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HEAT TRANSFER COMPOSITIONS

20240352297 ยท 2024-10-24

    Inventors

    Cpc classification

    International classification

    Abstract

    According to the present invention, there is provided a composition comprising 1,1-difluoroethylene (R-1132a), difluoromethane (R-32), 2,3,3,3-tetrafluoropropene (R-1234yf) and carbo dioxide (CO.sub.2, R-744). The invention also provides a composition R-1132a, R-32, R-1234yf and at least one compound selected from the group consisting of: pentafluoroethane (R-125), 1,1-difluoroethane (R-152a), 1,1,1,2-tetrafluoroethane (R-134a), trans-1,3,3,3-tetrafluoropropene (R-1234ze(E)) and 1,1,1,2,3,3,3-heptafluoropropane (R-227ea); optionally, the composition comprises at least one further compound selected from the group consisting of trifluoroethylene (R-1123), propane (R-290), propylene (R-1270), isobutane (R-600a) and carbon dioxide (CO.sub.2, R-744). The present invention also provides a composition comprising R-1132a, R-32 and R-1234yf.

    Claims

    1. A composition comprising 1,1-difluoroethylene (R-1132a), difluoromethane (R-32), 2,3,3,3-tetrafluoropropene (R-1234yf) and at least one compound selected from the group consisting of: pentafluoroethane (R-125), 1,1-difluoroethane (R-152a), 1,1,1,2-tetrafluoroethane (R-134a), trans-1,3,3,3-tetrafluoropropene (R-1234ze(E)) and 1,1,1,2,3,3,3-heptafluoropropane (R-227ea), optionally wherein the composition comprises at least one further compound selected from the group consisting of trifluoroethylene (R-1123), propane (R-290), propylene (R-1270), isobutane (R-600a) and carbon dioxide (CO.sub.2, R-744).

    2. A composition according to claim 1, wherein the composition comprises R-1132a, R-32 and R-1234yf in a combined amount of from about 1 to about 99 weight %, optionally from about 1 to about 90 weight %, preferably from about 1 to about 80 weight %, such as from about 1 to about 75 weight %, for example from about 1 to about 70 weight %, based on the total weight of the composition.

    3. A composition according to claim 1, wherein the composition comprises CO.sub.2 in an amount of from about 1 to about 30 weight %, for example from about 2 to about 20 weight %.

    4. A composition according to claim 1, wherein the composition comprises R-1123 in an amount of from about 1 to about 30 weight %, for example from about 2 or 5 to about 20 weight %.

    5. A composition according to claim 1, wherein the composition comprises R-134a in an amount of from about 1 to about 40 weight %, for example from about 2 to about 30 weight %.

    6. A composition according to claim 1, wherein the composition comprises R-125 in an amount of from about 1 to about 20 weight %, for example from about 2 to about 15 weight %.

    7. A composition according to claim 1, wherein the composition comprises R-1234ze(E) in an amount of from about 1 to about 40 weight %, for example from about 2 to about 30 weight %.

    8. A composition according to claim 1, wherein the composition comprises R-152a in an amount of from about 1 to about 30 weight %, for example from about 2 to about 20 weight %.

    9. A composition according to claim 1, wherein the composition comprises R-600a in an amount of from about 1 to about 20 weight %, such as from about 1 to about 10 weight %, preferably from about 1 to about 5 weight %.

    10. A composition according to claim 1, wherein the composition comprises R-290 in an amount of from about 1 to about 20 weight %, such as from about 1 to about 10 weight %, preferably from about 1 to about 5 weight %.

    11. A composition according to claim 1, wherein the composition comprises R-1270 in an amount of from about 1 to about 20 weight %, such as from about 1 to about 10 weight %, preferably from about 1 to about 5 weight %.

    12. A composition according to claim 1, wherein the composition comprises: R-1132a, R-32, R-1234yf and R-152a; R-1132a, R-32, R-1234yf and R-134a; R-1132a, R-32, R-1234yf and R-1234ze(E); R-1132a, R-32, R-1234yf and R-125; or R-1132a, R-32, R-1234yf and R-227ea.

