COMPOSITION CONTAINING REFRIGERANT, USE OF SAME, REFRIGERATOR HAVING SAME, AND METHOD FOR OPERATING SAID REFRIGERATOR

Information

  • Patent Application
  • 20220177763
  • Publication Number
    20220177763
  • Date Filed
    December 16, 2021
    2 years ago
  • Date Published
    June 09, 2022
    a year ago
Abstract
An object is to provide a novel low-GWP mixed refrigerant.
Description
TECHNICAL FIELD

The present disclosure relates to a composition comprising a refrigerant, use of the composition, a refrigerating machine comprising the composition, and a method for operating the refrigerating machine.


BACKGROUND ART

R410A is currently used as an air conditioning refrigerant for home air conditioners etc. R410A is a two-component mixed refrigerant of difluoromethane (CH2F2: HFC-32 or R32) and pentafluoroethane (C2HF5: HFC-125 or R125), and is a pseudo-azeotropic composition.


However, the global warming potential (GWP) of R410A is 2088. Due to growing concerns about global warming, R32, which has a GWP of 675, has been increasingly used.


For this reason, various low-GWP mixed refrigerants that can replace R410A have been proposed (PTL 1).


CITATION LIST
Patent Literature

PTL 1: WO2015/141678


SUMMARY

A composition comprising a refrigerant, the refrigerant comprising trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), 1,3,3,3-tetrafluoropropene (R1234ze), and carbon dioxide (CO2).


Advantageous Effects

The refrigerant according to the present disclosure has a low GWP.





BRIEF DESCRIPTION OF DRAWINGS


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



FIG. 2 is a diagram showing points L, L′, M, N, O, K, J″, J′, I″, I′, H′, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is 100 mass %.



FIG. 3 is a diagram showing points L, L′, M, N, O, K, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is 100 mass %.



FIG. 4 is a diagram showing points L, L′, M, N, O, K, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is 99.6 mass % (CO2 is present in an amount of 0.4 mass %).



FIG. 5 is a diagram showing points L, L′, M, N, O, K′, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is 99.0 mass % (CO2 is present in an amount of 1.0 mass %).



FIG. 6 is a diagram showing points L, L′, M, N, O, K′, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is 98.0 mass % (CO2 is present in an amount of 2.0 mass %).



FIG. 7 is a diagram showing points L, L′, M, N, O, K′, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is 97.0 mass % (CO2 is present in an amount of 3.0 mass %).



FIG. 8 is a diagram showing points L, L′, M, N, O, K, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is 96.0 mass % (CO2 is present in an amount of 4.0 mass %).



FIG. 9 is a diagram showing points L, L′, M, N, O, K, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is 95.0 mass % (CO2 is present in an amount of 5.0 mass %).



FIG. 10 is a diagram showing points L, L′, M, N, O, K, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132 (E), R32, and R1234ze is 94.5 mass % (CO2 is present in an amount of 5.5 mass %).



FIG. 11 is a diagram showing points L, L′, M, N, O, K, and H, and line segments that connect these points in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is 92.5 mass % (CO2 is present in an amount of 7.5 mass %).



FIG. 12 is a diagram showing points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, and line segments that connect these points in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is 100 mass %.



FIG. 13 is a diagram showing points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, and line segments that connect these points in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is 99.6 mass %.



FIG. 14 is a diagram showing points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, and line segments that connect these points in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is 99.0 mass %.



FIG. 15 is a diagram showing points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, and line segments that connect these points in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is 98.0 mass %.



FIG. 16 is a diagram showing points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, and line segments that connect these points in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is 97.0 mass %.



FIG. 17 is a diagram showing points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, and line segments that connect these points in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is 96.0 mass %.



FIG. 18 is a diagram showing points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, and line segments that connect these points in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is 95.0 mass %.



FIG. 19 is a diagram showing points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, and line segments that connect these points in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is 94.0 mass %.



FIG. 20 is a diagram showing points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, and line segments that connect these points in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is 92.5 mass %.





DESCRIPTION OF EMBODIMENTS

The present inventors conducted intensive studies to solve the above problem, and consequently found that a mixed refrigerant comprising trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), 1,3,3,3-tetrafluoropropene (R1234ze), and carbon dioxide (CO2) has the above properties.


The present disclosure has been completed as a result of further research based on this finding. The present disclosure includes the following embodiments.


Definition of Terms

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


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


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


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


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


In the present specification, a refrigerant having a “WCF lower flammability” means that the most flammable composition (worst case of formulation for flammability: WCF) has a burning velocity of 10 cm/s or less according to the US ANSI/ASHRAE Standard 34-2013.


1. Refrigerant
1.1 Refrigerant Component

The refrigerant according to the present disclosure comprises trans-1,2-difluoroethylene (HFO-1132(E)), trifluoroethylene (HFO-1123), difluoromethane (R32), 2,3,3,3-tetrafluoro-1-propene (R1234yf), and carbon dioxide (CO2).


The refrigerant according to the present disclosure has a low GWP.


The refrigerant is preferably as follows: in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,


(1) if 0<a≤0.4, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MN, NO, OK, KH, and HL that connect 7 points, i.e., points L, L′, M, N, O, K, and H, or on the straight lines LL′, L′M, MN, NO, OK, and KH (excluding the points L and H):


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point K (−2.5a+1.0, −0.25a+51.5, 1.75a+47.5), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


(2) if 0.4≤a≤7.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines LL′, L′M, MN, NO, OB″, B″K′, K′H, and HL that connect 8 points, i.e., points L, L′, M, N, O, B″, K′, and H, or on the straight lines LL′, L′M, MN, NO, OB″, and K′H (excluding the points L, B″, K′, and H), and


if 0.4≤a≤1.0, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0.0, −3.0a+52.6, 2.0a+47.4), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


if 1.0<a≤3.0, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+36.679, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0, −2.9a+52.5, 1.9a+47.5), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),


if 3.0<a≤5.0, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0, −2.9a+52.5, 1.9a+47.5), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), or


if 5.0<a≤7.5, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0, −2.8286a+52.105, 1.8286a+47.895), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).


In this case, the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 350 or less, and is classified under the category of WCF lower flammability.


The refrigerant is preferably as follows: in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,


(1) if 0<a≤5.5, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MN, NJ, JH, and HL that connect 6 points, points L, L′, M, N, J, and H, or on the straight lines LL′, L′M, MN, NJ, and JH (excluding the points L and H), and


if 0<a≤1.0, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (−0.3333a2−3.3667a+20.3, 36.6, 0.3333a2+2.3667a+43), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


if 1.0<a≤3.0, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (0.05a2−3.95a+20.5, 0.05a2−0.25a+36.8, −0.1a2+3.2a+42.7), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),


if 3.0<a≤5.0, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (0.05a2−4.05a+20.8, 36.5, −0.05a2+3.05a+42.7), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), or


if 5.0<a≤5.5, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (−3.6a+19.8, 36.5, 2.6a+43.7), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25),


(2) if 5.5<a≤7.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines LL′, L′M, MN, NB′, B′K′, K′H, and HL that connect 7 points, i.e., points L, L′, M, N, B′, K′, and H, or on the straight lines LL′, L′M, MN, NB′, K′H, and HL (excluding the points L, B′, K′, and H):


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point B′ (0.0, 36.5, −a+63.5),


point K′ (0.0, −2.8286a+52.105, 1.8281a+47.895), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).


In this case, the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 250 or less, and is classified under the category of WCF lower flammability.


The refrigerant is preferably as follows: in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,


coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132 (E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MI, IH, and HL that connect 5 points, i.e., points L, L′, M, I, and H, or on the straight lines LL′, L′M, MI, and IH (excluding the points L and H), and


if 0<a≤1.0, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (−0.1667a2−3.9333a+44.2, 18.1, 0.1667a2+2.9333a+37.7), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


if 1.0<a≤3.0, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (0.05a2−4.25a+44.3, 18.1, −0.05a2+3.25a+37.6), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),


if 3.0<a≤5.0, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (−0.05a2−3.45a+42.8, 0.05a2−0.45a+19.0, 2.9a+38.2), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), or


if 5.0<a≤7.5, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (0.1a2−4.85a+46.05, −0.02a2+0.21a+17.45, −0.08a2+3.64a+36.5), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).


In this case, the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 125 or less, and is classified under the category of WCF lower flammability.


The refrigerant according to the present disclosure may further comprise 2,3,3,3-tetrafluoro-1-propene (R1234yf).


When the refrigerant according to the present disclosure further comprises R1234yf, the refrigerant is preferably as follows: when the mass % of HFO-1132(E) is x, the mass % of R32 is y, the mass % of the sum of R1234ze and R1234yf is z, and the mass % of CO2 is a based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2,


if r=R1234yf/(R1234ze+R1234yf), and 0.1<r<1.0, coordinates (x,y,z) in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines LrL′r, L′rMr, MrNr, NrOr, OrB″r, B″rK′r, K′rHr, and HrLr that connect 8 points, i.e., points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, or on the straight lines LrL′r, L′rMr, MrNr, NrOr, OrB″r, and K′rHr (excluding the points Lr, B″r, K′r, and Hr), and


if 0<a≤1.0, the 8 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, −0.2778r2+0.4167r+18.061, 51.4−a−y),


point Nr (35.7, −0.2778r2+0.4167r+36.661, 51.4−a−y),


point Or (28.9, −0.2222r2−0.1333r+51.611, 71.1−a−y),


point B″r (0.0, (0.463a2−0.1852a−0.2778)r2+(−0.6945a2+0.2778a+0.4167)r+(0.2317a2−0.0927a+51.361), 51.4−a−y),


point K′r (0.0, (0.3705a2−0.1482a−0.6667)r2+(−0.2217a2+0.0887a−11.6)r+(0.0183a2−3.0073a+52.567), 100−a−y), and


point Hr ((2.4072a2−2.0739a−0.8889)r2+(−2.2779a2+1.5779a−8.4667)r+(0.0392a2−4.5732a+67.656), 0.0, 100−a−x),


if 1.0<a≤3.0, the 8 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (−0.1389a2+0.6945a−0.8334)r2+(0.2084a2−1.0418a+1.2501)r+(−0.0695a2+0.3475a+17.783), 51.4−a−y),


point Nr (35.7, −0.2778r2+0.4167r+36.661, 51.4−a−y),


point Or (28.9, (0.25a2−1.25a+1.2222)r2+(−0.275a2+1.375a−1.2333)r+(0.025a2−0.125a+51.711), 71.1−y−a),


point B″r (0.0, (0.25a2−1.0278a+0.7778)r2+(−0.275a2+1.2419a−0.9668)r+(0.075a2−0.364a+51.789), 100−a−y),


point K′r (0.0, (0.16667a2+0.2222a−0.8333)r2+(−0.3495a2+0.3645a−11.748)r+(0.1335a2−3.2395a+52.684), 100−a−y), and


point Hr ((−0.25003a2+0.8613a−1.1669)r2+(0.275a2−1.3914a−8.0502)r+(0.0245a2−4.4175a+67.515), 0.0, 100−a−x),


if 3.0<a≤5.0, the 8 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, 18.2, 33.2−a),


point Nr (35.7, (−0.1389a2+1.2501a−2.778)r2+(0.2084a2−1.8752a+4.167)r+(−0.0695a2+0.6255a+35.41), 51.4−a−y),


point Or (28.9, (0.1389a2−0.9723a+1.389)r2+(−0.2083a2+1.4585a−2.0845)r+(0.0695a2−0.4865a+52.395), 71.1−a−y),


point B″r (0.0, −0.0556r2+0.2833r+51.372, 100−a−y),


point K′r (0.0, (0.77775a2−6.2775a+13.166)r2+(−0.9665a2+8.0155a−29.148)r+(0.189a2−4.54a+56.086), 100−a−y), and


point Hr ((−0.72215a2+6.3327a−13.332)r2+(0.6835a2−6.3015a+3.003)r+(0.039a2−4.434a+67.434), 0.0, 100−x−a), or


if 5.0<a≤7.5, the 8 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (0.0592a2−0.6512a+1.776)r2+(−0.0355a2+0.3901a−1.062)r+(0.0029a2−0.0323a+18.29), 51.4−a−y),


point Nr (35.7, 36.8, 27.5−a),


point Or (28.9, 51.7, 19.4−a),


point B″r (0.0, −0.0556r2+0.2833r+51.372, 100−a−y),


point K′r (0.0, (0.10373a2−0.9189a+3.2232)r2+(−0.1285a2+1.2799a−16.419)r+(0.0252a2−3.1662a+53.312), 100−a−y), and


point Hr ((0.037a2−0.1293a−0.0008)r2+(−0.056a2+0.2a−11.017)r+(0.0719a2−4.8515a+68.7), 0.0, 100−a−x).


In this case, the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 350 or less, and is classified under the category of WCF lower flammability.


When the refrigerant according to the present disclosure further comprises R1234yf, the refrigerant is preferably as follows: when the mass % of HFO-1132(E) is x, the mass % of R32 is y, the mass % of the sum of R1234ze and R1234yf is z, and the mass % of CO2 is a based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2,


if r=R1234yf/(R1234ze+R1234yf), and 0.1≤r<1.0, coordinates (x,y,z) in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines LrL′r, L′rMr, MrIr, IrHr, and HrLr that connect 5 points, i.e., points Lr, L′r, Mr, Ir, and Hr, or on the straight lines LrL′r, L′rMr, MrIr, and IrHr, and


if 0<a≤1.0, the 5 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, −0.2778r2+0.4167r+18.061, 51.4−a−y),


point Ir ((1.1576a2−0.3243a−2.1111)r2+(−0.9a2−0.35a−10.233)r+(−0.255a2−3.828a+44.244), 100−a−x−z, (1.1572a2+0.3239a+1.8889)r2+(0.9042a2+0.3458a+10.367)r+(0.2525a2+2.8315a+37.644)), and


point Hr ((2.4072a2−2.0739a−0.8889)r2+(−2.2779a2+1.5779a−8.4667)r+(0.0392a2−4.5732a+67.656), 0.0, 100−a−x),


if 1.0<a≤3.0, the 5 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (−0.1389a2+0.6945a−0.8334)r2+(0.2084a2−1.0418a+1.2501)r+(−0.0695a2+0.3475a+17.783), 51.4−a−y),


point Ir ((−0.08337a2+0.8057a−2.0001)r2+(−0.0745a2−0.6105a−10.798)r+(0.108a2−4.346a+44.399), 100−a−x−z, (0.33337a2−1.5557a+2.2779)r2+(−0.225a2+1.508a+10.334)r+(−0.033a2+3.121a+37.64)), and


point Hr ((−0.25003a2+0.8613a−1.1669)r2+(0.275a2−1.3914a−8.0502)r+(0.0245a2−4.4175a+67.515), 0.0, 100−a−x),


if 3.0<a≤5.0, the 5 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, 18.2, 31.2−a),


point Ir ((−0.05554a2+0.8332a−2.3331)r2+(−0.2165a2+1.2485a−15.097)r+(0.1715a2−5.2775a+46.622), 100−a−x−z, (0.0556a2−0.8329a+2.6103)r2+(0.1915a2−1.0235a+14.18)r+(−0.1715a2+4.2775a+35.417)), and


point Hr ((−0.72215a2+6.3327a−13.332)r2+(0.6835a2−6.3015a+3.003)r+(0.039a2−4.434a+67.434), 0.0, 100−a−x), or


if 5.0<a≤7.5, the 5 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (0.0592a2−0.6512a+1.776)r2+(−0.0355a2+0.3901a−1.062)r+(0.0029a2−0.0323a+18.29), 51.4−a−y),


point Ir ((0.19254a2−1.8957a+5.1093)r2+(−0.3156a2+3.3386a−23.07)r+(0.1097a2−4.9961a+46.759), 100−a−x−z, (−0.0074a2−0.4187a+2.1117) r2+(0.0379a2+0.1335a+12.236) r+(−0.0571a2+3.3777a+37.055)), and


point Hr ((0.037a2−0.1293a−0.0008)r2+(−0.056a2+0.2a−11.017)r+(0.0719a2−4.8515a+68.7), 0.0, 100−x−a).


In this case, the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 125 or less, and is classified under the category of WCF lower flammability.


The refrigerant according to the present disclosure may further comprise other additional refrigerants in addition to HFO-1132 (E), R32, R1234ze, CO2, and R1234yf as long as the above properties and effects are not impaired. In this respect, the refrigerant according to the present disclosure preferably comprises HFO-1132(E), R32, R1234ze, and CO2 in a total amount of 99.5 mass % or more, more preferably 99.75 mass % or more, and even more preferably 99.9 mass % or more, based on the entire refrigerant. Further, the refrigerant according to the present disclosure may comprise HFO-1132(E), R32, R1234ze, CO2, and R1234yf in a total amount of 99.5 mass % or more, 99.75 mass % or more, or 99.9 mass % or more, based on the entire refrigerant.


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


1.2 Use

The refrigerant according to the present disclosure can be preferably used as a working fluid in a refrigerating machine.


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


2. 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 %.


2.1 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.


2.2 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.


Specifically, 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, CF3CH2F)


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


HFE-227ea (trifluoromethyl-tetrafluoroethyl ether, CF3CHFCF3)


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


The refrigerant composition according to the present disclosure may contain a tracer in a total amount 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 a tracer in a total amount of about 30 ppm to about 500 ppm, and more preferably about 50 ppm to about 300 ppm, based on the entire refrigerant composition.


2.3 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.


2.4 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.


2.5 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.


3. 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.


3.1 Refrigeration Oil

The refrigeration oil-containing working fluid 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, can be 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.


3.2 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.


4. Method for Operating Refrigerating Machine

The method for operating a refrigerating machine according to the present disclosure is a method for operating a refrigerating machine using the refrigerant according to the present disclosure.


Specifically, the method for operating a refrigerating machine according to the present disclosure comprises circulating the refrigerant according to the present disclosure in a refrigerating machine.


The embodiments are described above; however, it will be understood that various changes in forms and details can be made without departing from the spirit and scope of the claims.


Item 1.

A composition comprising a refrigerant, the refrigerant comprising trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), 1,3,3,3-tetrafluoropropene (R1234ze), and carbon dioxide (CO2).


Item 2.

The composition according to Item 1, wherein


in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,


(1) if 0<a≤0.4, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MN, NO, OK, KH, and HL that connect 7 points, i.e., points L, L′, M, N, O, K, and H, or on the straight lines LL′, L′M, MN, NO, OK, and KH (excluding the points L and H):


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point K (−2.5a+1.0, −0.25a+51.5, 1.75a+47.5), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


(2) if 0.4≤a≤7.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines LL′, L′M, MN, NO, OB″, B″K′, K′H, and HL that connect 8 points, i.e., points L, L′, M, N, O, B″, K′, and H, or on the straight lines LL′, L′M, MN, NO, OB″, and K′H (excluding the points L, B″, K′, and H), and


if 0.4≤a≤1.0, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0.0, −3.0a+52.6, 2.0a+47.4), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


if 1.0<a≤3.0, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+36.679, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0, −2.9a+52.5, 1.9a+47.5), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),


if 3.0<a≤5.0, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0, −2.9a+52.5, 1.9a+47.5), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), or


if 5.0<a≤7.5, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0, −2.8286a+52.105, 1.8286a+47.895), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25)


Item 3.

The composition according to Item 1,


wherein


in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,


(1) if 0<a≤5.5, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MN, NJ, JH, and HL that connect 6 points, i.e., points L, L′, M, N, J, and H, or on the straight lines LL′, L′M, MN, NJ, and JH (excluding the points L and H), and


if 0<a≤1.0, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (−0.3333a2−3.3667a+20.3, 36.6, 0.3333a2+2.3667a+43), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


if 1.0<a≤3.0, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (0.05a2−3.95a+20.5, 0.05a2−0.25a+36.8, −0.1a2+3.2a+42.7),


and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),


if 3.0<a≤5.0, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (0.05a2−4.05a+20.8, 36.5, −0.05a2+3.05a+42.7), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), or


if 5.0<a≤5.5, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (−3.6a+19.8, 36.5, 2.6a+43.7), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25),


(2) if 5.5<a≤7.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines LL′, L′M, MN, NB′, B′K′, K′H, and HL that connect 7 points, i.e., points L, L′, M, N, B′, K′, and H, or on the straight lines LL′, L′M, MN, NB′, K′H, and HL (excluding the points L, B′, K′, and H):


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point B′ (0.0, 36.5, −a+63.5),


point K′ (0.0, −2.8286a+52.105, 1.8281a+47.895), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).


Item 4.

The composition according to Item 1,


wherein


in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MI, IH, and HL that connect 5 points, i.e., points L, L′, M, I, and H, or on the straight lines LL′, L′M, MI, and IH (excluding the points L and H), and


if 0<a≤1.0, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (−0.1667a2−3.9333a+44.2, 18.1, 0.1667a2+2.9333a+37.7), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


if 1.0<a≤3.0, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (0.05a2−4.25a+44.3, 18.1, −0.05a2+3.25a+37.6), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),


if 3.0<a≤5.0, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (−0.05a2−3.45a+42.8, 0.05a2−0.45a+19.0, 2.9a+38.2), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), or


if 5.0<a≤7.5, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (0.1a2−4.85a+46.05, −0.02a2+0.21a+17.45, −0.08a2+3.64a+36.5), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).


Item 5.

The composition according to any one of Items 1 to 4, wherein the refrigerant further comprises 2,3,3,3-tetrafluoro-1-propene (R1234yf).


Item 6.

The composition according to Item 5,


wherein


in the refrigerant, when the mass % of HFO-1132(E) is x, the mass % of R32 is y, the mass % of the sum of R1234ze and R1234yf is z, and the mass % of CO2 is a based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2,


if r=R1234yf/(R1234ze+R1234yf), and 0.1≤r<1.0, coordinates (x,y,z) in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines LrL′r, L′rMr, MrNr, NrOr, OrB″r, B″rK′ r, K′rHr, and HrLr that connect 8 points, i.e., points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, or on the straight lines LrL′r, L′rMr, MrNr, NrOr, OrB″r, and K′rHr (excluding the points Lr, B″r, K′r, and Hr), and


if 0<a≤1.0, the 8 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, −0.2778r2+0.4167r+18.061, 51.4−a−y),


point Nr (35.7, −0.2778r2+0.4167r+36.661, 51.4−a−y),


point Or (28.9, −0.2222r2−0.1333r+51.611, 71.1−a−y),


point B″r (0.0, (0.463a2−0.1852a−0.2778)r2+(−0.6945a2+0.2778a+0.4167)r+(0.2317a2−0.0927a+51.361), 51.4−a−y),


point K′r (0.0, (0.3705a2−0.1482a−0.6667)r2+(−0.2217a2+0.0887a−11.6)r+(0.0183a2−3.0073a+52.567), 100−a−y), and


point Hr ((2.4072a2−2.0739a−0.8889)r2+(−2.2779a2+1.5779a−8.4667)r+(0.0392a2−4.5732a+67.656), 0.0, 100−a−x),


if 1.0<a≤3.0, the 8 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (−0.1389a2+0.6945a−0.8334)r2+(0.2084a2−1.0418a+1.2501)r+(−0.0695a2+0.3475a+17.783), 51.4−a−y),


point Nr (35.7, −0.2778r2+0.4167r+36.661, 51.4−a−y),


point Or (28.9, (0.25a2−1.25a+1.2222)r2+(−0.275a2+1.375a−1.2333)r+(0.025a2−0.125a+51.711), 71.1−y−a),


point B″r (0.0, (0.25a2−1.0278a+0.7778)r2+(−0.275a2+1.2419a−0.9668)r+(0.075a2−0.364a+51.789), 100−a−y),


point K′r (0.0, (0.16667a2+0.2222a−0.8333)r2+(−0.3495a2+0.3645a−11.748)r+(0.1335a2−3.2395a+52.684), 100−a−y), and


point Hr ((−0.25003a2+0.8613a−1.1669)r2+(0.275a2−1.3914a−8.0502)r+(0.0245a2−4.4175a+67.515), 0.0, 100−a−x),


if 3.0<a≤5.0, the 8 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, 18.2, 33.2−a),


point Nr (35.7, (−0.1389a2+1.2501a−2.778)r2+(0.2084a2−1.8752a+4.167)r+(−0.0695a2+0.6255a+35.41), 51.4−a−y),


point Or (28.9, (0.1389a2−0.9723a+1.389)r2+(−0.2083a2+1.4585a−2.0845)r+(0.0695a2−0.4865a+52.395), 71.1−a−y),


point B″r (0.0, −0.0556r2+0.2833r+51.372, 100−a−y),


point K′r (0.0, (0.77775a2−6.2775a+13.166)r2+(−0.9665a2+8.0155a−29.148)r+(0.189a2−4.54a+56.086), 100−a−y), and


point Hr ((−0.72215a2+6.3327a−13.332)r2+(0.6835a2−6.3015a+3.003)r+(0.039a2−4.434a+67.434), 0.0, 100−x−a), or


if 5.0<a≤7.5, the 8 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (0.0592a2−0.6512a+1.776)r2+(−0.0355a2+0.3901a−1.062)r+(0.0029a2−0.0323a+18.29), 51.4−a−y),


point Nr (35.7, 36.8, 27.5−a),


point Or (28.9, 51.7, 19.4−a),


point B″r (0.0, −0.0556r2+0.2833r+51.372, 100−a−y),


point K′r (0.0, (0.10373a2−0.9189a+3.2232)r2+(−0.1285a2+1.2799a−16.419)r+(0.0252a2−3.1662a+53.312), 100−a−y), and


point Hr ((0.037a2−0.1293a−0.0008)r2+(−0.056a2+0.2a−11.017)r+(0.0719a2−4.8515a+68.7), 0.0, 100−a−x).


Item 7.

The composition according to Item 6,


wherein


in the refrigerant, when the mass % of HFO-1132(E) is x, the mass % of R32 is y, the mass % of the sum of R1234ze and R1234yf is z, and the mass % of CO2 is a based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2,


if r=R1234yf/(R1234ze+R1234yf), and 0.1≤r<1.0, coordinates (x,y,z) in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines LrL′r, L′rMr, MrIr, IrHr, and HrLr that connect 5 points, i.e., points Lr, L′r, Mr, Ir, and Hr, or on the straight lines LrL′r, L′rMr, MrIr, and IrHr, and


if 0<a≤1.0, the 5 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, −0.2778r2+0.4167r+18.061, 51.4−a−y),


point Ir ((1.1576a2−0.3243a−2.1111)r2+(−0.9a2−0.35a−10.233)r+(−0.255a2−3.828a+44.244), 100−a−x−z, (1.1572a2+0.3239a+1.8889) r2+(0.9042a2+0.3458a+10.367) r+(0.2525a2+2.8315a+37.644)), and


point Hr ((2.4072a2−2.0739a−0.8889)r2+(−2.2779a2+1.5779a−8.4667)r+(0.0392a2−4.5732a+67.656), 0.0, 100−a−x),


if 1.0<a≤3.0, the 5 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (−0.1389a2+0.6945a−0.8334)r2+(0.2084a2−1.0418a+1.2501)r+(−0.0695a2+0.3475a+17.783), 51.4−a−y),


point Ir ((−0.08337a2+0.8057a−2.0001)r2+(−0.0745a=−0.6105a−10.798)r+(0.108a2−4.346a+44.399), 100−a−x−z, (0.33337a2−1.5557a+2.2779) r2+(−0.225a2+1.508a+10.334)r+(−0.033a2+3.121a+37.64)), and


point Hr ((−0.25003a2+0.8613a−1.1669)r2+(0.275a2−1.3914a−8.0502)r+(0.0245a2−4.4175a+67.515), 0.0, 100−a−x),


if 3.0<a≤5.0, the 5 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, 18.2, 31.2−a),


point Ir ((−0.05554a2+0.8332a−2.3331)r2+(−0.2165a2+1.2485a−15.097)r+(0.1715a2−5.2775a+46.622), 100−a−x−z, (0.0556a2−0.8329a+2.6103)r2+(0.1915a2−1.0235a+14.18)r+(−0.1715a2+4.2775a+35.417)), and


point Hr ((−0.72215a2+6.3327a−13.332)r2+(0.6835a2−6.3015a+3.003)r+(0.039a2−4.434a+67.434), 0.0, 100−a−x), or


if 5.0<a≤7.5, the 5 points are the following:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (0.0592a2−0.6512a+1.776)r2+(−0.0355a2+0.3901a−1.062)r+(0.0029a2−0.0323a+18.29), 51.4−a−y),


point Ir ((0.19254a2−1.8957a+5.1093)r2+(−0.3156a2+3.3386a−23.07)r+(0.1097a2−4.9961a+46.759), 100−a−x−z, (−0.0074a2−0.4187a+2.1117)r2+(0.0379a2+0.1335a+12.236)r+(−0.0571a2+3.3777a+37.055)), and


point Hr ((0.037a2−0.1293a−0.0008)r2+(−0.056a2+0.2a−11.017)r+(0.0719a2−4.8515a+68.7), 0.0, 100−x−a).


Item 8.

The composition according to any one of Items 1 to 7, for use as a working fluid for a refrigerating machine, wherein the composition further comprises a refrigeration oil.


Item 9.

The composition according to any one of Items 1 to 7, for use as an alternative refrigerant for R410A.


Item 10.

Use of the composition according to any one of Items 1 to 7 as an alternative refrigerant for R410A.


Item 11.

A refrigerating machine comprising the composition according to any one of Items 1 to 7 as a working fluid.


Item 12.

A method for operating a refrigerating machine, comprising circulating the composition according to any one of Items 1 to 7 as a working fluid in a refrigerating machine.


EXAMPLES

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


Example A

Mixed refrigerants were prepared by mixing HFO-1132(E), R32, R1234ze, and CO2 at mass % based on their sum shown in Tables 1 to 6.


The GWP of R410A (R32=50%/R125=50%) and the mixed refrigerants was evaluated based on the values stated in the Intergovernmental Panel on Climate Change (IPCC), fourth report.


