.2
122.5



ratio (relative to








that of R404A)








ASHRAE flammability
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L



classification




















Comparative
Comparative
Comparative
Comparative
Comparative




Item
Example 1-17
Example 1-18
Example 1-19
Example 1-20
Example 1-21




















Composition
HFO-1132(E)
55.0
57.0
59.0
60.0
70.0




proportions
HFO-1234yf
45.0
43.0
41.0
40.0
30.0





HFC-134a
0
0
0
0
0





HFC-143a
0
0
0
0
0





HFC-125
0
0
0
0
0
















GWP (AR4)
7
7
8
8
8




Discharge temperature
170.9
172.6
174.3
175.2
184.0




Saturation pressure
1.950
1.975
2.000
2.012
2.128




(40° C.)









Evaporating pressure
0.014
0.015
0.015
0.015
0.017




Compression ratio
134.9
133.2
131.5
130.7
123.8




COP ratio (relative to
111.9
112.1
112.3
112.4
113.5




that of R404A)









Refrigerating capacity
125.2
128.6
132.1
133.8
151.0




ratio (relative to









that of R404A)









ASHRAE flammability
Class 2
Class 2
Class 2
Class 2
Class 2




classification









Test Example 1-5

The GWP of each mixed refrigerant represented in Comparative Examples 1-22 to 1-36 and Reference Example 1-5 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.



















Evaporating temperature
10°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










The meaning of each of the above terms is the same as in Test Example 1-1.


The results in Test Example 1-5 are shown in Table 37. Table 37 shows Comparative Examples of the refrigerant 2C1 of the present disclosure. In Table 37, the meaning of each of the terms is the same as in Test Example 1-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 1-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 1-1. The flame velocity test was performed in the same manner as in Test Example 1-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 1-1.
















TABLE 37









Reference
Com-
Com-
Com-
Com-
Com-




Example
parative
parative
parative
parative
parative




1-5
Example
Example
Example
Example
Example


Item
Unit
(R404A)
1-22
1-23
1-24
1-25
1-26


















Composition
HFO-1132(E)
mass %
 0
 30.0
 40.0
 40.5
 41.3
 43.0


proportions
HFO-1234yf
mass %
 0
 70.0
 60.0
 59.5
 58.7
 57.0



HFC-134a
mass %
 4.0
 0
 0
 0
 0
 0



HFC-143a
mass %
 52.0
 0
 0
 0
 0
 0



HFC-125
mass %
 44.0
 0
 0
 0
 0
 0














GWP (AR4)

 3922
 6
 6
 6
 6
 7


Discharge temperature
° C.
 68.5
 72.4
 74.0
 74.1
 74.2
 74.4


Saturation pressure
MPa
 1.822
 1.592
 1.745
 1.752
 1.764
 1.788


(40° C.)









Evaporating pressure
MPa
 0.820
0.694
0.768
0.772
0.777
0.789


Compression ratio

 2.2
 2.3
 2.3
 2.3
 2.3
 2.3


COP ratio (relative to
%
100.0
103.1
101.9
101.8
101.7
101.5


that of R404A)









Refrigerating capacity
%
100.0
 91.2
 98.9
 99.3
 99.8
101.0


ratio (relative to









that of R404A)









ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification

























Com-
Com-
Com-
Com-
Com-




parative
parative
parative
parative
parative




Example
Example
Example
Example
Example



Item
1-27
1-28
1-29
1-30
1-31


















Composition
HFO-1132(E)
 45.0
47.0
49.2
51.0
53.5



proportions
HFO-1234yf
 55.0
53.0
50.8
49.0
46.5




HFC-134a
 0
 0
 0
 0
 0




HFC-143a
 0
 0
 0
 0
 0




HFC-125
 0
 0
 0
 0
 0














GWP (AR4)
 7
 7
 7
 7
 7



Discharge temperature
 74.7
 74.9
 75.2
 75.5
 75.8



Saturation pressure
 1.817
 1.844
 1.874
 1.898
 1.931



(40° C.)








Evaporating pressure
 0.803
 0.817
 0.832
 0.844
 0.860



Compression ratio
 2.3
 2.3
 2.3
 2.2
 2.2



COP ratio (relative to
101.3
101.1
100.9
100.8
100.6



that of R404A)








Refrigerating capacity
102.5
103.8
105.3
106.5
108.2



ratio (relative to








that of R404A)








ASHRAE flammability
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L



classification




















Com-
Com-
Com-
Com-
Com-





parative
parative
parative
parative
parative





Example
Example
Example
Example
Example




Item
1-32
1-33
1-34
1-35
1-36




















Composition
HFO-1132(E)
 55.0
 57.0
 59.0
 60.0
 70.0




proportions
HFO-1234yf
 45.0
 43.0
 41.0
 40.0
 30.0





HFC-134a
 0
 0
 0
 0
 0





HFC-143a
 0
 0
 0
 0
 0





HFC-125
 0
 0
 0
 0
 0
















GWP (AR4)
 7
 7
 8
 8
 8




Discharge temperature
 76.0
 76.2
 76.5
 76.6
 77.9




Saturation pressure
 1.950
 1.975
 2.000
 2.012
 2.128




(40° C.)









Evaporating pressure
 0.870
 0.882
 0.895
 0.901
 0.959




Compression ratio
 2.2
 2.2
 2.2
 2.2
 2.2




COP ratio (relative to
100.4
100.3
100.1
100.1
 99.5




that of R404A)









Refrigerating capacity
109.1
110.4
111.6
112.3
118.2




ratio (relative to









that of R404A)









ASHRAE flammability
Class 2
Class 2
Class 2
Class 2
Class 2




classification









Test Example 2-1

The GWP of each mixed refrigerant represented in Examples 2-1 to 2-6, Comparative Examples 2-1 to 2-9 and Reference Example 2-1 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).



















Evaporating temperature
−50°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










An “evaporating temperature of −50° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is −50° C. A “condensation temperature of 40° C.” means that the condensation temperature of such each mixed refrigerant in a condenser included in a refrigerating apparatus is 40° C.


The results in Test Example 2-1 are shown in Table 38. Table 38 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 38, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R404A.


In Table 38, the “Saturation pressure (40° C.)” represents the saturation pressure at a saturation temperature of 40° C. In Table 38, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant.


The coefficient of performance (COP) was determined according to the following expression.





COP=(Refrigerating capacity or heating capacity)/Power consumption


The compression ratio was determined by the following expression.





Compression ratio=Condensation pressure (Mpa)/Evaporating pressure (Mpa)


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. One having a flame velocity of 0 cm/s to 10 cm/s was rated as “Class 2L (lower flammability)”, one having a flame velocity of more than 10 cm/s was rated as “Class 2 (low flammability)”, and one causing no flame propagation was rated as “Class 1 (non-flammability)”. In Table 38, the “ASHRAE flammability classification” shows each result based on the criteria for determination.


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


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09.


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>





    • Test container: spherical container of 280 mm in diameter (internal volume: 12 L)

    • Test temperature: 60° C.±3° C.

    • Pressure: 101.3 kPa±0.7 kPa

    • Water content: 0.0088 g±0.0005 g per gram of dry air (water content at a relative humidity of 50% at 23° C.)

    • Mixing ratio of refrigerant composition/air: ±0.2 vol. % by 1 vol. %

    • Mixing of refrigerant composition: ±0.1 mass %

    • Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer

    • Electrode interval: 6.4 mm (¼ inches)

    • Spark: 0.4 seconds±0.05 seconds





Criteria for Determination:





    • A case where any flame was spread at more than 90 degrees around the ignition point: flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)



















TABLE 38









Reference









Example 2-1
Comparative
Comparative





Item
Unit
(R404A)
Example 2-1
Example 2-2
Example 2-1
Example 2-2
Example 2-3


















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0



HFC-134a
mass %
4.0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0














GWP (AR4)

3922
6
6
6
6
7


Discharge temperature
° C.
100.6
108.6
114.7
115.0
115.5
116.5


Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788


(40° C.)









Evaporating pressure
MPa
0.082
0.063
0.072
0.073
0.074
0.075


Compression ratio

22.2
25.3
24.1
24.0
23.9
23.8


COP ratio (relative to
%
100
106.2
106.2
106.2
106.2
106.2


that of R404A)









Refrigerating capacity
%
100
86.2
98.5
99.1
100
102.1


ratio (relative to









that of R404A)









ASHRAE

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


flammability









classification





















Comparative
Comparative



Item
Example 2-4
Example 2-5
Example 2-6
Example 2-3
Example 2-4


















Composition
HFO-1132(E)
45.0
47.0
49.2
51.0
53.5



proportions
HFO-1234yf
55.0
53.0
50.8
49.0
46.5




HFC-134a
0
0
0
0
0




HFC-143a
0
0
0
0
0




HFC-125
0
0
0
0
0














GWP (AR4)
7
7
7
7
7



Discharge temperature
117.6
118.8
120.0
121.0
122.4



Saturation pressure
1.817
1.844
1.874
1.898
1.931



(40° C.)








Evaporating pressure
0.077
0.079
0.081
0.083
0.085



Compression ratio
23.6
23.4
23.1
23.0
22.8



COP ratio (relative to
106.2
106.2
106.2
106.3
106.3



that of R404A)








Refrigerating capacity
104.5
106.9
109.5
111.7
114.6



ratio (relative to








that of R404A)








ASHRAE
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L



flammability








classification




















Comparative
Comparative
Comparative
Comparative
Comparative




Item
Example 2-5
Example 2-6
Example 2-7
Example 2-8
Example 2-9




















Composition
HFO-1132(E)
55.0
57.0
59.0
60.0
70.0




proportions
HFO-1234yf
45.0
43.0
41.0
40.0
30.0





HFC-134a
0
0
0
0
0





HFC-143a
0
0
0
0
0





HFC-125
0
0
0
0
0
















GWP (AR4)
7
7
8
8
8




Discharge temperature
123.3
124.4
125.5
126.0
131.7




Saturation pressure
1.950
1.975
2.000
2.012
2.128




(40° C.)









Evaporating pressure
0.086
0.088
0.090
0.091
0.099




Compression ratio
22.6
22.5
22.3
22.2
21.6




COP ratio (relative to
106.3
106.3
106.4
106.4
106.7




that of R404A)









Refrigerating capacity
116.4
118.7
121
122.2
133.3




ratio (relative to









that of R404A)









ASHRAE
Class 2
Class 2
Class 2
Class 2
Class 2




flammability









classification









Test Example 2-2

The GWP of each mixed refrigerant represented in Examples 2-7 to 2-12, Comparative Examples 2-10 to 2-18 and Reference Example 2-2 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.



















Evaporating temperature
−35°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










The meaning of each of the above terms is the same as in Test Example 2-1.


The results in Test Example 2-2 are shown in Table 39. Table 39 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 39, the meaning of each of the terms is the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 2-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 2-1. The flame velocity test was performed in the same manner as in Test Example 2-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 2-1.
















TABLE 39









Reference









Example 2-2
Comparative
Comparative





Item
Unit
(R404A)
Example 2-10
Example 2-11
Example 2-7
Example 2-8
Example 2-9


















Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0



HFC-134a
mass %
4.0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0














GWP (AR4)

3922
6
6
6
6
7


Discharge temperature
° C.
89.1
95.8
100.6
100.8
101.2
102.0


Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788


(40° C.)









Evaporating pressure
MPa
0.165
0.131
0.148
0.149
0.151
0.154


Compression ratio

11.0
12.2
11.8
11.7
11.7
11.6


COP ratio (relative to
%
100
105.1
104.8
104.7
104.7
104.7


that of R404A)









Refrigerating capacity
%
100
87.7
98.5
99.0
99.8
101.6


ratio (relative to









that of R404A)









ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification





















Comparative
Comparative



Item
Example 2-10
Example 2-11
Example 2-12
Example 2-12
Example 2-13


















Composition
HFO-1132(E)
45.0
47.0
49.2
51.0
53.5



proportions
HFO-1234yf
55.0
53.0
50.8
49.0
46.5




HFC-134a
0
0
0
0
0




HFC-143a
0
0
0
0
0




HFC-125
0
0
0
0
0














GWP (AR4)
7
7
7
7
7



Discharge temperature
102.9
103.8
104.7
105.5
106.6



Saturation pressure
1.817
1.844
1.874
1.898
1.931



(40° C.)








Evaporating pressure
0.157
0.160
0.164
0.167
0.171



Compression ratio
11.6
11.5
11.4
11.4
11.3



COP ratio (relative to
104.6
104.5
104.5
104.4
104.4



that of R404A)








Refrigerating capacity
103.7
105.7
108.0
109.8
112.3



ratio (relative to








that of R404A)








ASHRAE flammability
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L



classification




















Comparative
Comparative
Comparative
Comparative
Comparative




Item
Example 2-14
Example 2-15
Example 2-16
Example 2-17
Example 2-18




















Composition
HFO-1132(E)
55.0
57.0
59.0
60.0
70.0




proportions
HFO-1234yf
45.0
43.0
41.0
40.0
30.0





HFC-134a
0
0
0
0
0





HFC-143a
0
0
0
0
0





HFC-125
0
0
0
0
0
















GWP (AR4)
7
7
8
8
8




Discharge temperature
107.3
108.1
109.0
109.5
113.9




Saturation pressure
1.950
1.975
2.000
2.012
2.128




(40° C.)









Evaporating pressure
0.174
0.177
0.180
0.181
0.196




Compression ratio
11.2
11.2
11.1
11.1
10.8




COP ratio (relative to
104.4
104.3
104.3
104.3
104.3




that of R404A)









Refrigerating capacity
113.8
115.7
117.7
118.6
128.0




ratio (relative to









that of R404A)









ASHRAE flammability
Class 2
Class 2
Class 2
Class 2
Class 2




classification









Test Example 2-3

The GWP of each mixed refrigerant represented in Examples 2-13 to 2-18, Comparative Examples 2-19 to 2-27 and Reference Example 2-3 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.



















Evaporating temperature
−10°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










The meaning of each of the above terms is the same as in Test Example 2-1.


The results in Test Example 2-3 are shown in Table 40. Table 40 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 40, the meaning of each of the terms is the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 2-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 2-1. The flame velocity test was performed in the same manner as in Test Example 2-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 2-1.
















TABLE 40









Reference
Com-
Com-







Example
parative
parative







2-3
Example
Example
Example
Example
Example


Item
Unit
(R404A)
2-19
2-20
2-13
2-14
2-15


















Composition
HFO-1132(E)
mass %
  0
 30.0
 40.0
 40.5
 41.3
 43.0


proportions
HFO-1234yf
mass %
  0
 70.0
 60.0
 59.5
 58.7
 57.0



HFC-134a
mass %
  4.0
 0
 0
 0
 0
 0



HFC-143a
mass %
 52.0
 0
 0
 0
 0
 0



HFC-125
mass %
 44.0
 0
 0
 0
 0
 0














GWP (AR4)

3922
 6
 6
 6
 6
 7


Discharge temperature
° C.
 75.8
 80.8
 83.7
 83.9
 84.1
 84.5


Saturation pressure
MPa
  1.822
 1.592
 1.745
 1.752
 1.764
 1.788


(40° C.)









Evaporating pressure
MPa
  0.434
 0.357
 0.399
 0.401
 0.404
 0.411


Compression ratio

  4.2
 4.5
 4.4
 4.4
 4.4
 4.3


COP ratio (relative to
%
 100
103.8
102.9
102.9
102.8
102.7


that of R404A)









Refrigerating capacity
%
 100
 89.8
 98.7
 99.1
 99.8
101.2


ratio (relative to









that of R404A)









ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification





















Com-
Com-







parative
parative




Example
Example
Example
Example
Example



Item
2-16
2-17
2-18
2-21
2-22


















Composition
HFO-1132(E)
 45.0
 47.0
 49.2
 51.0
 53.5



proportions
HFO-1234yf
 55.0
 53.0
 50.8
 49.0
 46.5




HFC-134a
  0
 0
 0
 0
 0




HFC-143a
  0
 0
 0
 0
 0




HFC-125
  0
 0
 0
 0
 0














GWP (AR4)
  7
 7
 7
 7
 7



Discharge temperature
 85.1
 85.6
 86.2
 86.6
 87.3



Saturation pressure
  1.817
 1.844
 1.874
 1.898
 1.931



(40° C.)








Evaporating pressure
  0.419
 0.427
 0.436
 0.443
 0.452



Compression ratio
  4.3
 4.3
 4.3
 4.3
 4.3



COP ratio (relative to
 102.5
102.4
102.2
102.1
102.0



that of R404A)








Refrigerating capacity
 102.8
104.5
106.2
107.7
109.6



ratio (relative to








that of R404A)








ASHRAE flammability
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L



classification




















Com-
Com-
Com-
Com-
Com-





parative
parative
parative
parative
parative





Example
Example
Example
Example
Example




Item
2-23
2-24
2-25
2-26
2-27




















Composition
HFO-1132(E)
 55.0
 57.0
 59.0
 60.0
 70.0




proportions
HFO-1234yf
 45.0
 43.0
 41.0
 40.0
 30.0





HFC-134a
 0
 0
 0
 0
 0





HFC-143a
 0
 0
 0
 0
 0





HFC-125
 0
 0
 0
 0
 0
















GWP (AR4)
 7
 7
 8
 8
 8




Discharge temperature
 87.7
 88.2
 88.7
 88.9
 91.5




Saturation pressure
 1.950
 1.975
 2.000
 2.012
 2.128




(40° C.)









Evaporating pressure
 0.457
 0.465
 0.472
 0.475
 0.509




Compression ratio
 4.3
 4.3
 4.2
 4.2
 4.2




COP ratio (relative to
101.9
101.8
101.7
101.6
101.3




that of R404A)









Refrigerating capacity
110.8
112.3
113.8
114.5
121.7




ratio (relative to









that of R404A)









ASHRAE flammability
Class 2
Class 2
Class 2
Class 2
Class 2




classification









Test Example 2-4

The GWP of each mixed refrigerant represented in Examples 2-19 to 2-24, Comparative Examples 2-28 to 2-36 and Reference Example 2-4 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.



















Evaporating temperature
−80°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










The meaning of each of the above terms is the same as in Test Example 2-1.


The results in Test Example 2-4 are shown in Table 41. Table 41 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 41, the meaning of each of the terms is the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 2-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 2-1. The flame velocity test was performed in the same manner as in Test Example 2-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 2-1.
















TABLE 41









Reference
Comparative
Comparative







Example 2-4
Example
Example
Example
Example
Example



Unit
(R404A)
2-28
2-29
2-19
2-20
2-21


















Com-
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0


position
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0


pro-
HFC-134a
mass %
4.0
0
0
0
0
0


portions
HFC-143a
mass %
52.0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0














GWP (AR4)

3922
6
6
6
6
7


Discharge temperature
° C.
136.7
146.0
157.7
158.1
158.8
160.4


Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788


(40° C.)









Evaporating pressure
MPa
0.014
0.011
0.012
0.012
0.012
0.012


Compression ratio

134.6
149.1
150.8
150.2
149.3
147.2


COP ratio (relative to
%
100
112.6
110.3
110.3
110.4
110.6


that of R404A)









Refrigerating capacity
%
100
91.7
99.3
100.2
101.5
104.4


ratio (relative to









that of R404A)









ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification























Comparative
Comparative





Example
Example
Example
Example
Example





2-22
2-23
2-24
2-30
2-31






Composition
HFO-1132(E)
45.0
47.0
49.2
51.0
53.5



proportions
HFO-1234yf
55.0
53.0
50.8
49.0
46.5




HFC-134a
0
0
0
0
0




HFC-143a
0
0
0
0
0




HFC-125
0
0
0
0
0














GWP (AR4)
7
7
7
7
7



Discharge temperature
162.1
163.9
165.8
167.4
169.6



Saturation pressure
1.817
1.844
1.874
1.898
1.931



(40° C.)