    13. A composition according to claim 1, wherein the composition comprises: R-1132a, R-32, R-1234yf, CO.sub.2 and R-1234ze(E); R-1132a, R-32, R-1234yf, CO.sub.2 and R-125; R-1132a, R-32, R-1234yf, CO.sub.2 and R-152a; R-1132a, R-32, R-1234yf, CO.sub.2 and R-134a; R-1132a, R-32, R-1234yf, CO.sub.2 and R-227ea; R-1132a, R-32, R-1234yf, R-1123 and R-1234ze(E); R-1132a, R-32, R-1234yf, R-1123 and R-125; R-1132a, R-32, R-1234yf, R-1123 and R-152a; R-1132a, R-32, R-1234yf, R-1123 and R-134a; R-1132a, R-32, R-1234yf, R-1123 and R-227ea; R-1132a, R-32, R-1234yf, R-290 and R-1234ze(E); R-1132a, R-32, R-1234yf, R-290 and R-125; R-1132a, R-32, R-1234yf, R-290 and R-152a; R-1132a, R-32, R-1234yf, R-290 and R-134a; R-1132a, R-32, R-1234yf, R-290 and R-227ea; R-1132a, R-32, R-1234yf, R-1270 and R-1234ze(E); R-1132a, R-32, R-1234yf, R-1270 and R-125; R-1132a, R-32, R-1234yf, R-1270 and R-152a; R-1132a, R-32, R-1234yf, R-1270 and R-134a; R-1132a, R-32, R-1234yf, R-1270 and R-227ea; R-1132a, R-32, R-1234yf, R-600A and R-1234ze(E); R-1132a, R-32, R-1234yf, R-600A and R-125; R-1132a, R-32, R-1234yf, R-600A and R-152a; R-1132a, R-32, R-1234yf, R-600A and R-134a; R-1132a, R-32, R-1234yf, R-600A and R-227ea; R-1132a, R-32, R-1234yf, R-1234ze(E) and R-125; R-1132a, R-32, R-1234yf, R-1234ze(E) and R-152a; R-1132a, R-32, R-1234yf, R-1234ze(E) and R-134a; R-1132a, R-32, R-1234yf, R-1234ze(E) and R-227ea; R-1132a, R-32, R-1234yf, R-125 and R-152a; R-1132a, R-32, R-1234yf, R-125 and R-134a; R-1132a, R-32, R-1234yf, R-125 and R-227ea; R-1132a, R-32, R-1234yf, R-152a and R-134a; R-1132a, R-32, R-1234yf, R-152a and R-227ea; or R-1132a, R-32, R-1234yf, R-134a; and R-227ea.

    14. A composition according to claim 1, wherein the composition comprises: R-1132a, R-32, R-1234yf, CO.sub.2, R-1123 and R-1234ze(E); R-1132a, R-32, R-1234yf, CO.sub.2, R-1123 and R-125; R-1132a, R-32, R-1234yf, CO.sub.2, R-1123 and R-152a; R-1132a, R-32, R-1234yf, CO.sub.2, R-1123 and R-134a; R-1132a, R-32, R-1234yf, CO.sub.2, R-1123 and R-227ea; R-1132a, R-32, R-1234yf, CO.sub.2, R-290 and R-1234ze(E); R-1132a, R-32, R-1234yf, CO.sub.1, R-290 and R-125; R-1132a, R-32, R-1234yf, CO.sub.2, R-290 and R-152a; R-1132a, R-32, R-1234yf, CO.sub.2, R-290 and R-134a; R-1132a, R-32, R-1234yf, CO.sub.2, R-290 and R-227ea; R-1132a, R-32, R-1234yf, CO.sub.2, R-1270 and R-1234ze(E); R-1132a, R-32, R-1234yf, CO.sub.2, R-1270 and R-125; R-1132a, R-32, R-1234yf, CO.sub.2, R-1270 and R-152a; R-1132a, R-32, R-1234yf, CO.sub.2, R-1270 and R-134a; R-1132a, R-32, R-1234yf, CO.sub.2, R-1270 and R-227ea; R-1132a, R-32, R-1234yf, CO.sub.2, R-600a and R-1234ze(E); R-1132a, R-32, R-1234yf, CO.sub.2, R-600a and R-125; R-1132a, R-32, R-1234yf, CO.sub.2, R-600a and R-152a; R-1132a, R-32, R-1234yf, CO.sub.2, R-600a and R-134a; R-1132a, R-32, R-1234yf, CO.sub.2, R-600a and R-227ea; R-1132a, R-32, R-1234yf, R-1234ze(E), R-125 and R-152a; R-1132a, R-32, R-1234yf, R-1234ze(E), R-125 and R-134a; R-1132a, R-32, R-1234yf, R-1234ze(E), R-125 and R-227ea; R-1132a, R-32, R-1234yf, R-1234ze(E), R-152a and R-134a; R-1132a, R-32, R-1234yf, R-1234ze(E), R-152a and R-227ea; R-1132a, R-32, R-1234yf, R-1234ze(E), R-134a and R-227ea; R-1132a, R-32, R-1234yf, R-125, R-134a and R-227ea; R-1132a, R-32, R-1234yf, R-125, R-134a and R-152a; R-1132a, R-32, R-1234yf, R-125, R-152a and R-227ea; R-1132a, R-32, R-1234yf, R-227ea, R-152a and R-134a; R-1132a, R-32, R-1234yf, R-1123, R-290 and R-1234ze(E); R-1132a, R-32, R-1234yf, R-1123, R-290 and R-125; R-1132a, R-32, R-1234yf, R-1123, R-290 and R-152a; R-1132a, R-32, R-1234yf, R-1123, R-290 and R-134a; R-1132a, R-32, R-1234yf, R-1123, R-290 and R-227ea; R-1132a, R-32, R-1234yf, R-1123, R-1270 and R-1234ze(E); R-1132a, R-32, R-1234yf, R-1123, R-1270 and R-125; R-1132a, R-32, R-1234yf, R-1123, R-1270 and R-152a; R-1132a, R-32, R-1234yf, R-1123, R-1270 and R-134a; R-1132a, R-32, R-1234yf, R-1123, R-1270 and R-227ea; R-1132a, R-32, R-1234yf, R-1123, R-600a and R-1234ze(E); R-1132a, R-32, R-1234yf, R-1123, R-600a and R-125; R-1132a, R-32, R-1234yf, R-1123, R-600a and R-152a; R-1132a, R-32, R-1234yf, R-1123, R-600a and R-134a; R-1132a, R-32, R-1234yf, R-1123, R-600a and R-227ea; R-1132a, R-32, R-1234yf, R-290, R-1270 and R-1234ze(E); R-1132a, R-32, R-1234yf, R-290, R-1270 and R-125; R-1132a, R-32, R-1234yf, R-290, R-1270 and R-152a; R-1132a, R-32, R-1234yf, R-290, R-1270 and R-134a; R-1132a, R-32, R-1234yf, R-290, R-1270 and R-227ea; R-1132a, R-32, R-1234yf, R-290, R-600a and R-1234ze(E); R-1132a, R-32, R-1234yf, R-290, R-600a and R-125; R-1132a, R-32, R-1234yf, R-290, R-600a and R-152a; R-1132a, R-32, R-1234yf, R-290, R-600a and R-134a; R-1132a, R-32, R-1234yf, R-290, R-600a and R-227ea; R-1132a, R-32, R-1234yf, R-600a, R-1270 and R-1234ze(E); R-1132a, R-32, R-1234yf, R-600a, R-1270 and R-125; R-1132a, R-32, R-1234yf, R-600a, R-1270 and R-152a; R-1132a, R-32, R-1234yf, R-600a, R-1270 and R-134a; or R-1132a, R-32, R-1234yf, R-600a, R-1270 and R-227ea.