The GWP of HFO-1132(E), which was not stated therein, was assumed to be 1 from HFO-1132a (GWP=1 or less) and HFO-1123 (GWP=0.3, described in PTL 1). The refrigerating capacity of R410A and the mixed refrigerants was determined by performing theoretical refrigeration cycle calculations for the mixed refrigerants using the National Institute of Science and Technology (NIST) and Reference Fluid Thermodynamic and Transport Properties Database (Refprop 9.0) under the following conditions.


The COP ratio and the refrigerating capacity ratio of the mixed refrigerants relative to those of R410A were determined. The calculation conditions were as follows.


Evaporating temperature: 5° C.


Condensation temperature: 45° C.


Degree of superheating: 5 K


Degree of subcooling: 5 K


Compressor efficiency: 70%


Tables 1 to 6 show these values together with the GWP of each mixed refrigerant. The COP and refrigerating capacity are ratios relative to R410A.


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






COP
=



(

refrigerating





capacity





or





heating





capacity

)

/
power






consumption





















TABLE 1










Com Ex2
Com Ex3
Com Ex4
Com Ex5
Com Ex6
Com Ex7
Com Ex8


Item
Unit
Com Ex1
H
I
J
K
A
B
A′





HFO-1132 (E)
mass %
R410A
67.6
44.2
20.3
1.0
81.6
0.0
63.0


R32
mass %

0.0
18.1
35.6
51.5
18.4
17.8
37.0


R1234ze
mass %

32.4
37.7
43.1
47.5
0.0
82.2
0.0


CO2
mass %

0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

2088
3
125
250
350
125
125
250


COP ratio
% (relative to R410A)
100
101.4
101.7
103.0
104.5
98.7
107.8
98.7


Refrigerating
% (relative to R4104)
100
80.0
82.8
82.5
80.0
105.3
52.1
110.0


Capacity Ratio











Condensation Glide
° C.
0.1
4.5
6.6
7.4
6.9
0.3
10.4
0.1







Com Ex9
Com Ex10
Com Ex11
Com Ex12
Com Ex13
Com Ex14
Com Ex15
Com Ex16


Item
Unit
B′
A″
B″
L
L′
M
N
O





HFO-1132 (E)
mass %
0.0
48.2
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
36.5
51.8
51.4
0.0
10.0
18.1
36.7
51.6


R1234ze
mass %
63.5
0.0
48.6
28.0
32.8
33.3
27.6
19.5


CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

250
350
350
2
70
125
250
350


COP ratio
% (relative to R410A)
106.2
99.2
104.6
101.1
101.2
101.2
101.0
100.9


Refrigerating
% (relative to R410A)
68.0
112.1
79.2
82.6
83.4
85.5
92.8
99.7


Capacity Ratio











Condensation Glide
° C
9.5
0.0
7.0
3.9
5.4
5.8
4.7
3.0




















Com Ex17
Com Ex18
Com Ex19
Com Ex20
Com Ex21


Item
Unit
Com Ex1
H′
I′
I″
J′
J″





HFO-1132 (E)
mass %
R410A
51.5
39.8
27.6
16.7
8.6


R32
mass %

10.0
18.1
27.3
36.5
44.0


R1234ze
mass %

38.5
42.1
45.1
46.8
47.4


CO2
mass %

0.0
0.0
0.0
0.0
0.0


GWP

2088
70
125
187
249
300


COP ratio
% (relative to R410A)
100
101.8
102.3
102.9
103.5
104.0


Refrigerating
% (relative to R4104)
100
80.0
80.0
80.0
80.0
80.0


Capacity Ratio









Condensation Glide
° C.
0.1
6.4
7.4
8.0
7.9
7.5





















Com Ex22
Example1
Example2
Com Ex23
Com Ex24
Com Ex25
Com Ex26
Com Ex27


Item
Unit
H
I
J
K′ = B″
A
B
A′
B′





HFO-1132 (E)
mass %
65.8
42.6
18.9
0.0
81.2
0.0
62.6
0.0


R32
mass %
0.0
18.1
36.6
51.4
18.4
17.8
37.0
36.5


R1234ze
mass %
33.8
38.9
44.1
48.2
0.0
81.8
0.0
63.1


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

3
125
250
350
125
125
250
250


COP ratio
% (relative to R410A)
101.3
101.7
103.0
104.5
98.5
107.6
98.5
106.0


Refrigerating
% (relative to R410A)
80.0
82.8
82.5
80.0
106.1
53.0
110.7
68.9


Capacity Ratio











Condensation Glide
° C.
5.4
7.3
7.9
7.3
0.6
11.1
0.3
9.9























TABLE 2









Com Ex28
Com Ex29
Example3
Example4
Example5
Example6


Item
Unit
A″
L
L′
M
N
O





HFO-1132 (E)
mass %
47.8
72.0
57.2
48.6
35.7
28.9


R32
mass %
51.8
0.0
10.0
18.1
36.7
51.6


R1234ze
mass %
0.0
27.6
32.4
32.9
27.2
19.1


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4


GWP

350
2
70
125
250
350


COP ratio
% (relative to R410A)
99.0
100.8
100.9
100.9
100.8
100.8


Refrigerating
% (relative to R410A)
112.8
83.6
84.5
86.5
93.7
100.6


Capacity Ratio









Condensation Glide
° C.
0.2
4.4
5.8
6.1
4.9
3.2





















Com Ex30
Example7
Example8
Com Ex31
Com Ex32
Com Ex33
Com Ex34
Com Ex35


Item
Unit
H
I
J
K′
A
B
A′
B′





HFO-1132 (E)
mass %
63.2
40.1
16.6
0.0
80.6
0.0
62.0
0.0


R32
mass %
0.0
18.1
36.6
49.6
18.4
17.8
37.0
36.5


R1234ze
mass %
35.8
40.8
45.8
49.4
0.0
81.2
0.0
62.5


CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

3
125
250
338
125
125
250
250


COP ratio
% (relative to R410A)
101.1
101.6
103.0
104.3
98.2
107.4
98.2
105.7


Refrigerating
% (relative to R410A)
80.0
82.6
82.2
80.0
107.3
54.3
111.8
70.2


Capacity Ratio











Condensation Glide
° C.
6.5
8.2
8.7
8.1
1.0
12.1
0.7
10.5




















Com Ex36
Com Ex37
Com Ex38
Example9
Example10
Example11
Example12


Item
Unit
A″
B″
L
L′
M
N
O





HFO-1132 (E)
mass %
47.2
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
51.8
51.4
0.0
10.0
18.1
36.7
51.6


R1234ze
mass %
0.0
47.6
27.0
31.8
32.3
26.6
18.5


CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

350
350
2
70
125
250
350


COP ratio
% (relative to R410A)
98.8
104.2
100.4
100.5
100.6
100.5
100.5


Refrigerating
% (relative to R410A)
113.8
81.3
85.3
86.0
88.0
95.1
101.9


Capacity Ratio










Condensation Glide
° C.
0.5
7.7
5.1
6.4
6.6
5.2
3.5

























TABLE 3









Com Ex39
Example13
Example14
Com Ex40
Com 41
Com Ex42
Com Ex43
Com Ex44


Item
Unit
H
I
J
K′
A
B
A′
B′





HFO-1132 (E)
mass %
58.8
36.0
12.8
0.0
79.6
0.0
61.0
0.0


R32
mass %
0.0
18.1
36.5
46.7
18.4
17.8
37.0
36.5


R1234ze
mass %
39.2
43.9
48.7
51.3
0.0
80.2
0.0
61.5


CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

3
125
250
318
125
125
250
250


COP ratio
% (relative to R410A)
101
101.7
103.2
104.2
97.7
107.0
97.8
105.2


Refrigerating
% (relative to R410A)
80.0
82.4
81.7
80.0
109.3
56.5
113.6
72.3


Capacity Ratio











Condensation Glide
° C.
8.5
9.8
10.0
9.4
1.7
13.6
1.2
11.4




















Com Ex45
Com Ex46
Com Ex47
Example15
Example16
Example17
Example18


Item
Unit
A″
B″
L
L″
M
N
O





HFO-1132 (E)
mass %
46.2
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
51.8
51.4
0.0
10.0
18.1
36.7
51.6


R1234ze
mass %
0.0
46.6
26.0
30.8
31.3
25.6
17.5


CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

350
350
2
70
125
250
350


COP ratio
% (relative to R410A)
98.4
103.8
99.7
99.9
100.0
100.0
100.1


Refrigerating
% (relative to R410A)
115.5
83.5
88.0
83.5
90.4
97.5
104.2


Capacity Ratio










Condensation Glide
° C.
1.0
8.4
6.2
7.2
7.3
5.8
3.9





















Com Ex 48
Example19
Example20
Com Ex49
Com Ex50
Com Ex51
Com Ex52
Com Ex53


Item
Unit
H
I
J
K′
A
B
A′
B′





HFO-1132 (E)
mass %
54.5
32.0
9.1
0.0
78.6
0.0
60.0
0.0


R32
mass %
0.0
18.1
36.5
43.8
18.4
17.8
37.0
36.5


R1234ze
mass %
42.5
46.9
51.4
53.2
0.0
79.2
0.0
60.5


CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

3
125
250
299
125
125
250
250


COP ratio
% (relative to R410A)
100.7
101.7
103.3
104.0
97.2
106.6
97.4
104.8


Refrigerating
% (relative to R410A)
80.0
82.2
81.3
80.0
111.3
58.8
115.5
74.5


Capacity Ratio











Condensation Glide
° C.
10.4
11.4
11.2
10.7
2.4
15.1
1.7
12.3




















Com Ex54
Com Ex55
Com Ex56
Example21
Example22
Example23
Example24


Item
Unit
A″
B″
L
L′
M
N
O





HFO-1132 (E)
mass %
45.2
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
51.8
51.4
0.0
10.0
18.1
36.7
51.6


R1234ze
mass %
0.0
45.6
25.0
29.8
30.3
24.6
16.5


CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

350
350
2
70
125
250
350


COP ratio
% (relative to R410A)
98.1
103.4
99.1
99.4
99.5
99.5
99.6


Refrigerating
% (relative to R410A)
117.2
85.6
90.6
91.1
92.9
99.8
106.5


Capacity Ratio










Condensation Glide
° C.
1.5
9.0
7.1
8.0
7.9
6.2
4.3

























TABLE 4









Com Ex57
Example25
Example26
Com Ex58
Com Ex59
Com Ex60
Com Ex61
Com Ex62


Item
Unit
H
I
J
K′
A
B
A′
B′





HFO-1132 (E)
mass %
50.3
28.2
5.4
0.0
77.6
0.0
59.0
0.0


R32
mass %
0.0
18.0
36.5
40.9
18.4
17.8
37.0
36.5


R1234ze
mass %
45.7
49.8
54.1
55.1
0.0
78.2
0.0
59.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

3
125
250
279
125
125
250
250


COP ratio
% (relative to R410A)
100.7
101.9
103.5
103.9
96.7
106.3
97.0
104.4


Refrigerating
% (relative to R410A)
80.0
82.0
80.8
80.0
113.3
61.1
117.3
76.7


Capacity Ratio











Condensation Glide
° C.
12.3
13.0
12.4
12.0
3.0
16.4
2.2
13.0




















Com Ex63
Com Ex64
Com Ex65
Example27
Example28
Example29
Example30


Item
Unit
A″
B″
L
L′
M
N
O





HFO-1132 (E)
mass %
44.2
0.0
72.0
57.2
48.5
35.7
28.9


R32
mass %
51.8
51.4
0.0
10.0
18.2
36.7
51.6


R1234ze
mass %
0.0
44.6
24.0
28.8
29.3
23.6
15.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

350
350
2
70
125
250
350


COP ratio
% (relative to R410A)
97.7
103.0
98.5
98.8
99.0
99.1
99.2


Refrigerating
% (relative to R410A)
118.9
87.8
93.3
93.6
95.3
102.1
108.8


Capacity Ratio










Condensation Glide
° C.
2.0
9.6
7.9
8.7
8.5
6.6
4.7

























TABLE 5









Com Ex66
Example31
Example32
Com Ex67
Com Ex68
Com Ex69
Com Ex70
Com Ex71


Item
Unit
H
I
J
K′
A
B
A′
B′





HFO-1132 (E)
mass %
46.2
24.3
1.8
0.0
76.6
0.0
58.0
0.0


R32
mass %
0.0
18.0
36.5
38.0
18.4
17.8
37.0
36.5


R1234ze
mass %
48.8
52.7
56.7
57.0
0.0
77.2
0.0
58.5


CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

3
125
250
260
125
125
250
250


COP ratio
% (relative to R410A)
101
102.1
103.7
103.8
96.2
106.0
96.6
104.0


Refrigerating
% (relative to R410A)
80
81.7
80.2
80.0
115.2
63.4
119.1
78.8


Capacity Ratio











Condensation Glide
° C.
14.1
14.5
13.5
13.4
3.5
17.6
2.6
13.8




















Com Ex72
Com Ex73
Com Ex74
Example33
Example34
Example35
Example36


Item
Unit
A″
B″
L
L′
M
N
O





HFO-1132 (E)
mass %
43.2
0.0
72.0
57.2
48.5
35.6
28.9


R32
mass %
51.8
51.4
0.0
10.0
18.2
36.8
51.6


R1234ze
mass %
0.0
43.6
23.0
27.8
28.3
22.6
14.5


CO2
mass %
5.0
50
5.0
5.0
5.0
5.0
5.0


GWP

350
350
2
70
125
250
350


COP ratio
% (relative to R410A)
97.4
102.6
98.0
98.3
98.5
98.6
98.8


Refrigerating
% (relative to R410A)
129.6
89.9
96.0
96.1
97.8
104.5
111.1


Capacity Ratio










Condensation Glide
° C.
2.4
10.1
8.7
9.3
9.0
7.0
5.0





















Com Ex75
Example37
Com Ex76
Com Ex77
Com Ex78
Com Ex79
Com Ex80
Com Ex81


Item
Unit
H
I
K′ = J = B′
A
B
A′
A′′
B″





HFO-1132 (E)
mass %
44.2
22.4
0.0
76.1
0.0
57.5
42.7
0.0


R32
mass %
0.0
18.0
36.5
18.4
17.8
37.0
51.8
51.4


R1234ze
mass %
50.3
54.1
58.0
0.0
76.7
0.0
0.0
43.1


CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

4
125
250
125
125
250
350
350


COP ratio
% (relative to R410A)
100.8
102.2
103.8
96.0
105.9
96.4
97.2
102.4


Refrigerating
% (relative to R410A)
80.0
81.6
80.0
116.2
64.5
120.0
121.5
91.0


Capacity Ratio











Condensation Glide
° C.
15.0
15.2
14.1
3.7
18.1
2.9
2.6
10.4


















Com Ex82
Example38
Example39
Example40
Example41


Item
Unit
L
L′
M
N
O





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


R32
mass %
0.0
10.0
18.2
36.8
51.6


R1234ze
mass %
22.5
27.3
27.8
22.1
14.0


CO2
mass %
5.5
5.5
5.5
5.5
5.5


GWP

2
70
125
250
350


COP ratio
% (relative to R410A)
97.7
98.0
98.2
98.4
98.6


Refrigerating
% (relative to R410A)
97.3
97.4
99.0
105.6
112.2


Capacity Ratio








Condensation Glide
° C.
9.0
9.5
9.2
7.1
5.1

























TABLE 6









Com Ex83
Example47
Com Ex84
Com Ex85
Com Ex86
Com Ex87
Com Ex88
Com Ex89


Item
Unit
H
I
K′
A
B
A′
B′
A″





HFO-1132 (E)
mass %
36.3
15.3
0.0
74.1
0.0
55.5
0.0
40.7


R32
mass %
0.0
17.9
30.9
18.4
17.8
37.0
36.5
51.8


R1234ze
mass %
56.2
59.3
61.6
0.0
74.7
0.0
56.0
0.0


CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

4
125
212
125
125
250
250
350


COP ratio
% (relative to R410A)
101.2
102.7
103.8
95.1
105.3
95.7
103.1
96.6


Refrigerating
% (relative to R410A)
80.0
81.1
80.0
120.0
69.2
123.5
84.3
124.8


Capacity Ratio











Condensation Glide
° C.
18.5
18.0
16.8
4.6
20.2
3.6
15.3
3.3



















Com Ex90
Com Ex91
Example43
Example44
Example45
Example46


Item
Unit
B″
L
L′
M
N
O





HFO-1132 (E)
mass %
0.0
72.0
57.2
48.5
35.6
28.8


R32
mass %
51.4
0.0
10.0
18.2
36.8
51.7


R1234ze
mass %
41.1
20.5
25.3
25.8
20.1
12.0


CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5


GWP

350
2
70
125
250
350


COP ratio
% (relative to R410A)
101.6
96.6
97.0
97.2
97.5
97.8


Refrigerating
% (relative to R410A)
95.4
102.6
102.4
103.8
110.3
116.8


Capacity Ratio









Condensation Glide
° C.
11.2
10.1
10.4
10.0
7.7
5.6









A burning velocity test was performed using the apparatus shown in FIG. 1 in the following manner. First, the mixed refrigerants used had a purity of 99.5% or more, and were degassed by repeating a cycle of freezing, pumping, and thawing until no traces of air were observed on the vacuum gauge. The burning velocity was measured by the closed method. The initial temperature was ambient temperature. Ignition was performed by generating an electric spark between the electrodes in the center of a sample cell. The duration of the discharge was 1.0 to 9.9 ms, and the ignition energy was typically about 0.1 to 1.0 J. The spread of the flame was visualized using schlieren phctographs. A cylindrical container (inner diameter: 155 mm, length: 198 mm) equipped with two light transmission acrylic windows was used as the sample cell, and a xenon lamp was used as the light source. The propagation of flame was photographed with a schlieren system using a collimating lens and a high-speed digital video camera (frame rate: 600 fps), and recorded as video data on a PC. From the video image, flame propagation rate Sb (cm/sec) was measured. The burning velocity (Su) is expressed as the volume of unburned gas consumed by the flame surface of a unit area per unit time and was calculated by using the following formula.







S

u

=

Sb
*
ρ






u
/
ρ






b





ρu: adiabatic flame temperature (unburned)


ρb: adiabatic flame temperature (burned)


ρu represents the measurement temperature, and ρb represents the combustion of combustion gas and is calculated from isobaric specific heat.


Table 7 shows the results.















TABLE 7







Item
Unit
L
L′
M
N
O





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.1
36.7
51.6


R1234ze
mass %
28.0
32.8
33.3
27.6
19.5


CO2
mass %
0.0
0.0
0.0
0.0
0.0


Burning Velocity
cm/s
10
10
10
10
10





















Item
Unit
L
L′
M
N
O
L
L′
M
N
O





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.1
36.7
51.6
0.0
10.0
18.1
36.7
51.6


R1234ze
mass %
27.6
32.4
32.9
27.2
19.1
27.0
31.8
32.3
26.6
18.5


CO2
mass %
0.4
0.4
0.4
0.4
0.4
1.0
1.0
1.0
1.0
1.0



custom-character

cm/s
10
10
10
10
10
10
10
10
10
10





Item
Unit
L
L′
M
N
O
L
L′
M
N
O





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.1
36.7
51.6
0.0
10.0
18.1
36.7
51.6


R1234ze
mass %
26.0
30.8
31.3
25.6
17.5
25.0
29.8
30.3
24.6
16.5


CO2
mass %
2.0
2.0
2.0
2.0
2.0
3.0
3.0
3.0
3.0
3.0



custom-character

cm/s
10
10
10
10
10
10
10
10
10
10





Item
Unit
L
L′
M
N
O
L
L′
M
N
O





HFO-1132 (E)
mass %
72.0
57.2
48.5
35.7
28.9
72.0
57.2
48.5
35.6
28.9


R32
mass %
0.0
10.0
18.2
36.7
51.6
0.0
10.0
18.2
36.8
51.6


R1234ze
mass %
24.0
28.8
29.3
23.6
15.5
23.0
27.3
28.3
22.6
14.5


CO2
mass %
4.0
4.0
4.0
4.0
4.0
5.0
5.0
5.0
5.0
5.0



custom-character

cm/s
10
10
10
10
10
10
10
10
10
10





Item
Unit
L
L′
M
N
O
L
L′
M
N
O





HFO-1132 (E)
mass %
72.0
57.2
48.5
35.6
28.9
72.0
57.2
48.5
35.6
28.8


R32
mass %
0.0
10.0
18.2
36.8
51.6
0.0
10.0
18.2
36.8
51.7


R1234ze
mass %
22.5
27.3
27.8
22.1
14.0
20.5
25.3
25.8
20.1
12.0


CO2
mass %
5.5
5.5
5.5
5.5
5.5
7.5
7.5
7.5
7.5
7.5



custom-character

cm/s
10
10
10
10
10
10
10
10
10
10









From these results, it is understood that the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 350 or less, and is classified under the category of WCF lower flammability when the refrigerant is as follows: in the mixed refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,


(1) if 0<a≤0.4, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MN, NO, OK, KH, and HL that connect 7 points, i.e., points L, L′, M, N, O, K, and H, or on the straight lines LL′, L′M, MN, NO, OK, and KH (excluding the points L and H):


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point K (−2.5a+1.0, −0.25a+51.5, 1.75a+47.5), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


(2) if 0.4≤a≤7.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines LL′, L′M, MN, NO, OB″, B″K′, K′H, and HL that connect 8 points, i.e., points L, L′, M, N, O, B″, K′, and H, or on the straight lines LL′, L′M, MN, NO, OB″, and K′H (excluding the points L, B″, K′, and H), and


if 0.4≤a≤1.0, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0.0, −3.0a+52.6, 2.0a+47.4), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


if 1.0<a≤3.0, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+36.679, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0, −2.9a+52.5, 1.9a+47.5), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),


if 3.0<a≤5.0, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0, −2.9a+52.5, 1.9a+47.5), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), or


if 5.0<a≤7.5, the 8 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),


point B″ (0.0, 51.4, −a+48.6),


point K′ (0, −2.8286a+52.105, 1.8286a+47.895), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).


It is understood that the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 250 or less, and is classified under the category of WCF lower flammability when the refrigerant is as follows: in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,


(1) if 0<a≤5.5, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MN, NJ, JH, and HL that connect 6 points, i.e., points L, L′, M, N, J, and H, or on the straight lines LL′, L′M, MN, NJ, and JH (excluding the points L and H), and


if 0<a≤1.0, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (−0.3333a2−3.3667a+20.3, 36.6, 0.3333a2+2.3667a+43), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


if 1.0<a≤3.0, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (0.05a2−3.95a+20.5, 0.05a2−0.25a+36.8, −0.1a2+3.2a+42.7),


and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),


if 3.0<a≤5.0, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (0.05a2−4.05a+20.8, 36.5, −0.05a2+3.05a+42.7), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), or


if 5.0<a≤5.5, the 6 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point J (−3.6a+19.8, 36.5, 2.6a+43.7), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25),


(2) if 5.5<a≤7.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines LL′, L′M, MN, NB′, B′K′, K′H, and HL that connect 7 points, i.e., points L, L′, M, N, B′, K′, and H, or on the straight lines LL′, L′M, MN, NB′, K′H, and HL (excluding the points L, B′, K′, and H):


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),


point B′ (0.0, 36.5, −a+63.5),


point K′ (0.0, −2.8286a+52.105, 1.8281a+47.895), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).


It is understood that the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 125 or less, and is classified under the category of WCF lower flammability when the refrigerant is as follows: in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,


coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MI, IH, and HL that connect 5 points, i.e., points L, L′, M, I, and H, or on the straight lines LL′, L′M, MI, and IH (excluding the points L and H), and


if 0<a≤1.0, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (−0.1667a2−3.9333a+44.2, 18.1, 0.1667a2+2.9333a+37.7), and


point H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),


if 1.0<a≤3.0, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (0.05a2−4.25a+44.3, 18.1, −0.05a2+3.25a+37.6), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),


if 3.0<a≤5.0, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (−0.05a2−3.45a+42.8, 0.05a2−0.45a+19.0, 2.9a+38.2), and


point H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), or


if 5.0<a≤7.5, the 5 points are the following:


point L (72.0, 0.0, −a+28.0),


point L′ (57.2, 10.0, −a+32.8),


point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),


point I (0.1a2−4.85a+46.05, −0.02a2+0.21a+17.45, −0.08a2+3.64a+36.5), and


point H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).


The line segment where the refrigerating capacity is 80% relative to that of R410A is a curve that connects points K, J″, J′, I″, I′, H′, and H, as shown in FIG. 2; however, here, straight line KH or straight line K′H, where the refrigerating capacity is 80% or more, was used instead.


The approximate expressions that indicate the coordinates of the points were each determined as shown in Tables 8 to 11 below.









TABLE 8







A Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
81.6
81.2
80.6
80.6
79.6
78.6
78.6
77.6
76.6
76.6
76.1
74.1


R32
mass %
18.4
18.4
18.4
18.4
18.4
18.4
18.4
18.4
18.4
18.4
18.4
18.4


R1234ze
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0











a = CO2
a
a
a
a


x = HFO-1132E Approximate Expression
−a + 81.6
−a + 81.6
−a + 81.6
−a + 81.6


y = R32 Approximate Expression
18.4
18.4
18.4
18.4


z = R1234ze Approximate Expression
0.0
0.0
0.0
0.0







B Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
mass %
17.8
17.8
17.8
17.8
17.8
17.8
17.8
17.8
17.8
17.8
17.8
17.8


R1234ze
mass %
82.2
81.8
81.2
81.2
80.2
79.2
79.2
78.2
77.2
77.2
76.7
74.7











a = CO2
a
a
a
a


x = HFO-1132E Approximate Expression
0.0
0.0
0.0
0.0


y = R32 Approximate Expression
17.8
17.8
17.8
17.8


z = R1234ze Approximate Expression
−a + 82.2
−a + 82.2
−a + 82.2
−a + 82.2







A′ Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
63.0
62.6
62.0
62.0
61.0
60.0
60.0
59.0
58.0
58.0
57.5
55.5


R32
mass %
37.0
37.0
37.0
37.0
37.0
37.0
37.0
37.0
37.0
37.0
37.0
37.0


R1234ze
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0











a = CO2
a
a
a
a


x = HFO-1132E Approximate Expression
−a + 63.0
−a + 63.0
−a + 63.0
−a + 63.0


y = R32 Approximate Expression
37.0
37.0
37.0
37.0


z = R1234ze Approximate Expression
0.0
0.0
0.0
0.0







B′ Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
mass %
36.5
36.5
36.5
36.5
36.5
36.5
36.5
36.5
36.5
36.5
36.5
36.5


R1234ze
mass %
63.5
63.1
62.5
62.5
61.5
60.5
60.5
59.5
58.5
58.5
58.0
56.0











a = CO2
a
a
a
a


x = HFO-1132E Approximate Expression
0.0
0.0
0.0
0.0


y = R32 Approximate Expression
36.5
36.5
36.5
36.5


z = R1234ze Approximate Expression
−a + 63.5
−a + 63.5
−a + 63.5
−a + 63.5
















TABLE 9







A″ Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
48.2
47.8
47.2
47.2
46.2
45.2
45.2
44.2
43.2
43.2
42.7
40.7


R32
mass %
51.8
51.8
51.8
51.8
51.8
51.8
51.8
51.8
51.8
51.8
51.8
51.8


R1234ze
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0











a = CO2
a
a
a
a


x = HFO-1132E Approximate Expression
−a + 48.2
−a + 48.2
−a + 48.2
−a + 48.2


y = R32 Approximate Expression
51.8
51.8
51.8
51.8


z = R1234ze Approximate Expression
0.0
0.0
0.0
0.0







B″ Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R32
mass %
51.4
51.4
51.4
51.4
51.4
51.4
51.4
51.4
51.4
51.4
51.4
51.4


R1234ze
mass %
48.6
48.2
47.6
47.6
46.6
45.6
45.6
44.6
43.6
43.6
43.1
41.1











a = CO2
a
a
a
a


x = HFO-1132E Approximate Expression
0.0
0.0
0.0
0.0


y = R32 Approximate Expression
51.4
51.4
51.4
51.4


z = R1234ze Approximate Expression
−a + 48.6
−a + 48.6
−a + 48.6
−a + 48.6







L Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0


R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R1234ze
mass %
28.0
27.6
27.0
27.0
26.0
25.0
25.0
24.0
23.0
23.0
22.5
20.5











a = CO2
a
a
a
a


x = HFO-1132E Approximate Expression
72.0
72.0
72.0
72.0


y = R32 Approximate Expression
0.0
0.0
0.0
0.0


z = R1234ze Approximate Expression
−a + 28.0
−a + 28.0
−a + 28.0
−a + 28.0







L′ Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2


R32
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R1234ze
mass %
32.8
32.4
31.8
31.8
30.8
29.8
29.8
28.8
27.8
27.8
27.3
25.3











a = CO2
a
a
a
a


x = HFO-1132E Approximate Expression
57.2
57.2
57.2
57.2


y = R32 Approximate Expression
10.0
10.0
10.0
10.0


z = R1234ze Approximate Expression
−a + 32.8
−a + 32.8
−a + 32.8
−+B88:O126a + 32.8
















TABLE 10







M Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
48.6
48.6
48.6
48.6
48.6
48.6
48.6
48.5
48.5
48.5
48.5
48.5


R32
mass %
18.1
18.1
18.1
18.1
18.1
18.1
18.1
18.2
18.2
18.2
18.2
18.2


R1234ze
mass %
33.3
32.9
32.3
32.3
31.3
30.3
30.3
29.3
28.3
28.3
27.8
25.8











a = CO2
a
a
a
a


x = HFO-1132E
−0.019a + 48.618
−0.019a + 48.618
−0.019a + 48.618
−0.019a + 48.618