Evaporating pressure
0.013
0.013
0.013
0.014
0.014



Compression ratio
145.0
142.8
140.5
138.7
136.3



COP ratio (relative to
110.8
111.0
111.3
111.4
111.7



that of R404A)








Refrigerating capacity
107.8
111.3
115.1
118.2
122.5



ratio (relative to








that of R404A)








ASHRAE flammability
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L



classification






















Com-
Com-
Com-
Com-
Com-






parative
parative
parative
parative
parative






Example
Example
Example
Example
Example






2-32
2-33
2-34
2-35
2-36







Composition
HFO-1132(E)
55.0
57.0
59.0
60.0
70.0




proportions
HFO-1234yf
45.0
43.0
41.0
40.0
30.0





HFC-134a
0
0
0
0
0





HFC-143a
0
0
0
0
0





HFC-125
0
0
0
0
0
















GWP (AR4)
7
7
8
8
8




Discharge temperature
170.9
172.6
174.3
175.2
184.0




Saturation pressure
1.950
1.975
2.000
2.012
2.128




(40° C.)









Evaporating pressure
0.014
0.015
0.015
0.015
0.017




Compression ratio
134.9
133.2
131.5
130.7
123.8




COP ratio (relative to
111.9
112.1
112.3
112.4
113.5




that of R404A)









Refrigerating capacity
125.2
128.6
132.1
133.8
151.0




ratio (relative to









that of R404A)









ASHRAE flammability
Class 2
Class 2
Class 2
Class 2
Class 2




classification









Test Example 2-5

The GWP of each mixed refrigerant represented in Examples 2-25 to 2-30, Comparative Examples 2-37 to 2-45 and Reference Example 2-5 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 40° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using NIST and Refprop 9.0.



















Evaporating temperature
10°
C.



Condensation temperature
40°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










The meaning of each of the above terms is the same as in Test Example 2-1.


The results in Test Example 2-5 are shown in Table 42. Table 42 shows Examples and Comparative Examples of the refrigerant 2C2 of the present disclosure. In Table 42, the meaning of each of the terms is the same as in Test Example 2-1.


The coefficient of performance (COP) and the compression ratio were determined in the same manner as in Test Example 2-1.


The flammability of such each mixed refrigerant was determined in the same manner as in Test Example 2-1. The flame velocity test was performed in the same manner as in Test Example 2-1.


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09, with the same method and test conditions as in Test Example 2-1.

















TABLE 42










Reference










Example 2-5
Comparative
Comparative







Unit
(R404A)
Example 2-37
Example 2-38
Example 2-25
Example 2-26
Example 2-27





Composition
HFO-1132(E)
mass %
0
30.0
40.0
40.5
41.3
43.0


proportions
HFO-1234yf
mass %
0
70.0
60.0
59.5
58.7
57.0



HFC-134a
mass %
4.0
0
0
0
0
0



HFC-143a
mass %
52.0
0
0
0
0
0



HFC-125
mass %
44.0
0
0
0
0
0














GWP (AR4)

3922
6
6
6
6
7


Discharge temperature
° C.
68.5
72.4
74.0
74.1
74.2
74.4


Saturation pressure
MPa
1.822
1.592
1.745
1.752
1.764
1.788


(40° C.)









Evaporating pressure
MPa
0.820
0.694
0.768
0.772
0.777
0.789


Compression ratio

2.2
2.3
2.3
2.3
2.3
2.3


COP ratio (relative to
%
100.0
103.1
101.9
101.8
101.7
101.5


that of R404A)









Refrigerating capacity
%
100.0
91.2
98.9
99.3
99.8
101.0


ratio (relative to









that of R404A)









ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification





















Comparative
Comparative




Example 2-28
Example 2-29
Example 2-30
Example 2-39
Example 2-40





Composition
HFO-1132(E)
45.0
47.0
49.2
51.0
53.5


proportions
HFO-1234yf
55.0
53.0
50.8
49.0
46.5



HFC-134a
0
0
0
0
0



HFC-143a
0
0
0
0
0



HFC-125
0
0
0
0
0












GWP (AR4)
7
7
7
7
7


Discharge temperature
74.7
74.9
75.2
75.5
75.8


Saturation pressure
1.817
1.844
1.874
1.898
1.931


(40° C.)







Evaporating pressure
0.803
0.817
0.832
0.844
0.860


Compression ratio
2.3
2.3
2.3
2.2
2.2


COP ratio (relative to
101.3
101.1
100.9
100.8
100.6


that of R404A)







Refrigerating capacity
102.5
103.8
105.3
106.5
108.2


ratio (relative to







that of R404A)







ASHRAE flammability
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification




















Comparative
Comparative
Comparative
Comparative
Comparative





Example 2-41
Example 2-42
Example 2-43
Example 2-44
Example 2-45






Composition
HFO-1132(E)
55.0
57.0
59.0
60.0
70.0



proportions
HFO-1234yf
45.0
43.0
41.0
40.0
30.0




HFC-134a
0
0
0
0
0




HFC-143a
0
0
0
0
0




HFC-125
0
0
0
0
0














GWP (AR4)
7
7
8
8
8



Discharge temperature
76.0
76.2
76.5
76.6
77.9



Saturation pressure
1.950
1.975
2.000
2.012
2.128



(40° C.)








Evaporating pressure
0.870
0.882
0.895
0.901
0.959



Compression ratio
2.2
2.2
2.2
2.2
2.2



COP ratio (relative to
100.4
100.3
100.1
100.1
99.5



that of R404A)








Refrigerating capacity
109.1
110.4
111.6
112.3
118.2



ratio (relative to








that of R404A)








ASHRAE flammability
Class 2
Class 2
Class 2
Class 2
Class 2



classification









Test Example 3

The GWP of each mixed refrigerant represented in Examples 3-1 to 3-5, Comparative Examples 3-1 to 3-5, Reference Example 3-1 (R134a) and Reference Example 3-2 (R404A) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature, the saturation pressure at a saturation temperature of 45° C., the condensation pressure and the evaporating pressure of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).



















Evaporating temperature
−10°
C.



Condensation temperature
45°
C.



Superheating temperature
20
K



Subcooling temperature
0
K










Compressor efficiency
70%










An “evaporating temperature of −10° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is −10° C. A “condensation temperature of 45° C.” means that the condensation temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is 45° C.


The results in Test Example 3 are shown in Table 43. Table 43 shows Examples and Comparative Examples of the refrigerant 2C3 of the present disclosure. In Table 43, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R134a. In Table 43, the “Saturation pressure (45° C.)” represents the saturation pressure at a saturation temperature of 45° C. In Table 43, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant.


The coefficient of performance (COP) was determined according to the following expression.





COP=(Refrigerating capacity or heating capacity)/Power consumption


The critical temperature was determined by performing calculation by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. One having a flame velocity of 0 cm/s to 10 cm/s was rated as “Class 2L (lower flammability)”, one having a flame velocity of more than 10 cm/s was rated as “Class 2 (low flammability)”, and one causing no flame propagation was rated as “Class 1 (non-flammability)”. In Table 43, the “ASHRAE flammability classification” shows each result based on the criteria for determination.


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


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09.


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>





    • Test container: spherical container of 280 mm in diameter (internal volume: 12 L)

    • Test temperature: 60° C.±3° C.

    • Pressure: 101.3 kPa±0.7 kPa

    • Water content: 0.0088 g±0.0005 g per gram of dry air (water content at a relative humidity of 50% at 23° C.)

    • Mixing ratio of refrigerant composition/air: ±0.2 vol. % by 1 vol. %

    • Mixing of refrigerant composition: ±0.1 mass %

    • Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer

    • Electrode interval: 6.4 mm (¼ inches)

    • Spark: 0.4 seconds±0.05 seconds





Criteria for Determination:





    • A case where any flame was spread at more than 90 degrees around the ignition point: flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)



















TABLE 43









Reference









Example 3-1
Comparative
Comparative





Item
Unit
(R134a)
Example 3-1
Example 3-2
Example 3-1
Example 3-2
Example 3-3


















Composition
HFO-1132(E)
mass %
0
20.0
30.0
31.1
33.0
35.0


proportions
HFO-1234yf
mass %
0
80.0
70.0
68.9
67.0
65.0



HFC-134a
mass %
100.0
0
0
0
0
0



HFC-143a
mass %
0
0
0
0
0
0



HFC-125
mass %
0
0
0
0
0
0














GWP (AR4)

1430
5
6
6
6
6


Discharge temperature
° C.
86.9
86.3
86.9
87.2
87.9
88.5


Saturation pressure
MPa
1.160
1.607
1.795
1.814
1.848
1.883


(45° C.)









Evaporating pressure
MPa
0.201
0.311
0.355
0.360
0.368
0.376


Critical temperature
° C.
101.1
84.6
83.0
82.7
82.2
81.7


COP ratio (relative to
%
100.0
93.6
92.7
92.6
92.4
92.2


that of R134a)









Refrigerating capacity
%
100.0
132.3
148.3
150.0
152.8
155.8


ratio (relative to









that of R134a)









ASHRAE flammability

Class 1
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification
























Reference






Comparative
Comparative
Comparative
Example 3-2



Item
Example 3-4
Example 3-5
Example 3-3
Example 3-4
Example 3-5
(R404A)



















Composition
HFO-1132(E)
37.9
39.8
40.0
50.0
0.0
0



proportions
HFO-1234yf
62.1
60.2
60.0
50.0
100.0
0




HFC-134a
0
0
0
0
0
4.0




HFC-143a
0
0
0
0
0
52.0




HFC-125
0
0
0
0
0
44.0















GWP (AR4)
6
6
6
7
4
3922



Discharge temperature
89.4
90.0
90.1
93.0
72.2
81.7



Saturation pressure
1.930
1.963
1.966
2.123
1.154
2.052



(45° C.)









Evaporating pressure
0.388
0.397
0.397
0.437
0.222
0.434



Critical temperature
81.0
80.5
80.5
78.7
94.7
72.0



COP ratio (relative to
92.0
91.8
91.8
91.0
95.7
88.6



that of R134a)









Refrigerating capacity
159.8
162.7
162.9
176.6
96.2
164.4



ratio (relative to









that of R134a)









ASHRAE flammability
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 1



classification









Test Example 4

The GWP of each mixed refrigerant represented in Examples 4-1 to 4-7 and Comparative Examples 4-1 to 4-5 was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the discharge temperature and the saturation pressure at a saturation temperature of −10° C. of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).



















Evaporating temperature

C.



Condensation temperature
45°
C.



Superheating temperature
5
K



Subcooling temperature
5
K










Compressor efficiency
70%










An “evaporating temperature of 5° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is 5° C. A “condensation temperature of 45° C.” means that the condensation temperature of such each mixed refrigerant in a condenser included in a refrigerating apparatus is 45° C.


The results in Test Example 4 are shown in Table 44. Table 44 shows Examples and Comparative Examples of the refrigerant 2C4 of the present disclosure. In Table 44, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R1234yf. In Table 44, the “Saturation pressure (−10° C.)” represents the saturation pressure at a saturation temperature of −10° C., as a representative evaporating temperature value under refrigeration conditions. In Table 44, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant.


The coefficient of performance (COP) was determined according to the following expression.





COP=(Refrigerating capacity or heating capacity)/Power consumption


The critical temperature was determined by performing calculation by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. One having a flame velocity of 0 cm/s to 10 cm/s was rated as “Class 2L (lower flammability)”, one having a flame velocity of more than 10 cm/s was rated as “Class 2 (low flammability)”, and one causing no flame propagation was rated as “Class 1 (non-flammability)”. In Table 44, the “ASHRAE flammability classification” shows each result based on the criteria for determination.


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


The flammable range of the mixed refrigerant was measured by using a measurement apparatus (see FIG. 1T) based on ASTM E681-09.


Specifically, a spherical glass flask having an internal volume of 12 L was used so that the state of flame could be visually observed, and recorded and imaged, and the glass flask was set so that any gas was released through a lid at the top when an excess pressure was generated due to flame. The ignition method was made by generating ignition due to discharge from an electrode held at a height of ⅓ from the bottom.


<Test Conditions>





    • Test container: spherical container of 280 mm in diameter (internal volume: 12 L)

    • Test temperature: 60° C.±3° C.

    • Pressure: 101.3 kPa±0.7 kPa

    • Water content: 0.0088 g±0.0005 g per gram of dry air (water content at a relative humidity of 50% at 23° C.)

    • Mixing ratio of refrigerant composition/air: ±0.2 vol. % by 1 vol. %

    • Mixing of refrigerant composition: ±0.1 mass %

    • Ignition method: AC discharge, voltage 15 kV, current 30 mA, neon transformer

    • Electrode interval: 6.4 mm (¼ inches)

    • Spark: 0.4 seconds±0.05 seconds





Criteria for Determination:





    • A case where any flame was spread at more than 90 degrees around the ignition point: flame propagation (flammability)

    • A case where any flame was spread at 90 degrees or less around the ignition point: no flame propagation (non-flammability)



















TABLE 44









Comparative
Comparative






Item
Unit
Example 4-1
Example 4-2
Example 4-1
Example 4-2
Example 4-3
Example 4-4


















Composition
HFO-1132(E)
mass %
0
15.0
21.0
23.6
24.3
25.1


proportions
HFO-1234yf
mass %
100.0
85.0
79.0
76.4
75.7
74.9














GWP (AR4)

4
5
5
5
5
6


Discharge temperature
° C.
54.4
61.3
63.1
63.8
64.0
64.2


Saturation pressure
MPa
0.222
0.350
0.383
0.396
0.400
0.403


(−10° C.)









Critical temperature
° C.
94.7
88.1
85.9
85.0
84.8
84.5


COP ratio (relative to
%
100.0
99.1
98.8
98.6
98.5
98.4


that of R1234yf)









Refrigerating capacity
%
100.0
129.8
140.0
144.2
145.4
146.6


ratio (relative to









that of R1234yf)









ASHRAE flammability

Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L


classification






















Comparative
Comparative
Comparative



Item
Example 4-5
Example 4-6
Example 4-7
Example 4-3
Example 4-4
Example 4-5



















Composition
HFO-1132(E)
26.7
27.5
28.4
30.0
40.0
50.0



proportions
HFO-1234yf
73.3
72.5
71.6
70.0
60.0
50.0















GWP (AR4)
6
6
6
6
6
7



Discharge temperature
64.6
64.8
65.0
65.4
67.5
69.4



Saturation pressure
0.411
0.414
0.418
0.425
0.461
0.492



(−10° C.)









Critical temperature
84.0
83.8
83.5
83.0
80.5
78.7



COP ratio (relative to
98.3
98.2
98.2
98.0
97.2
96.6



that of R1234yf)









Refrigerating capacity
149.1
150.3
151.7
154.1
168.2
181.3



ratio (relative to









that of R1234yf)









ASHRAE flammability
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L
Class 2L



classification









Test Example 5

The GWP of each mixed refrigerant represented in Examples 5-1 to 5-13, Comparative Examples 5-1 to 5-3 and Reference Example 5-1 (R134a) was evaluated based on the value in the fourth report of IPCC.


The COP, the refrigerating capacity, the boiling point and the discharge temperature of such each mixed refrigerant were determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).



















Evaporating temperature
−30°
C.



Condensation temperature
30°
C.



Superheating temperature
5
K



Subcooling temperature
5
K










Compressor efficiency
70%










An “evaporating temperature of −30° C.” means that the evaporating temperature of such each mixed refrigerant in an evaporator included in a refrigerating apparatus is −30° C. A “condensation temperature of 30° C.” means that the condensation temperature of such each mixed refrigerant in a condenser included in a refrigerating apparatus is 30° C.


The results in Test Example 5 are shown in Table 45. Table 45 shows Examples and Comparative Examples of the refrigerant 2C5 of the present disclosure. In Table 45, the “COP ratio” and the “Refrigerating capacity ratio” each represent the proportion (%) relative to that of R1234yf. In Table 45, the “Discharge temperature (° C.)” represents the temperature at which the highest temperature in the refrigeration cycle is achieved in theoretical refrigeration cycle calculation with respect to such each mixed refrigerant. In Table 45, the “Boiling point (° C.)” represents the temperature at which a liquid phase of such each mixed refrigerant is at atmospheric pressure (101.33 kPa). In Table 45, “Power consumption (%) of driving force” represents the electric energy used for traveling an electric car, and is represented by the ratio to the power consumption in the case of HFO-1234yf as the refrigerant. In Table 45, “Heating power consumption (%)” represents the electric energy used for operating heating by an electric car, and is represented by the ratio to the power consumption in the case of HFO-1234yf as the refrigerant. In Table 45, the “Mileage” represents the relative proportion (%) of the mileage in traveling with heating when the mileage in travelling with no heating in an electric car in which a secondary battery having a certain electric capacitance is mounted is 100% (the consumption power in heating is 0).


The coefficient of performance (COP) was determined according to the following expression.





COP=(Refrigerating capacity or heating capacity)/Power consumption


The flammability of such each mixed refrigerant was determined by defining the mixed composition of such each mixed refrigerant as the WCF concentration, and measuring the flame velocity according to ANSI/ASHRAE Standard 34-2013. The flame velocity was measured as follows. First, the mixed refrigerant used had a purity of 99.5% or more, and degassing was made by repeating a cycle of freezing, pumping and thawing until no trace of air was observed on a vacuum gauge. The flame velocity was measured by a closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between electrodes at the center of a sample cell. The duration of discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of any flame was visualized using a schlieren photograph. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light-transmitting acrylic windows was used as the sample cell, and a xenon lamp was used as a light source. A schlieren image of any flame was recorded by a high-speed digital camera at a frame rate of 600 fps, and stored in a PC.


The heating method included using an electric heater system for heating in the case of any refrigerant having a boiling point of more than −40° C., or using a heat pump system for heating in the case of refrigerant having a boiling point of −40° C. or less.


The power consumption in use of heating was determined by the following expression.





Power consumption in use of heating=Heating capacity/Heating COP


Herein, the heating COP means “heating efficiency”.


The heating efficiency means that the heating COP is 1 in the case of an electric heater, and an electrode comparable with a driving force is consumed in heating. In other words, the consumption power in heating is expressed by E=E/(1+COP). On the other hand, the heating COP in the case of a heat pump was determined by performing theoretical refrigeration cycle calculation with respect to such each mixed refrigerant under the following conditions by using National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0).

    • Evaporating temperature −30° C.
    • Condensation temperature 30° C.
    • Superheating temperature 5 K
    • Subcooling temperature 5 K
    • Compressor efficiency 70%


The mileage was determined by the following expression.





Mileage=(Battery capacitance)/(Power consumption of driving force+Heating power consumption)
















TABLE 45









Reference
Comparative
Comparative





Item
Unit
Example 5-1
Example 5-1
Example 5-2
Example 5-1
Example 5-2
Example 5-3


















Composition
HFO-1132(E)
mass %
0.0
0
10.0
12.1
15.0
20.0


proportions
HFO-1234yf
mass %
0.0
100.0
90.0
87.9
85.0
80.0



HFC-134a
mass %
100.0
0.0
0.0
0.0
0.0
0.0














GWP (AR4)

1430
4
5
5
5
5


COP ratio (relative to
%
105
100
100
100
100
100


that of R1234yf)









Refrigerating capacity
%
99
100
123
128
134
145


ratio (relative to









that of R1234yf)









Power consumption
%
100
100
100
100
100
100


of driving force









Heating power
%
95
100
100
33
33
33


consumption









Mileage (without
%
100
100
100
100
100
100


heating)









Mileage (with
%
50
50
50
84
84
84


heating)









Discharge temperature
° C.
66.0
48.0
54.8
56.0
57.5
59.8


Flame velocity
cm/s
0.0
1.5
1.5
1.5
1.5
1.5


Boiling point
° C.
−26.1
−29.5
−38.8
−40.0
−41.4
−43.3


Saturation pressure
kPaG
−50.1
−39
−4.4
0.9
7.5
17.2


at −40° C.