    15. A composition according to claim 1, wherein the composition comprises: about 7 weight % R-1132a, about 50 weight % R-32 and about 43 weight % R-1234yf; about 7 weight % R-1132a, about 55 weight % R-32 and about 38 weight % R-1234yf; about 8 weight % R-1132a, about 40 weight % R-32 and about 52 weight % R-1234yf; about 8 weight % R-1132a, about 60 weight % R-32 and about 32 weight % R-1234yf; or about 10 weight % R-1132a, about 55 weight % R-32 and about 35 weight % R-1234yf; based on the total weight of the composition.

    Description

    DETAILED DESCRIPTION

    [0016] The compositions of the invention typically contain from about 1 or 2 or 3 or 4 to about 60% by weight R-1132a. Advantageously, such compositions comprise from about 1 or 2 or 3 or 4 to about 50% by weight R-1132a, such as from about 1 or 2 or 3 or 4 to about 40% by weight R-1132a, for example from about 1 or 2 or 3 or 4 to about 30% by weight R-1132a. Conveniently, the compositions of the invention comprise from about 1 or 2 or 3 or 4 to about 25% by weight R-1132a, such as from 2 to about 20% by weight R-1132a, for example 3 or 4 to about 20% by weight R-1132a. Preferably, such compositions comprise from about 5 to about 20% by weight R-1132a.

    [0017] The compositions of the invention typically contain from about 1 to about 99% by weight R-32 or from about 2 to about 98% by weight R-32. Advantageously, such compositions comprise from about 2 to about 95% by weight R-32, such as from about 3 to about 95% by weight R-32. Conveniently, the compositions of the invention comprise from about 5 to about 90% by weight R-32, such as from about 5 to about 85% by weight R-32, for example from about 10 to about 80% by weight R-32. Preferably, such compositions comprise from about 15 to about 75% by weight R-32, such as from about 15 to about 70% by weight R-32.

    [0018] The compositions of the invention typically contain from about 1 to about 99% by weight R-1234yf or from about 2 to about 98% by weight R-1234yf. Advantageously, such compositions comprise from about 2 to about 90% by weight R-1234yf, such as from 5 to about 90% by weight R-1234yf. Conveniently, the compositions of the invention comprise from about 7 to about 85% by weight R-1234yf, such as from about 8 to about 80% by weight R-1234yf. Preferably, such compositions comprise from about 10 to about 75% by weight R-1234yf, such as from about 10 to about 70% by weight R-1234yf, for example from about 10 to about 65% by weight R-1234yf.

    [0019] Conveniently, compositions of the invention comprise from about 1 to about 60% by weight R-1132a, from about 1 to about 99% by weight R-32, and from about 1 to about 99% by weight R-1234yf. Such compositions typically contain from about 1 to about 50% by weight R-1132a, from about 2 to about 97% by weight R-32, and from about 2 to about 97% by weight R-1234yf.