Approximate Expression






y = R32
 0.019a + 18.082
 0.019a + 18.082
 0.019a + 18.082
 0.019a + 18.082


Approximate Expression






z = R1234ze
  −a + 33.3
  −a + 33.3
  −a + 33.3
  −a + 33.3


Approximate Expression











N Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.6
35.6
35.6
35.6


R32
mass %
36.7
36.7
36.7
36.7
36.7
36.7
36.7
36.7
36.8
36.8
36.8
36.8


R1234ze
mass %
27.6
27.2
26.6
26.6
25.6
24.6
24.6
23.6
22.6
22.6
22.1
20.1











a = CO2
a
a
a
a


x = HFO-1132E
−0.0175a + 35.721 
−0.0175a + 35.721 
−0.0175a + 35.721 
−0.0175a + 35.721 


Approximate Expression






y = R32
0.0175a + 36.679
0.0175a + 36.679
0.0175a + 36.679
0.0175a + 36.679


Approximate Expression






z = R1234ze
  −a + 27.6
  −a + 27.6
  −a + 27.6
  −a + 27.6


Approximate Expression











O Approximate Expression




















CO2
mass %
0
0.4
1
1
2
3
3
4
5
5
5.5
7.5


HFO-1132E
mass %
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.8


R32
mass %
51.6
51.6
51.6
51.6
51.6
51.6
51.6
51.6
51.6
51.6
51.6
51.7


R1234ze
mass %
19.5
19.1
18.5
18.5
17.5
16.5
16.5
15.5
14.5
14.5
14
12











a = CO2
a
a
a
a


x = HFO-1132E
−0.0095a + 28.914 
−0.0095a + 28.914 
−0.0095a − 28.914 
−0.0095a + 28.914 


Approximate Expression






y = R32
0.0095a + 51.586
0.0095a + 51.586
0.0095a + 51.586
0.0095a + 51.586


Approximate Expression






z = R1234ze
  −a + 19.5
  −a + 19.5
  −a + 19.5
  −a + 19.5


Approximate Expression











H Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
67.6
65.8
63.2
63.2
58.8
54.5
54.5
50.3
46.2
46.2
44.2
36.3


R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R1234ze
mass %
32.4
33.8
35.8
35.8
39.2
42.5
42.5
45.7
48.8
48.8
50.3
56.2











a = CO2
a
a
a
a


x = HFO-1132E
0.1667a2
0.05a2
0.05a2
0.02a2


Approximate Expression
4.5667a + 67.6
4.55a + 67.7
4.55a + 67.7
4.21a + 66.75


y = R32
0.0
0.0
0.0
0.0


Approximate Expression






z = R1234ze
−0.1667a2
−0.05a2 +
−0.05a2 +
−0.02a2 +


Approximate Expression
3.5667a + 32.4
3.55a + 32.3
3.55a + 32.3
3.21a + 33.25
















TABLE 11







I Approximate Expression




















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
44.2
42.6
40.1
40.1
36.0
32.0
32.0
28.2
24.3
24.3
22.4
15.3


R32
mass %
18.1
18.1
18.1
18.1
18.1
18.1
18.1
18.0
18.0
18.0
18.0
17.9


R1234ze
mass %
37.7
38.9
40.8
40.8
43.9
46.9
46.9
49.8
52.7
52.7
54.1
59.3











a = CO2
a
a
a
a


x = HFO-1132E
0.1667a2 +
0.05a2
−0.05a2 − 3.45a +
0.1a2 − 4.85a +


Approximate
3.9333a + 44.2
4.25a + 44.3
42.8
46.05


Expression






y = R32
18.1
18.1
0.05a2 − 0.45a +
−0.02a2 + 0.21a +


Approximate


19.0
17.45


Expression






z = R1234ze
0.1667a2 +
−0.05a2 +
2.9a + 38.2
−0.08a2 + 3.64a +


Approximate
2.9333a + 37.7
3.25a + 37.6

36.5


Expression











J Approximate Expression



















CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5


HFO-1132E
mass %
20.3
18.9
16.6
16.6
12.8
9.1
9.1
5.4
1.8
1.8
0


R32
mass %
36.6
36.6
36.6
36.6
36.5
36.5
36.5
36.5
36.5
36.5
36.5


R1234ze
mass %
43.1
44.1
45.8
45.8
48.7
51.4
51.4
54.1
56.7
56.7
58











a = CO2
a
a
a
a


x = HFO-1132E
−0.3333a2
0.053a2
0.05a2
−3.6a + 19.8


Approximate
3.3667a + 20.3
3.95a + 20.5
4.05a + 20.8



Expression






y = R32
36.6
0.05a2
36.5
36.5


Approximate

0.25a + 36.8




Expression






z = R1234ze
0.3333a2 +
−0.1a2 +
−0.05a2 +
2.6a + 43.7


Approximate
2.3667a + 43.1
3.2a + 42.7
3.05a + 42.7



Expression











K and K′ Approximate Expression





















CO2
mass %
0.0
0.4
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
5.5
7.5


HFO-1132E
mass %
1.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
00
0.0
0.0
0.0
0


R32
mass %
51.5
51.4
51.4
49.6
49.6
46.7
43.8
43.8
40.9
38.0
38.0
36.5
30.9


R1234ze
mass %
47.5
48.2
48.2
49.4
49.4
51.3
53.2
53.2
55.1
57.0
57.0
58.0
61.6












a = CO2
a
a
a
a
a


x = HFO-1132E
−2.5a + 1.0
0.0
0.0
0.0
0.0


Approximate







Expression







y = R32
−0.25a + 51.5
−3.0a + 52.6
−2.9a + 52.5
−2.9a + 52.5
−2.8286a + 52.105


Approximate







Expression







z = R1234ze
1.75a + 47.5
2.0a + 47.4
1.9a + 47.5
1.9a + 47.5
1.8286a + 47.895


Approximate







Expression









Example B

Mixed refrigerants were prepared such that the mass % of HFO-1132 (E), the mass % of R32, the mass % of the sum of R1234ze and R1234yf, and the mass % of CO2 were as shown in Tables 12 to 20 based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2, and evaluated in the same manner as in Example A. Tables 12 to 20 show the results. The letter “r” represents R1234yf/(R1234ze+R1234yf).









TABLE 12





0% CO2


























Com Ex93
Com Ex94
Com Ex95
Com Ex96
Com Ex97
Com Ex98
Com Ex99
Com Ex100


Item
Unit
A
Btext missing or illegible when filed
A″text missing or illegible when filed
B″text missing or illegible when filed
Htext missing or illegible when filed
Itext missing or illegible when filed
K′text missing or illegible when filed
Ltext missing or illegible when filed





HFO-1132 (E)
mass %
81.6
0.0
48.2
0.0
66.8
43.2
0.0
72.0


R32
mass %
18.4
17.8
51.8
51.4
0.0
18.1
51.4
0.0


R1234(ze + ytext missing or illegible when filed )
mass %
0.0
82.2
0.0
48.6
33.2
38.7
48.6
28.0


CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

125
125
350
350
3
125
350
2


COP ratio
% (relative
98.7
107.4
99.2
104.4
101.4
101.6
104.4
101.0



to R410A)










Refrigerating
% (relative
105.3
53.2
112.1
80.0
80.0
82.8
80.0
83.0


Capacity Ratio
to R410A)










Condensation Glide
° C.
0.3
10.1
0.0
6.5
4.4
6.4
6.5
3.6







Com Ex101
Com Ex102
Com Ex103
Com Ex104
Com Ex105
Com Ex106
Com Ex107
Com Ex108


Item
Unit
Ltext missing or illegible when filed
Mtext missing or illegible when filed
Ntext missing or illegible when filed
Otext missing or illegible when filed
Btext missing or illegible when filed
Btext missing or illegible when filed
Htext missing or illegible when filed
Itext missing or illegible when filed





HFO-1132 (E)
mass %
57.2
48.6
35.7
28.9
0.0
0.0
63.2
38.6


R32
mass %
10.0
18.1
36.7
51.6
17.9
51.5
0.0
18.1


R1234(ze + ytext missing or illegible when filed )
mass %
32.8
33.3
27.6
19.5
82.1
48.5
36.8
43.3


CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

70
125
250
350
125
350
2
125


COP ratio
% (relative
101.0
101.0
100.8
100.9
105.7
103.3
101.0
101.1



to R410A)










Refrigerating
% (relative
84.0
86.0
93.3
100.0
57.6
83.4
80.0
82.6


Capacity Ratio
to R410A)










Condensation Glide
° C.
51
5.5
4.4
2.8
8.6
4.7
3.7
5.6







Com Ex109
Com Ex110
Com Ex111
Com Ex112
Com Ex113
Com Ex114
Com Ex115
Com Ex116


Item
Unit
K′text missing or illegible when filed
Ltext missing or illegible when filed
L′text missing or illegible when filed
Mtext missing or illegible when filed
Ntext missing or illegible when filed
Otext missing or illegible when filed
Btext missing or illegible when filed
Btext missing or illegible when filed





HFO-1132 (E)
mass %
0.0
72.0
57.2
48.6
35.7
28.9
0.0
0.0


R32
mass %
46.6
0.0
10.0
18.2
36.8
51.6
18.1
51.5


R1234(ze + ytext missing or illegible when filed )
mass %
53.4
28.0
32.8
33.2
27.5
19.5
81.9
48.5


CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

317
2
70
125
250
350
125
350


COP ratio
% (relative
103.5
100.5
100.3
100.3
100.3
100.5
103.6
102.2



to R410A)










Refrigerating
% (relative
80.0
84.6
86.0
88.3
95.3
101.5
62.5
87.3


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.4
2.7
3.9
4.1
3.2
2.1
6.8
2.7







Com Ex117
Com Ex118
Com Ex119
Com Ex120
Com Ex121
Com Ex122
Com Ex123
Com Ex124


Item
Unit
Htext missing or illegible when filed
Itext missing or illegible when filed
Ktext missing or illegible when filed
Ltext missing or illegible when filed
Ltext missing or illegible when filed
Mtext missing or illegible when filed
Ntext missing or illegible when filed
Otext missing or illegible when filed





HFO-1132 (E)
mass %
58.3
31.9
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
18.2
40.3
0.0
10.0
18.2
36.8
51.7


R1234(ze + ytext missing or illegible when filed )
mass %
41.7
49.9
59.7
28.0
32.8
33.2
27.5
19.4


CO2
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


GWP

2
125
274
2
69
125
250
350


COP ratio
% (relative
100.3
100.3
102.2
99.9
99.5
99.4
99.6
100.1



to R410A)










Refrigerating
% (relative
80.0
82.3
80.0
86.6
88.4
90.8
97.7
103.3


Capacity Ratio
to R410A)










Condensation Glide
° C.
2.9
4.4
4.0
1.7
2.6
2.7
1.9
1.2






text missing or illegible when filed indicates data missing or illegible when filed














TABLE 13





0.4% CO2


























Com Ex125
Com Ex126
Com Ex127
Com Ex128
Com Ex129
Example47
Com Ex130
Com Ex131


Item
Unit
A
Btext missing or illegible when filed
A″
B″text missing or illegible when filed
Htext missing or illegible when filed
Itext missing or illegible when filed
K′text missing or illegible when filed
Ltext missing or illegible when filed





HFO-1132 (E)
mass %
81.2
0.0
47.7
0.0
65.0
41.6
0.0
12.0


R32
mass %
18.4
17.8
51.9
51.4
0.0
18.1
50.2
0.0


R1234(ze + ytext missing or illegible when filed )
mass %
0.0
81.8
0.0
48.2
34.6
39.9
49.4
27.6


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

125
125
350
350
3
125
342
2


COP ratio
% (relative
98.5
107.2
99.0
104.2
101.2
101.5
104.3
100.7



to R410A)










Refrigerating
% (relative
106.1
54.1
112.8
80.9
80.0
82.8
80.0
84.1


Capacity Ratio
to R410A)










Condensation Glide
° C.
0.6
10.7
0.2
6.8
5.2
7.0
7.0
4.1







Example48
Example49
Example50
Example51
Com Ex132
Com Ex133
Com Ex134
Example52


Item

Ltext missing or illegible when filed
Mtext missing or illegible when filed
Ntext missing or illegible when filed
Otext missing or illegible when filed
Btext missing or illegible when filed
B″text missing or illegible when filed
Htext missing or illegible when filed
Itext missing or illegible when filed





HFO-1132 (E)
mass %
57.2
48.6
35.7
28.9
0.0
0.0
61.4
36.9


R32
mass %
10.0
18.1
36.7
51.6
17.9
51.5
0.0
18.1


R1234(ze + ytext missing or illegible when filed )
mass %
32.4
32.9
27.2
19.1
81.7
48.1
38.2
44.6


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

70
125
250
350
125
350
3
125


COP ratio
% (relative
100.7
100.7
100.6
100.7
105.5
103.2
100.8
101.1



to R410A)










Refrigerating
% (relative
85.0
87.0
94.2
100.9
58.5
84.2
80.0
82.6


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.5
5.8
4.6
3.0
9.2
5.0
4.5
6.1







Com Ex135
Com Ex136
Example53
Example54
Example55
Exarnp1e56
Com Ex137
Com Ex138


Item
Unit
K′text missing or illegible when filed
Ltext missing or illegible when filed
L′text missing or illegible when filed
Mtext missing or illegible when filed
Ntext missing or illegible when filed
Otext missing or illegible when filed
Btext missing or illegible when filed
Btext missing or illegible when filed





HFO-1132 (E)
mass %
0.0
72.0
57.2
48.6
35.7
28.9
0.0
0.0


R32
mass %
45.4
0.0
10.0
18.2
36.8
51.6
18.1
51.5


R1234(ze + ytext missing or illegible when filed )
mass %
54.2
21.6
32.4
32.8
27.1
19.1
81.5
48.1


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

309
2
70
125
250
350
125
350


COP ratio
% (relative
103.4
100.2
100.1
100.0
100.1
100.4
103.5
103.2



to R410A)










Refrigerating
% (relative
80.0
85.7
87.0
89.2
96.3
102.4
63.3
84.2


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.9
3.2
4.3
4.5
35
2.3
7.3
4.9







Com Ex139
Com Ex140
Com Ex141
Com Ex142
Com Ex143
Com Ex144
Com Ex145
Com Ex146


Item
Unit
Htext missing or illegible when filed
Itext missing or illegible when filed
K′text missing or illegible when filed
Ltext missing or illegible when filed
L′text missing or illegible when filed
Mtext missing or illegible when filed
Ntext missing or illegible when filed
Otext missing or illegible when filed





HFO-1132 (E)
mass %
56.3
30.1
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
18.2
39.1
0.0
10.0
18.2
36.8
51.7


R1234(ze + ytext missing or illegible when filed )
mass %
43.3
51.3
60.5
27.6
32.4
32.8
27.1
19.0


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.1
0.4
0.4


GWP

2
125
266
2
69
125
250
350


COP ratio
% (relative
100.1
100.3
102.1
99.7
99.3
99.2
99.5
99.9



to R410A)










Refrigerating
% (relative
80.0
82.2
80.0
87.6
89.4
91.8
98.6
104.1


Capacity Ratio
to R410A)










Condensation Glide
° C.
3.5
4.9
4.5
2.2
3.0
30
2.2
1.4






text missing or illegible when filed indicates data missing or illegible when filed














TABLE 14





1% CO2


























Com Ex147
Com Ex148
Com Ex149
Com Ex150
Com Ex151
Example57
Com Ex152
Com Ex153


Item
Unit
A
Br=0.1
A″
B″r=0.1
Hr=0.1
Ir=0.1
K′r=0.1
Lr=0.1





HFO-1132 (E)
mass %
80.6
0.0
47.2
0.0
62.2
39.0
0.0
72.0


R32
mass %
18.4
17.8
51.8
51.5
0.0
18.1
48.4
0.0


R1234(ze + yf)
mass %
0.0
81.2
0.0
47.5
36.8
41.9
50.6
27.0


CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

125
125
350
350
3
125
330
2


COP ratio
%
98.2
107.0
98.8
103.9
101.0
101.5
104.2
100.3



(relative











to R410A)










Refrigerating
%
107.3
55.4
113.8
82.2
80.0
82.6
80.0
85.7


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
1.0
11.7
0.5
7.2
6.4
8.0
7.8
4.8


Glide







Example58
Example59
Example60
Example61
Com Ex154
Com Ex155
Com Ex156
Example62


Item
Unit
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Br=0.5
B′r=0.5
Hr=0.5
Ir=0.5





HFO-1132 (E)
mass %
57.2
48.6
35.7
28.9
0.0
0.0
58.4
34.1


R32
mass %
10.0
18.1
36.7
51.6
17.9
51.5
0.0
18.1


R1234(ze + yf)
mass %
31.8
32.3
26.5
18.5
81.1
47.5
40.6
46.8


CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

70
125
250
350
125
350
3
125


COP ratio
%
100.4
100.4
100.3
100.4
105.3
103.0
100.6
101.0



(relative











to R410A)










Refrigerating
%
86.5
88.5
95.6
102.3
59.8
85.5
80.0
82.4


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
6.1
6.3
5.0
3.3
9.9
5.3
5.6
7.0


Glide







Com Ex157
Com Ex158
Example63
Example64
Example65
Example66
Com Ex159
Com Ex160


Item
Unit
K′r=0.5
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Br=0.5
B″r=0.5





HFO-1132 (E)
mas s%
0.0
72.0
57.2
48.6
35.7
28.9
0.0
0.0


R32
mass %
43.6
0.0
10.0
18.2
36.8
51.6
18.1
51.5


R1234(ze + yf)
mass %
55.4
27.0
31.8
32.2
26.5
18.5
80.9
47.5


CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

297
2
70
125
250
350
125
350


COP ratio
%
103.3
99.8
99.7
99.7
99.8
100.1
103.3
101.8



(relative











to R410A)










Refrigerating
%
80.0
87.3
88.5
90.7
97.6
103.7
64.6
89.4


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
6.6
3.9
4.9
4.9
3.8
2.6
7.9
3.3


Glide







Com Ex161
Com Ex162
Com Ex163
Com Ex164
Com Ex165
Com Ex166
Com Ex167
Com Ex168


Item
Unit
Hr=1
Ir=1
K′r=1
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
53.4
27.4
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
18.2
37.4
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
45.6
53.4
61.6
27.0
31.8
32.2
26.5
18.4


CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

2
125
255
2
69
125
250
350


COP ratio
%
99.9
100.3
102.0
99.3
99.0
98.9
99.2
99.7



(relative











to R410A)










Refrigerating
%
80.0
82.1
80.0
89.2
90.8
93.2
99.9
105.4


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
4.5
5.7
5.1
2.9
3.5
3.4
2.5
1.7


Glide
















TABLE 15





2% CO2


























Com Ex169
Com Ex170
Com Ex171
Com Ex172
Com Ex173
Example67
Com Ex174
Com Ex175


Item
Unit
A
Br=0.1
A″
B″r=0.1
Hr=0.1
Ir=0.1
K′r=0.1
Lr=0.1





HFO-1132 (E)
mass %
79.6
0.0
46.2
0.0
57.8
34.9
0.0
72.0


R32
mass %
18.4
17.8
51.8
51.4
0.0
18.1
45.5
0.0


R1234(ze + yf)
mass %
0.0
80.2
0.0
46.6
40.2
45.0
52.5
26.6


CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

125
125
350
350
3
125
310
2


COP ratio
%
97.7
106.6
98.4
103.5
100.8
101.5
104.0
99.6



(relative











to R410A)










Refrigerating
%
109.3
57.7
115.5
84.3
80.0
82.4
80.0
88.4


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
1.7
13.2
1.0
7.9
8.3
9.6
9.1
5.9


Glide







Example68
Example69
Example70
Example71
Com Ex176
Com Ex177
Com Ex178
Example72


Item
Unit
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Br=0.5
B″r=0.5
Hr=0.5
Ir=0.5





HFO-1132 (E)
mass %
57.2
48.6
35.7
28.9
0.0
0.0
53.8
9.8


R32
mass %
10.0
18.2
36.7
51.6
17.9
51.5
0.0
18.1


R1234(ze + yf)
mass %
30.8
31.2
25.6
17.5
80.1
46.5
44.2
50.1


CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

70
125
250
350
125
350
3
125


COP ratio
%
99.8
99.8
99.9
100.0
104.9
102.6
100.3
101.0



(relative











to R410A)










Refrigerating
%
89.0
91.0
97.9
104.6
62.0
87.6
80.0
82.1


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
6.9
7.0
5.5
3.7
11.2
6.0
7.4
8.5


Glide







Com Ex179
Com Ex180
Example73
Example74
Example75
Example76
Com Ex181
Com Ex182


Item
Unit
K′r=0.5
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Br=0.5
B″r=0.5





HFO-1132 (E)
mass %
0.0
72.0
57.2
48.6
35.7
28.9
0.0
0.0


R32
mass %
40.6
0.0
10.0
18.2
36.8
51.7
18.1
51.5


R1234(ze + yf)
mass %
57.4
26.0
30.8
31.2
25.5
17.4
79.9
46.5


CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

277
2
70
125
250
350
125
350


COP ratio
%
103.1
99.2
99.2
99.2
99.4
99.7
102.9
101.5



(relative











to R410A)










Refrigerating
%
80.0
89.9
91.0
93.1
99.9
106.0
66.7
91.4


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
7.8
5.0
5.7
5.6
4.3
3.0
8.9
3.9


Glide







Com Ex183
Com Ex184
Com Ex185
Com Ex186
Com Ex187
Com Ex188
Com Ex189
Com Ex190


Item
Unit
Hr=1
Ir=1
K′r=1
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
48.6
23.1
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
18.2
34.6
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
49.4
56.7
63.4
26.0
30.8
31.2
25.5
17.4


CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

2
125
236
2
69
125
250
350


COP ratio
%
99.7
100.2
101.7
98.7
98.5
98.5
98.8
99.3



(relative











to R410A)










Refrigerating
%
80.0
81.9
80.0
91.8
93.2
95.5
102.1
107.5


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
6.2
7.0
6.3
3.9
4.3
4.1
3.1
2.2


Glide
















TABLE 16





3% CO2


























Com Ex191
Com Ex192
Com Ex193
Com Ex194
Com Ex195
Example77
Com Ex196
Com Ex197


Item
Unit
A
Br=0.1
A″
B″r=0.1
Hr=0.1
Ir=0.1
K′r=0.1
Lr=0.1





HFO-1132 (E)
mass %
78.6
0.0
45.2
0.0
53.5
31.0
0.0
72.0


R32
mass %
18.4
17.8
51.8
51.4
0.0
18.0
42.8
0.0


R1234(ze + yf)
mass %
0.0
79.2
0.0
45.6
43.5
48.0
54.2
25.0


CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

125
125
350
350
3
125
292
2


COP ratio
%
97.2
106.2
98.1
103.1
100.6
101.6
103.8
99.0



(relative











to R410A)










Refrigerating
%
111.3
59.9
117.2
86.4
80.0
82.2
80.0
91.0


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
2.4
14.6
1.5
8.5
10.2
11.1
10.4
6.9


Glide







Example78
Example79
Example80
Example81
Com Ex198
Com Ex199
Com Ex200
Example82


Item
Unit
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Br=0.5
B″r=0.5
Hr=0.5
Ir=0.5





HFO-1132 (E)
mass %
57.2
48.6
35.7
28.9
0.0
0.0
49.4
25.6


R32
mass %
10.0
18.2
36.7
51.6
18.0
51.5
0.0
18.1


R1234(ze + yf)
mass %
29.8
30.2
24.6
16.5
79
45.5
47.6
53.3


CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

70
125
250
350
125
350
3
125


COP ratio
%
99.2
99.3
99.4
99.6
104.5
102.2
100.1
101.1



(relative











to R410A)










Refrigerating
%
91.6
93.6
100.3
106.8
64.3
89.7
80.0
81.9


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
7.7
7.6
5.9
4.1
12.4
6.6
9.2
9.9


Glide







Com Ex201
Com Ex202
Example83
Example84
Example85
Example86
Com Ex203
Com Ex204


Item
Unit
K′r=0.5
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Br=0.5
B″r=0.5





HFO-1132 (E)
mass %
0.0
72.0
57.2
48.6
35.7
28.9
0.0
0.0


R32
mass %
37.6
0.0
10.0
18.2
36.8
51.7
18.1
51.6


R1234(ze + yf)
mass %
59.4
25.0
29.8
30.2
24.5
16.4
78.9
45.4


CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

257
2
70
125
250
350
125
350


COP ratio
%
102.9
98.6
98.6
98.7
98.9
99.3
102.6
101.1



(relative











to R410A)










Refrigerating
%
80.0
92.6
93.5
95.5
102.2
102.2
68.9
93.5


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
9.1
6.0
6.5
6.3
4.8
3.4
10.0
4.4


Glide







Com Ex205
Com Ex206
Com Ex207
Com Ex208
Com Ex209
Com Ex210
Com Ex211
Com Ex212


Item
Unit
Hr=1
Ir=1
K′r=1
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
43.9
18.7
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
18.1
31.7
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
53.1
60.2
65.3
25.0
29.8
30.2
24.5
16.4


CO2
mass %
3.0
3.0
3.0
30
3.0
3.0
3.0
3.0


GWP

3
125
217
2
69
125
250
350


COP ratio
%
99.5
100.3
101.5
98.1
98.0
98.0
98.4
98.9



(relative











to R410A)










Refrigerating
%
80.0
81.4
80.0
94.4
95.7
97.8
104.3
109.6


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
7.9
83
7.5
4.9
5.1
4.8
3.6
2.6


Glide
















TABLE 17





4% CO2


























Com Ex213
Com Ex214
Com Ex215
Com Ex216
Com Ex217
Example87
Com Ex218
Com Ex219


Item
Unit
A
Br=0.1
A″
B″r=0.1
Hr=0.1
Ir=0.1
K′r=0.1
Lr=0.1





HFO-1132 (E)
mass %
77.6
0.0
44.2
0.0
49.2
26.9
0.0
72.0


R32
mass %
18.4
17.8
51.8
51.4
0.0
18.0
39.7
0.0


R1234(ze + yf)
mass %
0.0
78.2
0.0
44.6
46.8
51.1
56.3
24.0


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

125
125
350
350
3
125
271
2


COP ratio
%
96.7
105.9
97.7
102.7
100.6
101.8
103.7
98.4



(relative











to R410A)










Refrigerating
%
113.3
62.2
118.9
88.6
80.0
81.9
80.0
93.7


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
3.0
15.9
2.0
9.1
12.1
12.7
11.8
7.7


Glide







Example88
Example89
Example90
Example91
Com Ex220
Com Ex221
Com Ex222
Example92


Item
Unit
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Br=0.5
B″r=0.5
Hr=0.5
Ir=0.5





HFO-1132 (E)
mass %
57.2
48.6
35.7
28.9
0.0
0.0
44.8
21.5


R32
mass %
10.0
18.2
36.8
51.6
18.0
51.5
0.0
18.1


R1234(ze + yf)
mass %
28.8
29.2
23.5
15.5
78.0
44.5
51.2
56.4


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

70
125
250
350
125
350
3
125


COP ratio
%
98.7
98.8
98.9
99.1
104.2
101.8
100.1
101.2



(relative











to R410A)










Refrigerating
%
94.1
95.9
102.7
109.1
66.6
91.8
80.0
81.6


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
8.4
8.2
6.3
4.5
13.6
7.2
11.0
11.4


Glide







Com Ex223
Com Ex224
Example93
Example94
Example95
Example96
Com Ex225
Com Ex226


Item
Unit
K′r=0.5
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Br=0.5
B″r=0.5





HFO-1132 (E)
mass %
0.0
72.0
57.2
48.6
35.7
28.9
0.0
0.0


R32
mass %
34.8
0.0
10.0
18.2
36.8
51.7
18.0
51.6


R1234(ze + yf)
mass %
61.2
24.0
28.8
29.2
23.5
15.4
78.0
44.4


CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

238
2
70
125
250
350
125
350


COP ratio
%
102.7
98.0
98.1
98.2
98.5
98.9
102.3
100.8



(relative











to R410A)










Refrigerating
%
80.0
95.2
96.0
97.9
104.4
110.4
71.1
95.6


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
10.4
6.8
7.2
6.9
5.3
3.8
11.0
5.0


Glide













Com Ex227
Com Ex228
Com Ex229
Com Ex230
Com Ex231
Com Ex232
Com Ex233
Com Ex234


Item
Unit
Hr=1
Ir=1
K′r=1
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
39.5
14.8
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
18.1
28.9
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
56.5
63.1
67.1
24.0
28.8
29.2
23.5
15.4


CO2
mass %
4.0
4.0
40
4.0
4.0
4.0
4.0
4.0


GWP

3
125
198
2
69
125
250
350


COP ratio
%
99.4
100.4
101.3
98.7
98.5
98.5
98.8
99.3



(relative











to R410A)










Refrigerating
%
80.0
81.3
80.0
91.8
93.2
95.5
102.1
107.5


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
9.6
9.6
6.7
3.9
4.3
4.1
3.1
2.2


Glide
















TABLE 18





5% CO2


























Com Ex236
Com Ex237
Com Ex238
Com Ex239
Com Ex240
Example97
Com Ex241
Com Ex242


Item
Unit
A
Br=0.1
A″
B″r=0.1
Hr=0.1
Ir=0.1
K′r=0.1
Lr=0.1





HFO-1132 (E)
mass %
76.6
0.0
43.2
0.0
45.1
23.1
0.0
72.0


R32
mass %
18.4
17.8
51.8
51.4
0.0
18.0
36.8
0.0


R1234(ze + yf)
mass %
0.0
77.2
0.0
43.6
49.9
53.9
58.2
23.0


CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

125
125
350
350
3
125
252
2


COP ratio
%
96.2
105.6
97.4
102.3
100.6
101.9
103.6
97.9



(relative











to R410A)










Refrigerating
%
115.2
64.5
120.6
90.8
80.0
81.7
80.0
96.4


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
3.5
17.1
2.4
9.6
13.9
14.2
13.1
8.5


Glide







Example98
Example99
Example100
Example101
Com Ex243
Com Ex244
Com Ex245
Example102