Heating method
System
Electric
Electric
Electric
Heat pump
Heat pump
Heat pump




heater
heater
heater
















Item
Example 5-4
Example 5-5
Example 5-6
Example 5-7
Example 5-8
Example 5-9

















Composition
HFO-1132(E)
25.0
30.0
35.0
40.0
45.0
50.0


proportions
HFO-1234yf
75.0
70.0
65.0
60.0
55.0
50.0



HFC-134a
0.0
0.0
0.0
0.0
0.0
0.0













GWP (AR4)
6
6
6
6
7
7


COP ratio (relative to
100
100
100
100
100
100


that of R1234yf)








Refrigerating capacity
155
165
175
185
194
203


ratio (relative to








that of R1234yf)








Power consumption
100
100
100
100
100
100


of driving force








Heating power
33
33
33
33
33
33


consumption








Mileage (without
100
100
100
100
100
100


heating)








Mileage (with
84
84
84
84
84
84


heating)








Discharge temperature
61.9
63.9
65.8
67.6
69.3
70.9


Flame velocity
1.5
1.5
2.0
2.6
3.4
4.3


Boiling point
−44.7
−45.9
−46.9
−47.7
−48.4
−49.1


Saturation pressure
25.3
32.3
38.4
43.9
48.8
53.4


at −40° C.








Heating method
Heat pump
Heat pump
Heat pump
Heat pump
Heat pump
Heat pump






















Comparative



Item
Example 5-10
Example 5-11
Example 5-12
Example 5-13
Example 5-3


















Composition
HFO-1132(E)
55.0
60.0
65.0
72.0
75.0



proportions
HFO-1234yf
45.0
40.0
35.0
28.0
25.0




HFC-134a
0.0
0.0
0.0
0.0
0.0














GWP (AR4)
7
8
8
8
9



COP ratio (relative to
100
100
100
100
100



that of R1234yf)








Refrigerating capacity
212
220
229
240
245



ratio (relative to








that of R1234yf)








Power consumption
100
100
100
100
100



of driving force








Heating power
33
33
33
33
33



consumption








Mileage (without
100
100
100
100
100



heating)








Mileage (with
84
84
84
84
84



heating)








Discharge temperature
72.6
74.2
75.9
78.2
79.2



Flame velocity
5.3
6.5
7.8
9.9
10.9



Boiling point
−49.6
−50.2
−50.5
−51.2
−51.4



Saturation pressure
57.5
61.4
65.0
69.6
71.5



at −40° C.








Heating method
Heat pump
Heat pump
Heat pump
Heat pump
Heat pump









(2) Refrigerating Oil

A refrigerating oil as technique of second group can improve the lubricity in the refrigeration cycle apparatus and can also achieve efficient cycle performance by performing a refrigeration cycle such as a refrigeration cycle together with a refrigerant composition.


Examples of the refrigerating oil include oxygen-containing synthetic oils (e.g., ester-type refrigerating oils and ether-type refrigerating oils) and hydrocarbon refrigerating oils. In particular, ester-type refrigerating oils and ether-type refrigerating oils are preferred from the viewpoint of miscibility with refrigerants or refrigerant compositions. The refrigerating oils may be used alone or in combination of two or more.


The kinematic viscosity of the refrigerating oil at 40° C. is preferably 1 mm2/s or more and 750 mm2/s or less and more preferably 1 mm2/s or more and 400 mm2/s or less from at least one of the viewpoints of suppressing the deterioration of the lubricity and the hermeticity of compressors, achieving sufficient miscibility with refrigerants under low-temperature conditions, suppressing the lubrication failure of compressors, and improving the heat exchange efficiency of evaporators. Herein, the kinematic viscosity of the refrigerating oil at 100° C. may be, for example, 1 mm2/s or more and 100 mm2/s or less and is more preferably 1 mm2/s or more and 50 mm 2/s or less.


The refrigerating oil preferably has an aniline point of −100° C. or higher and 0° C. or lower. The term “aniline point” herein refers to a numerical value indicating the solubility of, for example, a hydrocarbon solvent, that is, refers to a temperature at which when equal volumes of a sample (herein, refrigerating oil) and aniline are mixed with each other and cooled, turbidity appears because of their immiscibility (provided in JIS K 2256). Note that this value is a value of the refrigerating oil itself in a state in which the refrigerant is not dissolved. By using a refrigerating oil having such an aniline point, for example, even when bearings constituting resin functional components and insulating materials for electric motors are used at positions in contact with the refrigerating oil, the suitability of the refrigerating oil for the resin functional components can be improved. Specifically, if the aniline point is excessively low, the refrigerating oil readily infiltrates the bearings and the insulating materials, and thus the bearings and the like tend to swell. On the other hand, if the aniline point is excessively high, the refrigerating oil does not readily infiltrate the bearings and the insulating materials, and thus the bearings and the like tend to shrink. Accordingly, the deformation of the bearings and the insulating materials due to swelling or shrinking can be prevented by using the refrigerating oil having an aniline point within the above-described predetermined range (−100° C. or higher and 0° C. or lower). If the bearings deform through swelling, the desired length of a gap at a sliding portion cannot be maintained. This may result in an increase in sliding resistance. If the bearings deform through shrinking, the hardness of the bearings increases, and consequently the bearings may be broken because of vibration of a compressor. In other words, the deformation of the bearings through shrinking may decrease the rigidity of the sliding portion. Furthermore, if the insulating materials (e.g., insulating coating materials and insulating films) of electric motors deform through swelling, the insulating properties of the insulating materials deteriorate. If the insulating materials deform through shrinking, the insulating materials may also be broken as in the case of the bearings, which also deteriorates the insulating properties. In contrast, when the refrigerating oil having an aniline point within the predetermined range is used as described above, the deformation of bearings and insulating materials due to swelling or shrinking can be suppressed, and thus such a problem can be avoided.


The refrigerating oil is used as a working fluid for a refrigerating machine by being mixed with a refrigerant composition. The content of the refrigerating oil relative to the whole amount of working fluid for a refrigerating machine is preferably 5 mass % or more and 60 mass % or less and more preferably 10 mass % or more and 50 mass % or less.


(2-1) Oxygen-Containing Synthetic Oil

An ester-type refrigerating oil or an ether-type refrigerating oil serving as an oxygen-containing synthetic oil is mainly constituted by carbon atoms and oxygen atoms. In the ester-type refrigerating oil or the ether-type refrigerating oil, an excessively low ratio (carbon/oxygen molar ratio) of carbon atoms to oxygen atoms increases the hygroscopicity, and an excessively high ratio of carbon atoms to oxygen atoms deteriorates the miscibility with a refrigerant. Therefore, the molar ratio is preferably 2 or more and 7.5 or less.


(2-1-1) Ester-Type Refrigerating Oil

Examples of base oil components of the ester-type refrigerating oil include dibasic acid ester oils of a dibasic acid and a monohydric alcohol, polyol ester oils of a polyol and a fatty acid, complex ester oils of a polyol, a polybasic acid, and a monohydric alcohol (or a fatty acid), and polyol carbonate oils from the viewpoint of chemical stability.


(Dibasic Acid Ester Oil)

The dibasic acid ester oil is preferably an ester of a dibasic acid such as oxalic acid, malonic acid, succinic acid, glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, sebacic acid, phthalic acid, isophthalic acid, or terephthalic acid, in particular, a dibasic acid having 5 to 10 carbon atoms (e.g., glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, or sebacic acid) and a monohydric alcohol having a linear or branched alkyl group and having 1 to 15 carbon atoms (e.g., methanol, ethanol, propanol, butanol, pentanol, hexanol, heptanol, octanol, nonanol, decanol, undecanol, dodecanol, tridecanol, tetradecanol, or pentadecanol). Specific examples of the dibasic acid ester oil include ditridecyl glutarate, di(2-ethylhexyl) adipate, diisodecyl adipate, ditridecyl adipate, and di(3-ethylhexyl) sebacate.


(Polyol Ester Oil)

The polyol ester oil is an ester synthesized from a polyhydric alcohol and a fatty acid (carboxylic acid), and has a carbon/oxygen molar ratio of 2 or more and 7.5 or less, preferably 3.2 or more and 5.8 or less.


The polyhydric alcohol constituting the polyol ester oil is a diol (e.g., ethylene glycol, 1,3-propanediol, propylene glycol, 1,4-butanediol, 1,2-butanediol, 2-methyl-1,3-propanediol, 1,5-pentanediol, neopentyl glycol, 1,6-hexanediol, 2-ethyl-2-methyl-1,3-propanediol, 1,7-heptanediol, 2-methyl-2-propyl-1,3-propanediol, 2,2-diethyl-1,3-propanediol, 1,8-octanediol, 1,9-nonanediol, 1,10-decanediol, 1,11-undecanediol, or 1,12-dodecanediol) or a polyol having 3 to 20 hydroxyl groups (trimethylolethane, trimethylolpropane, trimethylolbutane, di-(trimethylolpropane), tri-(trimethylolpropane), pentaerythritol, di-(pentaerythritol), tri-(pentaerythritol), glycerol, polyglycerol (glycerol dimer or trimer), 1,3,5-pentanetriol, sorbitol, sorbitan, a sorbitol-glycerol condensate, a polyhydric alcohol such as adonitol, arabitol, xylitol, or mannitol, a saccharide such as xylose, arabinose, ribose, rhamnose, glucose, fructose, galactose, mannose, sorbose, cellobiose, maltose, isomaltose, trehalose, sucrose, raffinose, gentianose, or melezitose, or a partially etherified product of the foregoing). One or two or more polyhydric alcohols may constitute an ester.


For the fatty acid constituting the polyol ester, the number of carbon atoms is not limited, but is normally 1 to 24. A linear fatty acid or a branched fatty acid is preferred. Examples of the linear fatty acid include acetic acid, propionic acid, butanoic acid, pentanoic acid, hexanoic acid, heptanoic acid, octanoic acid, nonanoic acid, decanoic acid, undecanoic acid, dodecanoic acid, tridecanoic acid, tetradecanoic acid, pentadecanoic acid, hexadecanoic acid, heptadecanoic acid, octadecanoic acid, nonadecanoic acid, eicosanoic acid, oleic acid, linoleic acid, and linolenic acid. The hydrocarbon group that bonds to a carboxy group may have only a saturated hydrocarbon or may have an unsaturated hydrocarbon. Examples of the branched fatty acid include 2-methylpropionic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2-dimethylpropionic acid, 2-methylpentanoic acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, 2-methylhexanoic acid, 3-methylhexanoic acid, 4-methylhexanoic acid, 5-methylhexanoic acid, 2,2-dimethylpentanoic acid, 2,3-dimethylpentanoic acid, 2,4-dimethylpentanoic acid, 3,3-dimethylpentanoic acid, 3,4-dimethylpentanoic acid, 4,4-dimethylpentanoic acid, 2-ethylpentanoic acid, 3-ethylpentanoic acid, 2,2,3-trimethylbutanoic acid, 2,3,3-trimethylbutanoic acid, 2-ethyl-2-methylbutanoic acid, 2-ethyl-3-methylbutanoic acid, 2-methylheptanoic acid, 3-methylheptanoic acid, 4-methylheptanoic acid, 5-methylheptanoic acid, 6-methylheptanoic acid, 2-ethylhexanoic acid, 3-ethylhexanoic acid, 4-ethylhexanoic acid, 2,2-dimethylhexanoic acid, 2,3-dimethylhexanoic acid, 2,4-dimethylhexanoic acid, 2,5-dimethylhexanoic acid, 3,3-dimethylhexanoic acid, 3,4-dimethylhexanoic acid, 3,5-dimethylhexanoic acid, 4,4-dimethylhexanoic acid, 4,5-dimethylhexanoic acid, 5,5-dimethylhexanoic acid, 2-propylpentanoic acid, 2-methyloctanoic acid, 3-methyloctanoic acid, 4-methyloctanoic acid, 5-methyloctanoic acid, 6-methyloctanoic acid, 7-methyloctanoic acid, 2,2-dimethylheptanoic acid, 2,3-dimethylheptanoic acid, 2,4-dimethylheptanoic acid, 2,5-dimethylheptanoic acid, 2,6-dimethylheptanoic acid, 3,3-dimethylheptanoic acid, 3,4-dimethylheptanoic acid, 3,5-dimethylheptanoic acid, 3,6-dimethylheptanoic acid, 4,4-dimethylheptanoic acid, 4,5-dimethylheptanoic acid, 4,6-dimethylheptanoic acid, 5,5-dimethylheptanoic acid, 5,6-dimethylheptanoic acid, 6,6-dimethylheptanoic acid, 2-methyl-2-ethylhexanoic acid, 2-methyl-3-ethylhexanoic acid, 2-methyl-4-ethylhexanoic acid, 3-methyl-2-ethylhexanoic acid, 3-methyl-3-ethylhexanoic acid, 3-methyl-4-ethylhexanoic acid, 4-methyl-2-ethylhexanoic acid, 4-methyl-3-ethylhexanoic acid, 4-methyl-4-ethylhexanoic acid, 5-methyl-2-ethylhexanoic acid, 5-methyl-3-ethylhexanoic acid, 5-methyl-4-ethylhexanoic acid, 2-ethylheptanoic acid, 3-methyloctanoic acid, 3,5,5-trimethylhexanoic acid, 2-ethyl-2,3,3-trimethylbutyric acid, 2,2,4,4-tetramethylpentanoic acid, 2,2,3,3-tetramethylpentanoic acid, 2,2,3,4-tetramethylpentanoic acid, and 2,2-diisopropylpropanoic acid. One or two or more fatty acids selected from the foregoing may constitute an ester.


One polyhydric alcohol may be used to constitute an ester or a mixture of two or more polyhydric alcohols may be used to constitute an ester. The fatty acid constituting an ester may be a single component, or two or more fatty acids may constitute an ester. The fatty acids may be individual fatty acids of the same type or may be two or more types of fatty acids as a mixture. The polyol ester oil may have a free hydroxyl group.


Specifically, the polyol ester oil is more preferably an ester of a hindered alcohol such as neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, di-(trimethylolpropane), tri-(trimethylolpropane), pentaerythritol, di-(pentaerythritol), or tri-(pentaerythritol); further preferably an ester of neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, pentaerythritol, or di-(pentaerythritol); and preferably an ester of neopentyl glycol, trimethylolpropane, pentaerythritol, di-(pentaerythritol), or the like and a fatty acid having 2 to 20 carbon atoms.


The fatty acid constituting such a polyhydric alcohol fatty acid ester may be only a fatty acid having a linear alkyl group or may be selected from fatty acids having a branched structure. A mixed ester of linear and branched fatty acids may be employed. Furthermore, two or more fatty acids selected from the above fatty acids may be used to constitute an ester.


Specifically, for example, in the case of a mixed ester of linear and branched fatty acids, the molar ratio of a linear fatty acid having 4 to 6 carbon atoms and a branched fatty acid having 7 to 9 carbon atoms is 15:85 to 90:10, preferably 15:85 to 85:15, more preferably 20:80 to 80:20, further preferably 25:75 to 75:25, and most preferably 30:70 to 70:30. The total content of the linear fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester is preferably 20 mol % or more. The fatty acid preferably has such a composition that both of sufficient miscibility with a refrigerant and viscosity required as a refrigerating oil are achieved. The content of a fatty acid herein refers to a value relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester contained in the refrigerating oil.


In particular, the refrigerating oil preferably contains an ester (hereafter referred to as a “polyhydric alcohol fatty acid ester (A)”) in which the molar ratio of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms is 15:85 to 90:10, the fatty acid having 4 to 6 carbon atoms contains 2-methylpropionic acid, and the total content of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms relative to the whole amount of fatty acid constituting the above ester is 20 mol % or more.


The polyhydric alcohol fatty acid ester (A) includes a complete ester in which all hydroxyl groups of a polyhydric alcohol are esterified, a partial ester in which some hydroxyl groups of a polyhydric alcohol are left without being esterified, and a mixture of a complete ester and a partial ester. The hydroxyl value of the polyhydric alcohol fatty acid ester (A) is preferably 10 mgKOH/g or less, more preferably 5 mgKOH/g or less, and most preferably 3 mgKOH/g or less.


For the fatty acid constituting the polyhydric alcohol fatty acid ester (A), the molar ratio of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms is 15:85 to 90:10, preferably 15:85 to 85:15, more preferably 20:80 to 80:20, further preferably 25:75 to 75:25, and most preferably 30:70 to 70:30. The total content of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester (A) is 20 mol % or more. In the case where the above conditions for the composition of the fatty acid are not satisfied, if difluoromethane is contained in the refrigerant composition, both of sufficient miscibility with the difluoromethane and viscosity required as a refrigerating oil are not easily achieved at high levels. The content of a fatty acid refers to a value relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester contained in the refrigerating oil.


Specific examples of the fatty acid having 4 to 6 carbon atoms include butanoic acid, 2-methylpropionic acid, pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2-dimethylpropionic acid, 2-methylpentanoic acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, and hexanoic acid. Among them, a fatty acid having a branched structure at an alkyl skeleton, such as 2-methylpropionic acid, is preferred.


Specific examples of the branched fatty acid having 7 to 9 carbon atoms include 2-methylhexanoic acid, 3-methylhexanoic acid, 4-methylhexanoic acid, 5-methylhexanoic acid, 2,2-dimethylpentanoic acid, 2,3-dimethylpentanoic acid, 2,4-dimethylpentanoic acid, 3,3-dimethylpentanoic acid, 3,4-dimethylpentanoic acid, 4,4-dimethylpentanoic acid, 2-ethylpentanoic acid, 3-ethylpentanoic acid, 1,1,2-trimethylbutanoic acid, 1,2,2-trimethylbutanoic acid, 1-ethyl-1-methylbutanoic acid, 1-ethyl-2-methylbutanoic acid, octanoic acid, 2-ethylhexanoic acid, 3-ethylhexanoic acid, 3,5-dimethylhexanoic acid, 2,4-dimethylhexanoic acid, 3,4-dimethylhexanoic acid, 4,5-dimethylhexanoic acid, 2,2-dimethylhexanoic acid, 2-methylheptanoic acid, 3-methylheptanoic acid, 4-methylheptanoic acid, 5-methylheptanoic acid, 6-methylheptanoic acid, 2-propylpentanoic acid, nonanoic acid, 2,2-dimethylheptanoic acid, 2-methyloctanoic acid, 2-ethylheptanoic acid, 3-methyloctanoic acid, 3,5,5-trimethylhexanoic acid, 2-ethyl-2,3,3-trimethylbutyric acid, 2,2,4,4-tetramethylpentanoic acid, 2,2,3,3-tetramethylpentanoic acid, 2,2,3,4-tetramethylpentanoic acid, and 2,2-diisopropylpropanoic acid.


The polyhydric alcohol fatty acid ester (A) may contain, as an acid constituent component, a fatty acid other than the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms as long as the molar ratio of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms is 15:85 to 90:10 and the fatty acid having 4 to 6 carbon atoms contains 2-methylpropionic acid.


Specific examples of the fatty acid other than the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms include fatty acids having 2 or 3 carbon atoms, such as acetic acid and propionic acid; linear fatty acids having 7 to 9 carbon atoms, such as heptanoic acid, octanoic acid, and nonanoic acid; and fatty acids having 10 to 20 carbon atoms, such as decanoic acid, undecanoic acid, dodecanoic acid, tridecanoic acid, tetradecanoic acid, pentadecanoic acid, hexadecanoic acid, heptadecanoic acid, octadecanoic acid, nonadecanoic acid, eicosanoic acid, and oleic acid.


When the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms are used in combination with fatty acids other than these fatty acids, the total content of the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms relative to the whole amount of fatty acid constituting the polyhydric alcohol fatty acid ester (A) is preferably 20 mol % or more, more preferably 25 mol % or more, and further preferably 30 mol % or more. When the content is 20 mol % or more, sufficient miscibility with difluoromethane is achieved in the case where the difluoromethane is contained in the refrigerant composition.


A polyhydric alcohol fatty acid ester (A) containing, as acid constituent components, only 2-methylpropionic acid and 3,5,5-trimethylhexanoic acid is particularly preferred from the viewpoint of achieving both necessary viscosity and miscibility with difluoromethane in the case where the difluoromethane is contained in the refrigerant composition.