    [0020] Conveniently, compositions of the invention comprise from about 2 to about 60% by weight R-1132a, from about 1 to about 97% by weight R-32, and from about 1 to about 97% by weight R-1234yf. Such compositions typically contain from about 2 to about 50% by weight R-1132a, from about 2 to about 96% by weight R-32, and from about 2 to about 96% by weight R-1234yf.

    [0021] Advantageously, compositions of the invention comprise from about 1 to about 40% by weight R-1132a, from about 5 to about 90% by weight R-32, and from about 5 to about 90% by weight R-1234yf; or from about 2 to about 40% by weight R-1132a, from about 5 to about 90% by weight R-32, and from about 5 to about 90% by weight R-1234yf; or from about 2 to about 40% by weight R-1132a, from about 4 to about 94% by weight R-32, and from about 4 to about 94% by weight R-1234yf.

    [0022] Preferably, compositions of the invention comprise from about 3 to about 20% by weight R-1132a, from about 10 to about 80% by weight R-32 and from about 10 to about 75% by weight R-1234yf; or from about 3 to about 30% by weight R-1132a, from about 10 to about 91% by weight R-32 and from about 6 to about 87% by weight R-1234yf.

    [0023] Conveniently, compositions of the invention comprise from about 5 to about 20% by weight R-1132a, from about 20 to about 70% by weight R-32 and from about 10 to about 65% by weight R-1234yf; or from about 4 to about 25% by weight R-1132a, from about 15 to about 88% by weight R-32 and from about 8 to about 81% by weight R-1234yf.

    [0024] Typically, the compositions of the invention contain R-1132a, R-32 and 1234yf in a combined amount of from about 1 to about 99 weight %, optionally from about 1 to about 90 weight %, preferably from about 1 to about 80 weight %, such as from about 1 to about 75 weight %, for example from about 1 to about 70 weight %, based on the total weight of the composition.

    [0025] Any of the above described compositions may additionally contain carbon dioxide (R-744, CO.sub.2). Adding R-744 has the advantage of reducing the R-1132a in the vapour phase and hence reducing potential flammability of the vapour phase, but tends to increase compressor discharge temperature and temperature glide.

    [0026] When present, the compositions of the invention typically contain from about 1 to about 30% by weight CO.sub.2. Preferably, such compositions contain from about 2 to about 15% or about 20% by weight CO.sub.2. In one embodiment, the compositions of the invention contain R-1132a and CO.sub.2 in a combined amount of from about 2 to about 50% by weight, such as from about 2 to about 40% by weight, for instance from about 4 to about 30% by weight, e.g. from about 5 to about 20% by weight.

    [0027] Any of the above described compositions may additionally contain 1,1,2-trifluoroethene (R-1123). An advantage of using R-1123 in the compositions of the invention is that it gives similar capacity to R-32 but it has negligible GWP. By incorporation of a proportion of R-1123 the overall GWP of a composition having similar capacity to R-410A may then be reduced compared to an equivalent ternary R-1132a/R-32/R-1234yf composition at constant R-1132a and R-1234yf proportions. R-1123 may only safely be used as a diluted component in compositions of the invention. The proportion of R-1123 in the compositions of the typically is such that the maximum molar concentration of R-1123 either in the composition of the invention as formulated or in its worst-case fractionated compositions (as defined in ASHRAE Standard 34 Appendix B) should be less than 40%.

    [0028] When present, the compositions of the invention typically contain from about 1 to about 30% by weight R-1123; or from about 2 or about 5 to about 30% by weight R-1123. Preferably, such compositions contain from about 5 to about 20% by weight R-1123 such as from about 5 to about 15% by weight, for example from about 5 to about 10% by weight R-1123.

    [0029] Alternatively, the compositions of the invention may contain less than about 8% or about 7% or about 6% or about 5% by weight R-1123, such as less than about 4% or about 3%/o by weight R-1132a, for example less than about 2% or about 1% by weight R-1123. Preferably, such compositions are substantially free of R-1123. Advantageously, the compositions of the invention contain no (readily detectable) R-1123.

    [0030] When the compositions of the invention contain R-134a, typically it is present in an amount of from about 1 to about 40 weight %, for example from about 2 to about 30 weight %.

    [0031] When present, the compositions of the invention typically contain R-125 in an amount of from about 1 to about 20 weight %, for example from about 2 to about 15 weight %.

    [0032] When the compositions of the invention contain R-1234ze(E), typically it is present in an amount of from about 1 to about 40 weight %, for example from about 2 to about 30 weight %.

    [0033] When present, the compositions of the invention typically contain R-152a in an amount of from about 1 to about 30 weight %, for example from about 2 to about 20 weight %.

    [0034] When the compositions of the invention contain R-600a, typically it is present in an amount of from about 1 to about 20 weight %, such as from about 1 to about 10 weight %, for example from about 1 to about 5 weight %.

    [0035] When present, the compositions of the invention typically contain R-290 in an amount of from about 1 to about 20 weight %, such as from about 1 to about 10 weight %, for example from about 1 to about 5 weight %.