Item
Unit
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Br=0.5
B″r=0.5
Hr=0.5
Ir=0.5





HFO-1132 (E)
mass %
57.2
48.6
35.7
28.9
0.0
0.0
40.6
17.5


R32
mass %
10.0
18.2
36.8
51.7
18.0
51.5
0.0
18.1


R1234(ze + yf)
mass %
27.8
28.2
22.5
14.4
77.0
43.5
54.4
59.4


CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

70
125
250
350
125
350
3
125


COP ratio
%
98.2
98.3
98.5
98.7
103.8
101.5
100.0
101.3



(relative











to R410A)










Refrigerating
%
96.6
98.3
105.0
111.4
68.9
94.0
80.0
81.4


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
9.0
8.7
6.7
4.8
14.7
7.7
12.7
12.7


Glide







Com Ex246
Com Ex247
Example103
Example104
Example105
Example106
Com Ex248
Com Ex249


Item
Unit
K′r=0.5
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Br=0.5
B″r=0.5





HFO-1132 (E)
mass %
0.0
72.0
57.2
48.6
35.7
28.9
0.0
0.0


R32
mass %
31.8
0.0
10.0
18.2
36.8
51.7
18.1
51.6


R1234(ze + yf)
mass %
63.2
23.0
27.8
28.2
22.5
14.4
76.9
43.4


CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

218
2
70
125
250
350
125
350


COP ratio
%
102.6
97.5
97.6
97.7
98.1
98.5
101.9
100.5



(relative











to R410A)










Refrigerating
%
80.0
97.9
98.5
100.3
106.7
112.6
73.4
97.7


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
11.8
7.6
7.8
7.4
5.7
4.2
11.9
5.5


Glide







Com Ex250
Com Ex251
Com Ex252
Com Ex253
Com Ex254
Com Ex255
Com Ex256
Com Ex257


Item
Unit
Hr=1
Ir=1
K′r=1
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
35.1
10.7
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
18.1
26.1
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
59.9
66.2
68.9
23.0
27.8
28.2
22.5
14.4


CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

3
125
217
2
69
125
250
350


COP ratio
%
99.3
100.3
101.5
98.1
98.0
98.0
98.4
98.9



(relative











to R410A)










Refrigerating
%
80.0
81.4
80.0
94.4
95.7
97.8
104.3
109.6


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
11.3
8.3
7.5
4.9
5.1
4.8
3.6
2.6


Glide
















TABLE 19





6% CO2


























Com Ex258
Com Ex259
Com Ex260
Com Ex261
Com Ex262
Example107
Com Ex263
Com Ex264


Item
Unit
A
Br=0.1
A″
B″r=0.1
Hr=0.1
Ir=0.1
K′r=0.1
Lr=0.1





HFO-1132 (E)
mass %
75.6
0.0
43.2
0.0
41.0
19.3
0.0
72.0


R32
mass %
18.4
17.8
51.8
51.4
0.0
18.0
33.9
0.0


R1234(ze + yf)
mass %
0.0
76.2
1.0
42.6
53.0
56.7
60.1
22.0


CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

125
125
350
350
3
125
271
2


COP ratio
%
96.7
105.9
97.7
102.7
100.6
101.8
103.7
98.4



(relative











to R410A)










Refrigerating
%
113.3
62.2
118.9
88.6
80.0
81.9
80.0
93.7


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
3.0
15.9
2.0
9.1
12.1
12.7
11.8
7.7


Glide







Example108
Example109
Example110
Example111
Com Ex265
Com Ex266
Com Ex267
Example112


Item
Unit
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Br=0.5
B″r=0.5
Hr=0.5
Ir=0.5





HFO-1132 (E)
mass %
57.2
48.6
35.7
28.9
0.0
0.0
36.4
13.7


R32
mass %
10.0
18.2
36.8
51.7
17.9
51.5
0.0
18.0


R1234(ze + yf)
mass %
26.8
27.2
21.5
13.4
76.1
42.5
57.6
62.3


CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

70
125
250
350
125
350
3
125


COP ratio
%
98.1
98.2
98.5
98.9
104.2
101.1
100.1
101.5



(relative











to R410A)










Refrigerating
%
96.0
97.9
104.4
110.4
66.6
96.1
80.0
81.1


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
7.2
6.9
5.3
3.8
13.6
8.2
14.5
14.1


Glide







Com Ex268
Com Ex269
Example113
Example114
Example115
Example116
Com Ex270
Com Ex271


Item
Unit
K′r=0.5
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Br=0.5
B″r=0.5





HFO-1132 (E)
mass %
0.0
72.0
57.2
48.6
35.7
28.9
0.0
0.0


R32
mass %
28.9
0.0
16.0
18.2
36.8
51.7
18.0
51.6


R1234(ze + yf)
mass %
65.1
22.0
26.8
27.2
21.5
13.4
76.0
42.4


CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

198
2
70
125
250
350
125
350


COP ratio
%
102.5
98.0
98.1
98.2
98.5
98.9
102.3
100.8



(relative











to R410A)










Refrigerating
%
80.0
95.2
96.0
97.9
104.4
110.4
71.1
95.6


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
13.2
6.8
72
6.9
5.3
3.8
11.0
5.0


Glide







Com Ex272
Com Ex273
Com Ex274
Com Ex275
Com Ex276
Com Ex277
Com Ex278
Com Ex279


Item
Unit
Hr=1
Ir=1
K′r=1
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
30.9
7.0
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
18.0
23.3
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
63.1
69.0
70.7
22.0
26.8
27.2
21.5
13.4


CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

3
125
198
2
69
125
250
350


COP ratio
%
99.4
100.4
101.3
98.7
98.5
98.5
98.8
99.3



(relative











to R410A)










Refrigerating
%
80.0
81.3
80.0
91.8
93.2
95.5
102.1
107.5


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
9.6
9.6
8.7
3.9
4.3
4.1
3.1
2.2


Glide
















TABLE 20





7.5% CO2


























Com Ex280
Com Ex281
Com Ex282
Com Ex283
Com Ex284
Example117
Com Ex285
Com Ex286


Item
Unit
A
Br=0.1
A″
B″r=0.1
Hr=0.1
Ir=0.1
K′r=0.1
Lr=0.1





HFO-1132 (E)
mass %
74.1
00
40.7
0.0
35.1
13.9
0.0
72.0


R32
mass %
18.4
17.8
51.8
51.4
0.0
17.9
29.5
0.0


R1234(ze + yf)
mass %
0.0
74.7
0.0
41.1
57.4
60.7
62.9
20.5


CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

125
125
350
350
4
125
204
2


COP ratio
%
95.1
104.9
96.6
101.4
101.0
102.5
103.5
96.5



(relative











to R410A)










Refrigerating
%
120.0
70.4
124.8
96.2
80.0
81.1
80.0
103.0


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
4.6
19.6
3.3
10.8
18.2
17.6
16.6
9.9


Glide







Example118
Example119
Example120
Example121
Com Ex287
Com Ex288
Com Ex289
Example122


Item
Unit
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Br=0.5
B″r=0.5
Hr=0.5
Ir=0.5





HFO-1132 (E)
mass %
57.2
48.6
35.7
28.9
0.0
0.0
30.3
8.0


R32
mass %
10.0
18.2
36.8
51.7
18.0
51.5
0.0
18.0


R1234(ze + yf)
mass %
25.3
25.7
20.0
11.9
74.5
41.0
62.2
66.5


CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

70
125
250
350
125
350
3
125


COP ratio
%
96.9
97.1
97.4
97.7
103.1
100.6
100.3
101.8



(relative











to R410A)










Refrigerating
%
102.9
104.4
110.8
117.1
74.7
99.4
80.0
80.6


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
10.1
9.6
7.4
5.4
17.0
8.9
17.0
16.1


Glide







Com Ex290
Com Ex291
Example123
Example124
Example125
Example126
Com Ex292
Com Ex293


Item
Unit
K′r=0.5
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Br=0.5
B″r=0.5





HFO-1132 (E)
mass %
0.0
72.0
57.2
48.6
35.7
28.9
0.0
0.0


R32
mass %
21.5
0.0
10.0
18.2
36.8
51.7
18.0
51.6


R1234(ze + yf)
mass %
68.0
20.5
25.3
25.7
20.0
11.9
74.5
40.9


CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

169
2
69
125
250
350
125
350


COP ratio
%
102.4
96.2
96.4
96.6
97.1
97.5
101.1
99.7



(relative











to R410A)










Refrigerating
%
80.0
104.4
104.6
106.3
112.4
118.1
79.1
103.0


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
15.3
9.1
9.0
8.5
6.5
4.9
14.0
6.7


Glide







Com Ex294
Com Ex295
Com Ex296
Com Ex297
Com Ex298
Com Ex299
Com Ex300
Com Ex301


Item
Unit
Hr=1
Ir=1
K′r=1
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
24.8
1.4
0.0
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
18.0
19.1
0.0
10.0
18.3
36.8
51.7


R1234(ze + yf)
mass %
67.7
73.1
73.4
20.5
25.3
25.6
20.0
11.9


CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

3
125
132
2
69
125
250
350


COP ratio
%
99.6
100.9
101.0
95.8
95.8
96.0
96.6
97.3



(relative











to R410A)










Refrigerating
%
80.0
80.1
80.0
106.0
106.7
108.5
114.2
119.2


Capacity
(relative










Ratio
to R410A)










Condensation
° C.
15.4
13.9
13.7
8.2
7.7
7.1
5.4
4.3


Glide









A burning velocity test was performed for these mixed refrigerants in the same manner as in Example A. Tables 21 and 22 show the results.

























TABLE 21







Item
Unit
Lr=0.1
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.1
36.7
51.6
0.0
10.0
18.2
36.8
51.6
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
27.6
32.4
32.9
27.2
19.1
27.6
32.4
32.8
27.1
19.1
27.6
32.4
32.8
27.1
19.0


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4


Burning Velocity
cm/s
10
10
10
10
10
10
10
10
10
10
10
10
10
10
10





Item
Unit
Lr=0.1
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.1
36.7
51.6
0.0
10.0
18.2
36.8
51.6
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
27.0
31.8
32.3
26.6
18.5
27.0
31.8
32.2
26.5
18.5
27.0
31.8
32.2
26.5
18.4


CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0


Burning Velocity
cm/s
10
10
10
10
10
10
10
10
10
10
10
10
10
10
10





Item
Unit
Lr=0.1
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.2
36.7
51.6
0.0
10.0
18.2
36.8
51.6
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
26.0
30.8
31.2
25.6
17.5
26.0
30.8
31.2
25.5
17.5
26.0
30.8
31.2
25.5
17.4


CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


Burning Velocity
cm/s
10
10
10
10
10
10
10
10
10
10
10
10
10
10
10





Item
Unit
Lr=0.1
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.2
36.7
51.6
0.0
10.0
18.2
36.8
51.7
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
25.0
29.8
30.3
24.6
16.5
25.0
29.8
30.2
24.5
16.5
25.0
29.8
30.2
24.5
16.4


CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


Burning Velocity
cm/s
10
10
10
10
10
10
10
10
10
10
10
10
10
10
10
































TABLE 22







Item
Unit
Lr=0.1
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.2
36.8
51.6
0.0
10.0
18.2
36.8
51.7
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
24.0
28.8
29.2
23.5
15.5
24.0
28.8
29.2
23.5
15.4
24.0
28.8
29.2
23.5
15.4


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


Burning Velocity
cm/s
10
10
10
10
10
10
10
10
10
10
10
10
10
10
10





Item
Unit
Lr=0.1
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.8
28.9
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.2
36.8
51.7
0.0
10.0
18.2
36.8
51.7
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
23.0
27.8
28.2
22.5
14.4
23.0
27.8
28.2
22.5
14.4
23.0
27.8
28.2
22.5
14.4


CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


Burning Velocity
cm/s
10
10
10
10
10
10
10
10
10
10
10
10
10
10
10





Item
Unit
Lr=0.1
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.2
36.8
51.7
0.0
10.0
18.2
36.8
51.7
0.0
10.0
18.2
36.8
51.7


R1234(ze + yf)
mass %
22.0
26.8
27.2
21.5
13.4
22.0
26.8
27.2
21.5
13.4
22.0
26.8
27.2
21.5
13.4


CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


Burning Velocity
cm/s
10
10
10
10
10
10
10
10
10
10
10
10
10
10
10





Item
Unit
Lr=0.1
L′r=0.1
Mr=0.1
Nr=0.1
Or=0.1
Lr=0.5
L′r=0.5
Mr=0.5
Nr=0.5
Or=0.5
Lr=1
L′r=1
Mr=1
Nr=1
Or=1





HFO-1132 (E)
mass %
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9
72.0
57.2
48.6
35.7
28.9


R32
mass %
0.0
10.0
18.2
36.8
51.7
0.0
10.0
18.2
36.8
51.7
0.0
10.0
18.3
36.8
51.7


R1234(ze + yf)
mass %
20.5
25.3
25.7
20.0
11.9
20.5
25.3
25.7
20.0
11.9
20.5
25.3
25.6
20.0
11.9


CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


Burning Velocity
cm/s
10
10
10
10
10
10
10
10
10
10
10
10
10
10
10









From these results, it is understood that the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 350 or less, and is classified under the category of WCF lower flammability when the refrigerant is as follows: in the mixed refrigerant, when the mass % of HFO-1132(E) is x, the mass % of R32 is y, the mass % of the sum of R1234ze and R1234yf is z, and the mass % of CO2 is a based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2,


if r=R1234yf/(R1234ze+R1234yf), and 0.1<r<1.0, coordinates (x,y,z) in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines LrL′r, L′rMr, MrNr, NrOr, OrB″r, B″rK′r, K′rHr, and HrLr that connect 8 points, i.e., points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, or on the straight lines LrL′r, L′rMr, MrNr, NrOr, OrB″r, and K′rHr (excluding the points Lr, B″r, K′r, and Hr), and


if 0<a≤1.0, the 8 points are as follows:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, −0.2778r2+0.4167r+18.061, 51.4−a−y),


point Nr (35.7, −0.2778r2+0.4167r+36.661, 51.4−a−y),


point Or (28.9, −0.2222r2−0.1333r+51.611, 71.1−a−y),


point B″r (0.0, (0.463a2−0.1852a−0.2778)r2+(−0.6945a2+0.2778a+0.4167)r+(0.2317a2−0.0927a+51.361), 51.4−a−y),


point K′r (0.0, (0.3705a2−0.1482a−0.6667)r2+(−0.2217a2+0.0887a−11.6)r+(0.0183a2−3.0073a+52.567), 100−a−y), and


point Hr ((2.4072a2−2.0739a−0.8889)r2+(−2.2779a2+1.5779a−8.4667)r+(0.0392a2−4.5732a+67.656), 0.0, 100−a−x),


if 1.0<a≤3.0, the 8 points are as follows:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (−0.1389a2+0.6945a−0.8334)r2+(0.2084a2−1.0418a+1.2501)r+(−0.0695a2+0.3475a+17.783), 51.4−a−y),


point Nr (35.7, −0.2778r2+0.4167r+36.661, 51.4−a−y),


point Or (28.9, (0.25a2−1.25a+1.2222)r2+(−0.275a2+1.375a−1.2333)r+(0.025a2−0.125a+51.711), 71.1−y−a),


point B″r (0.0, (0.25a2−1.0278a+0.7778)r2+(−0.275a2+1.2419a−0.9668)r+(0.075a2−0.364a+51.789), 100−a−y),


point K′r (0.0, (0.16667a2+0.2222a−0.8333)r2+(−0.3495a2+0.3645a−11.748)r+(0.1335a2−3.2395a+52.684), 100−a−y), and


point Hr ((−0.25003a2+0.8613a−1.1669)r2+(0.275a2−1.3914a−8.0502)r+(0.0245a2−4.4175a+67.515), 0.0, 100−a−x),


if 3.0<a≤5.0, the 8 points are as follows:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, 18.2, 33.2−a),


point Nr (35.7, (−0.1389a2+1.2501a−2.778)r2+(0.2084a2−1.8752a+4.167)r+(−0.0695a2+0.6255a+35.41), 51.4−a−y),


point Or (28.9, (0.1389a2−0.9723a+1.389)r2+(−0.2083a2+1.4585a−2.0845)r+(0.0695a2−0.4865a+52.395), 71.1−a−y),


point B″r (0.0, −0.0556r2+0.2833r+51.372, 100−a−y),


point K′r (0.0, (0.77775a2−6.2775a+13.166)r2+(−0.9665a2+8.0155a−29.148)r+(0.189a2−4.54a+56.086), 100−a−y), and


point Hr ((−0.72215a2+6.3327a−13.332)r2+(0.6835a2−6.3015a+3.003)r+(0.039a2−4.434a+67.434), 0.0, 100−x−a), or


if 5.0<a≤7.5, the 8 points are as follows:


point Lr (72.0, 0.0, 28.0−a),


point L′, (57.2, 10.0, 32.8−a),


point Mr (48.6, (0.0592a2−0.6512a+1.776)r2+(−0.0355a2+0.3901a−1.062)r+(0.0029a2−0.0323a+18.29), 51.4−a−y),


point Nr (35.7, 36.8, 27.5−a),


point Or (28.9, 51.7, 19.4−a),


point B″r (0.0, −0.0556r2+0.2833r+51.372, 100−a−y),


point K′r (0.0, (0.10373a2−0.9189a+3.2232)r2+(−0.1285a2+1.2799a−16.419)r+(0.0252a2−3.1662a+53.312), 100−a−y), and


point Hr ((0.037a2−0.1293a−0.0008)r2+(−0.056a2+0.2a−11.017)r+(0.0719a2−4.8515a+68.7), 0.0, 100−a−x).


It is also understood that the refrigerant according to the present disclosure has a refrigerating capacity of 80% or more relative to that of R410A and a GWP of 125 or less, and is classified under the category of WCF lower flammability when the refrigerant is as follows: in the mixed refrigerant, when the mass % of HFO-1132(E) is x, the mass % of R32 is y, the mass % of the sum of R1234ze and R1234yf is z, and the mass % of CO2 is a based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2,


if r=R1234yf/(R1234ze+R1234yf), and 0.1 r<1.0, coordinates (x,y,z) in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines LrL′r, L′rMr, MrIr, IrHr, and HrLr that connect 5 points, i.e., points Lr, L′r, Mr, Ir, and Hr, or on the straight lines LrL′r, L′rMr, MrIr, and IrHr, and


if 0<a≤1.0, the 5 points are as follows:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, −0.2778r2+0.4167r+18.061, 51.4−a−y),


point Ir ((1.1576a2−0.3243a−2.1111)r2+(−0.9a2−0.35a−10.233)r+(−0.255a2−3.828a+44.244), 100−a−x−z, (1.1572a2+0.3239a+1.8889)r2+(0.9042a2+0.3458a+10.367)r+(0.2525a2+2.8315a+37.644)), and


point Hr ((2.4072a2−2.0739a−0.8889)r2+(−2.2779a2+1.5779a−8.4667)r+(0.0392a2−4.5732a+67.656), 0.0, 100−a−x), if 1.0<a≤3.0, the 5 points are as follows:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (−0.1389a2+0.6945a−0.8334)r2+(0.2084a2−1.0418a+1.2501)r+(−0.0695a2+0.3475a+17.783), 51.4−a−y),


point Ir ((−0.08337a2+0.8057a−2.0001)r2+(−0.0745a2−0.6105a−10.798)r+(0.108a2−4.346a+44.399), 100−a−x−z, (0.33337a2−1.5557a+2.2779)r2+(−0.225a2+1.508a+10.334)r+(−0.033a2+3.121a+37.64)), and


point Hr ((−0.25003a2+0.8613a−1.1669)r2+(0.275a2−1.3914a−8.0502)r+(0.0245a2−4.4175a+67.515), 0.0, 100−a−x),


if 3.0<a≤5.0, the 5 points are as follows:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, 18.2, 31.2−a),


point Ir ((−0.05554a2+0.8332a−2.3331)r2+(−0.2165a4+1.2485a−15.097)r+(0.1715a2−5.2775a+46.622), 100−a−x−z, (0.0556a2−0.8329a+2.6103)r2+(0.1915a2−1.0235a+14.18)r+(−0.1715a2+4.2775a+35.417)), and


point Hr ((−0.72215a2+6.3327a−13.332)r2+(0.6835a2−6.3015a+3.003)r+(0.039a2−4.434a+67.434), 0.0, 100−a−x), or


if 5.0<a≤7.5, the 5 points are as follows:


point Lr (72.0, 0.0, 28.0−a),


point L′r (57.2, 10.0, 32.8−a),


point Mr (48.6, (0.0592a2−0.6512a+1.776)r2+(−0.0355a2+0.3901a−1.062)r+(0.0029a2−0.0323a+18.29), 51.4−a−y),


point Ir ((0.19254a2−1.8957a+5.1093)r2+(−0.3156a2+3.3386a−23.07)r+(0.1097a2−4.9961a+46.759), 100−a−x−z, (−0.0074a2−0.4187a+2.1117)r2+(0.0379a2+0.1335a+12.236)r+(−0.0571a2+3.3777a+37.055)), and point Hr ((0.037a2−0.1293a−0.0008)r2+(−0.056a2+0.2a−11.017)r+(0.0719a2−4.8515a+68.7), 0.0, 100−x−a).


The approximate expressions that indicate the coordinates of the points were each determined as shown below.









TABLE 23





Point Lr







Approximate Expression Using r











Lr(r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Specific Coordinates
HFO-1132E
mass %
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0



R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R1234(ze + yf)
mass %
28.0
28.0
28.0
27.6
27.6
27.6
27.0
27.0
27.0













a = CO2
mass %
0.0
0.4
1.0











r
x = HFO-1132E Approximate Expression
72.0
72.0
72.0


Approximate
y = R32 Approximate Expression
0.0
0.0
0.0


Expression
R1234(ze + yf) Approximate Expression
28.0
27.6
27.0


















Specific
HFO-1132E
mass %
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0


Coordinates
R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R1234(ze + yf)
mass %
26.0
26.0
26.0
25.0
25.0
25.0
24.0
24.0
24.0













a = CO2
mass %
2.0
3.0
4.0











r
x = HFO-1132E Approximate Expression
72.0
72.0
72.0


Approximate
y = R32 Approximate Expression
0.0
0.0
0.0


Expression
z = R1234(ze + yf) Approximate Expression
26.0
25.0
24.0


















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


Coordinates
R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R1234(ze + yf)
mass %
23.0
23.0
23.0
22.0
22.0
22.0
20.5
20.5
20.5













a = CO2
mass %
5.0
6.0
7.5











r
x = HFO-1132E Approximate Expression
72.0
72.0
72.0


Approximate
y = R32 Approximate Expression
0.0
0.0
0.0


Expression
z = R1234(ze + yf) Approximate Expression
23.0
22.0
20.5










Approximate Expression Using r and a


(0 < a ≤ 7.5)









Item
Unit
Lr(r = R1234yf/(R1234(yf + ze))























CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
6.0
7.5


HFO-1132 E
mass %
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0
72.0


R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


R1234(ze + yf)
mass %
28.0
27.6
27.0
27.0
26.0
25.0
25.0
24.0
23.0
23.0
22.0
20.5








a = CO2
a


x = HFO-1132E Approximate Expression
72.0


y = R32 Approximate Expression
0.0


z = R1234ze Approximate Expression
−a + 28.0
















TABLE 24





Point L′r







Approximate Expression Using r











Lr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Specific Coordinates
HFO-1132E
mass %
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2



R32
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0



R1234(ze + yf)
mass %
32.8
32.8
32.8
32.4
32.4
32.4
31.8
31.8
31.8













a = CO2
mass %
0.0
57.2
57.2











r
x = HFO-1132E Approximate Expression
10.0
10.0
10.0


Approximate
y = R32 Approximate Expression
32.8
32.4
31.8


Expression
R1234(ze + yf) Approximate Expression
28.0
27.6
27.0


















Specific
HFO-1132E
mass %
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2


Coordinates
R32
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0



R1234(ze + yf)
mass %
30.8
30.8
30.8
29.8
29.8
29.8
28.8
28.8
28.8













a = CO2
mass %
57.2
57.2
57.2











r
x = HFO-1132E Approximate Expression
10.0
10.0
10.0


Approximate
y = R32 Approximate Expression
30.8
29.8
28.8


Expression
z = R1234(ze + yf) Approximate Expression
26.0
25.0
24.0


















Specific
HFO-1132 (E)
mass %
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2


Coordinates
R32
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0



R1234(ze + yf)
mass %
27.8
27.8
27.8
26.8
26.8
26.8
25.3
25.3
25.3













a = CO2
mass %
5.0
6.0
7.5











r
x = HFO-1132E Approximate Expression
57.2
57.2
57.2


Approximate
y = R32 Approximate Expression
10.0
10.0
10.0


Expression
z = R1234(ze + yf) Approximate Expression
27.8
26.8
25.3










Approximate Expression Using r and a


(0 < a ≤ 7.5)









Item
Unit
L′r (r = R1234yf/(R1234(yf + ze))























CO2
mass %
0.0
0.4
1.0
1.0
2.0
3.0
3.0
4.0
5.0
5.0
6.0
7.5


HFO-1132 E
mass %
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2
57.2


R32
mass %
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0
10.0


R1234(ze + yf)
mass %
32.8
32.4
31.8
31.8
30.8
29.8
29.8
28.8
27.8
27.8
26.8
25.3








a = CO2
a


x = HFO-1132E Approximate Expression
57.2


y = R32 Approximate Expression
10.0


z = R1234ze Approximate Expression
−a + 32.8
















TABLE 25





Point Mr


Approximate Expression Using r and a







(0 < a ≤ 1.0)









Mr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Specific
HFO-1132 E
mass %
48.6
48.6
48.6
48.6
48.6
48.6
48.6
48.6
48.6


Coordinates
R32
mass %
18.1
18.2
18.2
18.1
18.2
18.2
18.1
18.2
18.2



R1234(ze + yf)
mass %
33.3
33.2
33.2
32.9
32.8
32.8
32.3
32.2
32.2













a = CO2
mass %
0.0
0.4
1.0









r
x = HFO-1132E Approximate Expression
48.6


Approximate
y = R32 Approximate Expression
−0.2778r2 + 0.4167r + 18.061


Expression
z = R1234(ze + yf) Approximate Expression
51.4 − a − y










(1.0 < a ≤ 3.0)













Mr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Approximate
HFO-1132 E
mass %
48.6
48.6
48.6
48.6
48.6
48.6
48.6
48.6
48.6


Expression of
R32
mass %
18.1
18.2
18.2
18.2
18.2
18.2
18.2
18.2
18.2


x, y, z Using a
R1234(ze + yf)
mass %
32.3
32.2
32.2
31.2
31.2
31.2
30.2
30.2
30.2


and r
a = CO2
mass %
1.0
1.0
1.0
2.0
2.0
2.0
3.0
3.0
3.0












x = HFO-1132E Approximate Expression
48.6
48.6
48.6



y = R32 Approximate Expression
-0.2778r2 + 0.4167r + 18.061
18.2
18.2



z = R1234(ze + yf) Approximate Expression
48.6
48.6
48.6












Approximate
y
a = CO2
1.0
2.0
3.0


Expression of

Quadric Coefficient
-0.2778
0.0
0.0


x, y, z Using a

Linear Coefficient
0.4167
0.0
0.0


and r

Zeroth Order Coefficient
18.061
18.2
18.2










x Approximate Expression
48.6



y Approximate Expression
(−0.1389a2 + 0.6945a − 0.8334)r2 + (0.2084a2 − 1.0418a + 1.2501)r +




(−0.0695a2 + 0.3475a + 17.783)



z Approximate Expression
51.4 − a − y










(3.0 < a ≤ 5.0)













Mr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Approximate
HFO-1132 E
mass %
48.6
48.6
48.6
48.6
48.6
48.6
48.6
48.6
48.6


Expression of
R32
mass %
18.2
18.2
18.2
18.2
18.2
18.2
18.2
18.2
18.2


x, y, z Using a
R1234(ze + yf)
mass %
30.2
30.2
30.2
29.2
29.2
29.2
28.2
28.2
28.2


and r
a = CO2
mass %
3.0
3.0
3.0
4.0
4.0
4.0
5.0
5.0
5.0












x = HFO-1132E Approximate Expression
48.6
48.6
48.6



y = R32 Approximate Expression
18.2
18.2
18.2



z = R1234(ze + yf) Approximate Expression
33.2 − a
33.2 − a
33.2 − a
















TABLE 26







Point Mr


Approximate Expression Using r and a


(5.0 < a ≤ 7.5)









Mr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Approximate
HFO-1132 E
mass %
48.6
48.6
48.6
48.6
48.6
48.6
48.6
48.6
48.6


Expression of
R32
mass %
18.2
18.2
18.2
18.2
18.2
18.2
18.2
18.2
18.3


x, y, z Using a
R1234(ze + yf)
mass %
28.2
28.2
28.2
27.2
27.2
27.2
25.7
25.7
25.6


and r
a = CO2
mass %
5.0
5.0
5.0
6.0
6.0
6.0
7.5
7.5
7.5











r
x = HFO-1132E Approximate Expression
48.6
48.6
48.6



y = R32 Approximate Expression
18.2
18.2
0.222r2 − 0.1333r + 18.211



z = R1234(ze + yf) Approximate Expression
28.2
27.2
25.7












Approximate
y
a = CO2
5.0
6.0
7.5


Expression of

Quadric Coefficient
0
0
0.222


x, y, z Using a

Linear Coefficient
0
0
−0.133


and r

Zeroth Order Coefficient
18.2
18.2
18.211










x Approximate Expression
48.6



y Approximate Expression
(0.0592a2 − 0.6512a + 1.776)r2 + (−0.0355a2 − 0.3901a − 1.062)r +




(0.0029a2 − 0.0323a + 18.29)



z Approximate Expression
51.4 − a − y
















TABLE 27





Point Nr


Approximate Expression Using r and a







(0 < a ≤ 1.0)