The polyhydric alcohol fatty acid ester may be a mixture of two or more esters having different molecular structures. In this case, individual molecules do not necessarily satisfy the above conditions as long as the whole fatty acid constituting a pentaerythritol fatty acid ester contained in the refrigerating oil satisfies the above conditions.


As described above, the polyhydric alcohol fatty acid ester (A) contains the fatty acid having 4 to 6 carbon atoms and the branched fatty acid having 7 to 9 carbon atoms as essential acid components constituting the ester and may optionally contain other fatty acids as constituent components. In other words, the polyhydric alcohol fatty acid ester (A) may contain only two fatty acids as acid constituent components or three or more fatty acids having different structures as acid constituent components, but the polyhydric alcohol fatty acid ester preferably contains, as an acid constituent component, only a fatty acid whose carbon atom (α-position carbon atom) adjacent to carbonyl carbon is not quaternary carbon. If the fatty acid constituting the polyhydric alcohol fatty acid ester contains a fatty acid whose α-position carbon atom is quaternary carbon, the lubricity in the presence of difluoromethane in the case where the difluoromethane is contained in the refrigerant composition tends to be insufficient.


The polyhydric alcohol constituting the polyol ester according to this embodiment is preferably a polyhydric alcohol having 2 to 6 hydroxyl groups.


Specific examples of the dihydric alcohol (diol) include ethylene glycol, 1,3-propanediol, propylene glycol, 1,4-butanediol, 1,2-butanediol, 2-methyl-1,3-propanediol, 1,5-pentanediol, neopentyl glycol, 1,6-hexanediol, 2-ethyl-2-methyl-1,3-propanediol, 1,7-heptanediol, 2-methyl-2-propyl-1,3-propanediol, 2,2-diethyl-1,3-propanediol, 1,8-octanediol, 1,9-nonanediol, 1,10-decanediol, 1,11-undecanediol, and 1,12-dodecanediol. Specific examples of the trihydric or higher alcohol include polyhydric alcohols such as trimethylolethane, trimethylolpropane, trimethylolbutane, di-(trimethylolpropane), tri-(trimethylolpropane), pentaerythritol, di-(pentaerythritol), tri-(pentaerythritol), glycerol, polyglycerol (glycerol dimer or trimer), 1,3,5-pentanetriol, sorbitol, sorbitan, sorbitol glycerol condensates, adonitol, arabitol, xylitol, and mannitol; saccharides such as xylose, arabinose, ribose, rhamnose, glucose, fructose, galactose, mannose, sorbose, and cellobiose; and partially etherified products of the foregoing. Among them, in terms of better hydrolysis stability, an ester of a hindered alcohol such as neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, di-(trimethylolpropane), tri-(trimethylolpropane), pentaerythritol, di-(pentaerythritol), or tri-(pentaerythritol) is preferably used; an ester of neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, pentaerythritol, or di-(pentaerythritol) is more preferably used; and neopentyl glycol, trimethylolpropane, pentaerythritol, or di-(pentaerythritol) is further preferably used. In terms of excellent miscibility with a refrigerant and excellent hydrolysis stability, a mixed ester of pentaerythritol, di-(pentaerythritol), or pentaerythritol and di-(pentaerythritol) is most preferably used.


Preferred examples of the acid constituent component constituting the polyhydric alcohol fatty acid ester (A) are as follows:

    • (i) a combination of 1 to 13 acids selected from butanoic acid, 2-methylpropionic acid, pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2-dimethylpropionic acid, 2-methylpentanoic acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, and hexanoic acid and 1 to 13 acids selected from 2-methylhexanoic acid, 3-methylhexanoic acid, 4-methylhexanoic acid, 5-methylhexanoic acid, 2,2-dimethylpentanoic acid, 2,3-dimethylpentanoic acid, 2,4-dimethylpentanoic acid, 3,3-dimethylpentanoic acid, 3,4-dimethylpentanoic acid, 4,4-dimethylpentanoic acid, 2-ethylpentanoic acid, 3-ethylpentanoic acid, and 2-ethyl-3-methylbutanoic acid;
    • (ii) a combination of 1 to 13 acids selected from butanoic acid, 2-methylpropionic acid, pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2-dimethylpropionic acid, 2-methylpentanoic acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, and hexanoic acid and 1 to 25 acids selected from 2-methylheptanoic acid, 3-methylheptanoic acid, 4-methylheptanoic acid, 5-methylheptanoic acid, 6-methylheptanoic acid, 2,2-dimethylhexanoic acid, 3,3-dimethylhexanoic acid, 4,4-dimethylhexanoic acid, 5,5-dimethylhexanoic acid, 2,3-dimethylhexanoic acid, 2,4-dimethylhexanoic acid, 2,5-dimethylhexanoic acid, 3,4-dimethylhexanoic acid, 3,5-dimethylhexanoic acid, 4,5-dimethylhexanoic acid, 2,2,3-trimethylpentanoic acid, 2,3,3-trimethylpentanoic acid, 2,4,4-trimethylpentanoic acid, 3,4,4-trimethylpentanoic acid, 2-ethylhexanoic acid, 3-ethylhexanoic acid, 2-propylpentanoic acid, 2-methyl-2-ethylpentanoic acid, 2-methyl-3-ethylpentanoic acid, and 3-methyl-3-ethylpentanoic acid; and
    • (iii) a combination of 1 to 13 acids selected from butanoic acid, 2-methylpropionic acid, pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, 2,2-dimethylpropionic acid, 2-methylpentanoic acid, 3-methylpentanoic acid, 4-methylpentanoic acid, 2,2-dimethylbutanoic acid, 2,3-dimethylbutanoic acid, 3,3-dimethylbutanoic acid, and hexanoic acid and 1 to 50 acids selected from 2-methyloctanoic acid, 3-methyloctanoic acid, 4-methyloctanoic acid, 5-methyloctanoic acid, 6-methyloctanoic acid, 7-methyloctanoic acid, 8-methyloctanoic acid, 2,2-dimethylheptanoic acid, 3,3-dimethylheptanoic acid, 4,4-dimethylheptanoic acid, 5,5-dimethylheptanoic acid, 6,6-dimethylheptanoic acid, 2,3-dimethylheptanoic acid, 2,4-dimethylheptanoic acid, 2,5-dimethylheptanoic acid, 2,6-dimethylheptanoic acid, 3,4-dimethylheptanoic acid, 3,5-dimethylheptanoic acid, 3,6-dimethylheptanoic acid, 4,5-dimethylheptanoic acid, 4,6-dimethylheptanoic acid, 2-ethylheptanoic acid, 3-ethylheptanoic acid, 4-ethylheptanoic acid, 5-ethylheptanoic acid, 2-propylhexanoic acid, 3-propylhexanoic acid, 2-butylpentanoic acid, 2,2,3-trimethylhexanoic acid, 2,2,3-trimethylhexanoic acid, 2,2,4-trimethylhexanoic acid, 2,2,5-trimethylhexanoic acid, 2,3,4-trimethylhexanoic acid, 2,3,5-trimethylhexanoic acid, 3,3,4-trimethylhexanoic acid, 3,3,5-trimethylhexanoic acid, 3,5,5-trimethylhexanoic acid, 4,4,5-trimethylhexanoic acid, 4,5,5-trimethylhexanoic acid, 2,2,3,3-tetramethylpentanoic acid, 2,2,3,4-tetramethylpentanoic acid, 2,2,4,4-tetramethylpentanoic acid, 2,3,4,4-tetramethylpentanoic acid, 3,3,4,4-tetramethylpentanoic acid, 2,2-diethylpentanoic acid, 2,3-diethylpentanoic acid, 3,3-diethylpentanoic acid, 2-ethyl-2,3,3-trimethylbutyric acid, 3-ethyl-2,2,3-trimethylbutyric acid, and 2,2-diisopropylpropionic acid.


Further preferred examples of the acid constituent component constituting the polyhydric alcohol fatty acid ester are as follows:

    • (i) a combination of 2-methylpropionic acid and 1 to 13 acids selected from 2-methylhexanoic acid, 3-methylhexanoic acid, 4-methylhexanoic acid, 5-methylhexanoic acid, 2,2-dimethylpentanoic acid, 2,3-dimethylpentanoic acid, 2,4-dimethylpentanoic acid, 3,3-dimethylpentanoic acid, 3,4-dimethylpentanoic acid, 4,4-dimethylpentanoic acid, 2-ethylpentanoic acid, 3-ethylpentanoic acid, and 2-ethyl-3-methylbutanoic acid;
    • (ii) a combination of 2-methylpropionic acid and 1 to 25 acids selected from 2-methylheptanoic acid, 3-methylheptanoic acid, 4-methylheptanoic acid, 5-methylheptanoic acid, 6-methylheptanoic acid, 2,2-dimethylhexanoic acid, 3,3-dimethylhexanoic acid, 4,4-dimethylhexanoic acid, 5,5-dimethylhexanoic acid, 2,3-dimethylhexanoic acid, 2,4-dimethylhexanoic acid, 2,5-dimethylhexanoic acid, 3,4-dimethylhexanoic acid, 3,5-dimethylhexanoic acid, 4,5-dimethylhexanoic acid, 2,2,3-trimethylpentanoic acid, 2,3,3-trimethylpentanoic acid, 2,4,4-trimethylpentanoic acid, 3,4,4-trimethylpentanoic acid, 2-ethylhexanoic acid, 3-ethylhexanoic acid, 2-propylpentanoic acid, 2-methyl-2-ethylpentanoic acid, 2-methyl-3-ethylpentanoic acid, and 3-methyl-3-ethylpentanoic acid; and
    • (iii) a combination of 2-methylpropionic acid and 1 to 50 acids selected from 2-methyloctanoic acid, 3-methyloctanoic acid, 4-methyloctanoic acid, 5-methyloctanoic acid, 6-methyloctanoic acid, 7-methyloctanoic acid, 8-methyloctanoic acid, 2,2-dimethylheptanoic acid, 3,3-dimethylheptanoic acid, 4,4-dimethylheptanoic acid, 5,5-dimethylheptanoic acid, 6,6-dimethylheptanoic acid, 2,3-dimethylheptanoic acid, 2,4-dimethylheptanoic acid, 2,5-dimethylheptanoic acid, 2,6-dimethylheptanoic acid, 3,4-dimethylheptanoic acid, 3,5-dimethylheptanoic acid, 3,6-dimethylheptanoic acid, 4,5-dimethylheptanoic acid, 4,6-dimethylheptanoic acid, 2-ethylheptanoic acid, 3-ethylheptanoic acid, 4-ethylheptanoic acid, 5-ethylheptanoic acid, 2-propylhexanoic acid, 3-propylhexanoic acid, 2-butylpentanoic acid, 2,2,3-trimethylhexanoic acid, 2,2,3-trimethylhexanoic acid, 2,2,4-trimethylhexanoic acid, 2,2,5-trimethylhexanoic acid, 2,3,4-trimethylhexanoic acid, 2,3,5-trimethylhexanoic acid, 3,3,4-trimethylhexanoic acid, 3,3,5-trimethylhexanoic acid, 3,5,5-trimethylhexanoic acid, 4,4,5-trimethylhexanoic acid, 4,5,5-trimethylhexanoic acid, 2,2,3,3-tetramethylpentanoic acid, 2,2,3,4-tetramethylpentanoic acid, 2,2,4,4-tetramethylpentanoic acid, 2,3,4,4-tetramethylpentanoic acid, 3,3,4,4-tetramethylpentanoic acid, 2,2-diethylpentanoic acid, 2,3-diethylpentanoic acid, 3,3-diethylpentanoic acid, 2-ethyl-2,3,3-trimethylbutyric acid, 3-ethyl-2,2,3-trimethylbutyric acid, and 2,2-diisopropylpropionic acid.


The content of the polyhydric alcohol fatty acid ester (A) is 50 mass % or more, preferably 60 mass % or more, more preferably 70 mass % or more, and further preferably 75 mass % or more relative to the whole amount of the refrigerating oil. The refrigerating oil according to this embodiment may contain a lubricating base oil other than the polyhydric alcohol fatty acid ester (A) and additives as described later. However, if the content of the polyhydric alcohol fatty acid ester (A) is less than 50 mass %, necessary viscosity and miscibility cannot be achieved at high levels.


In the refrigerating oil according to this embodiment, the polyhydric alcohol fatty acid ester (A) is mainly used as a base oil. The base oil of the refrigerating oil according to this embodiment may be a polyhydric alcohol fatty acid ester (A) alone (i.e., the content of the polyhydric alcohol fatty acid ester (A) is 100 mass %). However, in addition to the polyhydric alcohol fatty acid ester (A), a base oil other than the polyhydric alcohol fatty acid ester (A) may be further contained to the degree that the excellent performance of the polyhydric alcohol fatty acid ester (A) is not impaired. Examples of the base oil other than the polyhydric alcohol fatty acid ester (A) include hydrocarbon oils such as mineral oils, olefin polymers, alkyldiphenylalkanes, alkylnaphthalenes, and alkylbenzenes; and esters other than the polyhydric alcohol fatty acid ester (A), such as polyol esters, complex esters, and alicyclic dicarboxylic acid esters, and oxygen-containing synthetic oils (hereafter, may be referred to as “other oxygen-containing synthetic oils”) such as polyglycols, polyvinyl ethers, ketones, polyphenyl ethers, silicones, polysiloxanes, and perfluoroethers.


Among them, the oxygen-containing synthetic oil is preferably an ester other than the polyhydric alcohol fatty acid ester (A), a polyglycol, or a polyvinyl ether and particularly preferably a polyol ester other than the polyhydric alcohol fatty acid ester (A). The polyol ester other than the polyhydric alcohol fatty acid ester (A) is an ester of a fatty acid and a polyhydric alcohol such as neopentyl glycol, trimethylolethane, trimethylolpropane, trimethylolbutane, pentaerythritol, or dipentaerythritol and is particularly preferably an ester of neopentyl glycol and a fatty acid, an ester of pentaerythritol and a fatty acid, or an ester of dipentaerythritol and a fatty acid.


The neopentyl glycol ester is preferably an ester of neopentyl glycol and a fatty acid having 5 to 9 carbon atoms. Specific examples of the neopentyl glycol ester include neopentyl glycol di(3,5,5-trimethylhexanoate), neopentyl glycol di(2-ethylhexanoate), neopentyl glycol di(2-methylhexanoate), neopentyl glycol di(2-ethylpentanoate), an ester of neopentyl glycol and 2-methylhexanoic acid-2-ethylpentanoic acid, an ester of neopentyl glycol and 3-methylhexanoic acid-5-methylhexanoic acid, an ester of neopentyl glycol and 2-methylhexanoic acid-2-ethylhexanoic acid, an ester of neopentyl glycol and 3,5-dimethylhexanoic acid-4,5-dimethylhexanoic acid-3,4-dimethylhexanoic acid, neopentyl glycol dipentanoate, neopentyl glycol di(2-ethylbutanoate), neopentyl glycol di(2-methylpentanoate), neopentyl glycol di(2-methylbutanoate), and neopentyl glycol di(3-methylbutanoate).


The pentaerythritol ester is preferably an ester of pentaerythritol and a fatty acid having 5 to 9 carbon atoms. The pentaerythritol ester is, specifically, an ester of pentaerythritol and at least one fatty acid selected from pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, hexanoic acid, 2-methylpentanoic acid, 2-ethylbutanoic acid, 2-ethylpentanoic acid, 2-methylhexanoic acid, 3,5,5-trimethylhexanoic acid, and 2-ethylhexanoic acid.


The dipentaerythritol ester is preferably an ester of dipentaerythritol and a fatty acid having 5 to 9 carbon atoms. The dipentaerythritol ester is, specifically, an ester of dipentaerythritol and at least one fatty acid selected from pentanoic acid, 2-methylbutanoic acid, 3-methylbutanoic acid, hexanoic acid, 2-methylpentanoic acid, 2-ethylbutanoic acid, 2-ethylpentanoic acid, 2-methylhexanoic acid, 3,5,5-trimethylhexanoic acid, and 2-ethylhexanoic acid.


When the refrigerating oil according to this embodiment contains an oxygen-containing synthetic oil other than the polyhydric alcohol fatty acid ester (A), the content of the oxygen-containing synthetic oil other than the polyhydric alcohol fatty acid ester (A) is not limited as long as excellent lubricity and miscibility of the refrigerating oil according to this embodiment are not impaired. When a polyol ester other than the polyhydric alcohol fatty acid ester (A) is contained, the content of the polyol ester is preferably less than 50 mass %, more preferably 45 mass % or less, still more preferably 40 mass % or less, even more preferably 35 mass % or less, further preferably 30 mass % or less, and most preferably 25 mass % or less relative to the whole amount of the refrigerating oil. When an oxygen-containing synthetic oil other than the polyol ester is contained, the content of the oxygen-containing synthetic oil is preferably less than 50 mass %, more preferably 40 mass % or less, and further preferably 30 mass % or less relative to the whole amount of the refrigerating oil. If the content of the polyol ester other than the pentaerythritol fatty acid ester or the oxygen-containing synthetic oil is excessively high, the above-described effects are not sufficiently produced.


The polyol ester other than the polyhydric alcohol fatty acid ester (A) may be a partial ester in which some hydroxyl groups of a polyhydric alcohol are left without being esterified, a complete ester in which all hydroxyl groups are esterified, or a mixture of a partial ester and a complete ester. The hydroxyl value is preferably 10 mgKOH/g or less, more preferably 5 mgKOH/g or less, and most preferably 3 mgKOH/g or less.


When the refrigerating oil and the working fluid for a refrigerating machine according to this embodiment contain a polyol ester other than the polyhydric alcohol fatty acid ester (A), the polyol ester may contain one polyol ester having a single structure or a mixture of two or more polyol esters having different structures.


The polyol ester other than the polyhydric alcohol fatty acid ester (A) may be any of an ester of one fatty acid and one polyhydric alcohol, an ester of two or more fatty acids and one polyhydric alcohol, an ester of one fatty acid and two or more polyhydric alcohols, and an ester of two or more fatty acids and two or more polyhydric alcohols.


The refrigerating oil according to this embodiment may be constituted by only the polyhydric alcohol fatty acid ester (A) or by the polyhydric alcohol fatty acid ester (A) and other base oils. The refrigerating oil may further contain various additives described later. The working fluid for a refrigerating machine according to this embodiment may also further contain various additives. In the following description, the content of additives is expressed relative to the whole amount of the refrigerating oil, but the content of these components in the working fluid for a refrigerating machine is desirably determined so that the content is within the preferred range described later when expressed relative to the whole amount of the refrigerating oil.


To further improve the abrasion resistance and load resistance of the refrigerating oil and the working fluid for a refrigerating machine according to this embodiment, at least one phosphorus compound selected from the group consisting of phosphoric acid esters, acidic phosphoric acid esters, thiophosphoric acid esters, amine salts of acidic phosphoric acid esters, chlorinated phosphoric acid esters, and phosphorous acid esters can be added. These phosphorus compounds are esters of phosphoric acid or phosphorous acid and alkanol or polyether-type alcohol, or derivatives thereof.


Specific examples of the phosphoric acid ester include tributyl phosphate, tripentyl phosphate, trihexyl phosphate, triheptyl phosphate, trioctyl phosphate, trinonyl phosphate, tridecyl phosphate, triundecyl phosphate, tridodecyl phosphate, tritridecyl phosphate, tritetradecyl phosphate, tripentadecyl phosphate, trihexadecyl phosphate, triheptadecyl phosphate, trioctadecyl phosphate, trioleyl phosphate, triphenyl phosphate, tricresyl phosphate, trixylenyl phosphate, cresyldiphenyl phosphate, and xylenyldiphenyl phosphate.