    [0036] When the compositions of the invention contain R-1270, typically it is present in an amount of from about 1 to about 20 weight %, such as from about 1 to about 10 weight %, for example from about 1 to about 5 weight %.

    [0037] Preferred compositions of the invention containing 4 components include R-1132a, R-32, R-1234yf and R-152a; R-1132a, R-32B R-1234yf and R-134a; R-1132a, R-32, R-1234yf and R-1234ze(E); R-1132a, R-32, R-1234yf and R-125; or R-1132a. R-32, R-1234yf and R-227ea.

    [0038] For the avoidance of doubt, these compositions may contain the amounts of the identified components as hereinbefore described.

    [0039] Preferred compositions of the invention containing 5 components are set out in the following table, wherein Base represents RB132a, R-32 and R-1234yf. For the avoidance of doubt, these compositions may contain the amounts of the identified components as hereinbefore described.

    TABLE-US-00001 Base + CO.sub.2 and R-1234ze(E); Base + R-1123 and R-1234ze(E); Base + CO.sub.2 and R-125; Base + R-1123 and R-125; Base + CO.sub.2 and R-152a; Base + R-1123 and R-152a; Base + CO.sub.2 and R-134a; Base + R-1123 and R-134a; Base + CO.sub.2 and R-227ea; Base + R-1123 and R-227ea; Base + R-290 and R-1234ze(E); Base + R-1270 and R-1234ze(E); Base + R-290 and R-125; Base + R-1270 and R-125; Base + R-290 and R-152a; Base + R-1270 and R-152a; Base + R-290 and R-134a; Base + R-1270 and R-134a; Base + R-290 and R-227ea; Base + R-1270 and R-227ea; Base + R-600A and R-1234ze(E); Base + R-1234ze(E) and R-125; Base + R-600A and R-125; Base + R-1234ze(E) and R-152a; Base + R-600A and R-152a; Base + R-1234ze(E) and R-134a; Base + R-600A and R-134a; Base + R-1234ze(E) and R-227ea; Base + R-600A and R-227ea; Base + R-125 and R-152a; Base + R-152a and R-134a; Base + R-125 and R-134a; Base + R-152a and R-227ea; Base + R-125 and R-227ea; Base + R-134a; and R-227ea

    [0040] Preferred compositions of the invention containing 6 components are set out in the following table, wherein Base represents Ri 132a, R-32 and R-1234yf. For the avoidance of doubt, these compositions may contain the amounts of the identified components as hereinbefore described.

    TABLE-US-00002 Base + CO.sub.2, R-1123 and R-1234ze(E); Base + CO.sub.2, R-290 and R-1234ze(E); Base + CO.sub.2, R-1123 and R-125; Base + CO.sub.2, R-290 and R-125; Base + CO.sub.2, R-1123 and R-152a; Base + CO.sub.2, R-290 and R-152a; Base + CO.sub.2, R-1123 and R-134a; Base + CO.sub.2, R-290 and R-134a; Base + CO.sub.2, R-1123 and R-227ea; Base + CO.sub.2, R-290 and R-227ea; Base + CO.sub.2, R-1270 and R-1234ze(E); Base + CO.sub.2, R-600a and R-1234ze(E); Base + CO.sub.2, R-1270 and R-125; Base + CO.sub.2, R-600a and R-125; Base + CO.sub.2, R-1270 and R-152a; Base + CO.sub.2, R-600a and R-152a; Base + CO.sub.2, R-1270 and R-134a; Base + CO.sub.2, R-600a and R-134a; Base + CO.sub.2, R-1270 and R-227ea; Base + CO.sub.2, R-600a and R-227ea; Base + R-1234ze(E), R-125 and R-152a; Base + R-125, R-134a and R-227ea; Base + R-1234ze(E), R-125 and R-134a; Base + R-125, R-134a and R-152a; Base + R-1234ze(E), R-125 and R-227ea; Base + R-125, R-152a and R-227ea; Base + R-1234ze(E), R-152a and R-134a; Base + R-227ea, R-152a and R-134a; Base + R-1234ze(E), R-152a and R-227ea; Base + R-1234ze(E), R-134a and R-227ea; Base + R-1123, R-290 and R-1234ze(E); Base + R-1123, R-1270 and R-1234ze(E); Base + R-1123, R-290 and R-125; Base + R-1123, R-1270 and R-125; Base + R-1123, R-290 and R-152a; Base + R-1123, R-1270 and R-152a; Base + R-1123, R-290 and R-134a; Base + R-1123, R-1270 and R-134a; Base + R-1123, R-290 and R-227ea; Base + R-1123, R-1270 and R-227ea; Base + R-1123, R-600a and R-1234ze(E); Base + R-290, R-1270 and R-1234ze(E); Base + R-1123, R-600a and R-125; Base + R-290, R-1270 and R-125; Base + R-1123, R-600a and R-152a; Base + R-290, R-1270 and R-152a; Base + R-1123, R-600a and R-134a; Base + R-290, R-1270 and R-134a; Base + R-1123, R-600a and R-227ea; Base + R-290, R-1270 and R-227ea; Base + R-290, R-600a and R-1234ze(E); Base + R-600a, R-1270 and R-1234ze(E); Base + R-290, R-600a and R-125; Base + R-600a, R-1270 and R-125; Base + R-290, R-600a and R-152a; Base + R-600a, R-1270 and R-152a; Base + R-290, R-600a and R-134a; Base + R-600a, R-1270 and R-134a; or Base + R-290, R-600a and R-227ea; Base + R-600a, R-1270 and R-227ea.