Nr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Specific
HFO-1132 E
mass %
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.7


Coordinates
R32
mass %
36.7
36.8
36.8
36.7
36.8
36.8
36.7
36.8
36.8



R1234(ze + yf)
mass %
27.6
27.5
27.5
27.2
27.1
27.1
26.6
26.5
26.5



a = CO2
mass %
0.0
0.0
0.0
0.4
0.4
0.4
1.0
1.0
1.0









r
x = HFO-1132E
35.7


Approximate
Approximate Expression



Expression
y = R32 Approximate
−0.2778r2 + 0.4167r + 36.661



Expression




z = R1234(ze + yf)
51.4 − a − y



Approximate Expression










(1.0 < a ≤ 3.0)













Nr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Specific
HFO-1132 E
mass %
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.7


Coordinates
R32
mass %
36.7
36.8
36.8
36.7
36.8
36.8
36.7
36.8
36.8



R1234(ze + yf)
mass %
26.6
26.5
26.5
25.6
25.5
25.5
24.6
24.5
24.5



a = CO2
mass %
1.0
1.0
1.0
2.0
2.0
2.0
3.0
3.0
3.0









r
x = HFO-1132E
35.7


Approximate
Approximate Expression



Expression
y = R32 Approximate
−0.2778r2 + 0.4167r + 36.661



Expression




z = R1234(ze + yf)
51.4 − a − y



Approximate Expression










(3.0 < a ≤ 5.0)













Nr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Approximate
HFO-1132 E
mass %
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.7


Expression of
R32
mass %
36.7
36.8
36.8
36.8
36.8
36.8
36.8
36.8
36.8


x, y, z Using a
R1234(ze + yf)
mass %
24.6
24.5
24.5
23.5
23.5
23.5
22.5
22.5
22.5


and r
a = CO2
mass %
3.0
3.0
3.0
4.0
4.0
4.0
5.0
5.0
5.0












x = HFO-1132E
35.7
35.7
35.7



Approximate Expression






y = R32
−0.2778r2 + 0.4167r + 36.661
36.8
36.8



Approximate Expression






z = R1234(ze + yf)
64.3 − a − y
64.3 − a − y
64.3 − a − y



Approximate Expression















Approximate
y
a = CO2
3.0
4.0
5.0


Expression of

Quadric
−0.2778
0.0
0.0


x, y, z Using a

Coefficient





and r

Linear
0.4167
0.0
0.0




Coefficient







Zeroth Order
36.661
36.8
36.8




Coefficient













x Approximate Expression
35.7



y Approximate Expression
(−0.1389a2 + 1.2501a − 2.778)r2 + (0.2084a2 − 1.87525 + 4.167)r +




(−0.0695a2 + 0.6255a + 35.41)



z Approximate Expression
51.4 − y − a + B82:O108B81:O108B80:O108B77:O108B102AB68:O108
















TABLE 28







Point Nr


Approximate Expression Using r and a


(5.0 < a ≤ 7.5)











Nr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Approximate
HFO-1132E
mass %
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.7
35.7


Expression of
R32
mass %
36.8
36.8
36.8
36.8
36.8
36.8
36.8
36.8
36.8


x, y, z Using a
R1234(ze + yf)
mass %
22.5
22.5
22.5
21.5
21.5
21.5
20.0
20.0
20.0


and r
a = CO2
mass %
5.0
5.0
5.0
6.0
6.0
6.0
7.5
7.5
7.5










x = HFO-1132E Approximate Expression
35.7



y = R32 Approximate Expression
36.8



z = R1234(ze + yf) Approximate Expression
27.5-a
















TABLE 29







Point Or


Approximate Expression Using r and a











Oi (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0










(0 < a ≤ 1.0)


















Specific
HFO-1132E
mass %
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9


Coordinates
R32
mass %
51.6
51.6
51.7
51.6
51.6
51.7
51.6
51.6
51.7



R1234(ze + yf)
mass %
19.5
19.5
19.4
19.1
19.1
19.0
18.5
18.5
18.4



a = CO2
mass %
0.0
0.0
0.0
0.4
0.4
0.4
1.0
1.0
1.0









r
x = HFO-1132E Approximate
28.9


Approximate
Expression



Expression
y = R32 Approximate
−0.2222r2 − 0.1333r + 51.611



Expression




z = R1234(ze + yf)
71.1-a-y



Approximate Expression








(1.0 < a ≤ 3.0)


















Specific
HFO-1132E
mass %
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9


Coordinates
R32
mass %
51.6
51.6
51.7
51.6
51.7
51.7
51.6
51.7
51.7



R1234(ze + yf)
mass %
18.5
18.5
18.4
17.5
17.4
17.4
16.5
16.4
16.4



a = CO2
mass %
1.0
1.0
1.0
2.0
2.0
2.0
3.0
3.0
3.0











r
x = HFO-1132E Approximate
28.9
28.9
28.9


Approximate
Expression





Expression
y = R32 Approximate
0.2222r2 − 0.1333r +
−0.2778r2 + 0.4167r +
−0.2778r2 + 0.4167r +



Expression
51.611
51.561
51.561



z = R1234(ze + yf)
71.1-a-y
71.1-a-y
71.1-a-y



Approximate Expression















Approximate
y
a = CO2
1.0
2.0
3.0


Expression of

Quadric
0.2222
−0.2778
−0.2778


x, y, z Using a

Coefficent





and r

Linear
−0.1333
0.4167
0.4167




Coefficient







Zeroth Order
51.611
51.561
51.561




Coefficient













x Approximate Expression
28.9



y Approximate Expression
(0.25a2 − 1.25a + 1.2222)r2 + (−0.275a2 + 1.375a − 1.2333)r +




(0.025a2 − 0.125a + 51.711)



z Approximate Expression
71.1-y-a
















TABLE 30







Point Qr


Approximate Expression Using r and a











Oi (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0










(3.0 < a ≤ 5.0)


















Specific
HFO-1132E
mass %
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9


Coordinates
R32
mass %
51.6
51.7
51.7
51.6
51.7
51.7
51.7
51.7
51.7



R1234(ze + yf)
mass %
16.5
16.4
16.4
15.5
15.4
15.4
14.4
14.4
14.4



a = CO2
mass %
3.0
3.0
3.0
4.0
4.0
4.0
5.0
5.0
5.0











r
x = HFO-1132E
28.9
28.9
28.9


Approximate
Approximate Expression





Expression
y = R32 Approximate
−0.2778r2 + 0.4167r +
−2.778r2 + 0.4167r +
51.7



Expression
51.561
51.561




z = R1234(ze + yf)
71.1-a-y
71.1-a-y
71.1-a-y



Approximate Expression















Approximate
y
a = CO2
3.0
4.0
5.0


Expression of

Quadric
−0.2778
−0.2778
0.0


x, y, z Using a

Coefficent





and r

Linear
0.4167
0.4167
0.0




Coefficient







Zeroth Order
51.561
51.561
51.7




Coefficient













x Approximate Expression
28.9



y Approximate Expression
(0.1389a2 − 0.9723a + 1.389)r2 + (−0.2083a2 + 1.4585a − 2.0845)r +




(0.0695a2 − 0.4865a + 52.395)



z Approximate Expression
71.1-a-y







(5.0 < a ≤ 7.5)


















Approximate
HFO-1132E
mass %
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9
28.9


Expression of
R32
mass %
51.7
51.7
51.7
51.7
51.7
51.7
51.7
51.7
51.7


x, y, z Using a
R1234(ze + yf)
mass %
14.4
14.4
14.4
13.4
13.4
13.4
11.9
11.9
11.9


and r
a = CO2
mass %
5.0
5.0
5.0
6.0
6.0
6.0
7.5
7.5
7.5










x = HFO-1132E
28.9



Approximate Expression




y = R32 Approximate
51.7



Expression




z = R1234(ze + yf)
19.4-a



Approximate Expression
















TABLE 31







Point B″r


Approximate Expression Using r and a











B″r (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0










(0 < a ≤ 1.0)


















Approximate
HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Expression of
R32
mass %
51.4
51.5
51.5
51.4
51.5
51.5
51.5
51.5
51.5


x, y, z Using a
R1234(ze + yf)
mass %
48.6
48.5
48.5
48.2
48.1
48.1
47.5
47.5
47.5


and r
a = CO2
mass %
0.0
0.0
0.0
0.4
0.4
0.4
1.0
1.0
1.0












x = HFO-1132E Approximate
0.0
0.0
0.0



Expression






y = R32 Approximate Expression
−0.2778r2 + 0.4167r +
−0.2778r2 + 0.4167r +
51.5




51.361
51.361




z = R1234(ze + yf) Approximate
100-a-y
100-a-y
100-a-y



Expression















Approximate
y
a = CO2
0.0
0.4
1.0


Expression of

Quadric Coefficient
−0.2778
−0.2778
0.0


x, y, z Using a

Linear Coefficient
0.4167
0.4167
0.0


and r

Zeroth Order
51.361
51.361
51.5




Coefficient













x Approximate Expression
0.0



y Approximate Expression
(0.463a2 − 0.1852a − 0.2778)r2 + (−0.6945a2 + 0.2778a + 0.4167)r +




(0.2317a2 − 0.0927a + 51.361)



z Approximate Expression
51.4-a-y







(1.0 < a ≤ 3.0)


















Approximate
HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Expression of
R32
mass %
51.5
51.5
51.5
51.4
51.5
51.5
51.4
51.5
51.6


x, y, z Using a
R1234(ze + yf)
mass %
47.5
47.5
47.5
46.6
46.5
46.5
45.6
45.5
45.4


and r
a = CO2
mass %
1.0
1.0
1.0
2.0
2.0
2.0
3.0
3.0
3.0












x = HFO-1132E Approximate
0.0
0.0
0.0



Expression






y = R32 Approximate Expression
51.5
−0.02778r2 + 0.4167r +
−0.0556r2 + 0.2833r +





51.361
51.372



z = R1234(ze + yf) Approximate
100-a-y
100-a-y
100-a-y



Expression















Approximate
y
a = CO2
1.0
2.0
3.0


Expression of

Quadric Coefficient
0.0
−0.2778
−0.0556


x, y, z Using a

Linear Coefficient
0.0
0.4167
0.2833


and r

Zeroth Order
51.5
51.361
51.372




Coefficient













x Approximate Expression
0.0



y Approximate Expression
(0.25a2 − 1.0278a + 0.7778)r2 + (−0.275a2 + 1.2419a − 0.9668)r +




(0.075a2 − 0.364a + 51.789)



z Approximate Expression
100-a-y
















TABLE 32







Point B″r


Approximate Expression Using r and a











B″r (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0










(3.0 < a ≤ 5.0)


















Approximate
HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Expression of
R32
mass %
51.4
51.5
51.6
51.4
51.5
51.6
51.4
51.5
51.6


x, y, z Using a
R1234(ze + yf)
mass %
45.6
45.5
45.4
44.6
44.5
44.4
43.6
43.5
43.4


and r
a = CO2
mass %
3.0
3.0
3.0
4.0
4.0
4.0
5.0
5.0
5.0










x = HFO-1132E Approximate Expression
0.0



y = R32 Approximate Expression
−0.0556r2 + 0.2833r + 51.372



z = R1234(ze + yf) Approximate Expression
100-a-y







(5.0 < a ≤ 7.5)


















Specific
HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Coordinates
R32
mass %
51.4
51.5
51.6
51.4
51.5
51.6
51.4
51.5
51.6



R1234(ze + yf)
mass %
43.6
43.5
43.4
42.6
42.5
42.4
41.1
41.0
40.9



a = CO2
mass %
5.0
5.0
5.0
6.0
6.0
6.0
7.5
7.5
7.5









r
x = HFO-1132E Approximate Expression
0.0


Approximate
y = R32 Approximate Expression
−0.0556r2 + 0.2833r + 51.372


Expression
z = R1234(ze + yf) Approximate Expression
100.0-a-y
















TABLE 33







Point Hr


Approximate Expression Using r and a











Hr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0










(0 < a ≤ 1.0)


















Specfic
HFO-1132E
mass %
66.8
63.2
58.3
65.0
61.4
56.3
62.2
58.4
53.4


Coordinates
R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R1234(ze + yf)
mass %
33.2
36.8
41.7
34.6
38.2
43.3
36.8
40.6
45.6



CO2
mass %
0.0
0.0
0.0
0.4
0.4
0.4
1.0
1.0
1.0











r
x = HFO-1132E Approximate
−0.8889r2 − 8.4667r +
−1.3333r2 − 8.2r +
−0.5556r2 − 9.1667r +


Approximate
Expression
67.656
65.833
63.122


Expression
y = R32 Approximate Expression
0.0
0.0
0.0



z = R1234(ze + yf) Approximate
100-a-x
100-a-x
100-a-x



Expression















Approximate
x
a = CO2
0.0
0.4
1.0


Expression of

Quadric Coefficient
−0.8889
−1.3333
−0.5556


x, y, z Using a

Linear Coefficient
−8.4667
−8.2
−9.1667


and r

Zeroth Order
67.656
65.833
63.122




Coefficient













x Approximate Expression
(2.4072a2 − 2.0739a − 0.8889)r2 + (−2.2779a2 + 1.5779a − 8.4667)r +




(0.0392a2 − 4.5732a + 67.656)



y Approximate Expression
0.0



z Approximate Expression
100-a-x







(1.0 < a ≤ 3.0)


















Specific
HFO-1132E
mass %
62.2
58.4
53.4
57.8
53.8
48.6
53.5
49.4
43.9


Coordinates
R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R1234(ze + yf)
mass %
36.8
40.6
45.6
40.2
44.2
49.4
43.5
47.6
53.1



CO2
mass %
1.0
1.0
1.0
2.0
2.0
2.0
3.0
3.0
3.0











r
x = HFO-1132E Approximate
−0.5556r2 − 9.1667r +
−0.4444r2 − 9.7333r +
−0.8333r2 − 9.75r +


Approximate
Expression
63.122
58.778
54.483


Expression
y = Approximate Expression
0.0
0.0
0.0



z = R1234(ze + yf) Approximate
100-a-x
100-a-x
100-a-x



Expression















Approximate
x
a = CO2
1.0
2.0
3.0


Expression of

Quadric Coefficient
−0.5556
−0.4444
−0.8333


x, y, z Using a

Linear Coefficient
−9.1667
−9.7333
−9.75


and r

Zeroth Order
63.122
58.778
54.483




Coefficient













x Approximate Expression
(−0.25003a2 + 0.8613a − 1.1669)r2 + (0.275a2 − 1.3914a − 8.0502)r +




(0.0245a2 − 4.4175a + 67.515)



y Approximate Expression
0.0



z Approximate Expression
100-a-x
















TABLE 34







Point Hr


Approximate Expression Using r and a











Hr (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0










(3.0 < a ≤ 5.0)


















Specific
HFO-1132E
mass %
53.5
49.4
43.9
49.2
44.8
39.5
45.1
40.6
35.1


Coordinates
R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R1234(ze + yf)
mass %
43.5
47.6
53.1
46.8
51.2
56.5
49.9
54.4
59.9



CO2
mass %
3.0
3.0
3.0
4.0
4.0
4.0
5.0
5.0
5.0











r
x = HFO-1132E Approximate
−0.8333r2 − 9.75r +
0.4444r2 − 11.267r −
0.2778r2 − 11.417r +


Approximate
Expression
54.483
50.322
46.239


Expression
y = R32 Approximate Expression
0.0
0.0
0.0



z = R1234(ze + yf) Approximate
100-a-x
100-a-x
100-a-x



Expression















Approximate
x
a = CO2
3.0
4.0
5.0


Expression of

Quadric Coefficient
−0.8333
0.4444
0.2778


x, y, z Using a

Linear Coefficient
−9.75
−11.267
−11.417


and r

Zeroth Order
54.483
50.322
46.239




Coefficient













x Approximate Expression
(−0.72215a2 + 6.3327a − 13.332)r2 + (0.6835a2 − 63015a + 3.003)r +




(0.039a2 − 4.434a + 67.434)



y Approximate Expression
0.0



z Approximate Expression
100-a-x







(5.0 < a ≤ 7.5)


















Specific
HFO-1132E
mass %
45.1
40.6
35.1
41.0
36.4
30.9
35.1
30.3
24.8


Coordinates
R32
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0



R1234(ze + yf)
mass %
49.9
54.4
59.9
53.0
57.6
63.1
57.4
62.2
67.7



CO2
mass %
5.0
5.0
5.0
6.0
6.0
6.0
7.5
7.5
7.5











r
x = HFO-1132E Approximate
0.2778r2 − 11.417r +
0.5556r2 − 11.833r +
1.1111r2 − 12.667r +


Approximate
Expression
46.239
42.178
36.356


Expression
y = R32 Approximate Expression
0.0
0.0
0.0



z = R1234(ze + yf) Approximate
100-a-x
100-a-x
100-a-x



Expression















Approximate
x
a = CO2
5.0
6.0
7.5


Expression of

Quadric Coefficient
0.2778
0.5556
1.1111


x, y, z Using a

Linear Coefficient
−11.417
−11.833
−12.667


and r

Zeroth Order
46.239
42.178
36.356




Coefficient













x Approximate Expression
(0.037a2 − 0.1293a − 0.0008)r2 + (−0.056a2 + 0.2a − 11.017)r +




(0.0719a2 − 4.8515a + 68.7)



y Approximate Expression
0.0



z Approximate Expression
100-a-x
















TABLE 35







Point K′r


Approximate Expression Using r and a











K′r (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0










(0 < a ≤ 1.0)


















Specific
HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Coordinates
R32
mass %
51.4
46.6
40.3
50.2
45.4
39.1
48.4
43.6
37.4



R1234(ze + yf)
mass %
48.6
53.4
59.7
49.4
54.2
60.5
50.6
55.4
61.6



CO2
mass %
0.0
0.0
0.0
0.4
0.4
0.4
1.0
1.0
1.0











r
x = HFO-1132E Approximate
0.0
0.0
0.0


Approximate
Expression





Expression
y = R32 Approximate Expression
−0.6667r2 − 11.6r +
−0.6667r2 − 11.6r +
−0.4444r2 − 11.733r +




52.567
51.367
49.578



z = R1234(ze + yf) Approximate
100-a-y
100-a-y
100-a-y



Expression















Approximate
y
a = CO2
0.0
0.4
1.0


Expression of

Quadric Coefficient
−0.6667
−0.6667
−0.4444


x, y, z Using a

Linear Coefficient
−11.6
−11.6
−11.733


and r

Zeroth Order
52.567
51.367
49.578




Coefficient













x Approximate Expression
0.0



y Approximate Expresson
(0.3705a2 − 0.1482a − 0.6667)r2 + (−0.2217a2 + 0.0887a − 11.6)r +




(0.0183a2 − 3.0073a + 52.567)



z Approximate Expression
100-a-y







(1.0 < a ≤ 3.0)


















Specific
HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Coordinates
R32
mass %
48.4
43.6
37.4
45.5
40.6
34.6
42.8
37.6
31.7



R1234(ze + yf)
mass %
50.6
55.4
61.6
52.5
57.4
63.4
54.4
59.4
65.3



CO2
mass %
1.0
1.0
1.0
2.0
2.0
2.0
3.0
3.0
3.0











r
x = HFO-1132E Approximate
0.0
0.0
0.0


Approximate
Expression





Expression
y = R32 Approximate Expression
−0.4444r2 − 11.733r +
0.2778r2 − 12.417r +
1.3333r2 − 13.8r +




49.578
46.739
44.167



z = R1234(ze + yf) Approximate
100-a-y
100-a-y
100-a-y



Expression















Approximate
y
a = CO2
1.0
2.0
3.0


Expression of

Quadric Coefficient
−0.4444
0.2778
1.3333


x, y, z Using a

Linear Coefficient
−11.733
−12.417
−13.8


and r

Zeroth Order
49.578
46.739
44.167




Coefficient













x Approximate Expression
0.0



y Approximate Expression
(0.16667a2 + 0.2222a − 0.8333)r2 + (−0.3495a2 + 0.3645a − 11.748)r +




(0.1335a2 − 3.2395a + 52.684)



z Approximate Expression
100-a-y
















TABLE 36







Point K′r


Approximate Expression Using r and a











K′r (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0










(3.0 < a ≤ 5.0)


















Specific
HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Coordinates
R32
mass %
42.8
37.6
31.7
39.7
34.8
28.9
36.8
31.3
26.1



R1234(ze + yf)
mass %
54.4
59.4
65.3
56.3
61.2
67.1
58.2
63.2
68.9



CO2
mass %
3.0
3.0
3.0
4.0
4.0
4.0
5.0
5.0
5.0











r
x = HFO-1132E Approximate
0.0
0.0
0.0


Approximate
Expression





Expression
y = R32 Approximate Expression
1.3333r2 − 13.8r +
0.5r2 − 12.55r +
1.2222r2 − 13.233r +




44.167
40.95
38.111



z = R1234(ze + yf) Approximate
100-a-y
100-a-y
100-a-y



Expression















Approximate
y
a = CO2
3.0
4.0
5.0


Expression of

Quadric Coefficient
1.3333
0.5
1.2222


x, y, z Using a

Linear Coefficient
−13.8
−12.55
−13.233


and r

Zeroth Order
44.167
40.95
38.111




Coefficient













x Approximate Expression
0.0



y Approximate Expression
(0.77775a2 − 6.2775a + 13.166)r2 + (−0.9665a2 + 8.0155a − 29.148)r +




(0.189a2 − 4.54a + 56.086)



z Approximate Expression
100-a-y







(5.0 < a ≤ 7.5)


















Specific
HFO-1132E
mass %
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0
0.0


Coordinates
R32
mass %
36.8
31.8
26.1
33.9
28.9
23.3
29.6
24.5
19.1



R1234(ze + yf)
mass %
58.2
63.2
68.9
60.1
65.1
70.7
62.9
68.0
73.4



CO2
mass %
5.0
5.0
5.0
6.0
6.0
6.0
7.5
7.5
7.5











r
x = HFO-1132E Approximate
0.0
0.0
0.0


Approximate
Expression





Expression
y = R32 Approximate Expression
1.2222r2 − 13.233r +
1.4444r2 − 13.367r +
2.1667r2 − 14.05r +




38.111
35.222
30.983



z = R1234(ze + yf) Approximate
100-a-y
100-a-y
100-a-y



Expression















Approximate
y
a = CO2
5.0
6.0
7.5


Expression of

Quadric Coefficient
1.2222
1.4444
2.1667


x, y, z Using a

Linear Coefficient
−13.233
−13.367
−14.05


and r

Zeroth Order
38.111
35.222
30.983




Coefficient













x Approximate Expression
0.0



y Approximate Expression
(0.10373a2 − 0.9189a + 3.2232)r2 + (−0.1285a2 + 1.2799a − 16.419)r +




(0.0252a2 − 3.1662a + 53.312)



z Approximate Expression
100-a-y
















TABLE 37







Point Ir


Approximate Expression Using r and a


(0 < a ≤1.0)











Ir (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Specific
HFO-1132E
mass %
43.2
38.6
31.9
41.6
36.9
30.1
39.0
34.1
27.4


Coordinates
R32
mass %
18.1
18.1
18.2
18.1
18.1
18.2
18.1
18.1
18.2



R1234(ze + yf)
mass %
38.7
43.3
49.9
39.9
44.6
51.3
41.9
46.8
53.4



CO2
mass %
0.0
0.0
0.0
0.4
0.4
0.4
1.0
1.0
1.0











r
x = HFO-1132E Approximate
−2.1111r2 − 10.233r +
−2.0556r2 − 10.517r +
−1.2778r2 − 11.483r +


Approximate
Expression
44.244
42.672
40.161


Expression
y = R32 Approximate Expression
100-a-x-z
100-a-x-z
100-a-x-z



z = R1234(ze + yf) Approximate
1.8889r2 + 10.367r +
1.8333r2 + 10.65r +
1.0556r2 + 11.617r +



Expression
37.644
38.817
40.728












Approximate
x
a = CO2
0.0
0.4
1.0


Expression of

Quadric Coefficient
−2.1111
−2.0556
−1.2778


x, y, z Using a

Linear Coefficient
−10.233
−10.517
−11.483


and r

Zeroth Order
44.244
42.672
40.161




Coefficient






z
a = CO2
0.0
0.4
1.0




Quadric Coefficient
1.8889
1.8333
1.0556




Linear Coefficient
10.367
10.65
11.617




Zeroth Order
37.644
38.817
40.728




Coefficient













x Approximate Expression
(1.1576a2 − 0.3243a − 2.1111)r2 + (−0.9a2 − 035a − 10.233)r +




(−0.255a2 − 3.828a + 44.244)



y Approximate Expression
100-a-x-z



z Approximate Expression
(−1.1572a2 + 0.3239a + 1.8889)r2 + (0.9042a2 + 0.3458a + 10.367)r +




(0.2525a2 + 2.8315a + 37.644)
















TABLE 38







Point Ir


Approximate Expression Using r and a


(1.0 < a ≤ 3.0)











Ir (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Specific
HFO-1132E
mass %
39.0
34.1
27.4
34.9
29.8
23.1
31.0
25.6
18.7


Coordinates
R32
mass %
18.1
18.1
18.2
18.1
18.1
18.2
18.0
18.1
18.1



R1234(ze + yf)
mass %
41.9
46.8
53.4
45.0
50.1
56.7
48.0
53.3
60.2



CO2
mass %
1.0
1.0
1.0
2.0
2.0
2.0
3.0
3.0
3.0











r
x = HFO-1132E Approximate
−1.2778r2 − 11.483r +
−0.7222r2 − 12.317r +
−0.3333r2 − 13.3r +


Approximate
Expression
40.161
36.139
32.333


Expression
y = R32 Approximate Expression
100-a-x-z
100-a-x-z
100-a-x-z



z = R1234(ze + yf) Approximate
1.0556r2 + 11.617r +
0.5r2 + 12.45r +
0.6111r2 + 12.883r +



Expression
40.728
43.75
46.706












a  custom-character
x
a = CO2
1.0
2.0
3.0



custom-character


Quadric Coefficient
−1.2778
−0.7222
−0.3333


x, y, z

Linear Coefficient
−11.483
−12.317
−13.3


Approximate

Zeroth Order
40.161
36.139
32.333


Expression

Coefficient






z
a = CO2
1.0
2.0
3.0




Quadric Coefficient
1.0556
0.5
0.6111




Linear Coefficient
11.617
12.45
12.833




Zeroth Order
40.728
43.75
46.705




Coefficient













x Approximate Expression
(−0.08337a2 + 0.8057a − 2.0001)r2 + (−0.0745a2 − 0.6105a − 10.798)r +




(0.108a2 − 4.346a + 44.399)



y Approximate Expression
100-a-x-z



z Approximate Expression
(0.33337a2 − 1.5557a + 2.2779)r2 + (−0.225a2 + 1.508a + 10.334)r +




(−0.033a2 + 3.121a + 37.64)
















TABLE 39







Point Ir


Approximate Expression Using r and a


(3.0 < a ≤ 5.0)











Ir (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Specific
HFO-1132E
mass %
31.0
25.6
18.7
26.9
21.5
14.8
23.1
17.5
10.7


Coordinates
R32
mass %
18.0
18.1
18.1
18.0
18.1
18.1
18.0
18.1
18.1



R1234(ze + yf)
mass %
48.0
53.3
60.2
51.1
56.4
63.1
53.9
59.4
66.2



CO2
mass %
3.0
3.0
3.0
4.0
4.0
4.0
5.0
5.0
5.0











r
x = HFO-1132E Approximate Expression
−0.3333r2 − 13.3r + 32.333
0.1111r2 − 13.567r + 28.256
0.4444r2 + 14.267r + 24.522


Approximate
y = R32 Approximate Expression
100-x-z-a
100-x-z-a
100-x-z-a


Expression
z = R1234(ze + yf) Approximate Expression
0.6111r2 + 12.883r + 46.706
0.1667r2 + 13.15r + 49.783
−0.1667r2 + 13.85r + 52.517












Approximate
x
a = CO2
3.0
4.0
5.0


Expression of

Quadric Coefficient
−0.3333
0.1111
0.4444


x, y, z Using a

Linear Coefficient
−13.3
−13.567
−14.267


and r

Zeroth Order Coefficient
32.333
28.256
24.522



z
a = CO2
3.0
4.0
5.0




Quadric Coefficient
0.6111
0.1667
−0.1667




Linear Coefficient
12.833
13.15
13.85




Zeroth Order Coefficient
46.706
49.783
52.517










x Approximate Expression
(−0.05554a2 + 0.8332a − 2.3331)r2 + (−0.2165a2 + 1.2485a − 15.097)r +




(0.1715a2 − 5.2775a + 46.622)



y Approximate Expression
100-x-z-a



z Approximate Expression
(0.0556a2 − 0.8329a + 2.6103)r2 + (0.1915a2 − 1.0235a + 14.18)r +




(−0.1715a2 + 4.2775a + 35.417)
















TABLE 40







Point Ir











Ir (r = R1234ze/(R1234ze + R1234yf))

















Item
Unit
0.1
0.5
1.0
0.1
0.5
1.0
0.1
0.5
1.0





















Specific
HFO-1132E
mass %
23.1
17.5
10.7
19.3
13.7
7.0
13.9
8.0
1.4


Coordinates
R32
mass %
18.0
18.1
18.1
18.0
18.0
18.0
17.9
18.0
18.0



R1234(ze + yf)
mass %
53.9
59.4
66.2
56.7
62.3
69.0
60.7
66.5
73.1



CO2
mass %
5.0
5.0
5.0
6.0
6.0
6.0
7.5
7.5
7.5











r
x = HFO-1132E Approximate Expression
0.4444r2 − 14.267r + 24.522
0.6667r2 − 14.4r + 20.733
1.7222r2 − 15.783r + 15.461


Approximate
y = R32 Approximate Expression
100-a-x-z
100-a-x-z
100-a-x-z


Expression
z = R1234(ze + yf) Approximate Expression
−0.1667r2 + 13.85r + 52.517
−0.6667r2 + 14.4r + 55.267
−1.4444r2 + 15.367r + 59.178












a custom-character
x
a = CO2
5.0
6.0
7.5



custom-character


Quadric Coefficient
0.4444
0.6667
1.7222


x, y, z

Linear Coefficient
−14.267
−14.4
−15.783


Approximate

Zeroth Order Coefficient
24.522
20.733
15.461


Expression
z
a = CO2
5.0
6.0
7.5




Quadric Coefficient
−0.1667
−0.6667
−1.4444




Linear Coefficient
13.85
14.4
15.367




Zeroth Order Coefficient
52.517
55.267
59.178










x Approximate Expression
(0.19254a2 − 1.8957a + 5.1093)r2 + (−0.3156a2 + 3.3386a − 23.07)r +




(0.1097a2 − 4.9961a + 46.759)



y Approximate Expression
100-a-x-z



z Approximate Expression
(−0.0074a2 − 0.4187a + 2.1117)r2 + (0.0379a2 + 0.1335a + 12.236)r +




(−0.0571a2 + 3.3777a + 37.055)









Example C

Mixed refrigerants were prepared such that the mass % of HFO-1132(E), the mass % of R32, the mass % of the sum of R1234ze and R1234yf, and the mass % of CO2 were as shown in Tables 41 to 72 based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2, and evaluated in the same manner as in Example A. Tables 41 to 72 show the results. The letter “r” represents R1234yf/(R1234ze+R1234yf).