Examples of the acidic phosphoric acid ester include monobutyl acid phosphate, monopentyl acid phosphate, monohexyl acid phosphate, monoheptyl acid phosphate, monooctyl acid phosphate, monononyl acid phosphate, monodecyl acid phosphate, monoundecyl acid phosphate, monododecyl acid phosphate, monotridecyl acid phosphate, monotetradecyl acid phosphate, monopentadecyl acid phosphate, monohexadecyl acid phosphate, monoheptadecyl acid phosphate, monooctadecyl acid phosphate, monooleyl acid phosphate, dibutyl acid phosphate, dipentyl acid phosphate, dihexyl acid phosphate, diheptyl acid phosphate, dioctyl acid phosphate, dinonyl acid phosphate, didecyl acid phosphate, diundecyl acid phosphate, didodecyl acid phosphate, ditridecyl acid phosphate, ditetradecyl acid phosphate, dipentadecyl acid phosphate, dihexadecyl acid phosphate, diheptadecyl acid phosphate, dioctadecyl acid phosphate, and dioleyl acid phosphate.


Examples of the thiophosphoric acid ester include tributyl phosphorothionate, tripentyl phosphorothionate, trihexyl phosphorothionate, triheptyl phosphorothionate, trioctyl phosphorothionate, trinonyl phosphorothionate, tridecyl phosphorothionate, triundecyl phosphorothionate, tridodecyl phosphorothionate, tritridecyl phosphorothionate, tritetradecyl phosphorothionate, tripentadecyl phosphorothionate, trihexadecyl phosphorothionate, triheptadecyl phosphorothionate, trioctadecyl phosphorothionate, trioleyl phosphorothionate, triphenyl phosphorothionate, tricresyl phosphorothionate, trixylenyl phosphorothionate, cresyldiphenyl phosphorothionate, and xylenyldiphenyl phosphorothionate.


The amine salt of an acidic phosphoric acid ester is an amine salt of an acidic phosphoric acid ester and a primary, secondary, or tertiary amine that has a linear or branched alkyl group and that has 1 to 24 carbon atoms, preferably 5 to 18 carbon atoms.


For the amine constituting the amine salt of an acidic phosphoric acid ester, the amine salt is a salt of an amine such as a linear or branched methylamine, ethylamine, propylamine, butylamine, pentylamine, hexylamine, heptylamine, octylamine, nonylamine, decylamine, undecylamine, dodecylamine, tridecylamine, tetradecylamine, pentadecylamine, hexadecylamine, heptadecylamine, octadecylamine, oleylamine, tetracosylamine, dimethylamine, diethylamine, dipropylamine, dibutylamine, dipentylamine, dihexylamine, diheptylamine, dioctylamine, dinonylamine, didecylamine, diundecylamine, didodecylamine, ditridecylamine, ditetradecylamine, dipentadecylamine, dihexadecylamine, diheptadecylamine, dioctadecylamine, dioleylamine, ditetracosylamine, trimethylamine, triethylamine, tripropylamine, tributylamine, tripentylamine, trihexylamine, triheptylamine, trioctylamine, trinonylamine, tridecylamine, triundecylamine, tridodecylamine, tritridecylamine, tritetradecylamine, tripentadecylamine, trihexadecylamine, triheptadecylamine, trioctadecylamine, trioleylamine, or tritetracosylamine. The amine may be a single compound or a mixture of two or more compounds.


Examples of the chlorinated phosphoric acid ester include tris(dichloropropyl) phosphate, tris(chloroethyl) phosphate, tris(chlorophenyl) phosphate, and polyoxyalkylene-bis[di(chloroaklyl)] phosphate. Examples of the phosphorous acid ester include dibutyl phosphite, dipentyl phosphite, dihexyl phosphite, diheptyl phosphite, dioctyl phosphite, dinonyl phosphite, didecyl phosphite, diundecyl phosphite, didodecyl phosphite, dioleyl phosphite, diphenyl phosphite, dicresyl phosphite, tributyl phosphite, tripentyl phosphite, trihexyl phosphite, triheptyl phosphite, trioctyl phosphite, trinonyl phosphite, tridecyl phosphite, triundecyl phosphite, tridodecyl phosphite, trioleyl phosphite, triphenyl phosphite, and tricresyl phosphite. Mixtures of these compounds can also be used.


When the refrigerating oil and the working fluid for a refrigerating machine according to this embodiment contain the above-described phosphorus compound, the content of the phosphorus compound is not limited, but is preferably 0.01 to 5.0 mass % and more preferably 0.02 to 3.0 mass % relative to the whole amount of the refrigerating oil (relative to the total amount of the base oil and all the additives). The above-described phosphorus compounds may be used alone or in combination of two or more.


The refrigerating oil and the working fluid for a refrigerating machine according to this embodiment may contain a terpene compound to further improve the thermal and chemical stability. The “terpene compound” in the present invention refers to a compound obtained by polymerizing isoprene and a derivative thereof, and a dimer to an octamer of isoprene are preferably used. Specific examples of the terpene compound include monoterpenes such as geraniol, nerol, linalool, citral (including geranial), citronellol, menthol, limonene, terpinerol, carvone, ionone, thujone, camphor, and borneol; sesquiterpenes such as farnesene, farnesol, nerolidol, juvenile hormone, humulene, caryophyllene, elemene, cadinol, cadinene, and tutin; diterpenes such as geranylgeraniol, phytol, abietic acid, pimaragen, daphnetoxin, taxol, and pimaric acid; sesterterpenes such as geranylfarnesene; triterpenes such as squalene, limonin, camelliagenin, hopane, and lanosterol; and tetraterpenes such as carotenoid.


Among these terpene compounds, the terpene compound is preferably monoterpene, sesquiterpene, or diterpene, more preferably sesquiterpene, and particularly preferably α-farnesene (3,7,11-trimethyldodeca-1,3,6,10-tetraene) and/or β-farnesene (7,11-dimethyl-3-methylidenedodeca-1,6,10-triene). In the present invention, the terpene compounds may be used alone or in combination of two or more.


The content of the terpene compound in the refrigerating oil according to this embodiment is not limited, but is preferably 0.001 to 10 mass %, more preferably 0.01 to 5 mass %, and further preferably 0.05 to 3 mass % relative to the whole amount of the refrigerating oil. If the content of the terpene compound is less than 0.001 mass %, an effect of improving the thermal and chemical stability tends to be insufficient. If the content is more than 10 mass %, the lubricity tends to be insufficient. The content of the terpene compound in the working fluid for a refrigerating machine according to this embodiment is desirably determined so that the content is within the above preferred range when expressed relative to the whole amount of the refrigerating oil.


The refrigerating oil and the working fluid for a refrigerating machine according to this embodiment may contain at least one epoxy compound selected from phenyl glycidyl ether-type epoxy compounds, alkyl glycidyl ether-type epoxy compounds, glycidyl ester-type epoxy compounds, allyloxirane compounds, alkyloxirane compounds, alicyclic epoxy compounds, epoxidized fatty acid monoesters, and epoxidized vegetable oils to further improve the thermal and chemical stability.


Specific examples of the phenyl glycidyl ether-type epoxy compound include phenyl glycidyl ether and alkylphenyl glycidyl ethers. The alkylphenyl glycidyl ether herein is an alkylphenyl glycidyl ether having 1 to 3 alkyl groups with 1 to 13 carbon atoms. In particular, the alkylphenyl glycidyl ether is preferably an alkylphenyl glycidyl ether having one alkyl group with 4 to 10 carbon atoms, such as n-butylphenyl glycidyl ether, i-butylphenyl glycidyl ether, sec-butylphenyl glycidyl ether, tert-butylphenyl glycidyl ether, pentylphenyl glycidyl ether, hexylphenyl glycidyl ether, heptylphenyl glycidyl ether, octylphenyl glycidyl ether, nonylphenyl glycidyl ether, or decylphenyl glycidyl ether.


Specific examples of the alkyl glycidyl ether-type epoxy compound include decyl glycidyl ether, undecyl glycidyl ether, dodecyl glycidyl ether, tridecyl glycidyl ether, tetradecyl glycidyl ether, 2-ethylhexyl glycidyl ether, neopentyl glycol diglycidyl ether, trimethylolpropane triglycidyl ether, pentaerythritol tetraglycidyl ether, 1,6-hexanediol diglycidyl ether, sorbitol polyglycidyl ether, polyalkylene glycol monoglycidyl ether, and polyalkylene glycol diglycidyl ether.


Specific examples of the glycidyl ester-type epoxy compound include phenyl glycidyl ester, alkyl glycidyl esters, and alkenyl glycidyl esters. Preferred examples of the glycidyl ester-type epoxy compound include glycidyl-2,2-dimethyloctanoate, glycidyl benzoate, glycidyl acrylate, and glycidyl methacrylate.


Specific examples of the allyloxirane compound include 1,2-epoxystyrene and alkyl-1,2-epoxystyrenes.


Specific examples of the alkyloxirane compound include 1,2-epoxybutane, 1,2-epoxypentane, 1,2-epoxyhexane, 1,2-epoxyheptane, 1,2-epoxyoctane, 1,2-epoxynonane, 1,2-epoxydecane, 1,2-epoxyundecane, 1,2-epoxydodecane, 1,2-epoxytridecane, 1,2-epoxytetradecane, 1,2-epoxypentadecane, 1,2-epoxyhexadecane, 1,2-epoxyheptadecane, 1,1,2-epoxyoctadecane, 2-epoxynonadecane, and 1,2-epoxyeicosane.


Specific examples of the alicyclic epoxy compound include 1,2-epoxycyclohexane, 1,2-epoxycyclopentane, 3,4-epoxycyclohexylmethyl-3,4-epoxycyclohexane carboxylate, bis(3,4-epoxycyclohexylmethyl) adipate, exo-2,3-epoxynorbornane, bis(3,4-epoxy-6-methylcyclohexylmethyl) adipate, 2-(7-oxabicyclo[4.1.0]hept-3-yl)-spiro(1,3-dioxane-5,3′-[7]oxabicyclo[4.1.0]heptane, 4-(1′-methylepoxyethyl)-1,2-epoxy-2-methylcyclohexane, and 4-epoxyethyl-1,2-epoxycyclohexane.


Specific examples of the epoxidized fatty acid monoester include esters of an epoxidized fatty acid having 12 to 20 carbon atoms and an alcohol having 1 to 8 carbon atoms, phenol, or an alkylphenol. In particular, butyl, hexyl, benzyl, cyclohexyl, methoxyethyl, octyl, phenyl, and butyl phenyl esters of epoxystearic acid are preferably used.


Specific examples of the epoxidized vegetable oil include epoxy compounds of vegetable oils such as soybean oil, linseed oil, and cottonseed oil.


Among these epoxy compounds, phenyl glycidyl ether-type epoxy compounds, alkyl glycidyl ether-type epoxy compounds, glycidyl ester-type epoxy compounds, and alicyclic epoxy compounds are preferred.


When the refrigerating oil and the working fluid for a refrigerating machine according to this embodiment contain the above-described epoxy compound, the content of the epoxy compound is not limited, but is preferably 0.01 to 5.0 mass % and more preferably 0.1 to 3.0 mass % relative to the whole amount of the refrigerating oil. The above-described epoxy compounds may be used alone or in combination of two or more.


The kinematic viscosity of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) at 40° C. is preferably 20 to 80 mm2/s, more preferably 25 to 75 mm2/s, and most preferably 30 to 70 mm2/s. The kinematic viscosity at 100° C. is preferably 2 to 20 mm2/s and more preferably 3 to 10 mm2/s. When the kinematic viscosity is more than or equal to the lower limit, the viscosity required as a refrigerating oil is easily achieved. On the other hand, when the kinematic viscosity is less than or equal to the upper limit, sufficient miscibility with difluoromethane in the case where the difluoromethane is contained as a refrigerant composition can be achieved.


The volume resistivity of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) is not limited, but is preferably 1.0×1012 Ω·cm or more, more preferably 1.0×1013 Ω·cm or more, and most preferably 1.0×1014 Ω·cm or more. In particular, when the refrigerating oil is used for sealed refrigerating machines, high electric insulation tends to be required. The volume resistivity refers to a value measured at 25° C. in conformity with JIS C 2101 “Testing methods of electrical insulating oils”.


The water content of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) is not limited, but is preferably 200 ppm or less, more preferably 100 ppm or less, and most preferably 50 ppm or less relative to the whole amount of the refrigerating oil. In particular, when the refrigerating oil is used for sealed refrigerating machines, the water content needs to be low from the viewpoints of the thermal and chemical stability of the refrigerating oil and the influence on electric insulation.


The acid number of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) is not limited, but is preferably 0.1 mgKOH/g or less and more preferably 0.05 mgKOH/g or less to prevent corrosion of metals used for refrigerating machines or pipes. In the present invention, the acid number refers to an acid number measured in conformity with JIS K 2501 “Petroleum products and lubricants—Determination of neutralization number”.


The ash content of the refrigerating oil containing the polyhydric alcohol fatty acid ester (A) is not limited, but is preferably 100 ppm or less and more preferably 50 ppm or less to improve the thermal and chemical stability of the refrigerating oil and suppress the generation of sludge and the like. The ash content refers to an ash content measured in conformity with JIS K 2272 “Crude oil and petroleum products—Determination of ash and sulfated ash”.


(Complex Ester Oil)

The complex ester oil is an ester of a fatty acid and a dibasic acid, and a monohydric alcohol and a polyol. The above-described fatty acid, dibasic acid, monohydric alcohol, and polyol can be used.


Examples of the fatty acid include the fatty acids mentioned in the polyol ester.


Examples of the dibasic acid include oxalic acid, malonic acid, succinic acid, glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, sebacic acid, phthalic acid, isophthalic acid, and terephthalic acid.


Examples of the polyol include the polyhydric alcohols in the polyol ester. The complex ester is an ester of such a fatty acid, dibasic acid, and polyol, each of which may be constituted by a single component or a plurality of components.


(Polyol Carbonate Oil)

The polyol carbonate oil is an ester of a carbonic acid and a polyol.


Examples of the polyol include the above-described diols and polyols.


The polyol carbonate oil may be a ring-opened polymer of a cyclic alkylene carbonate.


(2-1-2) Ether-Type Refrigerating Oil

The ether-type refrigerating oil is, for example, a polyvinyl ether oil or a polyoxyalkylene oil.


(Polyvinyl Ether Oil)

Examples of the polyvinyl ether oil include polymers of a vinyl ether monomer, copolymers of a vinyl ether monomer and a hydrocarbon monomer having an olefinic double bond, and copolymers of a monomer having an olefinic double bond and a polyoxyalkylene chain and a vinyl ether monomer.


The carbon/oxygen molar ratio of the polyvinyl ether oil is preferably 2 or more and 7.5 or less and more preferably 2.5 or more and 5.8 or less. If the carbon/oxygen molar ratio is smaller than the above range, the hygroscopicity increases. If the carbon/oxygen molar ratio is larger than the above range, the miscibility deteriorates. The weight-average molecular weight of the polyvinyl ether is preferably 200 or more and 3000 or less and more preferably 500 or more and 1500 or less.


The pour point of the polyvinyl ether oil is preferably −30° C. or lower. The surface tension of the polyvinyl ether oil at 20° C. is preferably 0.02 N/m or more and 0.04 N/m or less. The density of the polyvinyl ether oil at 15° C. is preferably 0.8 g/cm3 or more and 1.8 g/cm3 or less. The saturated water content of the polyvinyl ether oil at a temperature of 30° C. and a relative humidity of 90% is preferably 2000 ppm or more.


The refrigerating oil may contain polyvinyl ether as a main component. In the case where HFO-1234yf is contained as a refrigerant, the polyvinyl ether serving as a main component of the refrigerating oil has miscibility with HFO-1234yf. When the refrigerating oil has a kinematic viscosity at 40° C. of 400 mm2/s or less, HFO-1234yf is dissolved in the refrigerating oil to some extent. When the refrigerating oil has a pour point of −30° C. or lower, the flowability of the refrigerating oil is easily ensured even at positions at which the temperature of the refrigerant composition and the refrigerating oil is low in the refrigerant circuit. When the refrigerating oil has a surface tension at 20° C. of 0.04 N/m or less, the refrigerating oil discharged from a compressor does not readily form large droplets of oil that are not easily carried away by a refrigerant composition. Therefore, the refrigerating oil discharged from the compressor is dissolved in HFO-1234yf and is easily returned to the compressor together with HFO-1234yf.


When the refrigerating oil has a kinematic viscosity at 40° C. of 30 mm2/s or more, an insufficient oil film strength due to excessively low kinematic viscosity is suppressed, and thus good lubricity is easily achieved. When the refrigerating oil has a surface tension at 20° C. of 0.02 N/m or more, the refrigerating oil does not readily form small droplets of oil in a gas refrigerant inside the compressor, which can suppress discharge of a large amount of refrigerating oil from the compressor. Therefore, a sufficient amount of refrigerating oil is easily stored in the compressor.


When the refrigerating oil has a saturated water content at 30° C./90% RH of 2000 ppm or more, a relatively high hygroscopicity of the refrigerating oil can be achieved. Thus, when HFO-1234yf is contained as a refrigerant, water in HFO-1234yf can be captured by the refrigerating oil to some extent. HFO-1234yf has a molecular structure that is easily altered or deteriorated because of the influence of water contained. Therefore, the hydroscopic effects of the refrigerating oil can suppress such deterioration.


Furthermore, when a particular resin functional component is disposed in the sealing portion or sliding portion that is in contact with a refrigerant flowing through the refrigerant circuit and the resin functional component is formed of any of polytetrafluoroethylene, polyphenylene sulfide, phenolic resin, polyamide resin, chloroprene rubber, silicon rubber, hydrogenated nitrile rubber, fluororubber, and hydrin rubber, the aniline point of the refrigerating oil is preferably set within a particular range in consideration of the adaptability with the resin functional component. By setting the aniline point in such a manner, for example, the adaptability of bearings constituting the resin functional component with the refrigerating oil is improved. Specifically, if the aniline point is excessively low, the refrigerating oil readily infiltrates bearings or the like, and the bearings or the like readily swell. On the other hand, if the aniline point is excessively high, the refrigerating oil does not readily infiltrate bearings or the like, and the bearings or the like readily shrink. Therefore, by setting the aniline point of the refrigerating oil within a particular range, the swelling or shrinking of the bearings or the like can be prevented. Herein, for example, if each of the bearings or the like deforms through swelling or shrinking, the desired length of a gap at a sliding portion cannot be maintained. This may increase the sliding resistance or decrease the rigidity of the sliding portion. However, when the aniline point of the refrigerating oil is set within a particular range as described above, the deformation of the bearings or the like through swelling or shrinking is suppressed, and thus such a problem can be avoided.


The vinyl ether monomers may be used alone or in combination of two or more. Examples of the hydrocarbon monomer having an olefinic double bond include ethylene, propylene, various butenes, various pentenes, various hexenes, various heptenes, various octenes, diisobutylene, triisobutylene, styrene, α-methylstyrene, and various alkyl-substituted styrenes. The hydrocarbon monomers having an olefinic double bond may be used alone or in combination of two or more.


The polyvinyl ether copolymer may be a block copolymer or a random copolymer. The polyvinyl ether oils may be used alone or in combination of two or more.


A polyvinyl ether oil preferably used has a structural unit represented by general formula (1) below.




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(In the formula, R1, R2, and R3 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 8 carbon atoms, R4 represents a divalent hydrocarbon group having 1 to 10 carbon atoms or an ether bond oxygen-containing divalent hydrocarbon group having 2 to 20 carbon atoms, R5 represents a hydrocarbon group having 1 to 20 carbon atoms, m represents a number at which the average of m in the polyvinyl ether is 0 to 10, R1 to R5 may be the same or different in each of structural units, and when m represents 2 or more in one structural unit, a plurality of R4O may be the same or different.)