    [0041] The invention further provides a composition comprising from about 6 to about 18 weight % R-1132a, from about 20 to about 65 weight % R-32 and from about 15 to about 60 weight % R-1234yf. For simplicity, this will be referred to hereinafter as the first ternary composition of the invention.

    [0042] Typically, the first ternary composition of the invention contains from about 6 to about 15 weight % R-1132a, preferably from about 6 to about 12 weight %, such as from about 7 to about 10 weight %. For example, the first ternary composition of the invention comprises from about 6 to about 7 weight % of R-1132a.

    [0043] Conveniently, the first ternary composition of the invention contains from about 25 to about 65 weight % R-32, preferably from about 35 to about 60 weight %, such as from about 40 to about 60 weight %.

    [0044] Typically, the first ternary composition of the invention contains from about 20 to about 60 weight % R-1234yf, preferably from about 25 to about 55 weight %, such as from about 30 to about 55 weight %.

    [0045] In one embodiment, the first ternary composition of the invention comprises from about 6 to about 8 wt. % R-1132a, from about 42 to about 45 wt. % R-32 and from about 47 to about 51 wt. % R-1234yf.

    [0046] Preferred first ternary compositions of the invention include blends of: about 7 weight % R-1132a, about 50 weight % R-32 and about 43 weight % R-1234yf; about 7 weight % R-1132a, about 55 weight % R-32 and about 38 weight % R-1234yf; about 8 weight % R-1132a, about 40 weight % R-32 and about 52 weight % R-1234yf; about 8 weight % R-1132a, about 60 weight % R-32 and about 32 weight % R-1234yf; and about 10 weight % R-1132a, about 55 weight % R-32 and about 35 weight % R-1234yf.

    [0047] In one embodiment, the tolerances (e.g. manufacturing tolerances) in such compositions are +0.5%/1% R-1132a; 1% R-32; 1.5% R-1234yf by weight

    [0048] In one embodiment of the present invention, there is provided the use of a composition comprising a POE lubricant and the first ternary composition of the invention as a replacement for an existing heat transfer composition in a commercial air conditioning system. Preferably, the existing heat transfer composition is R-410A.

    [0049] In another embodiment of the present invention, there is provided the use of a composition comprising a POE lubricant and the first ternary composition of the invention as a replacement for an existing heat transfer composition in a commercial refrigeration system. Conveniently, the existing heat transfer composition is R-410A.

    [0050] The invention further provides a composition comprising from about 6 to about 18 weight % R-1132a, from about 5 to about 35 weight % R-32 and from about 47 to about 89 weight % R-1234yf. For simplicity, this will be referred to hereinafter as the second ternary composition of the invention.

    [0051] Typically, the second ternary composition of the invention contains from about 6 to about 15 weight % R-1132a, preferably from about 7 to about 12 weight %, such as from about 7 to about 10 weight %.

    [0052] Conveniently, the second ternary composition of the invention contains from about 6 to about 30 weight % R-32, preferably from about 7 to about 20 weight %, such as from about 8 to about 15 weight %, for example from about 9 to about 13 weight %.

    [0053] Typically, the second ternary composition of the invention contains from about 55 to about 88 weight % R-1234yf, preferably from about 60 to about 87 weight %, such as from about 75 to about 85 weight % for example from about 78 to about 84 weight %.

    [0054] A preferred second ternary compositions of the invention is a blend of about 7 weight % R-1132a, about 50 weight % R-32 and about 43 weight % R-1234yf;

    [0055] According to another aspect of the present invention, there is provided a composition comprising 1,1-difluoroethene (R-1132a), difluoromethane (R-32), 2,3,3,3-tetrafluoropropene (R-1234yf) and carbon dioxide (CO.sub.2, R-744). For simplicity, this will be referred to hereinafter as an alternative quaternary composition of the invention.

    [0056] The alternative quaternary composition of the invention may comprise from about 2 to about 15 weight % of R-1132a, from about 20 to about 60 weight % of R-32, from about 25 to about 70 weight % of R-1234yf and from about 2 to about 12 weight % of CO.sub.2 based on the total weight of the composition.

    [0057] The alternative quaternary composition of the invention may comprise from about 4 to about 10 weight % of R-1132a, from about 30 to about 48 weight % of R-32 from about 34 to about 64 weight % of R-1234yf and from about 2 to about 8 weight % of CO.sub.2, such as from about 4 to about 10 weight % of R-1132a, from about 36 to about 48 weight % of R-32, from about 37 to about 57 weight % of R-1234yf and from about 3 to about 5 weight % of CO.sub.2 based on the total weight of the composition.