TABLE 41





0.4% CO2


r = 0























Item
Unit
Com Ex302
Example127
Com Ex303
Com Ex304
Example128
Example129
Com Ex305





HFO-1132 (E)
mass %
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
54.6
49.6
39.6
54.6
49.6
39.6
29.6


R1234(ze + yf) (r = 0)
mass %
35.0
40.0
50.0
25.0
30.0
40.0
50.0


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

371
337
270
370
337
270
203


COP ratio
% (relative to R410A)
101
103.2
104.0
101.6
101.9
102.6
103.6


Refrigerating Capacity
% (relative to R410A)
90
86.0
78.6
96.7
93.1
85.5
77.7


Ratio










Condensation Glide
° C.
5.6
6.5
8.6
4.1
5.1
7.1
9.1





Item
Unit
Com Ex306
Exemple130
Example131
Com Ex307
Com Ex308
Example132
Com Ex309





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


R32
mass %
54.6
44.6
34.6
19.6
34.6
24.6
14.6


R1234(ze + yf) (r = 0)
mass %
15.0
25.0
35.0
50.0
25.0
35.0
45.0


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

370
303
236
136
235
169
102


COP ratio
% (relative to R410A)
100.5
100.9
101.6
103.2
100.4
101.3
102.4


Refrigerating Capacity
% (relative to R410A)
103.5
96.1
88.3
76.0
94.8
86.7
78.1


Ratio










Condensation Glide
° C.
2.5
4.4
6.4
9.3
4.5
6.5
8.3

















Item
Unit
Com Ex310
Example133
Com Ex311
Com Ex312
Example134
Com Ex313





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


R32
mass %
19.6
14.6
9.6
12.1
7.1
2.1


R1234(ze + yf) (r = 0)
mass %
30.0
35.0
40.0
27.5
32.5
37.5


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4


GWP

135
101
68
84
50
17


COP ratio
% (relative to R410A)
100.6
101.2
101.7
100.4
101.0
101.6


Refrigerating Capacity
% (relative to R410A)
88.7
84.3
79.7
88.1
83.4
78.6


Ratio









Condensation Glide
° C.
5.6
6.5
7.2
5.0
5.7
6.2
















TABLE 42





0.4% CO2


r = 0.25























Item
Unit
Com Ex314
Example135
Com Ex315
Com Ex316
Example136
Example137
Com Ex317





HFO-1132 (E)
mass %
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
54.6
49.6
34.6
54.6
49.6
39.6
24.6


R1234(ze + yf) (r = 0.25)
mass %
35.0
40.0
55.0
25.0
30.0
40.0
55.0


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

371
337
237
370
331
210
169


COP ratio
% (relative to R410A)
102.4
102.6
103.7
101.3
101.5
102.0
103.3


Refrigerating Capacity
% (relative to R410A)
91.3
87.8
76.9
97.9
94.5
87.3
75.7


Ratio










Condensation Glide
° C.
4.7
5.5
8.2
3.5
4.3
6.0
8.7





Item
Unit
Com Ex318
Example138
Example139
Com Ex319
Com Ex320
Example140
Com Ex321





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


R32
mass %
54.6
44.6
34.6
19.6
34.6
24.6
9.6


R1234(ze + yf) (r = 0.25)
mass %
15.0
25.0
35.0
50.0
25.0
35.0
50.0


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

370
303
236
135
235
168
68


COP ratio
% (relative to R410A)
100.4
100.7
101.1
102.4
100.1
100.8
102.3


Refrigerating Capacity
% (relative to R410A)
104.2
97.3
89.9
77.9
96.0
88.1
75.3


Ratio










Condensation Glide
° C.
2.2
3.7
5.4
8.1
3.9
5.6
7.8

















Item
Unit
Com Ex322
Example141
Com Ex323
Com Ex324
Example142
Com Ex325





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


R32
mass %
19.6
14.6
4.6
12.1
7.1
0.0


R1234(ze + yf) (r = 0.25)
mass %
30.0
35.0
45.0
27.5
32.5
39.6


CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4


GWP

134
101
34
84
50
3


COP ratio
% (relative to R410A)
100.2
100.7
101.7
100.1
100.6
101.3


Refrigerating Capacity
% (relative to R410A)
89.9
85.6
76.6
89.2
84.7
77.9


Ratio









Condensation Glide
° C.
4.8
5.6
6.7
4.4
5.0
5.4
















TABLE 43







0.4% CO2


r = 0.5



















Item
Unit
Com Ex326
Example143
Example144
Com Ex327
Com Ex328
Example145
Example146






HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0



R32
mass %
54.6
49.6
39.6
34.6
54.6
49.6
39.6



R1234 (ze + yf)
mass %
35.0
40.0
50.0
55.0
25.0
30.0
40.0



(r = 0.5)











CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4



GWP

370
337
270
236
370
337
270



COP ratio
% (relative
102
102.1
102.5
102.9
101.1
101.2
101.4




to R410A)










Refrigerating
% (relative
93
89.6
82.7
79.0
99.0
95.8
89.0



Capacity Ratio
to R410A)










Condensation Glide
° C.
3.8
4.5
6.1
6.9
2.8
3.5
5.0






Item
Unit
Com Ex329
Com Ex330
Example147
Example148
Com Ex331
Com Ex332
Example149






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



R32
mass %
24.6
54.6
39.6
29.6
19.6
34.6
24.6



R1234 (ze + yf)
mass %
55.0
15.0
30.0
40.0
50.0
25.0
35.0



(r = 0.5)











CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4



GWP

169
370
269
202
135
235
168



COP ratio
% (relative
102.4
100.2
100.5
100.9
101.7
99.8
100.3




to R410A)










Refrigerating
% (relative
77.7
104.9
95.0
87.7
79.8
97.1
89.6



Capacity Ratio
to R410A)










Condensation Glide
° C.
7.4
1.8
3.8
5.3
6.9
3.2
4.7






Item
Unit
Example150
Com Ex333
Com Ex334
Example151
Example152
Com Ex335
Com Ex336
Example153





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


R32
mass %
19.6
9.6
19.6
14.6
9.6
4.6
12.1
7.1


R1234 (ze + yf)
mass %
40.0
50.0
30.0
35.0
40.0
45.0
27.5
32.5


(r = 0.5)











CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

135
68
134
101
67
34
84
50


COP ratio
% (relative
100.6
101.6
99.8
100.2
100.7
101.1
99.7
100.2



to R410A)










Refrigerating
% (relative
85.6
77.1
91.1
87.0
82.7
78.1
90.3
85.9


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.5
6.7
4.1
4.8
5.3
5.7
3.7
4.2
















TABLE 44







0.4% CO2


r = 0.75



















Item
Unit
Com Ex337
Example154
Example155
Com Ex338
Com Ex339
Example156
Example157
Com Ex340





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
54.6
49.6
39.6
29.6
54.6
49.6
39.6
24.6


R1234 (ze + yf)
mass %
35.0
40.0
50.0
60.0
25.0
30.0
40.0
55.0


(r = 0.75)











CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

370
337
270
203
370
336
269
169


COP ratio
% (relative
101.6
101.7
101.9
102.9
100.8
100.8
100.9
101.6



to R410A)










Refrigerating
% (relative
94.4
91.3
84.7
77.4
100.2
97.2
90.7
79.7


Capacity Ratio
to R410A)










Condensation Glide
° C.
3.0
3.5
4.9
6.4
2.3
2.8
4.0
6.2





Item
Unit
Com Ex341
Example158
Example159
Com Ex342
Com Ex343
Example160
Example161
Com Ex344





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


R32
mass %
54.6
39.6
29.6
14.6
34.6
24.6
19.6
9.6


R1234 (ze + yf)
mass %
15.0
30.0
40.0
55.0
25.0
35.0
40.0
50.0


(r = 0.75)











CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4
0.4
0.4


GWP

370
269
202
101
235
168
135
57


COP ratio
% (relative
100.1
100.1
100.4
101.3
99.6
99.8
100.1
100.9



to R410A)










Refrigerating
% (relative
105.6
96.3
89.3
77.5
98.2
91.0
87.1
78.7


Capacity Ratio
to R410A)










Condensation Glide
° C.
1.4
3.0
4.3
6.4
2.6
3.9
4.5
5.7





Item
Unit
Com Ex345
Example162
Example163
Com Ex346
Com Ex347
Example164







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




R32
mass %
19.6
14.6
9.6
4.6
12.1
7.1




R1234 (ze + yf)
mass %
30.0
35.0
40.0
45.0
27.5
32.5




(r = 0.75)











CO2
mass %
0.4
0.4
0.4
0.4
0.4
0.4




GWP

134
101
67
34
84
50




COP ratio
% (relative
99.5
99.8
100.1
100.6
99.4
99.8





to R410A)










Refrigerating
% (relative
92.3
88.3
84.1
79.7
91.3
87.1




Capacity Ratio
to R410A)










Condensation Glide
° C.
3.4
4.0
4.5
4.9
3.1
3.5
















TABLE 45







1% CO2


r = 0


















Item
Unit
Com Ex348
Example165
Com Ex349
Com Ex350
Example166
Example167
Com Ex351





HFO-1132 (E)
mass %
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
54.0
49.0
39.0
54.0
49.0
39.0
29.0


R1234 (ze + yf)
mass %
35.0
40.0
50.0
25.0
30.0
40.0
50.0


(r = 0)










CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

367
333
266
366
333
266
199


COP ratio
% (relative
103
102.9
103.8
101.4
101.6
102.3
103.3



to R410A)









Refrigerating
% (relative
91
86.9
79.4
97.6
94.0
86.4
78.6


Capacity Ratio
to R410A)









Condensation Glide
° C.
6.0
7.0
9.1
4.5
5.5
7.6
9.7





Item
Unit
Com Ex352
Example168
Example169
Com Ex353
Com Ex354
Example170
Com Ex355





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


R32
mass %
54.0
39.0
29.0
19.0
34.0
24.0
14.0


R1234 (ze + yf)
mass %
15.0
30.0
40.0
50.0
25.0
35.0
45.0


(r = 0)










CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

366
265
198
132
231
165
98


COP ratio
% (relative
100.3
101.0
101.8
103.0
100.2
101.0
102.1



to R410A)









Refrigerating
% (relative
104.4
93.2
85.2
76.9
95.8
87.6
79.0


Capacity Ratio
to R410A)









Condensation Glide
° C.
2.9
5.8
8.0
10.0
5.0
7.1
9.0





Item
Unit
Com Ex356
Example171
Com Ex357
Com Ex358
Example172
Com Ex359






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



R32
mass %
24.0
14.0
4.0
11.5
6.5
0.0



R1234 (ze + yf)
mass %
25.0
35.0
45.0
27.5
32.5
39.0



(r = 0)










CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0



GWP

164
97
30
80
46
3



COP ratio
% (relative
99.9
100.9
102.1
100.1
100.7
101.4




to R410A)









Refrigerating
% (relative
93.9
85.2
75.9
89.0
84.4
78.1



Capacity Ratio
to R410A)









Condensation Glide
° C.
5.2
7.1
8.5
5.6
6.4
7.1
















TABLE 46







1% CO2


r = 0.25


















Item
Unit
Com Ex360
Example173
Com Ex361
Com Ex362
Example174
Example175
Com Ex363





HFO-1132 (E)
mass %
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
54.0
49.0
34.0
54.0
49.0
39.0
24.0


R1234 (ze + yf)
mass %
35.0
40.0
55.0
25.0
30.0
40.0
55.0


(r = 0.25)










CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

367
333
233
366
333
266
165


COP ratio
% (relative
102.2
102.4
103.5
101.1
101.3
101.7
103.0



to R410A)









Refrigerating
% (relative
92.2
88.7
77.7
98.8
95.4
88.1
76.6


Capacity Ratio
to R410A)









Condensation Glide
° C.
5.1
6.0
8.8
3.9
4.7
6.5
9.4





Item
Unit
Com Ex364
Example176
Example177
Com Ex365
Com Ex366
Example178
Com Ex367





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


R32
mass %
54.0
39.0
29.0
19.0
34.0
24.0
9.0


R1234 (ze + yf)
mass %
15.0
30.0
40.0
50.0
25.0
35.0
50.0


(r = 0.25)










CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

366
265
198
131
231
164
64


COP ratio
% (relative
100.1
100.6
101.2
102.2
99.9
100.5
102.0



to R410A)









Refrigerating
% (relative
105.1
94.5
86.9
78.8
96.9
89.0
76.2


Capacity Ratio
to R410A)









Condensation Glide
° C.
2.5
5.0
6.9
8.7
4.3
6.2
8.5





Item
Unit
Com Ex368
Example179
Com Ex369
Com Ex370
Example180







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




R32
mass %
24.0
14.0
4.0
11.5
6.5




R1234 (ze + yf)
mass %
25.0
35.0
45.0
27.5
32.5




(r = 0.25)










CO2
mass %
1.0
1.0
1.0
1.0
1.0




GWP

164
97
30
80
46




COP ratio
% (relative
99.6
100.4
101.4
99.8
100.3





to R410A)









Refrigerating
% (relative
95.0
86.6
77.5
90.2
85.7




Capacity Ratio
to R410A)









Condensation Glide
° C.
4.5
6.2
7.5
5.0
5.6
















TABLE 47







1% CO2


r = 0.5


















Item
Unit
Com Ex371
Example181
Example182
Com Ex372
Com Ex373
Example183
Com Ex184





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
54.0
49.0
39.0
29.0
54.0
49.0
39.0


R1234 (ze + yf)
mass %
35.0
40.0
50.0
60.0
25.0
30.0
40.0


(r = 0.5)










CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

366
333
266
199
366
332
265


COP ratio
% (relative
102
101.9
102.3
103.0
100.8
100.9
101.2



to R410A)









Refrigerating
% (relative
94
90.5
83.5
76.1
100.0
96.7
89.9


Capacity Ratio
to R410A)









Condensation Glide
° C.
4.2
5.0
6.6
8.3
3.2
3.9
5.5





Item
Unit
Com Ex374
Com Ex375
Example185
Example186
Com Ex376
Com Ex377
Example187





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


R32
mass %
24.0
54.0
39.0
29.0
14.0
34.0
24.0


R1234 (ze + yf)
mass %
55.0
15.0
30.0
40.0
55.0
25.0
35.0


(r = 0.5)










CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

165
366
265
198
98
231
164


COP ratio
% (relative
102.2
100.0
100.2
100.7
101.9
99.6
100.0



to R410A)









Refrigerating
% (relative
78.6
105.8
95.9
88.6
76.5
98.0
90.5


Capacity Ratio
to R410A)









Condensation Glide
° C.
8.0
2.1
4.2
5.8
8.2
3.7
5.2





Item
Unit
Com Ex378
Com Ex379
Example188
Com Ex380
Com Ex381
Example189






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



R32
mass %
9.0
24.0
14.0
4.0
11.5
6.5



R1234 (ze + yf)
mass %
50.0
25.0
35.0
45.0
27.5
32.5



(r = 0.5)










CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0



GWP

64
164
97
30
80
46



COP ratio
% (relative
101.3
99.3
99.9
100.8
99.5
99.9




to R410A)









Refrigerating
% (relative
78.0
96.0
88.0
79.1
91.3
86.9



Capacity Ratio
to R410A)









Condensation Glide
° C.
7.4
3.9
5.3
6.5
4.3
4.9
















TABLE 48







1% CO2


r = 0.75



















Item
Unit
Com Ex382
Example190
Example191
Com Ex383
Com Ex384
Example192
Example193
Example194





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
54.0
49.0
39.0
24.0
54.0
49.0
39.0
29.0


R1234 (ze + yf)
mass %
35.0
40.0
50.0
65.0
25.0
30.0
40.0
50.0


(r = 0.75)











CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

366
333
266
165
366
332
265
198


COP ratio
% (relative
101.4
101.5
101.6
102.5
100.6
100.6
100.7
101.0



to R410A)










Refrigerating
% (relative
95.3
92.2
85.5
74.3
101.1
98.1
91.6
84.4


Capacity Ratio
to R410A)










Condensation Glide
° C.
3.4
4.0
5.4
7.8
2.6
3.2
4.4
6.0





Item
Unit
Com Ex385
Com Ex386
Example195
Example196
Example197
Com Ex387
Com Ex388
Example198





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


R32
mass %
19.0
54.0
39.0
29.0
19.0
9.0
34.0
24.0


R1234 (ze + yf)
mass %
60.0
15.0
30.0
40.0
50.0
60.0
25.0
35.0


(r = 0.75)











CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0
1.0


GWP

131
365
265
198
131
64
231
164


COP ratio
% (relative
101.8
99.8
99.9
100.1
100.7
101.6
99.3
99.6



to R410A)










Refrigerating
% (relative
76.6
106.5
97.2
90.2
82.5
73.9
99.1
91.9


Capacity Ratio
to R410A)










Condensation Glide
° C.
7.6
1.8
3.4
4.8
6.3
7.6
3.0
4.4





Item
Unit
Example199
Com Ex389
Com Ex390
Example200
Example201
Com Ex391
Example202






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



R32
mass %
14.0
4.0
24.0
14.0
4.0
11.5
6.5



R1234 (ze + yf)
mass %
45.0
55.0
25.0
35.0
45.0
27.5
32.5



(r = 0.75)











CO2
mass %
1.0
1.0
1.0
1.0
1.0
1.0
1.0



GWP

97
30
164
97
30
79
46



COP ratio
% (relative
100.2
101.1
99.0
99.5
100.3
99.1
99.5




to R410A)










Refrigerating
% (relative
84.0
75.1
97.1
89.3
80.6
92.3
88.1



Capacity Ratio
to R410A)










Condensation Glide
° C.
5.8
6.8
3.2
4.5
5.6
3.7
4.2
















TABLE 49







2% CO2


r = 0


















Item
Unit
Com Ex392
Example203
Com Ex393
Com Ex394
Example204
Example205
Com Ex395





HFO-1132 (E)
mass %
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
58.0
48.0
33.0
58.0
48.0
38.0
23.0


R1234 (ze + yf)
mass %
30.0
40.0
55.0
20.0
30.0
40.0
55.0


(r = 0)










CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

393
327
226
393
326
259
159


COP ratio
% (relative
102
102.6
104.0
100.8
101.2
101.9
103.6



to R410A)









Refrigerating
% (relative
96
88.4
77.0
102.7
95.5
87.9
76.0


Capacity Ratio
to R410A)









Condensation Glide
° C.
5.8
7.8
11.2
4.2
6.2
8.4
11.8





Item
Unit
Com Ex396
Example206
Example207
Com Ex397
Com Ex398
Example208
Com Ex399





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


R32
mass %
58.0
38.0
28.0
18.0
38.0
23.0
8.0


R1234 (ze + yf)
mass %
10.0
30.0
40.0
50.0
20.0
35.0
50.0


(r = 0)










CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

392
259
192
125
258
158
57


COP ratio
% (relative
99.8
100.6
101.4
102.6
99.5
100.5
102.3



to R410A)









Refrigerating
% (relative
109.5
94.7
86.8
78.4
101.3
89.1
76.0


Capacity Ratio
to R410A)









Condensation Glide
° C.
2.6
6.6
8.9
11.0
4.7
8.0
10.9





Item
Unit
Com Ex400
Example209
Com Ex401
Com Ex402
Example210







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




R32
mass %
23.0
13.0
3.0
13.0
5.5




R1234 (ze + yf)
mass %
25.0
35.0
45.0
25.0
32.5




(r = 0)










CO2
mass %
2.0
2.0
2.0
2.0
2.0




GWP

157
90
23
90
40




COP ratio
% (relative
99.4
100.4
101.5
99.4
100.1





to R410A)









Refrigerating
% (relative
95.5
86.8
77.5
92.9
86.0




Capacity Ratio
to R410A)









Condensation Glide
° C.
6.0
8.1
9.8
5.1
7.5
















TABLE 50







2% CO2


r = 0.25



















Item
Unit
Com Ex403
Example211
Example212
Com Ex404
Com Ex405
Example213
Example214
Com Ex406





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
58.0
48.0
38.0
28.0
58.0
48.0
38.0
23.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
20.0
30.0
40.0
55.0


(r = 0.25)











CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

393
326
259
192
393
326
259
158


COP ratio
% (relative
101.7
102.0
102.7
103.6
100.6
100.9
101.4
102.7



to R410A)










Refrigerating
% (relative
97.0
90.2
82.9
75.3
103.7
96.9
89.6
78.0


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.0
6.8
8.8
10.5
3.7
5.4
7.3
10.4





Item
Unit
Com Ex407
Example215
Example216
Example217
Com Ex408
Com Ex409
Example218
Example219





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


R32
mass %
58.0
43.0
33.0
23.0
13.0
38.0
23.0
13.0


R1234 (ze + yf)
mass %
10.0
25.0
35.0
45.0
55.0
20.0
35.0
45.0


(r = 0.25)











CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

392
292
225
158
91
258
158
91


COP ratio
% (relative
99.7
100.0
100.5
101.3
102.3
99.2
100.1
101.0



to R410A)










Refrigerating
% (relative
110.0
99.7
92.3
84.4
76.0
102.2
90.6
82.2


Capacity Ratio
to R410A)










Condensation Glide
° C.
2.4
4.8
6.7
8.8
10.6
4.1
7.0
8.9





Item
Unit
Com Ex410
Com Ex411
Example220
Example221
Com Ex412
Example222







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




R32
mass %
8.0
23.0
13.0
0.0
13.0
5.5




R1234 (ze + yf)
mass %
50.0
25.0
35.0
48.0
25.0
32.5




(r = 0.25)











CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0




GWP

57
157
90
3
90
40




COP ratio
% (relative
101.5
99.1
99.9
101.2
99.1
99.7





to R410A)










Refrigerating
% (relative
77.8
96.6
88.2
76.3
94.0
87.3




Capacity Ratio
to R410A)










Condensation Glide
° C.
9.7
5.3
7.2
9.0
5.5
6.7
















TABLE 51







2% CO2


r = 0.5



















Item
Unit
Com Ex413
Example223
Example224
Com Ex414
Com Ex415
Example225
Example226
Example227





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
58.0
48.0
38.0
28.0
58.0
48.0
38.0
28.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
20.0
30.0
40.0
50.0


(r = 0.5)











CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

393
326
259
192
393
326
259
192


COP ratio
% (relative
101
101.6
102.0
102.7
100.4
100.5
100.8
101.4



to R410A)










Refrigerating
% (relative
98
91.9
85.0
77.5
104.6
98.3
91.4
84.0


Capacity Ratio
to R410A)










Condensation Glide
° C.
4.2
5.7
7.4
9.3
3.2
4.6
6.2
8.1





Item
Unit
Com Ex416
Com Ex417
Example228
Example229
Example230
Com Ex418
Com Ex419
Example231





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


R32
mass %
18.0
58.0
43.0
33.0
23.0
13.0
38.0
23.0


R1234 (ze + yf)
mass %
60.0
10.0
25.0
35.0
45.0
55.0
20.0
35.0


(r = 0.5)











CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

125
392
292
225
158
91
258
157


COP ratio
% (relative
102.3
99.5
99.7
100.0
100.6
101.5
99.0
99.6



to R410A)










Refrigerating
% (relative
76.0
110.4
100.9
93.8
86.2
78.0
103.2
92.0


Capacity Ratio
to R410A)










Condensation Glide
° C.
9.9
2.1
4.1
5.7
7.6
9.3
3.6
6.1





Item
Unit
Example232
Com Ex420
Com Ex421
Example233
Example234
Com Ex422
Example235






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



R32
mass %
13.0
3.0
23.0
13.0
0.0
13.0
5.5



R1234 (ze + yf)
mass %
45.0
55.0
25.0
35.0
48.0
25.0
32.5



(r = 0.5)











CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0



GWP

90
23
157
90
3
90
39



COP ratio
% (relative
100.4
101.4
98.8
99.5
100.7
98.8
99.4




to R410A)










Refrigerating
% (relative
83.9
74.9
97.6
89.6
77.8
95.0
88.5



Capacity Ratio
to R410A)










Condensation Glide
° C.
7.8
9.1
4.6
5.3
8.0
4.9
5.9
















TABLE 52







2% CO2


r = 0.75



















Item
Unit
Com Ex423
Example236
Example237
Com Ex424
Com Ex425
Example238
Example239
Example240





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
58.0
48.0
38.0
23.0
58.0
48.0
38.0
28.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
65.0
20.0
30.0
40.0
50.0


(r = 0.75)











CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

393
326
259
158
393
326
259
191


COP ratio
% (relative
101.0
101.1
101.3
102.2
100.2
100.2
100.3
100.7



to R410A)










Refrigerating
% (relative
99.8
93.7
86.9
75.7
105.5
99.6
93.0
85.9


Capacity Ratio
to R410A)










Condensation Glide
° C.
3.5
4.7
6.2
8.8
2.7
3.8
5.2
6.8





Item
Unit
Com Ex426
Com Ex427
Example241
Example242
Example243
Com Ex428
Com Ex429
Example244





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


R32
mass %
13.0
58.0
43.0
33.0
23.0
8.0
38.0
23.0


R1234 (ze + yf)
mass %
65.0
10.0
25.0
35.0
45.0
60.0
20.0
35.0


(r = 0.75)











CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0
2.0


GWP

91
392
292
225
158
57
258
157


COP ratio
% (relative
101.9
99.4
99.4
99.6
100.0
101.2
98.8
99.2



to R410A)










Refrigerating
% (relative
73.7
110.9
102.0
95.3
87.9
75.4
104.1
93.4


Capacity Ratio
to R410A)










Condensation Glide
° C.
9.4
1.9
3.5
4.8
6.4
8.8
3.1
5.2





Item
Unit
Example245
Com Ex430
Com Ex431
Example246
Example247
Com Ex432
Example248






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



R32
mass %
13.0
0.0
23.0
13.0
3.0
13.0
5.5



R1234 (ze + yf)
mass %
45.0
58.0
25.0
35.0
45.0
25.0
32.5



(r = 0.75)











CO2
mass %
2.0
2.0
2.0
2.0
2.0
2.0
2.0



GWP

90
3
157
90
23
89
39



COP ratio
% (relative
99.8
101.0
98.5
99.0
99.8
98.5
99.0




to R410A)










Refrigerating
% (relative
85.5
73.7
98.7
90.9
82.2
96.0
89.7



Capacity Ratio
to R410A)










Condensation Glide
° C.
6.7
8.2
4.0
5.4
6.7
4.3
5.2
















TABLE 53







3% CO2


r = 0


















Item
Unit
Com Ex433
Example249
Com Ex434
Com Ex435
Example250
Example251
Com Ex436





HFO-1132 (E)
mass %
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
57.0
47.0
32.0
57.0
47.0
37.0
22.0


R1234 (ze + yf)
mass %
30.0
40.0
55.0
20.0
30.0
40.0
55.0


(r = 0)










CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

387
320
219
386
319
252
152


COP ratio
% (relative
102
102.2
103.7
100.4
100.9
101.6
103.2



to R410A)









Refrigerating
% (relative
97
89.8
78.4
104.2
97.0
89.4
77.4


Capacity Ratio
to R410A)









Condensation Glide
° C.
6.4
8.6
12.1
4.8
6.9
9.2
12.8





Item
Unit
Com Ex437
Example252
Example253
Com Ex438
Com Ex439
Example254
Com Ex440





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


R32
mass %
57.0
37.0
27.0
12.0
37.0
22.0
7.0


R1234 (ze + yf)
mass %
10.0
30.0
40.0
55.0
20.0
35.0
50.0


(r = 0)










CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

386
252
185
85
251
151
51


COP ratio
% (relative
99.4
100.2
101.0
102.8
99.0
100.2
101.9



to R410A)









Refrigerating
% (relative
111.1
96.2
88.3
75.6
102.9
90.7
77.6


Capacity Ratio
to R410A)









Condensation Glide
° C.
3.1
7.3
9.7
13.1
5.3
8.8
12.1





Item
Unit
Com Ex441
Example255
Com Ex442
Com Ex443
Example256







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




R32
mass %
22.0
12.0
0.0
12.0
4.5




R1234 (ze + yf)
mass %
25.0
35.0
47.0
25.0
32.5




(r = 0)










CO2
mass %
3.0
3.0
3.0
3.0
3.0




GWP

151
84
3
83
33




COP ratio
% (relative
99.0
100.0
101.3
98.9
99.7





to R410A)









Refrigerating
% (relative
97.1
88.4
77.2
94.6
87.7




Capacity Ratio
to R410A)