At least one of R1, R2, and R3 in the general formula (1) preferably represents a hydrogen atom. In particular, all of R1, R2, and R3 preferably represent a hydrogen atom. In the general formula (1), m preferably represents 0 or more and 10 or less, particularly preferably 0 or more and 5 or less, further preferably 0. R5 in the general formula (1) represents a hydrocarbon group having 1 to 20 carbon atoms. Specific examples of the hydrocarbon group include alkyl groups such as a methyl group, an ethyl group, a n-propyl group, an isopropyl group, a n-butyl group, an isobutyl group, a sec-butyl group, a tert-butyl group, various pentyl groups, various hexyl groups, various heptyl groups, and various octyl groups; cycloalkyl groups such as a cyclopentyl group, a cyclohexyl group, various methylcyclohexyl groups, various ethylcyclohexyl groups, and various dimethylcyclohexyl groups; aryl groups such as a phenyl group, various methylphenyl groups, various ethylphenyl groups, and various dimethylphenyl groups; and arylalkyl groups such as a benzyl group, various phenylethyl groups, and various methylbenzyl groups. Among the alkyl groups, the cycloalkyl groups, the phenyl group, the aryl groups, and the arylalkyl groups, alkyl groups, in particular, alkyl groups having 1 to 5 carbon atoms are preferred. For the polyvinyl ether oil contained, the ratio of a polyvinyl ether oil with R5 representing an alkyl group having 1 or 2 carbon atoms and a polyvinyl ether oil with R5 representing an alkyl group having 3 or 4 carbon atoms is preferably 40%:60% to 100%:0%.


The polyvinyl ether oil according to this embodiment may be a homopolymer constituted by the same structural unit represented by the general formula (1) or a copolymer constituted by two or more structural units. The copolymer may be a block copolymer or a random copolymer.


The polyvinyl ether oil according to this embodiment may be constituted by only the structural unit represented by the general formula (1) or may be a copolymer further including a structural unit represented by general formula (2) below. In this case, the copolymer may be a block copolymer or a random copolymer.




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(In the formula, R6 to R9 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 20 carbon atoms.)


The vinyl ether monomer is, for example, a compound represented by general formula (3) below.




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(In the formula, R1, R2, R3, R4, R5, and m have the same meaning as R1, R2, R3, R4, R5, and m in the general formula (1), respectively.)


Examples of various polyvinyl ether compounds corresponding to the above polyvinyl ether compound include vinyl methyl ether; vinyl ethyl ether; vinyl-n-propyl ether; vinyl-isopropyl ether; vinyl-n-butyl ether; vinyl-isobutyl ether; vinyl-sec-butyl ether; vinyl-tert-butyl ether; vinyl-n-pentyl ether; vinyl-n-hexyl ether; vinyl-2-methoxyethyl ether; vinyl-2-ethoxyethyl ether; vinyl-2-methoxy-1-methylethyl ether; vinyl-2-methoxy-propyl ether; vinyl-3,6-dioxaheptyl ether; vinyl-3,6,9-trioxadecyl ether; vinyl-1,4-dimethyl-3,6-dioxaheptyl ether; vinyl-1,4,7-trimethyl-3,6,9-trioxadecyl ether; vinyl-2,6-dioxa-4-heptyl ether; vinyl-2,6,9-trioxa-4-decyl ether; 1-methoxypropene; 1-ethoxypropene; 1-n-propoxypropene; 1-isopropoxypropene; 1-n-butoxypropene; 1-isobutoxypropene; 1-sec-butoxypropene; 1-tert-butoxypropene; 2-methoxypropene; 2-ethoxypropene; 2-n-propoxypropene; 2-isopropoxypropene; 2-n-butoxypropene; 2-isobutoxypropene; 2-sec-butoxypropene; 2-tert-butoxypropene; 1-methoxy-1-butene; 1-ethoxy-1-butene; 1-n-propoxy-1-butene; 1-isopropoxy-1-butene; 1-n-butoxy-1-butene; 1-isobutoxy-1-butene; 1-sec-butoxy-1-butene; 1-tert-butoxy-1-butene; 2-methoxy-1-butene; 2-ethoxy-1-butene; 2-n-propoxy-1-butene; 2-isopropoxy-1-butene; 2-n-butoxy-1-butene; 2-isobutoxy-1-butene; 2-sec-butoxy-1-butene; 2-tert-butoxy-1-butene; 2-methoxy-2-butene; 2-ethoxy-2-butene; 2-n-propoxy-2-butene; 2-isopropoxy-2-butene; 2-n-butoxy-2-butene; 2-isobutoxy-2-butene; 2-sec-butoxy-2-butene; and 2-tert-butoxy-2-butene. These vinyl ether monomers can be produced by a publicly known method.


The end of the polyvinyl ether compound having the structural unit represented by the general formula (1) can be converted into a desired structure by a method described in the present disclosure and a publicly known method. Examples of the group introduced by conversion include saturated hydrocarbons, ethers, alcohols, ketones, amides, and nitriles.


The polyvinyl ether compound preferably has the following end structures.




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(In the formula, R11, R21, and R31 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 8 carbon atoms, R41 represents a divalent hydrocarbon group having 1 to 10 carbon atoms or an ether bond oxygen-containing divalent hydrocarbon group having 2 to 20 carbon atoms, R51 represents a hydrocarbon group having 1 to 20 carbon atoms, m represents a number at which the average of m in the polyvinyl ether is 0 to 10, and when m represents 2 or more, a plurality of R41O may be the same or different.)




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(In the formula, R61, R71, R81, and R91 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 20 carbon atoms.)




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(In the formula, R12, R22, and R32 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 8 carbon atoms, R42 represents a divalent hydrocarbon group having 1 to 10 carbon atoms or an ether bond oxygen-containing divalent hydrocarbon group having 2 to 20 carbon atoms, R52 represents a hydrocarbon group having 1 to 20 carbon atoms, m represents a number at which the average of m in the polyvinyl ether is 0 to 10, and when m represents 2 or more, a plurality of R42O may be the same or different.)




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(In the formula, R62, R72, R82, and R92 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 20 carbon atoms.)




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(In the formula, R13, R23, and R33 may be the same or different and each represent a hydrogen atom or a hydrocarbon group having 1 to 8 carbon atoms.)


The polyvinyl ether oil according to this embodiment can be produced by polymerizing the above-described monomer through, for example, radical polymerization, cationic polymerization, or radiation-induced polymerization. After completion of the polymerization reaction, a typical separation/purification method is performed when necessary to obtain a desired polyvinyl ether compound having a structural unit represented by the general formula (1).


(Polyoxyalkylene Oil)

The polyoxyalkylene oil is a polyoxyalkylene compound obtained by, for example, polymerizing an alkylene oxide having 2 to 4 carbon atoms (e.g., ethylene oxide or propylene oxide) using water or a hydroxyl group-containing compound as an initiator. The hydroxyl group of the polyoxyalkylene compound may be etherified or esterified. The polyoxyalkylene oil may contain an oxyalkylene unit of the same type or two or more oxyalkylene units in one molecule. The polyoxyalkylene oil preferably contains at least an oxypropylene unit in one molecule.


Specifically, the polyoxyalkylene oil is, for example, a compound represented by general formula (9) below.





R101—[(OR102)k—OR103]l  (9)


(In the formula, R101 represents a hydrogen atom, an alkyl group having 1 to 10 carbon atoms, an acyl group having 2 to 10 carbon atoms, or an aliphatic hydrocarbon group having 2 to 6 bonding sites and 1 to 10 carbon atoms, R102 represents an alkylene group having 2 to 4 carbon atoms, R103 represents a hydrogen atom, an alkyl group having 1 to 10 carbon atoms, or an acyl group having 2 to 10 carbon atoms, 1 represents an integer of 1 to 6, and k represents a number at which the average of k×1 is 6 to 80.)


In the general formula (9), the alkyl group represented by R101 and R103 may be a linear, branched, or cyclic alkyl group. Specific examples of the alkyl group include a methyl group, an ethyl group, a n-propyl group, an isopropyl group, various butyl groups, various pentyl groups, various hexyl groups, various heptyl groups, various octyl groups, various nonyl groups, various decyl groups, a cyclopentyl group, and a cyclohexyl group. If the number of carbon atoms of the alkyl group exceeds 10, the miscibility with a refrigerant deteriorates, which may cause phase separation. The number of carbon atoms of the alkyl group is preferably 1 to 6.


The acyl group represented by R101 and R103 may have a linear, branched, or cyclic alkyl group moiety. Specific examples of the alkyl group moiety of the acyl group include various groups having 1 to 9 carbon atoms that are mentioned as specific examples of the alkyl group. If the number of carbon atoms of the acyl group exceeds 10, the miscibility with a refrigerant deteriorates, which may cause phase separation. The number of carbon atoms of the acyl group is preferably 2 to 6.


When R101 and R103 each represent an alkyl group or an acyl group, R101 and R103 may be the same or different.


Furthermore, when 1 represents 2 or more, a plurality of R103 in one molecule may be the same or different.


When R101 represents an aliphatic hydrocarbon group having 2 to 6 bonding sites and 1 to 10 carbon atoms, the aliphatic hydrocarbon group may be a linear group or a cyclic group. Examples of the aliphatic hydrocarbon group having two bonding sites include an ethylene group, a propylene group, a butylene group, a pentylene group, a hexylene group, a heptylene group, an octylene group, a nonylene group, a decylene group, a cyclopentylene group, and a cyclohexylene group. Examples of the aliphatic hydrocarbon group having 3 to 6 bonding sites include residual groups obtained by removing hydroxyl groups from polyhydric alcohols such as trimethylolpropane, glycerol, pentaerythritol, sorbitol, 1,2,3-trihydroxycyclohexane, and 1,3,5-trihydroxycyclohexane.


If the number of carbon atoms of the aliphatic hydrocarbon group exceeds 10, the miscibility with a refrigerant deteriorates, which may cause phase separation. The number of carbon atoms is preferably 2 to 6.


R102 in the general formula (9) represents an alkylene group having 2 to 4 carbon atoms. Examples of the oxyalkylene group serving as a repeating unit include an oxyethylene group, an oxypropylene group, and an oxybutylene group. The polyoxyalkylene oil may contain an oxyalkylene group of the same type or two or more oxyalkylene groups in one molecule, but preferably contains at least an oxypropylene unit in one molecule. In particular, the content of the oxypropylene unit in the oxyalkylene unit is suitably 50 mol % or more.


In the general formula (9), 1 represents an integer of 1 to 6, which can be determined in accordance with the number of bonding sites of R11. For example, when R101 represents an alkyl group or an acyl group, l represents 1. When R101 represents an aliphatic hydrocarbon group having 2, 3, 4, 5, and 6 bonding sites, 1 represents 2, 3, 4, 5, and 6, respectively. Preferably, l represents 1 or 2. Furthermore, k preferably represents a number at which the average of k×1 is 6 to 80.


For the structure of the polyoxyalkylene oil, a polyoxypropylene diol dimethyl ether represented by general formula (10) below and a poly(oxyethylene/oxypropylene) diol dimethyl ether represented by general formula (11) below are suitable from the viewpoints of economy and the above-described effects. Furthermore, a polyoxypropylene diol monobutyl ether represented by general formula (12) below, a polyoxypropylene diol monomethyl ether represented by general formula (13) below, a poly(oxyethylene/oxypropylene) diol monomethyl ether represented by general formula (14) below, a poly(oxyethylene/oxypropylene) diol monobutyl ether represented by general formula (15) below, and a polyoxypropylene diol diacetate represented by general formula (16) below are suitable from the viewpoint of economy and the like.





CH3O—(C3H6O)h—CH3  (10)


(In the formula, h represents 6 to 80.)





CH3O—(C2H4O)i—(C3H6O)j—CH3  (11)


(In the formula, i and j each represent 1 or more and the sum of i and j is 6 to 80.)





C4H9O—(C3H6O)h—H  (12)


(In the formula, h represents 6 to 80.)





CH3O—(C3H6O)h—H  (13)


(In the formula, h represents 6 to 80.)





CH3O—(C2H4O)i—(C3H6O)j—H  (14)


(In the formula, i and j each represent 1 or more and the sum of i and j is 6 to 80.)





C4H9O—(C2H4O)i—(C3H6O)j—H  (15)


(In the formula, i and j each represent 1 or more and the sum of i and j is 6 to 80.)





CH3COO—(C3H6O)h—COCH3  (16)


(In the formula, h represents 6 to 80.)


The polyoxyalkylene oils may be used alone or in combination of two or more.


(2-2) Hydrocarbon Refrigerating Oil

The hydrocarbon refrigerating oil that can be used is, for example, an alkylbenzene.


The alkylbenzene that can be used is a branched alkylbenzene synthesized from propylene polymer and benzene serving as raw materials using a catalyst such as hydrogen fluoride or a linear alkylbenzene synthesized from normal paraffin and benzene serving as raw materials using the same catalyst. The number of carbon atoms of the alkyl group is preferably 1 to 30 and more preferably 4 to 20 from the viewpoint of achieving a viscosity appropriate as a lubricating base oil. The number of alkyl groups in one molecule of the alkylbenzene is dependent on the number of carbon atoms of the alkyl group, but is preferably 1 to 4 and more preferably 1 to 3 to control the viscosity within the predetermined range.


The hydrocarbon refrigerating oil preferably circulates through a refrigeration cycle system together with a refrigerant. Although it is most preferable that the refrigerating oil is soluble with a refrigerant, for example, a refrigerating oil (e.g., a refrigerating oil disclosed in Japanese Patent No. 2803451) having low solubility can also be used as long as the refrigerating oil is capable of circulating through a refrigeration cycle system together with a refrigerant. To allow the refrigerating oil to circulate through a refrigeration cycle system, the refrigerating oil is required to have a low kinematic viscosity. The kinematic viscosity of the hydrocarbon refrigerating oil at 40° C. is preferably 1 mm2/s or more and 50 mm2/s or less and more preferably 1 mm2/s or more and 25 mm2/s or less.


These refrigerating oils may be used alone or in combination of two or more.


The content of the hydrocarbon refrigerating oil in the working fluid for a refrigerating machine may be, for example, 10 parts by mass or more and 100 parts by mass or less and is more preferably 20 parts by mass or more and 50 parts by mass or less relative to 100 parts by mass of the refrigerant composition.


(2-3) Additive

The refrigerating oil may contain one or two or more additives.


Examples of the additives include an acid scavenger, an extreme pressure agent, an antioxidant, an antifoaming agent, an oiliness improver, a metal deactivator such as a copper deactivator, an anti-wear agent, and a compatibilizer.


Examples of the acid scavenger that can be used include epoxy compounds such as phenyl glycidyl ether, alkyl glycidyl ether, alkylene glycol glycidyl ether, cyclohexene oxide, α-olefin oxide, and epoxidized soybean oil; and carbodiimides. Among them, phenyl glycidyl ether, alkyl glycidyl ether, alkylene glycol glycidyl ether, cyclohexene oxide, and α-olefin oxide are preferred from the viewpoint of miscibility. The alkyl group of the alkyl glycidyl ether and the alkylene group of the alkylene glycol glycidyl ether may have a branched structure. The number of carbon atoms may be 3 or more and 30 or less, and is more preferably 4 or more and 24 or less and further preferably 6 or more and 16 or less. The total number of carbon atoms of the α-olefin oxide may be 4 or more and 50 or less, and is more preferably 4 or more and 24 or less and further preferably 6 or more and 16 or less. The acid scavengers may be used alone or in combination of two or more.


The extreme pressure agent may contain, for example, a phosphoric acid ester. Examples of the phosphoric acid ester that can be used include phosphoric acid esters, phosphorous acid esters, acidic phosphoric acid esters, and acidic phosphorous acid esters. The extreme pressure agent may contain an amine salt of a phosphoric acid ester, a phosphorous acid ester, an acidic phosphoric acid ester, or an acidic phosphorous acid ester.


Examples of the phosphoric acid ester include triaryl phosphates, trialkyl phosphates, trialkylaryl phosphates, triarylalkyl phosphates, and trialkenyl phosphates. Specific examples of the phosphoric acid ester include triphenyl phosphate, tricresyl phosphate, benzyl diphenyl phosphate, ethyl diphenyl phosphate, tributyl phosphate, ethyl dibutyl phosphate, cresyl diphenyl phosphate, dicresyl phenyl phosphate, ethylphenyl diphenyl phosphate, diethylphenyl phenyl phosphate, propylphenyl diphenyl phosphate, dipropylphenyl phenyl phosphate, triethylphenyl phosphate, tripropylphenyl phosphate, butylphenyl diphenyl phosphate, dibutylphenyl phenyl phosphate, tributylphenyl phosphate, trihexyl phosphate, tri(2-ethylhexyl) phosphate, tridecyl phosphate, trilauryl phosphate, trimyristyl phosphate, tripalmityl phosphate, tristearyl phosphate, and trioleyl phosphate.


Specific examples of the phosphorous acid ester include triethyl phosphite, tributyl phosphite, triphenyl phosphite, tricresyl phosphite, tri(nonylphenyl) phosphite, tri(2-ethylhexyl) phosphite, tridecyl phosphite, trilauryl phosphite, triisooctyl phosphite, diphenylisodecyl phosphite, tristearyl phosphite, and trioleyl phosphite.


Specific examples of the acidic phosphoric acid ester include 2-ethylhexyl acid phosphate, ethyl acid phosphate, butyl acid phosphate, oleyl acid phosphate, tetracosyl acid phosphate, isodecyl acid phosphate, lauryl acid phosphate, tridecyl acid phosphate, stearyl acid phosphate, and isostearyl acid phosphate.


Specific examples of the acidic phosphorous acid ester include dibutyl hydrogen phosphite, dilauryl hydrogen phosphite, dioleyl hydrogen phosphite, distearyl hydrogen phosphite, and diphenyl hydrogen phosphite. Among the phosphoric acid esters, oleyl acid phosphate and stearyl acid phosphate are suitably used.


Among amines used for amine salts of phosphoric acid esters, phosphorous acid esters, acidic phosphoric acid esters, or acidic phosphorous acid esters, specific examples of mono-substituted amines include butylamine, pentylamine, hexylamine, cyclohexylamine, octylamine, laurylamine, stearylamine, oleylamine, and benzylamine. Specific examples of di-substituted amines include dibutylamine, dipentylamine, dihexylamine, dicyclohexylamine, dioctylamine, dilaurylamine, distearylamine, dioleylamine, dibenzylamine, stearyl-monoethanolamine, decyl-monoethanolamine, hexyl-monopropanolamine, benzyl-monoethanolamine, phenyl-monoethanolamine, and tolyl-monopropanolamine. Specific examples of tri-substituted amines include tributylamine, tripentylamine, trihexylamine, tricyclohexylamine, trioctylamine, trilaurylamine, tristearylamine, trioleylamine, tribenzylamine, dioleyl-monoethanolamine, dilauryl-monopropanolamine, dioctyl-monoethanolamine, dihexyl-monopropanolamine, dibutyl-monopropanolamine, oleyl-diethanolamine, stearyl-dipropanolamine, lauryl-diethanolamine, octyl-dipropanolamine, butyl diethanolamine, benzyl-diethanolamine, phenyl-diethanolamine, tolyl-dipropanolamine, xylyl-diethanolamine, triethanolamine, and tripropanolamine.


Examples of extreme pressure agents other than the above-described extreme pressure agents include extreme pressure agents based on organosulfur compounds such as monosulfides, polysulfides, sulfoxides, sulfones, thiosulfinates, sulfurized fats and oils, thiocarbonates, thiophenes, thiazoles, and methanesulfonates; extreme pressure agents based on thiophosphoric acid esters such as thiophosphoric acid triesters; extreme pressure agents based on esters such as higher fatty acids, hydroxyaryl fatty acids, polyhydric alcohol esters, and acrylic acid esters; extreme pressure agents based on organochlorine compounds such as chlorinated hydrocarbons, e.g., chlorinated paraffin and chlorinated carboxylic acid derivatives; extreme pressure agents based on fluoroorganic compounds such as fluorinated aliphatic carboxylic acids, fluorinated ethylene resins, fluorinated alkylpolysiloxanes, and fluorinated graphites; extreme pressure agents based on alcohols such as higher alcohols; and extreme pressure agents based on metal compounds such as naphthenic acid salts (e.g., lead naphthenate), fatty acid salts (e.g., lead fatty acid), thiophosphoric acid salts (e.g., zinc dialkyldithiophosphate), thiocarbamic acid salts, organomolybdenum compounds, organotin compounds, organogermanium compounds, and boric acid esters.