    [0058] Typically, the alternative quaternary composition of the present invention contains from about 4 or 5 or 6 to about 10 weight % of R-1132a, preferably from about 4 or 5 or 6 to about 9 weight %, such as from about 4 or 5 or 6 to about 8 weight % based on the total weight of the composition.

    [0059] Conveniently, the alternative quaternary composition of the invention contains from about 32 to about 44 weight % of R-32, preferably from about 36 to about 44 weight %, such as from about 36 to about 40 weight % based on the total weight of the composition.

    [0060] Typically, the alternative quaternary composition of the invention contains from about 34 to about 60 weight % of R-1234yf, preferably from about 39 to about 56 weight %, such as from about 43 to about 54 weight %, for example from about 43 to about 51 weight % based on the total weight of the composition.

    [0061] Preferably, the alternative quaternary composition of the invention contains from about 2 or 3 to about 7 weight % of CO.sub.2, such as from about 3 or 4 to about 6 weight %, for example from about 3 to about 5 weight % based on the total weight of the composition.

    [0062] Preferred alternative quaternary compositions of the invention include the blends of: [0063] about 6 weight % R-1132a, about 40 weight % R-32, about 51 weight % R-1234yf and about 3 weight % CO.sub.2: [0064] about 7 weight % R-1132a, about 36 weight % R-32, about 54 weight % R-1234yf and about 3 weight % CO.sub.2; [0065] about 9 weight % R-1132a, about 44 weight % R-32, about 43 weight % R-1234yf and about 4 weight % CO.sub.2; or [0066] about 7 weight % R-1132a, about 30 weight % R-32, about 60 weight % R-1234yf and about 3 weight % CO.sub.2; [0067] based on the total weight of the composition.

    [0068] In one embodiment, the tolerances (e.g. manufacturing tolerances) in such compositions are +1%/0.5% CO.sub.2; +0.5%/1% R-1132a; 1% R-32; 22% R-1234yf by weight.

    [0069] For completeness, it is noted that phrases such as the compositions or the compositions of the invention and the like as used in the paragraphs below refer to the compositions disclosed on pages 3 to 11 of the present specification; this includes the compositions of the invention (e.g. pages 3 to 8), first ternary compositions of the invention (e.g. pages 8 to 9), second ternary compositions of the invention (e.g. pages 9 to 10) and alternative quaternary compositions of the invention (e.g. pages 10 to 11).

    [0070] In an embodiment, the compositions may consist essentially of the stated components. By the term consist essentially of, we include the meaning that the compositions of the invention contain substantially no other components, particularly no further (hydro)(fluoro)compounds (e.g. (hydro)(fluoro)alkanes or (hydro)(fluoro)alkenes) known to be used in heat transfer compositions. The term consist of is included within the meaning of consist essentially of.

    [0071] In an embodiment, the compositions of the invention are substantially free of any component that has heat transfer properties (other than the components specified). For instance, the compositions of the invention may be substantially free of any other hydrofluorocarbon compound.

    [0072] By substantially no and substantially free of, we include the meaning that the compositions of the invention contain 0.5% by weight or less of the stated component, preferably 0.4%, 0.3%, 0.2% or 0.1% or less, based on the total weight of the composition.

    [0073] In one embodiment, the compositions of the present invention are substantially free of trifluoroiodomethane (CF.sub.3I).

    [0074] All of the chemicals herein described are commercially available. For example, the fluorochemicals may be obtained from Apollo Scientific (UK) and carbon dioxide may be obtained from liquefied gas suppliers such as Linde AG.

    [0075] As used herein, all % amounts mentioned in compositions herein, including in the claims, are by weight based on the total weight of the compositions, unless otherwise stated.

    [0076] By the term about, as used in connection with numerical values of amounts of components in % by weight, we include the meaning of 0.5% by weight, for example 0.5% by weight.

    [0077] For the avoidance of doubt, it is to be understood that the stated upper and lower values for ranges of amounts of components in the compositions of the invention described herein may be interchanged in any way, provided that the resulting ranges fall within the broadest scope of the invention.

    [0078] The compositions of the invention have zero ozone depletion potential.

    [0079] Typically, the compositions of the invention have a GWP of less than about 650, such as less than about 600, for example less than about 500. Preferably, the compositions of the invention have a GWP of less than about 480, such as less than about 450, for example less than about 400. Conveniently, the compositions of the invention have a GWP of less than about 300, such as from about 220 to about 300, for example less than about 280, for instance less than about 250.

    [0080] Typically, the compositions of the invention are of reduced flammability hazard when compared to R-1132a.

    [0081] Flammability may be determined in accordance with ASHRAE Standard 34 incorporating the ASTM Standard E-681 with test methodology as per Addendum 34p dated 2004, the entire content of which is incorporated herein by reference.