Condensation Glide
° C.
6.7
9.0
11.3
7.0
8.5
















TABLE 54







3% CO2


r = 0.25


















Item
Unit
Com Ex444
Example257
Example258
Com Ex445
Com Ex446
Example259
Example260





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
57.0
47.0
37.0
27.0
57.0
47.0
37.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
30.0
30.0
40.0


(r = 0.25)










CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

387
320
253
186
386
319
252


COP ratio
% (relative
101.3
101.7
102.3
103.3
100.2
100.5
101.0



to R410A)









Refrigerating
% (relative
98.5
91.6
84.4
76.7
105.2
98.4
91.1


Capacity Ratio
to R410A)









Condensation Glide
° C.
5.6
7.5
9.6
11.8
4.3
6.1
8.1





Item
Unit
Example261
Com Ex447
Com Ex448
Example262
Example263
Com Ex449
Com Ex450





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


R32
mass %
27.0
17.0
57.0
37.0
27.0
12.0
37.0


R1234 (ze + yf)
mass %
50.0
60.0
10.0
30.0
40.0
55.0
20.0


(r = 0.25)










CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

185
118
386
252
185
84
251


COP ratio
% (relative
101.8
102.9
99.3
99.8
100.4
101.9
98.8



to R410A)









Refrigerating
% (relative
83.5
75.4
111.6
97.6
90.0
77.6
103.8


Capacity Ratio
to R410A)









Condensation Glide
° C.
10.3
12.5
2.9
6.4
8.6
11.8
4.7





Item
Unit
Example264
Example265
Com Ex451
Com Ex452
Example266
Com Ex453
Example267





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


R32
mass %
22.0
12.0
2.0
22.0
12.0
12.0
4.5


R1234 (ze + yf)
mass %
35.0
45.0
55.0
25.0
35.0
25.0
32.5


(r = 0.25)










CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

151
84
17
150
83
83
33


COP ratio
% (relative
99.7
100.6
101.6
98.7
99.5
98.6
99.3



to R410A)









Refrigerating
% (relative
92.2
83.8
74.7
98.2
89.8
95.6
89.0


Capacity Ratio
to R410A)









Condensation Glide
° C.
7.9
10.0
11.7
6.1
8.1
6.4
7.8
















TABLE 55







3% CO2


r = 0.5



















Item
Unit
Com Ex454
Example268
Example269
Com Ex455
Com Ex456
Example270
Example271
Example272





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
57.0
47.0
37.0
22.0
57.0
47.0
37.0
27.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
65.0
20.0
30.0
40.0
50.0


(r = 0.5)











CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

386
319
252
152
386
319
252
185


COP ratio
% (relative
101
101.2
101.6
102.8
100.0
100.2
100.4
101.0



to R410A)










Refrigerating
% (relative
100
93.4
86.4
74.9
106.2
99.8
92.9
85.4


Capacity Ratio
to R410A)










Condensation Glide
° C.
4.8
6.4
8.3
11.3
3.8
5.2
7.0
9.0





Item
Unit
Com Ex457
Com Ex458
Example273
Example274
Example275
Com Ex459
Com Ex460
Example276





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


R32
mass %
17.0
57.0
37.0
27.0
17.0
7.0
37.0
22.0


R1234 (ze + yf)
mass %
60.0
10.0
30.0
40.0
50.0
60.0
20.0
35.0


(r = 0.5)











CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

118
386
252
185
118
51
251
151


COP ratio
% (relative
101.9
99.2
99.4
99.9
100.6
101.6
98.6
99.2



to R410A)










Refrigerating
% (relative
77.5
112.0
99.0
91.6
83.7
75.0
104.8
93.6


Capacity Ratio
to R410A)










Condensation Glide
° C.
11.0
2.6
5.6
7.5
9.5
11.2
4.2
6.9





Item
Unit
Example277
Com Ex461
Com Ex462
Example278
Example279
Com Ex463
Example280






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



R32
mass %
12.0
2.0
22.0
12.0
2.0
12.0
4.5



R1234 (ze + yf)
mass %
45.0
55.0
25.0
35.0
45.0
25.0
32.5



(r = 0.5)











CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0



GWP

84
17
150
83
16
83
33



COP ratio
% (relative
100.0
100.9
98.4
99.0
99.9
98.3
98.9




to R410A)










Refrigerating
% (relative
85.5
76.4
99.2
91.2
82.3
96.7
90.2



Capacity Ratio
to R410A)










Condensation Glide
° C.
8.8
10.4
5.4
7.2
8.8
5.7
7.0
















TABLE 56







3% CO2


r = 0.75



















Item
Unit
Com Ex464
Example281
Example282
Example283
Com Ex465
Com Ex466
Example284
Example285





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
57.0
47.0
37.0
27.0
22.0
57.0
47.0
37.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
65.0
20.0
30.0
40.0


(r = 0.75)











CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

386
319
252
185
152
386
319
252


COP ratio
% (relative
100.7
100.7
100.9
101.5
101.9
99.8
99.8
99.9



to R410A)










Refrigerating
% (relative
101.3
95.2
88.4
81.0
77.1
107.1
101.1
94.5


Capacity Ratio
to R410A)










Condensation Glide
° C.
4.1
5.4
7.0
8.8
9.8
3.3
4.4
5.9





Item
Unit
Example286
Com Ex467
Com Ex468
Example287
Example288
Example289
Com Ex469
Com Ex470





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


R32
mass %
27.0
12.0
57.0
37.0
27.0
17.0
7.0
37.0


R1234 (ze + yf)
mass %
50.0
65.0
10.0
30.0
40.0
50.0
60.0
20.0


(r = 0.75)











CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

185
84
386
251
184
117
50
251


COP ratio
% (relative
100.3
101.6
99.1
99.1
99.3
99.9
100.8
98.4



to R410A)










Refrigerating
% (relative
87.3
75.2
112.5
100.3
93.2
85.5
76.9
105.7


Capacity Ratio
to R410A)










Condensation Glide
° C.
7.7
10.5
2.4
4.8
6.4
8.2
10.0
3.7





Item
Unit
Example290
Example291
Com Ex471
Com Ex472
Example292
Example293
Com Ex473
Example294





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


R32
mass %
22.0
12.0
2.0
22.0
12.0
2.0
12.0
4.5


R1234 (ze + yf)
mass %
35.0
45.0
55.0
25.0
35.0
45.0
25.0
32.5


(r = 0.75)











CO2
mass %
3.0
3.0
3.0
3.0
3.0
3.0
3.0
3.0


GWP

151
83
16
150
83
16
83
32


COP ratio
% (relative
98.7
99.4
100.2
98.1
98.6
99.4
98.1
98.5



to R410A)










Refrigerating
% (relative
95.0
87.1
78.1
100.3
92.5
83.8
97.7
91.4


Capacity Ratio
to R410A)










Condensation Glide
° C.
6.0
7.7
9.2
4.7
6.3
7.8
5.1
6.2
















TABLE 57







4% CO2


r = 0



















Item
Unit
Com Ex474
Example295
Example296
Com Ex475
Com Ex476
Example297
Example298
Example299





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
56.0
46.0
36.0
26.0
56.0
46.0
36.0
26.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
20.0
30.0
40.0
50.0


(r = 0)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

380
313
246
179
379
313
246
179


COP ratio
% (relative
101
101.9
102.8
104.0
100.1
100.5
101.2
102.3



to R410A)










Refrigerating
% (relative
98.6
91.3
83.8
75.9
105.8
98.5
90.9
83.0


Capacity Ratio
to R410A)










Condensation Glide
° C.
7.1
9.4
11.8
14.3
5.4
7.6
10.0
12.6





Item
Unit
Com Ex477
Com Ex478
Example300
Example301
Example302
Com Ex479
Com Ex480
Example303





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


R32
mass %
16.0
56.0
41.0
31.0
21.0
11.0
36.0
26.0


R1234 (ze + yf)
mass %
60.0
10.0
25.0
35.0
45.0
55.0
20.0
30.0


(r = 0)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

112
379
279
212
145
78
245
178


COP ratio
% (relative
103.5
99.0
99.5
100.2
101.2
102.5
98.6
99.3



to R410A)










Refrigerating
% (relative
74.7
112.6
101.6
93.8
85.7
77.1
104.4
96.4


Capacity Ratio
to R410A)










Condensation Glide
° C.
15.0
3.6
6.8
9.2
11.8
14.2
5.9
8.4





Item
Unit
Example304
Com Ex481
Com Ex482
Example305
Example306
Com Ex483
Example307






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



R32
mass %
16.0
1.0
21.0
11.0
6.0
11.0
3.5



R1234 (ze + yf)
mass %
40.0
55.0
25.0
35.0
40.0
25.0
32.5



(r = 0)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0



GWP

111
10
144
77
43
76
26



COP ratio
% (relative
100.3
102.4
98.6
99.5
100.1
98.5
99.2




to R410A)










Refrigerating
% (relative
88.0
74.4
98.6
90.0
85.5
96.2
89.4



Capacity Ratio
to R410A)










Condensation Glide
° C.
10.9
14.2
7.5
10.0
11.1
7.9
9.6
















TABLE 58





4% CO2


r = 0.25
























Item
Unit
Com Ex484
Example308
Example309
Com Ex485
Com Ex486
Example310
Example311
Example312





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
56.0
45.0
36.0
26.0
56.0
46.0
36.0
26.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
20.0
30.0
40.0
50.0


(r = 0.25)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

380
313
246
179
379
312
245
178


COP ratio
% (relative
101.0
101.3
102.0
103.0
99.9
100.1
100.6
101.4



to R410A)










Refrigerating
% (relative
100.1
93.1
85.8
78.2
106.8
99.9
92.6
85.0


Capacity Ratio
to R410A)










Condensation Glide
° C.
6.3
8.2
10.5
12.8
4.8
6.7
8.9
11.2





Item
Unit
Com Ex487
Com Ex488
Example313
Example314
Example315
Com Ex489
Com Ex490
Example316





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


R32
mass %
16.0
56.0
41.0
31.0
21.0
6.0
36.0
26.0


R1234 (ze + yf)
mass %
60.0
10.0
26.0
36.0
45.0
60.0
20.0
30.0


(r = 0.25)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

112
379
278
212
145
44
245
178


COP ratio
% (relative
102.5
98.9
99.2
99.7
100.5
102.1
98.4
98.9



to R410A)










Refrigerating
% (relative
76.9
113.1
102.8
95.4
87.5
74.6
105.4
97.7


Capacity Ratio
to R410A)










Condensation Glide
° C.
13.5
3.4
6.0
8.2
10.6
13.9
5.3
7.5















Item
Unit
Example317
Com Ex491
Com Ex492
Example318
Example319
Com Ex493
Example320





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


R32
mass %
16.0
1.0
21.0
11.0
5.0
11.0
3.5


R1234 (ze + yf)
mass %
40.0
55.0
25.0
35.0
40.0
25.0
32.5


(r = 0.25)










CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

111
10
144
77
43
76
26


COP ratio
% (relative
99.7
101.2
98.2
99.0
99.5
98.2
98.8



to R410A)









Refrigerating
% (relative
89.6
75.3
99.8
91.4
87.0
97.3
90.6


Capacity Ratio
to R410A)









Condensation Glide
° C.
9.8
12.9
6.8
9.0
10.1
7.2
8.8
















TABLE 59





4% CO3


r = 0.5
























Item
Unit
Com Ex494
Example321
Example322
Com Ex495
Com Ex496
Example323
Example324
Example325





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
56.0
46.0
36.0
21.0
56.0
46.0
36.0
26.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
65.0
20.0
30.0
40.0
50.0


(r = 0.5)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

380
313
246
145
379
312
245
178


COP ratio
% (relative
101
100.8
101.3
102.5
99.7
99.8
100.1
100.7



to R410A)










Refrigerating
% (relative
101
94.9
87.9
76.4
107.7
101.3
94.4
86.9


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.5
7.1
9.1
12.3
4.3
5.9
7.7
9.8





Item
Unit
Com Ex477
Com Ex478
Example300
Example301
Example302
Com Ex479
Com Ex480
Example303





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


R32
mass %
16.0
56.0
41.0
31.0
21.0
6.0
36.0
26.0


R1234 (ze + yf)
mass %
60.0
10.0
25.0
35.0
45.0
60.0
20.0
30.0


(r = 0.5)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

111
379
278
211
144
44
244
177


COP ratio
% (relative
101.6
98.8
98.9
99.2
99.8
101.3
98.2
98.5



to R410A)










Refrigerating
% (relative
78.9
113.6
104.0
96.9
89.3
76.6
106.3
99.0


Capacity Ratio
to R410A)










Condensation Glide
° C.
12.0
3.1
5.3
7.2
9.3
12.4
4.8
6.7


















Item
Unit
Example330
Com Ex501
Com Ex502
Example331
Example332
Com Ex503
Example333





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


R32
mass %
16.0
1.0
21.0
11.0
6.0
11.0
3.5


R1234 (ze + yf)
mass %
40.0
55.0
25.0
35.0
40.0
25.0
32.5


(r = 0.5)










CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

110
10
144
77
43
76
26


COP ratio
% (relative
99.1
100.5
97.9
98.6
99.0
97.9
98.4



to R410A)









Refrigerating
% (relative
91.2
78.0
100.9
92.8
88.5
98.3
91.9


Capacity Ratio
to R410A)









Condensation Glide
° C.
8.7
11.6
6.1
8.1
9.1
6.6
8.0
















TABLE 60





4% CO2


r = 0.75
























Item
Unit
Com Ex504
Example334
Example335
Example336
Com Ex505
Com Ex506
Example337
Example338





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
56.0
46.0
35.0
26.0
16.0
56.0
46.0
36.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
70.0
20.0
30.0
40.0


(r = 0.75)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

379
312
245
178
111
379
312
245


COP ratio
% (relative
100.3
100.4
100.6
101.2
102.1
99.4
99.4
99.6



to R410A)










Refrigerating
% (relative
102.8
96.7
89.9
82.5
74.4
108.7
102.7
96.1


Capacity Ratio
to R410A)










Condensation Glide
° C.
4.7
6.0
7.7
9.8
11.9
3.8
5.0
6.6





Item
Unit
Example339
Com Ex507
Com Ex508
Example340
Example341
Example342
Com Ex509
Com Ex510





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


R32
mass %
26.0
11.0
56.0
41.0
31.0
21.0
1.0
36.0


R1234 (ze + yf)
mass %
50.0
65.0
10.0
25.0
35.0
45.0
65.0
20.0


(r = 0.75)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

178
77
379
278
211
144
10
244


COP ratio
% (relative
100.0
101.2
98.7
98.6
98.8
99.2
100.9
98.0



to R410A)










Refrigerating
% (relative
88.8
76.7
114.1
105.1
98.4
91.0
73.6
107.3


Capacity Ratio
to R410A)










Condensation Glide
° C.
8.5
11.6
2.9
4.7
6.2
8.1
11.9
4.3





Item
Unit
Example343
Example344
Example345
Com Ex511
Example346
Example347
Com Ex512
Examp1e348





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


R32
mass %
26.0
16.0
6.0
21.0
11.0
6.0
11.0
3.5


R1234
mass %
30.0
40.0
50.0
25.0
35.0
40.0
25.0
32.5


(ze + yf)











(r = 0.75)











CO2
mass %
4.0
4.0
4.0
4.0
4.0
4.0
4.0
4.0


GWP

177
110
43
143
76
43
76
26


COP ratio
% (relative
98.1
98.6
99.4
97.7
98.2
98.5
97.6
98.1



to R410A)










Refrigerating
% (relative
100.3
92.7
84.3
101.9
94.1
89.9
99.3
93.1


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.8
7.7
9.6
5.4
7.2
8.1
5.9
7.2
















TABLE 61





5% CO2


r = 0
























Item
Unit
Com Ex513
Example349
Example350
Com Ex514
Com Ex515
Example351
Example352
Example353





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
55.0
45.0
35.0
25.0
55.0
45.0
35.0
25.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
20.0
30.0
40.0
50.0


(r = 0)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

373
306
239
173
373
306
239
172


COP ratio
% (relative
101
101.5
102.5
103.7
99.7
100.1
100.9
101.9



to R410A)










Refrigerating
% (relative
100
92.8
85.2
77.3
107.3
100.0
92.4
84.5


Capacity Ratio
to R410A)










Condensation Glide
° C.
7.7
10.1
12.7
15.3
5.9
8.2
10.8
13.5





Item
Unit
Com Ex516
Com Ex517
Example354
Example355
Example356
Com Ex518
Com Ex519
Example357





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


R32
mass %
15.0
55.0
40.0
30.0
20.0
10.0
35.0
25.0


R1234 (ze + yf)
mass %
60.0
10.0
25.0
35.0
46.0
55.0
20.0
30.0


(r = 0)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

105
372
272
205
138
71
238
171


COP ratio
% (relative
103.2
98.6
99.1
99.8
100.9
102.1
98.2
98.9



to R410A)










Refrigerating
% (relative
76.2
114.2
103.2
95.3
87.2
78.7
106.0
97.9


Capacity Ratio
to R410A)










Condensation Glide
° C.
15.1
4.1
7.4
10.0
12.7
15.3
6.5
9.1


















Item
Unit
Example358
Com Ex520
Com Ex521
Example359
Example360
Com Ex522
Example361





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


R32
mass %
15.0
0.0
20.0
10.0
5.0
10.0
2.5


R1234 (ze + yf)
mass %
40.0
55.0
25.0
35.0
40.0
25.0
32.5


(r = 0)










CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

104
4
137
70
37
70
19


COP ratio
% (relative
99.9
101.7
98.3
99.1
99.7
98.0
98.8



to R410A)









Refrigerating
% (relative
89.6
76.0
100.2
91.6
87.1
97.9
91.0


Capacity Ratio
to R410A)









Condensation Glide
° C.
11.8
15.4
8.2
10.8
12.1
8.7
10.5
















TABLE 62





5% CO2


r = 0.25
























Item
Unit
Com Ex523
Example362
Example363
Com Ex524
Com Ex525
Example364
Example365
Example366





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
55.0
45.0
35.0
20.0
55.0
45.0
35.0
25.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
65.0
20.0
30.0
40.0
50.0


(r = 0.25)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

373
306
239
139
373
306
239
172


COP ratio
% (relative
100.6
101.0
101.7
103.2
99.5
99.8
100.3
101.1



to R410A)










Refrigerating
% (relative
101.6
94.6
87.3
75.6
108.3
101.5
94.2
86.5


Capacity Ratio
to R410A)










Condensation Glide
° C.
6.9
9.0
11.3
15.0
5.4
7.3
9.6
12.1





Item
Unit
Com Ex526
Com Ex527
Example367
Example368
Example369
Com Ex528
Com Ex529
Example370





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


R32
mass %
10.0
55.0
40.0
30.0
20.0
5.0
35.0
25.0


R1234 (ze + yf)
mass %
65.0
10.0
25.0
36.0
45.0
60.0
20.0
30.0


(r = 0.25)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

71
372
272
205
138
37
238
171


COP ratio
% (relative
102.8
98.5
98.8
99.3
100.1
101.8
98.0
98.5



to R410A)










Refrigerating
% (relative
74.0
114.7
104.4
96.9
89.4
76.2
107.0
99.3


Capacity Ratio
to R410A)










Condensation Glide
° C.
15.7
3.8
6.6
8.9
11.4
15.0
5.9
8.2





Item
Unit
Example371
Example372
Com Ex530
Com Ex531
Example373
Example374
Com Ex532
Example375





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


R32
mass %
15.0
5.0
0.0
20.0
10.0
5.0
10.0
2.5


R1234 (ze + yf)
mass %
40.0
50.0
55.0
25.0
35.0
40.0
25.0
32.5


(r = 0.25)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

104
37
3
137
70
37
70
19


COP ratio
% (relative
99.3
100.3
100.8
97.8
98.6
99.1
97.7
92.3



to R410A)










Refrigerating
% (relative
91.2
82.5
77.9
101.4
93.0
88.7
98.9
92.3


Capacity Ratio
to R410A)










Condensation Glide
° C.
10.7
18.1
14.2
7.6
9.9
11.1
8.0
9.7
















TABLE 63





5% CO2


r = 0.5
























Item
Unit
Com Ex533
Example376
Example377
Com Ex534
Com Ex535
Example378
Example379
Example380





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
55.0
45.0
35.0
20.0
55.0
45.0
35.0
25.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
65.0
20.0
30.0
40.0
50.0


(r = 0.5)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

373
306
239
138
373
306
239
172


COP ratio
% (relative
100
100.5
100.9
102.2
99.3
99.4
99.7
100.3



to R410A)










Refrigerating
% (relative
103
96.4
89.4
77.9
109.3
102.9
95.9
88.5


Capacity Ratio
to R410A)










Condensation Glide
° C.
6.0
7.8
9.9
13.4
4.8
6.5
8.4
10.7





Item
Unit
Com Ex536
Com Ex537
Example381
Example382
Example383
Com Ex538
Com Ex539
Example384





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


R32
mass %
10.0
55.0
40.0
30.0
20.0
5.0
35.0
25.0


R1234 (ze + yf)
mass %
65.0
10.0
25.0
35.0
45.0
60.0
20.0
30.0


(r = 0.5)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

71
382
282
205
138
37
238
171


COP ratio
% (relative
101.8
98.4
98.5
98.8
99.5
100.9
97.8
98.1



to R410A)










Refrigerating
% (relative
76.2
115.2
105.6
98.4
90.8
78.1
107.9
100.6


Capacity Ratio
to R410A)










Condensation Glide
° C.
14.2
3.6
5.9
7.9
10.2
13.6
5.4
7.3


















Item
Unit
Example385
Example386
Com Ex540
Example387
Example388
Com Ex541
Example389





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


R32
mass %
15.0
5.0
20.0
10.0
5.0
10.0
2.5


R1234 (ze + yf)
mass %
40.0
50.0
25.0
35.0
40.0
25.0
32.5


(r = 0.5)










CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

104
37
137
70
36
69
19


COP ratio
% (relative
98.7
99.6
97.5
98.2
98.6
97.4
98.0



to R410A)









Refrigerating
% (relative
92.8
94.3
102.5
94.4
90.1
100.0
93.6


Capacity Ratio
to R410A)









Condensation Glide
° C.
9.6
11.8
6.8
9.0
10.1
7.4
8.9
















TABLE 64





5% CO2


r = 0.75
























Item
Unit
Com Ex542
Example390
Example391
Example392
Com Ex543
Com Ex544
Example393
Example394





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
55.0
45.0
35.0
25.0
15.0
55.0
45.0
35.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
70.0
20.0
30.0
40.0


(r = 0.75)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

373
306
239
172
105
372
305
238


COP ratio
% (relative
100.0
100.0
100.3
100.9
101.8
99.1
99.1
99.2



to R410A)










Refrigerating
% (relative
104.4
98.2
91.3
84.0
75.9
110.2
104.2
97.6


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.3
6.7
8.5
10.7
13.0
4.3
5.6
7.3





Item
Unit
Com Ex395
Com Ex545
Com Ex546
Example396
Example397
Example398
Com Ex547
Example399





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


R32
mass %
25.0
5.0
55.0
40.0
30.0
20.0
10.0
35.0


R1234 (ze + yf)
mass %
50.0
70.0
10.0
25.0
35.0
45.0
55.0
20.0


(r = 0.75)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

171
37
372
271
204
137
70
238


COP ratio
% (relative
99.6
101.4
98.3
98.3
98.4
98.8
99.7
97.6



to R410A)










Refrigerating
% (relative
90.3
73.6
115.7
106.7
99.9
92.5
84.4
108.9


Capacity Ratio
to R410A)










Condensation Glide
° C.
9.3
13.8
3.3
5.2
6.9
8.9
11.2
4.8





Item
Unit
Example400
Example401
Example402
Com Ex548
Example403
Example404
Com Ex549
Example405





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


R32
mass %
25.0
15.0
5.0
20.0
10.0
5.0
10.0
2.5


R1234 (ze + yf)
mass %
30.0
40.0
50.0
25.0
35.0
40.0
25.0
32.5


(r = 0.75)











CO2
mass %
5.0
5.0
5.0
5.0
5.0
5.0
5.0
5.0


GWP

171
104
36
137
70
36
69
19


COP ratio
% (relative
97.7
98.2
99.0
97.2
97.8
98.1
97.2
97.7



to R410A)










Refrigerating
% (relative
101.9
94.3
85.9
103.5
95.8
91.6
101.0
94.8


Capacity Ratio
to R410A)










Condensation Glide
° C.
6.5
8.5
10.6
6.1
9.1
9.1
6.7
8.1
















TABLE 65





5.59% CO2


r = 0
























Item
Unit
Com Ex550
Example406
Example407
Com Ex551
Com Ex552
Example408
Example409
Example410





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
54.5
44.5
34.5
24.5
54.5
44.5
34.5
24.5


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
20.0
30.0
40.0
50.0


(r = 0)











CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

370
303
236
169
369
302
236
169


COP ratio
% (relative
101
101.4
102.3
103.6
99.5
100.0
100.7
101.8



to R410A)










Refrigerating
% (relative
101
93.5
85.9
78.1
108.1
100.8
93.1
85.2


Capacity Ratio
to R410A)










Condensation Glide
° C.
8.0
10.4
13.1
15.8
6.2
8.5
11.1
13.9





Item
Unit
Com Ex553
Com Ex554
Example411
Example412
Example413
Example414
Com Ex555
Com Ex556





HFO-1132 (E)
mass %
20.0
30.0
30.0
30.0
3.0
30.0
30.0
40.0


R32
mass %
14.5
54.5
44.5
34.5
24.5
14.5
4.5
34.5


R1234 (ze + yf)
mass %
60.0
10.0
20.0
30.0
40.0
50.0
60.0
20.0


(r = 0)











CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

102
369
302
235
168
101
34
265


COP ratio
% (relative
103.1
98.4
98.7
99.2
100.1
101.3
102.6
98.0



to R410A)










Refrigerating
% (relative
76.9
115.0
107.7
100.0
92.1
83.8
74.9
106.8


Capacity Ratio
to R410A)










Condensation Glide
° C.
16.6
4.3
6.4
8.9
11.7
14.5
17.0
6.8





Item
Unit
Example415
Example416
Example417
Com Ex557
Example418
Example419
Com Ex558
Example420





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


R32
mass %
24.5
14.5
4.5
19.5
14.5
4.5
9.5
4.5


R1234 (ze + yf)
mass %
30.0
40.0
50.0
25.0
30.0
40.0
25.0
30.0


(r = 0)











CO2
mass %
5.5
5.5
5.5
5.5
5.5
5.5
5.5
5.5


GWP

168
101
34
134
100
33
66
33


COP ratio
% (relative
98.7
98.7
100.9
97.9
98.4
99.5
97.8
98.3



to R410A)










Refrigerating
% (relative
98.7
90.4
81.5
101.0
96.8
87.9
98.7
94.2


Capacity Ratio
to R410A)










Condensation Glide
° C.
9.4
12.2
14.8
8.5
9.9
12.6
9.0
10.3
















TABLE 66





5.5% CO2


r = 0.25
























Item
Unit
Com Ex559
Example421
Example422
Com Ex560
Com Ex561
Example423
Example424
Example425





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
54.0
44.0
34.0
19.0
54.0
44.0
34.0
24.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
65.0
20.0
30.0
40.0
50.0


(r = 0.25)











CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

366
299
232
132
366
299
232
165


COP ratio
% (relative
100.3
100.7
101.4
103.0
99.1
99.4
99.9
100.8



to R410A)










Refrigerating
% (relative
103.1
96.1
88.8
77.1
109.9
103.0
95.7
88.0


Capacity Ratio
to R410A)










Condensation Glide
° C.
7.5
9.6
12.1
16.0
5.9
7.9
10.3
12.9





Item
Unit
Com Ex562
Com Ex563
Example426
Example427
Example428
Example429
Com Ex564
Com Ex565





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


R32
mass %
9.0
54.0
44.0
34.0
24.0
14.0
0.0
34.0


R1234 (ze + yf)
mass %
65.0
10.0
20.0
30.0
40.0
50.0
64.0
20.0


(r = 0.25)











CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

65
365
298
232
165
98
4
231


COP ratio
% (relative
102.5
98.1
98.3
98.6
99.3
100.3
101.8
97.6



to R410A)










Refrigerating
% (relative
75.6
116.3
109.5
102.2
94.6
86.5
74.0
108.5


Capacity Ratio
to R410A)










Condensation Glide
° C.
16.9
4.3
6.1
8.4
10.9
13.6
17.1
6.5





Item
Unit
Example430
Example431
Example432
Com Ex566
Example433
Example434
Com Ex567
Example435





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


R32
mass %
24.0
14.0
24.0
14.0
4.0
4.0
14.0
4.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
20.0
30.0
40.0
20.0
30.0


(r = 0.25)











CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

164
97
30
164
97
30
96
29


COP ratio
% (relative
98.1
98.9
100.0
97.1
97.8
98.7
96.9
97.7



to R410A)










Refrigerating
% (relative
100.9
92.8
84.2
107.0
98.9
90.3
104.8
96.3


Capacity Ratio
to R410A)










Condensation Glide
° C.
8.9
11.5
14.1
6.9
9.4
12.0
7.5
10.0
















TABLE 67





5.5% CO2


r = 0.5
























Item
Unit
Com Ex568
Example436
Example437
Example438
Com Ex569
Com Ex570
Example439
Example440





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
54.0
44.0
34.0
24.0
14.0
54.0
44.0
34.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
70.0
20.0
30.0
40.0


(r = 0.5)











CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

366
299
232
265
98
366
299
232


COP ratio
% (relative
100
100.1
100.6
101.4
102.5
98.9
99.0
99.3



to R410A)










Refrigerating
% (relative
105
97.9
90.9
83.3
75.2
110.9
104.4
97.4


Capacity Ratio
to R410A)










Condensation Glide
° C.
6.6
8.5
10.7
13.1
15.6
5.3
7.0
9.1





Item
Unit
Example441
Com Ex571
Com Ex572
Example442
Example443
Example444
Example445
Com Ex573