The antioxidant that can be used is, for example, a phenol-based antioxidant or an amine-based antioxidant. Examples of the phenol-based antioxidant include 2,6-di-tert-butyl-4-methylphenol (DBPC), 2,6-di-tert-butyl-4-ethylphenol, 2,2′-methylenebis(4-methyl-6-tert-butylphenol), 2,4-dimethyl-6-tert-butylphenol, 2,6-di-tert-butylphenol, di-tert-butyl-p-cresol, and bisphenol A. Examples of the amine-based antioxidant include N,N′-diisopropyl-p-phenylenediamine, N,N′-di-sec-butyl-p-phenylenediamine, phenyl-α-naphthylamine, N,N′-di-phenyl-p-phenylenediamine, and N,N-di(2-naphthyl)-p-phenylenediamine. An oxygen scavenger that captures oxygen can also be used as the antioxidant.


The antifoaming agent that can be used is, for example, a silicon compound.


The oiliness improver that can be used is, for example, a higher alcohol or a fatty acid.


The metal deactivator such as a copper deactivator that can be used is, for example, benzotriazole or a derivative thereof.


The anti-wear agent that can be used is, for example, zinc dithiophosphate.


The compatibilizer is not limited, and can be appropriately selected from commonly used compatibilizers. The compatibilizers may be used alone or in combination of two or more. Examples of the compatibilizer include polyoxyalkylene glycol ethers, amides, nitriles, ketones, chlorocarbons, esters, lactones, aryl ethers, fluoroethers, and 1,1,1-trifluoroalkanes. The compatibilizer is particularly preferably a polyoxyalkylene glycol ether.


The refrigerating oil may optionally contain, for example, a load-bearing additive, a chlorine scavenger, a detergent dispersant, a viscosity index improver, a heat resistance improver, a stabilizer, a corrosion inhibitor, a pour-point depressant, and an anticorrosive.


The content of each additive in the refrigerating oil may be 0.01 mass % or more and 5 mass % or less and is preferably 0.05 mass % or more and 3 mass % or less. The content of the additive in the working fluid for a refrigerating machine constituted by the refrigerant composition and the refrigerating oil is preferably 5 mass % or less and more preferably 3 mass % or less.


The refrigerating oil preferably has a chlorine concentration of 50 ppm or less and preferably has a sulfur concentration of 50 ppm or less.


(3) Refrigerant Cycle Apparatus

A refrigerant cycle apparatus that uses one of the above-described refrigerant 1A, refrigerant 1B, refrigerant 1C, refrigerant 1D, refrigerant 1E, refrigerant 2A, refrigerant 2B, refrigerant 2C, refrigerant 2D, and refrigerant 2E and also uses refrigeration oil is described below. The refrigerant cycle apparatus is a refrigerant cycle apparatus for freezing or cold storage, and is typically called a cold-storage showcase or a freezing showcase. Representative forms of cold-storage showcases and freezing showcases include an open type showcase that blocks outside air from entering a display chamber by forming an air curtain, and a closed type showcase (reach-in showcase) that blocks outside air from entering a display chamber by a glass panel or the like. Moreover, the representative forms include a built-in showcase in which refrigeration cycle devices, such as a compressor and a condenser, are built in the showcase, and a separate-installation type showcase that is connected to a refrigerating machine including a compressor and a condenser via a refrigerant pipe. Furthermore, the temperature zones to be used include a freezing zone and a cold-storage zone. The freezing zone is, for example, for ice creams or for frozen foods. The cold-storage zone is, for example, for drinking water or alcohol, or for perishable foods.


(3-1) Built-in Type Showcase


FIG. 3 is a vertically sectioned side view of a built-in open showcase that is an example of a cold-storage showcase.


A showcase body 101 constituting the open showcase has a rectangular shape in front view and plan view. The showcase body 101 includes a top panel portion 102 located at the top, a machine chamber 103 located at the bottom, and a display chamber 104 located between the top panel portion 102 and the machine chamber 103.


The display chamber 104 is surrounded by a ceiling portion 104b, a bottom surface portion 104c, and a rear surface wall 104a. The rear surface wall 104a is inclined to gradually protrude forward as the rear surface wall 104a extends from the ceiling portion 104b to the bottom surface portion 104c. The rear surface wall 104a is provided with shelfs 105 of four stages spaced apart at a predetermined interval. Products such as foods and drinks for sale are placed and displayed on each of the shelfs 105.


The rear surface wall 104a of the display chamber 104 has a plurality of cooling blow-out ports 106. Cold air flows from the cooling blow-out ports 106 to the products placed on the shelfs 105 as described later.


An air-curtain blow-out port 108 is formed in the ceiling portion 104b. The air-curtain blow-out port 108 blows out cold air that inhibits air from entering the display chamber 104 from the outside of the showcase body 101.


The inside of the top panel portion 102 is hollow, and an air-curtain duct 109 for guiding the cold air to the air-curtain blow-out port 108 is formed. A proximal end portion of the air-curtain duct 109 communicates with a cold-air circulation duct 110 which will be described later.


A suction port 111 is provided at the bottom surface portion 104c serving as an upper surface of the machine chamber 103. The suction port 111 sucks the cold air blown out from the cooling blow-out ports 106 of the rear surface wall 104a and air-curtain cold air blown out from the air-curtain blow-out port 108 of the ceiling portion 104b. The suction port 111 is positioned such that no obstruction is present between the suction port 111 and the air-curtain blow-out port 108. Thus, the air-curtain cold air blown out from the air-curtain blow-out port 108 is smoothly sucked into the suction port 111 and stably forms an air curtain without being obstructed by the shelfs 105.


A compressor 121, a condenser 122, an expansion valve 123, and an air fan 125 are disposed in the machine chamber 103.


The cold-air circulation duct 110 is formed between the rear surface wall 104a and a partition plate 115. An exhaust duct 117 is formed between the partition plate 115 and a showcase rear surface portion 101a.


The cold-air circulation duct 110, at the lower end thereof, communicates with the suction port 111. The cold-air circulation duct 110 communicates with each cooling blow-out port 106 of the rear surface wall 104a. Moreover, the cold-air circulation duct 110, at the upper end thereof, communicates with the air-curtain duct 109.


A cold-air circulation fan 113 is disposed in the cold-air circulation duct 110, at a position at a predetermined distance from the suction port 111. An evaporator 124 is disposed downwind of the cold-air circulation fan 113 in the cold-air circulation duct 110. The evaporator 124 constitutes a refrigerant cycle together with the compressor 121, the condenser 122, the expansion valve 123, a receiver 126, a dryer 127, and an accumulator 128 via a refrigerant pipe 129. The dryer 127 contains a drying agent to prevent clogging of the expansion valve 123.


An air ventilation port 107 is formed in a front surface portion of the machine chamber 103. The air ventilation port 107 takes in outside air into a machine chamber 33 upon driving of the air fan 125 for cooling the condenser 122.


The machine chamber 103 communicates with the exhaust duct 117. An upper end portion of the exhaust duct 117 serves as an opening 117a and is open to the outside. Thus, the air taken into the machine chamber 103 from the air ventilation port 107 circulates in the machine chamber 103, then rises through the exhaust duct 117, and is exhausted from the opening 117a to the outside.


In the open showcase thus configured, the compressor 121 is driven, and the air fan 125 and the cold-air circulation fan 113 are driven. The refrigerant is compressed in the compressor 121, and the refrigerant is guided as a high-temperature high-pressure gas refrigerant to the condenser 122. The air fan 125 takes in the air into the machine chamber 103 via the air ventilation port 107 formed in the front surface portion of the machine chamber 103, and causes the air to pass through the condenser 122.


In the condenser 122, a gas refrigerant exchanges heat with the air taken into the machine chamber 33 by the air fan 125 and is condensed. The air after the heat exchange flows in the peripheral area of from the condenser 122 to the compressor 121 to cool the condenser 122 and the compressor 121. The air which has been turned into high-temperature air is then guided by the exhaust duct 117 and is exhausted upward from the opening 117a.


A liquid refrigerant liquefied in the condenser 122 is decompressed by the expansion valve 123 and is guided to the evaporator 124. In the evaporator 124, the refrigerant exchanges heat with the air sent from the cold-air circulation fan 113 and is evaporated. At this time, the refrigerant takes heat from the air and is evaporated, and the refrigerant flows to the compressor 121.


The air (cold air) which has exchanged heat with the refrigerant and has been turned into low-temperature air in the evaporator 124 rises through the cold-air circulation duct 110 and is guided forward from each cooling blow-out port 106 in the middle of the cold-air circulation duct 110. The cold air which has passed through each cooling blow-out port 106 flows to the display chamber 104. In other words, the cold air is blown out to products placed on each shelf 105 from the corresponding cooling blow-out port 106, and the products are cooled with the cold air.


The cold air which has reached the upper end portion of the cold-air circulation duct 110 flows to the air-curtain duct 109, and is blown out downward from the air-curtain blow-out port 108 on the front surface side. The air curtain can almost block the entry of the outside air from the outside to the display chamber 104.


Both the cold air blown out from the air-curtain blow-out port 108 and the cold air blown out from the cooling blow-out ports 106 are sucked into the suction port 111. The cold air which have provided the functions are mixed to each other and sucked into the suction port 111.


(3-2) Separate-installation Type Showcase


FIG. 4 illustrates a separate-installation type showcase cooling apparatus. A showcase cooling apparatus 201 cools a plurality of showcases 210a to 210j (see FIG. 5 for the showcase 210i and the showcase 210j) installed in a store interior 202 of a convenience store (shop). A refrigerating machine 206 connected to the respective showcases 210a to 210j via refrigerant pipes 207 and 208 is installed outside the store. The showcases 210a to 210j and the refrigerating machine 206 constitute the showcase cooling apparatus 201.


The showcases 210a to 210j are open showcases. The showcases 210a, and 210c to 210f are for displaying chilled foods (products) in the inner spaces (display chambers) to sell the chilled foods. The inner spaces of the showcases 210a, and 210c to 210f are cooled to a relatively low cold-storage temperature zone (0° C. to +5° C.) that is suitable for cooling chilled foods. The showcase 210b is for displaying packed meals (products) in the inner space (display chamber) to sell the packed meals. The inner space is cooled to a relatively high cold-storage temperature zone (+15° C. to +20° C.) that is suitable for cooling packed meals. Moreover, the showcases 210a and 210b can be used while display is switched between the display of chilled foods and the display of packed meals. The showcase 210i and the showcase 210j are freezing showcases for displaying frozen foods and ice creams in a frozen state (−20° C. to −25° C.). In the showcase 210i and the showcase 210j, the target value of the evaporation temperature of an evaporator 271, which will be described later, is set to, for example, −30° C. to −40° C., and a compressor 257 and so forth are controlled. In a refrigerant cycle apparatus for freezing or cold storage, the target value of the evaporation temperature of the evaporator 271 is selected from a range of +10° C. to −45° C.


The showcases 210g and 210h are closed type showcases having transparent glass panels and installed on a wall surface of the store. The showcases 210g and 210h are for displaying the above-described chilled foods (products) in the inner spaces (display chambers) to sell the chilled foods. The inner spaces of the showcases 210g and 210h are cooled to a relatively low cold-storage temperature zone (0° C. to +5° C.) that is suitable for cooling the chilled foods. The respective showcases 210a to 210j are connected in parallel with respect to the refrigerating machine 206 by the refrigerant pipes 207 and 208.


Next, devices that constitute a refrigerant circuit in the showcase cooling apparatus 201 are described with reference to FIG. 5.


The showcase cooling apparatus 201 includes a dual refrigerant cycle including a high-stage-side refrigerant circuit 250 in which the above-described refrigerant (any one of the refrigerant 1A, the refrigerant 1, the refrigerant 1C, the refrigerant 1D, the refrigerant 1E, the refrigerant 2A, the refrigerant 2B, the refrigerant 2C, the refrigerant 2D, and the refrigerant 2E) is enclosed; and a plurality of low-stage-side refrigerant circuits 270 in which a carbon dioxide refrigerant (CO2 refrigerant) is enclosed. The high-stage-side refrigerant circuit 250 mainly includes a compressor 257 whose operating frequency is variably controllable, a radiator 258, an expansion valve 259, and a plurality of evaporators 271 connected in parallel. The low-stage-side refrigerant circuit 270 mainly includes a compressor 273, a radiator 274, an expansion valve 276, an evaporator 277, a dryer 281, a receiver 282, and an accumulator 283. In this case, the showcase 210i and the showcase 210j each include the low-stage-side refrigerant circuit 270.


A fan 251 that air-cools the compressor 257, the radiator 258, the expansion valve 259, and the radiator 258 of the high-stage-side refrigerant circuit 250 are installed in the refrigerating machine 206.


One of the low-stage-side refrigerant circuits 270, the evaporator 271 of the corresponding high-stage-side refrigerant circuit 250, and a cold-air circulation fan 280 that causes cold air which has exchanged heat with the radiator 274 of the low-stage-side refrigerant circuit 270 to circulate in the inner space are installed in each of the showcase 210i and the showcase 210j. The inlet of each evaporator 271 of the high-stage-side refrigerant circuit 250 is connected to the refrigerant pipe 207, the outlet thereof is connected to the refrigerant pipe 208 and cascade-connected to the radiator 274 of the low-stage-side refrigerant circuit 270 of corresponding one of the showcases 210a to 210h in terms of the heat exchange, and the components constitute a cascade heat exchanger 290. The cascade heat exchanger 290 is thermally insulated from the peripheral area. Thus, the radiator 271 of the low-stage-side refrigerant circuit 270 constituting the cascade heat exchanger 290 is the most stable in terms of the temperature.


Note that the inner space of a cold-storage showcase such as the showcase 210a is cooled by the evaporator 271 of the high-stage-side refrigerant circuit 250. Thus, a cold-air circulation fan 280a that causes the cold air which has exchanged heat with the evaporator 271 to circulate in the inner space is provided.


(3-3) Refrigerant Circuit Used for Refrigerant Cycle Apparatus for Freezing or Cold Storage

The built-in type showcase described in the above-mentioned (3-1) employs simple, single-stage compression refrigerant cycle. Moreover, the separate-installation type showcase cooling apparatus 201 described in the above-mentioned (3-2) employs a refrigerant circuit including a dual refrigerant cycle. Instead of these refrigerant circuits, or by adding a function to these refrigerant circuits, it is preferable to employ a refrigerant circuit as follows in the refrigerant cycle apparatus for freezing or cold storage.


3-3-1

It is also preferable to add a function of intermediate injection as illustrated in FIG. 6 to the refrigerant circuit described in the above-mentioned (3-1) illustrated in FIG. 3. An intermediate injection circuit 140 is added to the refrigerant cycle apparatus for freezing or cold storage. The intermediate injection circuit 140 guides a portion of a high-pressure refrigerant flowing between the receiver 126 and the dryer 127 to the middle of a compression chamber in the compressor 121 via an expansion valve 141. The refrigerant decompressed in the expansion valve 141 and having an intermediate pressure cools the refrigerant in the middle of compression in the compressor 121, thereby increasing compression efficiency. In particular, in the refrigerant cycle apparatus for freezing or cold storage, the compression ratio tends to increase, and hence the effect of the intermediate injection is large. The refrigerant that is input from the intermediate injection circuit 140 into the compressor 121 may be a gas refrigerant; however, the refrigerant is preferably a gas-liquid two-phase refrigerant in a slightly moist state.


3-3-2

To decrease the lower limit value of the capacity, it is preferable to add a bypass circuit 150 as illustrated in FIG. 7 to the refrigerant circuit described in the above-mentioned (3-1) illustrated in FIG. 3. In a case where the capacity of the compressor 121 is not able to be decreased and when there is a request for further decreasing the capacity of freezing or cold storage, the refrigerant cycle apparatus for freezing or cold storage can satisfy the request by opening an open-close valve 151 of the bypass circuit 150.


3-3-3

It is also preferable to add a function of suction injection as illustrated in FIG. 8 to the refrigerant circuit described in the above-mentioned (3-1) illustrated in FIG. 3. A suction injection circuit 160 is added to the refrigerant cycle apparatus for freezing or cold storage. The suction injection circuit 160 guides a portion of a high-pressure refrigerant flowing between the dryer 127 and the expansion valve 123 to the suction side of the compressor 121 via an expansion valve 161. When the discharge refrigerant temperature of the compressor 121 is high and the expansion valve 161 is opened, the refrigerant decompressed in the expansion valve 161 and having a low pressure is sucked into the compressor 121, thereby decreasing the discharge refrigerant temperature of the compressor 121.


3-3-4

It is also preferable to add a function of intermediate injection and a function of subcooling as illustrated in FIG. 9 to the refrigerant circuit described in the above-mentioned (3-1) illustrated in FIG. 3. An intermediate injection circuit 170 and an economizer heat exchanger 175 are added to the refrigerant cycle apparatus for freezing or cold storage. The intermediate injection circuit 170 guides a portion of a high-pressure refrigerant flowing between the receiver 126 and the dryer 127 to the middle of a compression chamber in the compressor 121 via an expansion valve 171. The economizer heat exchanger 175 causes an intermediate-pressure refrigerant decompressed by the expansion valve 171 and having a decreased temperature to exchange heat with a high-pressure refrigerant flowing between the receiver 126 and the dryer 127 to decrease the temperature of the high-pressure refrigerant. Thus, the high-pressure refrigerant is turned into a subcooling state, and controllability of the downstream-side expansion valve 123 increases. Moreover, the refrigerant decompressed by the expansion valve 141 and having an intermediate pressure cools the refrigerant in the middle of the compression in the compressor 121, thereby increasing compression efficiency.


3-3-5

The refrigerant cycle apparatus for freezing or cold storage preferably employs a two-stage compression and one-stage expansion refrigerant circuit as illustrated in FIG. 10A instead of the single-stage compression refrigerant circuit described in the above-mentioned (3-1) and (3-2). In the refrigerant circuit, the refrigerant discharged from a low-stage compressor 321a is sucked into a high-stage compressor 321b. The refrigerant discharged from the high-stage compressor 321b dissipates heat and is liquefied in a condenser 322. The refrigerant flowing from the condenser 322 to an expansion valve 323 via a receiver 326, an economizer heat exchanger 375, and a dryer 327 is decompressed by the expansion valve 323 and flows into an evaporator 324. The refrigerant evaporated in the evaporator 324 is sucked into the low-stage compressor 321a via an accumulator 328. A portion of the high-pressure refrigerant flowing between the receiver 326 and the dryer 327 flows between the low-stage compressor 321a and the high-stage compressor 321b via an expansion valve 371 and the economizer heat exchanger 375 of the intermediate injection circuit 170.


A control unit (not illustrated) including a microcomputer or the like that controls the expansion valve 371 first calculates an outlet superheating degree of the economizer heat exchanger 375 from a difference in temperature (Th2−Th3) of temperature sensors Th2 and Th3. Next, the control unit controls the opening degree of the expansion valve 371 so that the outlet superheating degree approaches a constant target superheating degree. Alternatively, the outlet superheating degree may be calculated from a difference in temperature between a detection temperature of the temperature sensor Th2 and a saturation temperature Tps2 calculated from a detection value of a pressure sensor PS2. Moreover, when a temperature of a discharged gas refrigerant from the high-stage compressor 321b (a detection temperature of the temperature sensor Th1) or a degree of superheating (a detection temperature of the temperature sensor Th1 minus a saturation temperature calculated by subtracting a detection value of a pressure sensor PS1) exceeds a threshold, the control unit switches control of the expansion valve 371 from control based on the outlet superheating degree of the economizer heat exchanger 375 to control of decreasing the temperature of the discharged gas refrigerant of the compressor 321b. The control of decreasing the temperature of the discharged gas refrigerant of the compressor 321b controls the expansion valve 371 so that the refrigerant is turned into a gas-liquid two-phase state.


A control unit that controls the expansion valve 323 first calculates an outlet superheating degree of the evaporator 324 from a difference in temperature of temperature sensors Th4 and Th5 (a detection temperature of the temperature sensor Th5—a detection temperature of the temperature sensor Th4). Next, the control unit controls the opening degree of the expansion valve 323 so that the outlet superheating degree of the evaporator 324 meets a constant target superheating degree. Alternatively, the outlet superheating degree of the evaporator 324 may be calculated from a difference in temperature between a detection temperature of the temperature sensor Th5 and a saturation temperature Tps3 calculated from a detection value of a pressure sensor PS3.