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


R32
mass %
24.0
9.0
54.0
44.0
34.0
24.0
14.0
34.0


R1234 (ze + yf)
mass %
50.0
65.0
10.0
20.0
30.0
40.0
50.0
20.0


(r = 0.5)











CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

165
64
365
29
231
164
97
231


COP ratio
% (relative
100.0
101.5
98.0
98.1
98.3
98.7
99.6
97.4



to R410A)










Refrigerating
% (relative
90.0
77.7
116.8
110.5
103.6
96.2
88.4
109.5


Capacity Ratio
to R410A)










Condensation Glide
° C.
11.5
15.3
4.0
5.6
7.5
9.7
12.2
5.9





Item
Unit
Example446
Example447
Example448
Com Ex574
Example449
Example450
Com Ex575
Example451





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


R32
mass %
15.0
5.0
5.0
24.0
14.0
4.0
14.0
4.0


R1234 (ze + yf)
mass %
39.0
49.0
50.0
20.0
3.0
40.0
20.0
30.0


(r = 0.5)











CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

104
37
37
164
94
30
96
29


COP ratio
% (relative
98.3
99.2
99.6
96.9
97.4
98.2
96.7
97.4



to R410A)










Refrigerating
% (relative
95.2
86.8
84.3
107.9
100.2
91.8
105.7
97.4


Capacity Ratio
to R410A)










Condensation Glide
° C.
10.1
12.6
11.8
6.4
8.6
11.0
7.0
9.3
















TABLE 68





5.5% CO2


r = 0.75
























Item
Unit
Com Ex576
Example452
Example453
Example454
Com Ex577
Com Ex578
Example455
Example456





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
54.0
44.0
34.0
24.0
9.0
54.0
44.0
34.0


R1234 (ze + yf)
mass %
30.0
40.0
50.0
60.0
70.0
20.0
30.0
40.0


(r = 0.75)











CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

366
299
232
165
64
366
299
232


COP ratio
% (relative
99.6
99.7
99.9
100.6
102.0
98.7
98.7
98.8



to R410A)










Refrigerating
% (relative
105.9
99.7
92.8
85.4
72.8
11.8
105.8
99.1


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.8
7.3
9.3
11.5
15.2
4.8
6.2
7.9





Item
Unit
Example457
Example458
Com Ex579
Com Ex580
Example459
Example460
Example461
Example462





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


R32
mass %
24.0
14.0
4.0
54.0
44.0
34.0
24.0
14.0


R1234 (ze + yf)
mass %
50.0
60.0
70.0
10.0
20.0
30.0
40.0
50.0


(r = 0.75)











CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

165
97
30
365
298
231
164
97


COP ratio
% (relative
99.3
100.1
101.1
97.9
97.9
97.9
98.2
98.9



to R410A)










Refrigerating
% (relative
91.9
84.0
75.1
117.3
11.5
105.0
978
90.1


Capacity Ratio
to R410A)










Condensation Glide
° C.
10.1
12.6
15.0
3.8
5.0
6.6
8.6
10.9





Item
Unit
Example463
Com Ex581
Example464
Example465
Example466
Com Ex582
Example467
Example468





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


R32
mass %
4.0
34.0
24.0
14.0
4.0
24.0
14.0
4.0


R1234 (ze + yf)
mass %
60.0
20.0
30.0
40.0
50.0
20.0
30.0
40.0


(r = 0.75)











CO2
mass %
6.0
6.0
6.0
6.0
6.0
6.0
6.0
6.0


GWP

30
231
164
97
30
163
96
29


COP ratio
% (relative
99.8
97.2
97.3
97.8
98.7
96.7
97.0
97.7



to R410A)










Refrigerating
% (relative
81.6
110.4
103.5
95.9
87.6
108.8
101.4
93.2


Capacity Ratio
to R410A)










Condensation Glide
° C.
13.4
5.4
7.1
9.3
11.6
5.8
7.8
10.0













Item
Unit
Com Ex583
Example469





HFO-1132 (E)
mass %
60.0
60.0


R32
mass %
14.0
4.0


R1234 (ze + yf)
mass %
20.0
30.0


(r = 0.75)





CO2
mass %
6.0
6.0


GWP

96
29


COP ratio
% (relative
96.5
97.0



to R410A)




Refrigerating
% (relative
106.5
98.6


Capacity Ratio
to R410A)




Condensation Glide
° C.
6.5
8.5
















TABLE 69





7.5% CO2


r = 0
























Item
Unit
Com Ex584
Example470
Example471
Com Ex585
Com Ex586
Example472
Example473
Example474





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
20.0
20.0
20.0
20.0


R32
mass %
57.5
42.5
32.5
17.5
57.5
42.5
32.5
22.5


R1234 (ze + yf)
mass %
25.0
40.0
50.0
65.0
15.0
30.0
40.0
50.0


(r = 0)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

390
289
223
122
389
289
222
155


COP ratio
% (relative
100
100.7
101.7
103.8
98.7
99.2
100.0
101.2



to R410A)










Refrigerating
% (relative
107
96.5
88.9
76.9
114.7
103.8
96.1
88.2


Capacity Ratio
to R410A)










Condensation Glide
° C.
8.0
11.8
14.7
19.1
6.1
9.6
12.5
15.5





Item
Unit
Com Ex587
Com Ex588
Example475
Example476
Example477
Example478
Com Ex589
Com Ex590





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


R32
mass %
7.5
57.5
42.5
32.5
22.5
12.5
0.0
37.5


R1234 (ze + yf)
mass %
65.0
5.0
20.0
30.0
40.0
50.0
62.5
15.0


(r = 0)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

55
389
288
222
155
88
4
255


COP ratio
% (relative
103.2
97.5
97.9
98.5
99.4
100.7
102.3
97.0



to R410A)










Refrigerating
% (relative
75.6
121.6
110.8
103.1
9.1
86.9
75.7
113.8


Capacity Ratio
to R410A)










Condensation Glide
° C.
20.0
4.2
7.4
10.1
13.1
16.3
19.9
6.5





Item
Unit
Example479
Example480
Example481
Com Ex591
Example482
Example483
Com Ex592
Example484





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


R32
mass %
22.5
12.5
2.5
22.5
12.5
2.5
12.5
2.5


R1234 (ze + yf)
mass %
30.0
40.0
50.0
20.0
30.0
40.0
20.0
30.0


(r = 0)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

154
87
20
154
87
20
86
19


COP ratio
% (relative
97.9
99.0
100.2
96.7
97.6
98.7
96.5
97.5



to R410A)










Refrigerating
% (relative
101.8
93.5
84.7
108.4
100.0
91.2
106.3
97.5


Capacity Ratio
to R410A)










Condensation Glide
° C.
10.7
13.8
16.8
8.4
11.3
14.4
9.0
12.0
















TABLE 70





7.5% CO2


r = 0.25
























Item
Unit
Com Ex593
Example485
Example486
Example487
Com Ex594
Com Ex595
Example488
Example489





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
57.5
42.5
32.5
22.5
12.5
57.5
42.5
32.5


R1234 (ze + yf)
mass %
25.0
40.0
50.0
60.0
70.0
15.0
30.0
40.0


(r = 0.25)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

390
289
222
155
88
389
289
222


COP ratio
% (relative
99.6
100.2
100.9
102.0
103.2
98.5
98.9
99.4



to R410A)










Refrigerating
% (relative
108.7
98.4
91.0
83.4
75.1
115.5
105.3
98.0


Capacity Ratio
to R410A)










Condensation Glide
° C.
7.3
10.6
13.2
16.1
18.9
5.7
8.7
11.3





Item
Unit
Example490
Com Ex596
Com Ex597
Example491
Example492
Example493
Example494
Com Ex598





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


R32
mass %
22.5
7.5
57.5
42.5
32.5
22.5
12.5
37.5


R1234 (ze + yf)
mass %
50.0
65.0
5.0
20.0
30.0
40.0
50.0
15.0


(r = 0.25)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

155
54
389
288
221
154
88
254


COP ratio
% (relative
100.3
102.1
97.5
97.7
98.1
98.8
99.8
96.8



to R410A)










Refrigerating
% (relative
90.3
77.9
121.9
111.9
104.6
96.9
88.9
114.6


Capacity Ratio
to R410A)










Condensation Glide
° C.
14.1
18.5
4.1
6.9
9.2
12.0
14.9
6.1





Item
Unit
Example495
Example496
Example497
Com Ex599
Example498
Example499
Com Ex600
Example500





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


R32
mass %
22.5
12.5
2.5
22.5
12.5
2.5
12.5
2.5


R1234 (ze + yf)
mass %
30.0
40.0
50.0
20.0
30.0
40.0
20.0
30.0


(r = 0.25)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

154
87
20
154
87
20
86
19


COP ratio
% (relative
97.5
98.4
99.5
96.5
97.2
98.1
96.3
97.1



to R410A)










Refrigerating
% (relative
103.2
95.2
86.6
109.4
101.3
92.8
107.3
98.8


Capacity Ratio
to R410A)










Condensation Glide
° C.
9.8
12.0
15.6
7.8
10.5
13.3
8.0
11.2
















TABLE 71





7.5% CO2


r = 0.5
























Item
Unit
Com Ex601
Example501
Example502
Example503
Com Ex602
Com Ex603
Example504
Example505





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
57.5
42.5
32.5
22.5
12.5
57.5
42.5
32.5


R1234 (ze + yf)
mass %
25.0
40.0
50.0
60.0
70.0
15.0
30.0
40.0


(r = 0.5)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

390
289
222
155
88
389
289
222


COP ratio
% (relative
99
99.6
100.1
101.0
102.1
98.3
98.5
98.8



to R410A)










Refrigerating
% (relative
110
100.2
93.1
85.6
77.5
116.2
106.7
99.7


Capacity Ratio
to R410A)










Condensation Glide
° C.
6.6
9.4
11.8
14.5
17.3
5.3
7.9
10.1





Item
Unit
Example506
Example507
Com Ex604
Com Ex605
Example508
Example509
Example510
Example511





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


R32
mass %
22.5
12.5
2.5
57.5
42.5
32.5
22.5
12.5


R1234 (ze + yf)
mass %
50.0
60.0
70.0
5.0
20.0
30.0
40.0
50..0


(r = 0.5)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

155
88
21
289
288
221
154
87


COP ratio
% (relative
99.5
100.6
101.6
97.4
97.5
97.7
98.2
99.1



to R410A)










Refrigerating
% (relative
92.3
84.3
75.5
122.1
112.9
106.0
98.6
90.7


Capacity Ratio
to R410A)










Condensation Glide
° C.
12.7
15.5
18.3
3.9
6.3
8.3
10.8
13.5





Item
Unit
Example512
Com Ex606
Example513
Example514
Example515
Com Ex607
Example516
Example517





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


R32
mass %
2.5
37.5
22.5
12.5
2.5
22.5
12.5
2.5


R1234 (ze + yf)
mass %
60.0
15.0
30.0
40.0
50.0
20.0
30.0
40.0


(r = 0.5)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

20
254
154
87
20
153
86
19


COP ratio
% (relative
100.1
96.7
97.1
97.8
98.8
96.3
96.8
97.6



to R410A)










Refrigerating
% (relative
82.2
115.4
104.6
96.8
88.4
110.3
102.6
94.3


Capacity Ratio
to R410A)










Condensation Glide
° C.
16.4
5.7
8.9
11.5
14.3
7.2
9.6
12.3













Item
Unit
Com Ex608
Example518





HFO-1132 (E)
mass %
60.0
60.0


R32
mass %
12.5
2.5


R1234 (ze + yf)
mass %
20.0
30.0


(r = 0.5)





CO2
mass %
7.5
7.5


GWP

86
19


COP ratio
% (relative
96.0
96.8



to R410A)




Refrigerating
% (relative
108.2
100.0


Capacity Ratio
to R410A)




Condensation Glide
° C.
7.9
10.5
















TABLE 72





7.5% CO2


r = 0.75
























Item
Unit
Com Ex609
Example519
Example520
Example521
Com Ex610
Com Ex611
Example522
Example523





HFO-1132 (E)
mass %
10.0
10.0
10.0
10.0
10.0
20.0
20.0
20.0


R32
mass %
57.5
42.5
32.5
22.5
7.5
57.5
42.5
32.5


R1234 (ze + yf)
mass %
25.0
40.0
50.0
60.0
75.0
15.0
30.0
40.0


(r = 0.75)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

389
289
222
155
54
389
289
221


COP ratio
% (relative
99.1
99.2
99.4
100.1
101.7
98.2
98.1
98.3



to R410A)










Refrigerating
% (relative
111.1
102.0
95.1
87.7
75.1
117.0
108.1
101.4


Capacity Ratio
to R410A)










Condensation Glide
° C.
5.9
8.3
10.4
12.9
17.1
4.9
7.0
8.9





Item
Unit
Example524
Example525
Com Ex612
Com Ex613
Example526
Example527
Example528
Example529





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


R32
mass %
22.5
12.5
0.0
57.5
42.5
32.5
22.5
12.5


R1234 (ze + yf)
mass %
50.0
60.0
72.5
5.0
20.0
30.0
40.0
50.0


(r = 0.75)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

154
87
4
389
288
221
154
87


COP ratio
% (relative
98.8
99.7
100.9
97.4
97.3
97.3
97.6
98.4



to R410A)










Refrigerating
% (relative
94.2
86.3
75.0
122.4
113.8
107.3
100.2
92.5


Capacity Ratio
to R410A)










Condensation Glide
° C.
11.3
14.0
17.5
3.8
5.7
7.5
9.6
12.2





Item
Unit
Example530
Com Ex614
Example531
Example531
Example532
Com Ex615
Example533
Example534





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


R32
mass %
2.5
37.5
22.5
12.5
2.5
22.5
12.5
2.5


R1234 (ze + yf)
mass %
60.0
15.0
30.0
40.0
50.0
20.0
30.0
40.0


(r = 0.75)











CO2
mass %
7.5
7.5
7.5
7.5
7.5
7.5
7.5
7.5


GWP

20
254
154
87
20
153
86
19


COP ratio
% (relative
99.4
96.5
96.7
97.3
98.1
96.0
9.4
97.2



to R410A)










Refrigerating
% (relative
84.0
116.1
105.9
98.3
90.0
111.2
103.8
95.7


Capacity Ratio
to R410A)










Condensation Glide
° C.
15.0
5.3
8.1
10.4
13.1
6.7
8.8
11.3













Item
Unit
Com Ex616
Example535





HFO-1132 (E)
mass %
60.0
60.0


R32
mass %
12.5
2.5


R1234 (ze + yf)
mass %
20.0
30.0


(r = 0.75)





CO2
mass %
7.5
7.5


GWP

86
19


COP ratio
% (relative
95.8
96.4



to R410A)




Refrigerating
% (relative
109.0
101.1


Capacity Ratio
to R410A)




Condensation Glide
° C.
7.4
9.7









DESCRIPTION OF THE REFERENCE NUMERALS




  • 1: Sample cell


  • 2: High-speed camera


  • 3: Xenon lamp


  • 4: Collimating lens


  • 5: Collimating lens


  • 6: Ring filter


Claims
  • 1. A composition comprising a refrigerant, the refrigerant comprising trans-1,2-difluoroethylene (HFO-1132(E)), difluoromethane (R32), 1,3,3,3-tetrafluoropropene (R1234ze), and carbon dioxide (CO2).
  • 2. The composition according to claim 1, wherein in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,(1) if 0<a≤0.4, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MN, NO, OK, KH, and HL that connect 7 points, i.e.,points L, L′, M, N, O, K, and H, or on the straight lines LL′, L′M, MN, NO, OK, and KH (excluding the points L and H):point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),point K (−2.5a+1.0, −0.25a+51.5, 1.75a+47.5), andpoint H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4), (2) if 0.4≤a≤7.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines LL′, L′M, MN, NO, OB″, B″K′, K′H, and HL that connect 8 points, i.e., points L, L′, M, N, O, B″, K′, and H, or on the straight lines LL′, L′M, MN, NO, OB″, and K′H (excluding the points L, B″, K′, and H), andif 0.4≤a≤1.0, the 8 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),point B″ (0.0, 51.4, −a+48.6),point K′ (0.0, −3.0a+52.6, 2.0a+47.4), andpoint H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),if 1.0<a≤3.0, the 8 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+36.679, 0.0175a+36.679, −a+27.6),point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),point B″ (0.0, 51.4, −a+48.6),point K′ (0, −2.9a+52.5, 1.9a+47.5), andpoint H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),if 3.0<a≤5.0, the 8 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),point B″ (0.0, 51.4, −a+48.6),point K′ (0, −2.9a+52.5, 1.9a+47.5), andpoint H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), orif 5.0<a≤7.5, the 8 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),point O (−0.0095a+28.914, 0.0095a+51.586, −a+19.5),point B″ (0.0, 51.4, −a+48.6),point K′ (0, −2.8286a+52.105, 1.8286a+47.895), andpoint H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).
  • 3. The composition according to claim 1, wherein in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a,(1) if 0<a≤5.5, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MN, NJ, JH, and HL that connect 6 points, i.e., points L, L′, M, N, J, and H, or on the straight lines LL′, L′M, MN, NJ, and JH (excluding the points L and H), andif 0<a≤1.0, the 6 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),point J (−0.3333a2−3.3667a+20.3, 36.6, 0.3333a2+2.3667a+43), andpoint H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),if 1.0<a≤3.0, the 6 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),point J (0.05a2−3.95a+20.5, 0.05a2−0.25a+36.8, −0.1a2+3.2a+42.7), andpoint H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),if 3.0<a≤5.0, the 6 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),point J (0.05a2−4.05a+20.8, 36.5, −0.05a2+3.05a+42.7), andpoint H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), orif 5.0<a≤5.5, the 6 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),point J (−3.6a+19.8, 36.5, 2.6a+43.7), andpoint H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25), (2) if 5.5<a≤7.5, coordinates (x,y,z) in the ternary composition diagram are within the range of a figure surrounded by straight lines LL′, L′M, MN, NB′, B′K′, K′H, and HL that connect 7 points, i.e., points L, L′, M, N, B′, K′, and H, or on the straight lines LL′, L′M, MN, NB′, K′H, and HL (excluding the points L, B′, K′, and H):point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point N (−0.0175a+35.721, 0.0175a+36.679, −a+27.6),point B′ (0.0, 36.5, −a+63.5),point K′ (0.0, −2.8286a+52.105, 1.8281a+47.895), andpoint H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).
  • 4. The composition according to claim 1, wherein in the refrigerant, when the mass % of HFO-1132(E), R32, R1234ze, and CO2 based on their sum is respectively represented by x, y, z, and a, coordinates (x,y,z) in a ternary composition diagram in which the sum of HFO-1132(E), R32, and R1234ze is (100−a) mass % are within the range of a figure surrounded by straight lines LL′, L′M, MI, IH, and HL that connect 5 points, i.e., points L, L′, M, I, and H, or on the straight lines LL′, L′M, MI, and IH (excluding the points L and H), andif 0<a≤1.0, the 5 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point I (−0.1667a2−3.9333a+44.2, 18.1, 0.1667a2+2.9333a+37.7), andpoint H (0.1667a2−4.5667a+67.6, 0.0, −0.1667a2+3.5667a+32.4),if 1.0<a≤3.0, the 5 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point I (0.05a2−4.25a+44.3, 18.1, −0.05a2+3.25a+37.6), andpoint H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3),if 3.0<a≤5.0, the 5 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point I (−0.05a2−3.45a+42.8, 0.05a2−0.45a+19.0, 2.9a+38.2), andpoint H (0.05a2−4.55a+67.7, 0.0, −0.05a2+3.55a+32.3), orif 5.0<a≤7.5, the 5 points are the following:point L (72.0, 0.0, −a+28.0),point L′ (57.2, 10.0, −a+32.8),point M (−0.019a+48.618, 0.019a+18.082, −a+33.3),point I (0.1a2−4.85a+46.05, −0.02a2+0.21a+17.45,−0.08a2+3.64a+36.5), andpoint H (0.02a2−4.21a+66.75, 0.0, −0.02a2+3.21a+33.25).
  • 5. The composition according to claim 1, wherein the refrigerant further comprises 2,3,3,3-tetrafluoro-1-propene (R1234yf).
  • 6. The composition according to claim 5, wherein in the refrigerant, when the mass % of HFO-1132(E) is x, the mass % of R32 is y, the mass % of the sum of R1234ze and R1234yf is z, and the mass % of CO2 is a based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2,if r=R1234yf/(R1234ze+R1234yf), and 0.1<r<1.0, coordinates (x,y,z) in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines LrL′r, L′rMr, MrNr, NrOr, OrB″r, B″rK′r, K′rHr, and HrLr that connect 8 points, i.e., points Lr, L′r, Mr, Nr, Or, B″r, K′r, and Hr, or on the straight lines LrL′r, L′rMr, MrNr, NrOr, OrB″r, and K′rHr (excluding the points Lr, B″r, K′r, and Hr), andif 0<a≤1.0, the 8 points are the following:point Lr (72.0, 0.0, 28.0−a),point L′r (57.2, 10.0, 32.8−a),point Mr (48.6, −0.2778r2+0.4167r+18.061, 51.4−a−y),point Nr (35.7, −0.2778r2+0.4167r+36.661, 51.4−a−y),point Or (28.9, −0.2222r2−0.1333r+51.611, 71.1−a−y),point B″r (0.0, (0.463a2−0.1852a−0.2778)r2+(−0.6945a2+0.2778a+0.4167)r+(0.2317a2−0.0927a+51.361), 51.4−a−y),point K′r (0.0, (0.3705a2−0.1482a−0.6667)r2+(−0.2217a2+0.0887a−11.6)r+(0.0183a2−3.0073a+52.567), 100−a−y), andpoint Hr ((2.4072a2−2.0739a−0.8889)r2+(−2.2779a2+1.5779a−8.4667)r+(0.0392a2−4.5732a+67.656), 0.0, 100−a−x),if 1.0<a≤3.0, the 8 points are the following:point Lr (72.0, 0.0, 28.0−a),point L′r (57.2, 10.0, 32.8−a),point Mr (48.6, (−0.1389a2+0.6945a−0.8334)r2+(0.2084a2−1.0418a+1.2501)r+(−0.0695a2+0.3475a+17.783), 51.4−a−y),point Nr (35.7, −0.2778r2+0.4167r+36.661, 51.4−a−y),point Or (28.9, (0.25a2−1.25a+1.2222)r2+(−0.275a2+1.375a−1.2333)r+(0.025a2−0.125a+51.711), 71.1−y−a),point B″r (0.0, (0.25a2−1.0278a+0.7778)r2+(−0.275a2+1.2419a−0.9668)r+(0.075a2−0.364a+51.789), 100−a−y),point K′r (0.0, (0.16667a2+0.2222a−0.8333)r2+(−0.3495a2+0.3645a−11.748)r+(0.1335a2−3.2395a+52.684), 100−a−y), andpoint Hr((−0.25003a2+0.8613a−1.1669)r2+(0.275a2−1.3914a−8.0502)r+(0.0245a2−4.4175a+67.515), 0.0, 100−a−x),if 3.0<a≤5.0, the 8 points are the following:point Lr (72.0, 0.0, 28.0−a),point L′r (57.2, 10.0, 32.8−a),point Mr (48.6, 18.2, 33.2−a),point Nr (35.7, (−0.1389a2+1.2501a−2.778)r2+(0.2084a2−1.8752a+4.167)r+(−0.0695a2+0.6255a+35.41), 51.4−a−y),point Or (28.9, (0.1389a2−0.9723a+1.389)r2+(−0.2083a2+1.4585a−2.0845)r+(0.0695a2−0.4865a+52.395), 71.1−a−y),point B″r (0.0, −0.0556r2+0.2833r+51.372, 100−a−y),point K′r (0.0, (0.77775a2−6.2775a+13.166)r2+(−0.9665a2+8.0155a−29.148)r+(0.189a2−4.54a+56.086), 100−a−y), andpoint Hr ((−0.72215a2+6.3327a−13.332)r2+(0.6835a2−6.3015a+3.003)r+(0.039a2−4.434a+67.434), 0.0, 100−x−a), orif 5.0<a≤7.5, the 8 points are the following:point Lr (72.0, 0.0, 28.0−a),point L′r (57.2, 10.0, 32.8−a),point Mr (48.6, (0.0592a2−0.6512a+1.776)r2+(−0.0355a2+0.3901a−1.062)r+(0.0029a2−0.0323a+18.29), 51.4−a−y),point Nr (35.7, 36.8, 27.5−a),point Or (28.9, 51.7, 19.4−a),point B″r (0.0, −0.0556r2+0.2833r+51.372, 100−a−y),point K′r (0.0, (0.10373a2−0.9189a+3.2232)r2+(−0.1285a2+1.2799a−16.419)r+(0.0252a2−3.1662a+53.312), 100−a−y), andpoint Hr((0.037a2−0.1293a−0.0008)r2+(−0.056a2+0.2a−11.017)r+(0.0719a2−4.8515a+68.7), 0.0, 100−a−x).
  • 7. The composition according to claim 6, wherein in the refrigerant, when the mass % of HFO-1132(E) is x, the mass % of R32 is y, the mass % of the sum of R1234ze and R1234yf is z, and the mass % of CO2 is a based on the sum of HFO-1132(E), R32, R1234ze, R1234yf, and CO2,if r=R1234yf/(R1234ze+R1234yf), and 0.1<r<1.0, coordinates (x,y,z) in a ternary composition diagram having HFO-1132(E) as a first vertex, R32 as a second vertex, and the sum of 1234ze and R1234yf as a third vertex in which the sum of HFO-1132(E), R32, R1234ze, and R1234yf is (100−a) mass % are within the range of a figure surrounded by straight lines LrL′r, L′rMr, MrIr, IrHr, and HrLr that connect 5 points, i.e., points Lr, L′r, Mr, Ir, and Hr, or on the straight lines LrL′r, L′rMr, MrIr, and IrHr, andif 0<a≤1.0, the 5 points are the following:point Lr (72.0, 0.0, 28.0−a),point L′r (57.2, 10.0, 32.8−a),point Mr (48.6, −0.2778r2+0.4167r+18.061, 51.4−a−y),point Ir ((1.1576a2−0.3243a−2.1111)r2+(−0.9a2−0.35a−10.233)r+(−0.255a2−3.828a+44.244), 100−a−x−z, (1.1572a2+0.3239a+1.8889)r2+(0.9042a2+0.3458a+10.367)r+(0.2525a2+2.8315a+37.644)), andpoint Hr ((2.4072a2−2.0739a−0.8889)r2+(−2.2779a2+1.5779a−8.4667)r+(0.0392a2−4.5732a+67.656), 0.0, 100−a−x),if 1.0<a≤3.0, the 5 points are the following:point Lr (72.0, 0.0, 28.0−a),point L′r (57.2, 10.0, 32.8−a),point Mr (48.6, (−0.1389a2+0.6945a−0.8334)r2+(0.2084a2−1.0418a+1.2501)r+(−0.0695a2+0.3475a+17.783), 51.4−a−y),point Ir ((−0.08337a2+0.8057a−2.0001)r2+(−0.0745a2−0.6105a−10.798)r+(0.108a2−4.346a+44.399), 100−a−x−z, (0.33337a2−1.5557a+2.2779)r2+(−0.225a2+1.508a+10.334)r+(−0.033a2+3.121a+37.64)), andpoint Hr ((−0.25003a2+0.8613a−1.1669)r2+(0.275a2−1.3914a−8.0502)r+(0.0245a2−4.4175a+67.515), 0.0, 100−a−x),if 3.0<a≤5.0, the 5 points are the following:point Lr (72.0, 0.0, 28.0−a),point L′r (57.2, 10.0, 32.8−a),point Mr (48.6, 18.2, 31.2−a),point Ir ((−0.05554a2+0.8332a−2.3331)r2+(−0.2165a2+1.2485a−15.097)r+(0.1715a2−5.2775a+46.622), 100−a−x−z, (0.0556a2−0.8329a+2.6103)r2+(0.1915a2−1.0235a+14.18)r+(−0.1715a2+4.2775a+35.417)), andpoint Hr((−0.72215a2+6.3327a−13.332)r2+(0.6835a2−6.3015a+3.003)r+(0.039a2−4.434a+67.434), 0.0, 100−a−x), orif 5.0<a≤7.5, the 5 points are the following:point Lr (72.0, 0.0, 28.0−a),point L′r (57.2, 10.0, 32.8−a),point Mr (48.6, (0.0592a2−0.6512a+1.776)r2+(−0.0355a2+0.3901a−1.062)r+(0.0029a2−0.0323a+18.29), 51.4−a−y),point Ir ((0.19254a2−1.8957a+5.1093)r2+(−0.3156a2+3.3386a−23.07)r+(0.1097a2−4.9961a+46.759), 100−a−x−z, (−0.0074a2−0.4187a+2.1117)r2+(0.0379a2+0.1335a+12.236)r+(−0.0571a2+3.3777a+37.055)), andpoint Hr((0.037a2−0.1293a−0.0008)r2+(−0.056a2+0.2a−11.017)r+(0.0719a2−4.8515a+68.7), 0.0, 100−x−a).
  • 8. The composition according to claim 1, for use as a working fluid for a refrigerating machine, wherein the composition further comprises a refrigeration oil.
  • 9. The composition according to claim 1, for use as an alternative refrigerant for R410A.
  • 10. Use of the composition according to claim 1 as an alternative refrigerant for R410A.
  • 11. A refrigerating machine comprising the composition according to claim 1 as a working fluid.
  • 12. A method for operating a refrigerating machine, comprising circulating the composition according to claim 1 as a working fluid in a refrigerating machine.
Priority Claims (2)
Number Date Country Kind
2019-114156 Jun 2019 JP national
2020-019121 Feb 2020 JP national
Continuations (1)
Number Date Country
Parent PCT/JP2020/024049 Jun 2020 US
Child 17553103 US