FIG. 10B illustrates a pressure and a specific enthalpy at each of points a to i in the two-stage compression and single-stage expansion refrigerant circuit illustrated in FIG. 10A.


3-3-6

The refrigerant cycle apparatus for freezing or cold storage preferably employs a two-stage compression and two-stage expansion refrigerant circuit as illustrated in FIG. 11 instead of the single-stage compression refrigerant circuit described in the above-mentioned (3-1) and (3-2). In the refrigerant circuit, the refrigerant discharged from a low-stage compressor 421a is sucked into a high-stage compressor 421b. The refrigerant discharged from the high-stage compressor 421b dissipates heat and is liquefied in a condenser 422. The refrigerant flowing from the condenser 422 to a first-stage expansion valve 423a is decompressed in the expansion valve 423a and turned into an intermediate pressure. Then, the refrigerant flowing to a second-stage expansion valve 423b via a receiver 426 and a dryer 427 is decompressed by the expansion valve 423b and turned into a low pressure, and flows into an evaporator 424. The refrigerant evaporated in the evaporator 424 is sucked into the low-stage compressor 421a via an accumulator 428. An intermediate-pressure gas refrigerant flowing from an upper space of the receiver 426 to a bypass circuit 470 flows to a portion between the low-stage compressor 421a and the high-stage compressor 421b.


A control unit that controls the first-stage expansion valve 423a adjusts the opening degree of the expansion valve 423a so that a detection value (high pressure) of a pressure sensor PS11 that measures the pressure of a discharge gas refrigerant of the high-stage compressor 421b falls within a predetermined range. When it is determined that the pressure of the discharge gas refrigerant of the compressor 421b is excessively high, the control unit increases the opening degree of the expansion valve 423a to decrease the high pressure.


A control unit that controls the second-stage expansion valve 423b first calculates an outlet superheating degree of the evaporator 424 from a difference in temperature of temperature sensors Th14 and Th15 (a detection temperature of the temperature sensor Th15—a detection temperature of the temperature sensor Th14). Next, the control unit controls the opening degree of the expansion valve 423b so that the outlet superheating degree of the evaporator 424 meets a constant target superheating degree.



FIG. 11B illustrates a pressure and a specific enthalpy at each of points p to x in the two-stage compression and two-stage expansion refrigerant circuit illustrated in FIG. 11A.


3-3-7

It is also preferable to employ a refrigerant circuit having a hot-gas defrosting function as illustrated in FIG. 12 instead of the refrigerant circuit described in the above-mentioned (3-1). A four-way switching valve 529 is provided in a refrigerant circuit of a refrigerant cycle apparatus for freezing or cold storage. The refrigerant discharged from a compressor 521 enters a condenser 522 via the four-way switching valve 529, dissipates heat, and is liquefied in a freezing or cold-storage operation. The refrigerant output from the condenser 522 passes through a receiver 526 and a dryer 527, is decompressed in an expansion valve 523, and enters an evaporator 524 in a two-phase state. The refrigerant evaporated in the evaporator is sucked into the compressor 521 via the four-way switching valve 529 and an accumulator 528. In contrast, when it is determined that the evaporator 524 is frosted in the freezing or cold-storage operation, the control unit switches the four-way switching valve 529 (see a flow path indicated by dotted lines of the four-way switching valve 529 in FIG. 12) to perform a hot-gas defrosting operation. In the hot-gas defrosting operation, a high-temperature gas refrigerant (hot gas) discharged from the compressor 521 enters the heat exchanger 524 via the four-way switching valve 529. The heat exchanger 524 that functions as the evaporator 524 in the freezing or cold-storage operation functions as the condenser 524 in the hot-gas defrosting operation. Thus, the frost on the heat exchanger 524 is molten.


3-3-8

As described above, the refrigerant cycle apparatus for freezing or cold storage can use various refrigerant circuits depending on the request. Moreover, each refrigerant circuit has a variety of combinations of devices.


The compressor is appropriately selected from a rotary compressor, a reciprocation compressor, a scroll compressor, a screw compressor, and the like.


The condenser is not limited to the air-cooling condenser, and a water-cooling condenser can be selected.


For the evaporator, either of air-cooling type and water-cooling type can be selected likewise.


For the expansion valve, a mechanical expansion valve can be used alternatively to an electronic expansion valve (electric expansion valve). Moreover, a capillary tube can be used as decompressing means instead of the expansion valve.


Furthermore, various combinations of control can be applied to the control of each refrigerant circuit. For the capacity control of the compressor, control on the number of rotations in case of an inverter compressor, control on the number of a plurality of constant-speed compressors, or another control can be performed alternatively to the capacity control using the above-described bypass circuit 150. For the method of defrosting, any one of various methods can be selected, the various methods including, for example, a method of melting frost of an evaporation liquid by stopping the compressor and rotating a fan, a method using an electric heater, and a method of melting frost by spraying water, alternatively to the above-described hot-gas defrosting.


3-3-9

The showcase has been described in the above-mentioned embodiment as the refrigerant cycle apparatus for freezing or cold storage; however, even a refrigerant cycle apparatus mounted on a maritime container or a refrigerant cycle apparatus for a warehouse preferably uses any one of the above-described refrigerant 1A, refrigerant 1, refrigerant 1C, refrigerant 1D, refrigerant 1E, refrigerant 2A, refrigerant 2B, refrigerant 2C, refrigerant 2D, and refrigerant 2E.


3-3-10

In the above-described cold-storage showcase or freezing showcase, the target value of the evaporation temperature of the evaporator is selected from the range of +10° C. to −45° C.; however, when a dual refrigerant cycle as illustrated in FIG. 5 or a refrigerant cycle that performs two-stage compression as illustrated in FIGS. 10A and 11A is employed, the target value of the evaporation temperature of the evaporator can be set in a further low range of −20° C. to −65° C. A refrigerant cycle apparatus for freezing installed on a fishing boat for the purpose of deep-sea fishing may set the target value of such a low evaporation temperature.


3-3-11

In the above-described showcase cooling apparatus 201, the refrigerant according to the present disclosure (any one of the refrigerant 1A, the refrigerant 1, the refrigerant 1C, the refrigerant 1D, the refrigerant 1E, the refrigerant 2A, the refrigerant 2B, the refrigerant 2C, the refrigerant 2D, and the refrigerant 2E) is enclosed in the high-stage-side refrigerant circuit 250, and a carbon dioxide refrigerant (CO2 refrigerant) is enclosed in the plurality of low-stage-side refrigerant circuits 270. However, the combination of refrigerants is not limited to the above combination. In the dual refrigerant cycle, the high-stage-side refrigerant circuit may have enclosed therein a flammable refrigerant such as propane, and the low-stage-side refrigerant circuit may have enclosed therein the refrigerant according to the present disclosure.


4

The respective embodiments have been described above, and it is understood that the embodiments and details can be modified in various ways without departing from the idea and scope of the present disclosure described in the claims.


REFERENCE SIGNS LIST






    • 1A, 1, 1C, 1D, 1E: refrigerant


    • 2A, 2B, 2C, 2D, 2E: refrigerant


    • 121, 257, 273: compressor


    • 321
      a, 321b, 421a, 421b, 521: compressor


    • 122, 322, 422, 522: condenser (radiator)


    • 258, 274: radiator


    • 123, 259, 276, 323, 423a, 423b, 523: expansion valve (decompressing portion)


    • 124, 271, 277, 324, 424, 524: evaporator (heat absorber)

    • A in FIGS. 2A and 2B: any mass ratio providing a flame velocity of 5 cm/s as measured according to ANSI/ASHRAE Standard 34-2013 and a concentration (mass %) of HFC-32 of 1.0 mass %

    • B in FIGS. 2A and 2B: any mass ratio providing a concentration (mass %) of HFC-32 of 1.0 mass % and a refrigerating capacity relative to that of R404A of 95%

    • C in FIGS. 2A and 2B: any mass ratio providing a refrigerating capacity relative to that of R404A of 95% and a GWP of 125

    • D in FIGS. 2A and 2B: any mass ratio providing a GWP of 125 and a flame velocity of 5 cm/s as measured according to ANSI/ASHRAE Standard 34-2013

    • E in FIGS. 2A and 2B: any mass ratio providing a refrigerating capacity relative to that of R404A of 95% and a GWP of 100

    • F in FIGS. 2A and 2B: any mass ratio providing a GWP of 100 and a flame velocity of 5 cm/s as measured according to ANSI/ASHRAE Standard 34-2013

    • a in FIGS. 2A and 2B: any straight line indicating any mass ratio providing a concentration (mass %) of HFC-32 of 1.0 mass %

    • b in FIGS. 2A and 2B: any curve indicating any mass ratio providing a refrigerating capacity relative to that of R404A of 95%

    • c in FIGS. 2A and 2B: any straight line indicating any mass ratio providing a GWP of 125

    • d in FIGS. 2A and 2B: any curve indicating any mass ratio providing a flame velocity of 5 cm/s as measured according to ANSI/ASHRAE Standard 34-2013

    • e in FIGS. 2A and 2B: any straight line indicating any mass ratio providing a GWP of 100

    • f in FIGS. 2A and 2B: any straight line indicating any mass ratio providing a GWP of 200

    • P in FIGS. 2A and 2B: any mass ratio providing a pressure at 40° C. of 1.85 MPa and a concentration (mass %) of HFC-32 of 1.0 mass %

    • B in FIGS. 2A and 2B: any mass ratio providing a concentration (mass %) of HFC-32 of 1.0 mass % and a refrigerating capacity relative to that of R404A of 95%

    • Q in FIGS. 2A and 2B: any mass ratio providing a refrigerating capacity relative to that of R404A of 95% and a concentration (mass %) of HFO-1132(E) of 1.0 mass %

    • R in FIGS. 2A and 2B: any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % and a GWP of 200

    • S in FIGS. 2A and 2B: any mass ratio providing a GWP of 200 and a pressure at 40° C. of 1.85 MPa

    • p in FIGS. 2A and 2B: any straight line indicating any mass ratio providing a concentration (mass %) of HFC-32 of 1.0 mass %

    • q in FIGS. 2A and 2B: any curve indicating any mass ratio providing a refrigerating capacity relative to that of R404A of 95%

    • r in FIGS. 2A and 2B: any straight line indicating any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass %

    • s in FIGS. 2A and 2B: any straight line indicating any mass ratio providing a GWP of 200

    • t in FIGS. 2A and 2B: any curve indicating any mass ratio providing a pressure at 40° C. of 1.85 MPa

    • u in FIGS. 2A and 2B: any straight line indicating any mass ratio providing a GWP of 100

    • A in FIG. 2C: any mass ratio providing a flame velocity of 3.0 cm/s as measured according to ANSI/ASHRAE Standard 34-2013 and a concentration (mass %) of HFO-1123 of 1.0 mass %

    • B in FIG. 2C: any mass ratio providing a concentration (mass %) of HFO-1123 of 1.0 mass % and a refrigerating capacity relative to that of R404A of 85%

    • C in FIG. 2C: any mass ratio providing a refrigerating capacity relative to that of R404A of 85% and a concentration (mass %) of HFO-1132(E) of 1.0 mass %

    • D in FIG. 2C: any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % and a saturation pressure at 40° C. of 2.25 MPa

    • E in FIG. 2C: any mass ratio providing a saturation pressure at 40° C. of 2.25 MPa and a flame velocity of 3.0 cm/s as measured according to ANSI/ASHRAE Standard 34-2013

    • F in FIG. 2C: any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % and a saturation pressure at 40° C. of 2.15 MPa

    • G in FIG. 2C: any mass ratio providing a saturation pressure at 40° C. of 2.15 MPa and a flame velocity of 3.0 cm/s as measured according to ANSI/ASHRAE Standard 34-2013

    • H in FIG. 2C: any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass % and a COP relative to that of R404A of 100%

    • I in FIG. 2C: any mass ratio providing a COP relative to that of R404A of 100% and a saturation pressure at 40° C. of 2.15 MPa

    • a in FIG. 2C: any straight line indicating any mass ratio providing a concentration (mass %) of HFO-1123 of 1.0 mass %

    • b in FIG. 2C: any curve indicating any mass ratio providing a refrigerating capacity relative to that of R404A of 85%

    • c in FIG. 2C: any straight line indicating any mass ratio providing a concentration (mass %) of HFO-1132(E) of 1.0 mass %

    • d in FIG. 2C: any curve indicating any mass ratio providing a saturation pressure at 40° C. of 2.25 MPa

    • e in FIG. 2C: any straight line indicating any mass ratio providing a flame velocity of 3.0 cm/s as measured according to ANSI/ASHRAE Standard 34-2013

    • f in FIG. 2C: any curve indicating any mass ratio providing a saturation pressure at 40° C. of 2.15 MPa

    • g in FIG. 2C: any curve indicating any mass ratio providing a COP relative to that of R404A of 100%


    • 1 in FIG. 1T: Charge line


    • 2 in FIG. 1T: Sampling line


    • 3 in FIG. 1T: Thermometer


    • 4 in FIG. 1T: Pressure gauge


    • 5 in FIG. 1T: Electrode


    • 6 in FIG. 1T: Stirring blade (made of PTFE)


    • 1 in FIG. 2E: Ignition source


    • 2 in FIG. 2E: Sample inlet


    • 3 in FIG. 2E: Springs


    • 4 in FIG. 2E: 12-liter glass flask


    • 5 in FIG. 2E: Electrodes


    • 6 in FIG. 2E: Stirrer


    • 7 in FIG. 2E: Insulated chamber





CITATION LIST
Patent Literature



  • PTL 1: International Publication No. 2015/141678

  • PTL 2: Japanese Unexamined Patent Application Publication No. 2018-184597


Claims
  • 1. A refrigerant cycle apparatus for freezing or cold storage comprising: a refrigerant circuit including a compressor, a radiator, a decompressing portion, and a heat absorber; anda refrigerant enclosed in the refrigerant circuit and containing at least 1,2-difluoroethylene.
  • 2. The refrigeration cycle apparatus for freezing or cold storage according to claim 1, wherein the refrigerant contains CO2, trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (R1234yf); wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z, if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass % are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B″D and straight line CI):point I (0.0, 72.0, 28.0-w)point J (18.3, 48.5, 33.2-w)point K (36.8, 35.6, 27.6-w)point L (51.7, 28.9, 19.4-w)point B″ (−1.5278w2+2.75w+50.5, 0.0, 1.5278w2-3.75w+49.5)point D (−2.9167w+40.317, 0.0, 1.9167w+59.683)point C (0.0, −4.9167w+58.317, 3.9167w+41.683); if 1.2<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding the points on straight line B″D and straight line CI):point I (0.0, 72.0, 28.0-w)point J (18.3, 48.5, 33.2-w)point K (36.8, 35.6, 27.6-w)point L (51.7, 28.9, 19.4-w)point B″ (51.6, 0.0, 48.4-w)point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)point C (0.0, 0.1081w2-5.169w+58.447, −0.1081w2+4.169w+41.553); and if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, curve KL, straight line LB″, straight line B″D, straight line DC, and straight line CI that connect the following 7 points or on these line segments (excluding points on straight line B″D and straight line CI):point I (0.0, 72.0, 28.0-w)point J (18.3, 48.5, 33.2-w)point K (36.8, 35.6, 27.6-w)point L (51.7, 28.9, 19.4-w)point B″ (51.6, 0.0, 48.4-w)point D (−2.8w+40.1, 0.0, 1.8w+59.9)point C (0.0, 0.0667w2-4.9667w+58.3, −0.0667w2+3.9667w+41.7),and curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28-w),curve JK is represented by coordinates (x, 0.0095x2−1.2222x+67.676, −0.0095x2+0.2222x+32.324-w), andcurve KL is represented by coordinates (x, 0.0049x2−0.8842x+61.488, −0.0049x2−0.1158x+38.512).
  • 3. The refrigeration cycle apparatus for freezing or cold storage according to claim 1, wherein the refrigerant contains CO2, trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), and 2,3,3,3-tetrafluoro-1-propene (R1234yf);wherein when the mass % of CO2, R32, HFO-1132(E), and R1234yf based on their sum in the refrigerant is respectively represented by w, x, y, and z, if 0<w≤1.2, coordinates (x,y,z) in a ternary composition diagram in which the sum of R32, HFO-1132(E), and R1234yf is (100-w) mass % are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):point I (0.0, 72.0, 28.0-w)point J (18.3, 48.5, 33.2-w)point K (36.8, 35.6, 27.6-w)point F (−0.0833w+36.717, −4.0833w+5.1833, 3.1666w+58.0997)point C (0.0, −4.9167w+58.317, 3.9167w+41.683); if 1.2<w≤1.3, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KF, straight line FC, and straight line CI that connect the following 5 points or on these line segments (excluding points on straight line CI):point I (0.0, 72.0, 28.0-w)point J (18.3, 48.5, 33.2-w)point K (36.8, 35.6, 27.6-w)point F (36.6, −3w+3.9, 2w+59.5)point C (0.0, 0.1081w2-5.169w+58.447, −0.1081w2+4.169w+41.553); if 1.3<w≤4.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line CI):point I (0.0, 72.0, 28.0-w)point J (18.3, 48.5, 33.2-w)point K (36.8, 35.6, 27.6-w)point B′(36.6, 0.0, −w+63.4)point D (−2.8226w+40.211, 0.0, 1.8226w+59.789)point C (0.0, 0.1081w2-5.169w+58.447, −0.1081w2+4.169w+41.553); and if 4.0<w≤7.0, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by curve IJ, curve JK, straight line KB′, straight line B′D, straight line DC, and straight line CI that connect the following 6 points or on these line segments (excluding points on straight line CI):point I (0.0, 72.0, 28.0-w)point J (18.3, 48.5, 33.2-w)point K (36.8, 35.6, 27.6-w)point B′ (36.6, 0.0, −w+63.4)point D (−2.8w+40.1, 0.0, 1.8w+59.9)point C (0.0, 0.0667w2-4.9667w+58.3, −0.0667w2+3.9667w+41.7),and curve IJ is represented by coordinates (x, 0.0236x2−1.716x+72, −0.0236x2+0.716x+28-w), andcurve JK is represented by coordinates (x, 0.0095x2−1.2222x+67.676, −0.0095x2+0.2222x+32.324-w).
  • 4. A refrigerant cycle apparatus for freezing or cold storage comprising: a refrigerant circuit including a compressor, a radiator, a decompressing portion, and a heat absorber; anda refrigerant enclosed in the refrigerant circuit,
  • 5. The refrigeration cycle apparatus for freezing or cold storage according to claim 4, wherein a content rate of HFO-1132(E) is 31.1 to 37.9 mass % and a content rate of HFO-1234yf is 68.9 to 62.1 mass %, based on a total mass of HFO-1132(E) and HFO-1234yf.
  • 6. A refrigerant cycle apparatus for freezing or cold storage comprising: a refrigerant circuit including a compressor, a radiator, a decompressing portion, and a heat absorber; anda refrigerant enclosed in the refrigerant circuit,
  • 7. A refrigerant cycle apparatus for freezing or cold storage comprising: a refrigerant circuit including a compressor, a radiator, a decompressing portion, and a heat absorber; anda refrigerant enclosed in the refrigerant circuit,
Priority Claims (11)
Number Date Country Kind
2018-134448 Jul 2018 JP national
2018-227398 Dec 2018 JP national
2018-230259 Dec 2018 JP national
2019-013974 Jan 2019 JP national
2019-013979 Jan 2019 JP national
2019-018617 Feb 2019 JP national
2019-078133 Apr 2019 JP national
2019-084708 Apr 2019 JP national
2019-112406 Jun 2019 JP national
2019-115584 Jun 2019 JP national
PCT/JP2019/027031 Jul 2019 WO international
Continuation in Parts (1)
Number Date Country
Parent 17260762 Jan 2021 US
Child 18431360 US