    [0082] In one aspect, the compositions have one or more of (a) a higher lower flammable limit; (b) a higher ignition energy (c) a higher auto-ignition temperature; or (d) a lower burning velocity compared to R-1132a alone. Preferably, the compositions of the invention are less flammable compared to R-1132a in one or more of the following respects: lower flammable limit at 23 C.; lower flammable limit at 60 C.; breadth of flammable range at 23 C. or 60 C.; auto-ignition temperature (thermal decomposition temperature); minimum ignition energy in dry air or burning velocity. The flammable limits and burning velocity being determined according to the methods specified in ASHRAE-34 and the auto-ignition temperature being determined in a 500 ml glass flask by the method of ASTM E659-78.

    [0083] In a preferred embodiment, the compositions of the invention are non-flammable. For example, the compositions of the invention are non-flammable at a test temperature of 60 C. using the ASHRAE-34 methodology. Advantageously, the mixtures of vapour that exist in equilibrium with the compositions of the invention at any temperature between about 20 C. and 60 C. are also non-flammable.

    [0084] In some applications it may not be necessary for the formulation to be classed as non-flammable by the ASHRAE-34 methodology. It is possible to develop fluids whose flammability limits will be sufficiently reduced in air to render them safe for use in the application, for example if it is physically not possible to make a flammable mixture by leaking the refrigeration equipment charge into the surrounds.

    [0085] In one embodiment, the compositions of the invention have a flammability classifiable as 1 or 2L according to the ASHRAE standard 34 classification method, indicating non-flammability (class 1) or a weakly flammable fluid with flame speed lower than 10 cm/s (class 2L).

    [0086] Based on the burning velocity data for a ternary composition of R-1132a/R-32/R-1234yf (40/49/11% by volume; burning velocity of 11.4 cm/s) and the literature values of burning velocities R-32/R-1234yf mixtures (Laminar flame speeds of 2,3,3,3-tetrafluoropropene mixtures Papas, P et al. Proceedings of the Combustion Institute 36 (2017) 1145-1154, which is incorporated herein by reference in its entirety), we estimate that the compositions of the present invention will achieve a burning velocity of less than about 10 cm/s if the molar (volume) concentration of R-1132a in their worst-case fractionated formulations (WCFF, as defined in ASHRAE Standard 34 Appendix B), is less than about 35% v/v and preferably less than about 30% v/v.

    [0087] Accordingly, without wishing to be bound by theory, it is postulated that the compositions of the present invention will achieve a burning velocity of less than about 10 cm/s (and hence a 2L flammability classification) if the molar (volume) concentration of R-1132a in their worst-case fractionated formulations (WCFF, as defined in ASHRAE Standard 34 Appendix B), is less than about 35% v/v and preferably less than about 30% v/v.

    [0088] Therefore, in one embodiment, the compositions of the present invention have the molar (volume) concentration of R-1132a in their worst-case fractionated formulations (WCFF, as defined in ASHRAE Standard 34 Appendix B) of less than about 35% v/v and preferably less than about 30% v/v.

    [0089] In one embodiment, the compositions of the present invention have a burning velocity of less than about 10 cm/s, preferably less than about 9.5 cm/s, for example less than about 9 cm/s, such as less than about 8.5 cm/s or less than about 8 cm/s.

    [0090] For example, a preferred alternative quaternary composition of the present invention has about 28% v/v of R-1132a in its WCFF and a burning velocity of about 8.7 cm/s.

    [0091] The present invention also provides a vessel comprising the composition of the present invention in an amount of up to about 90% v/v based on the total volume of the vessel, wherein the vessel has a temperature of about 40 C. and wherein the composition comprises R-1132a in a molar volume concentration of less than about 35% v/v, preferably less than about 30% v/v, based on the total volume of the composition. Preferably, the vessel is a cylinder.

    [0092] For the avoidance of doubt, it is to be understood that v/v as used herein denotes molar volume concentration.

    [0093] The compositions of the invention preferably have a temperature glide in an evaporator or condenser of less than about 10K, preferably less than about 7 or about 6K, even more preferably less than about 5K, such as less than about 4K and even more preferably less than about 1K.

    [0094] It is believed that the compositions of the invention exhibit a completely unexpected combination of low-/non-flammability, low GWP, improved lubricant miscibility and improved refrigeration performance properties. Some of these refrigeration performance properties are explained in more detail below.

    [0095] The compositions of the invention typically have a volumetric refrigeration capacity that is at least 80% of that of R-410A, such as at least 85% of that of R-410A. Preferably, the compositions of the invention have a volumetric refrigeration capacity that is at least 90% of that of R-410A, for example from about 95% to about 130% of that of R-410A. In one embodiment, the compositions of the invention have a volumetric refrigeration capacity that is within about 15% of that of R-410A, such as about 10% of that of R-410A, even more preferably within about 5% of that of R-410A.

    [0096] In one embodiment, the cycle efficiency (Coefficient of Performance, COP) of the compositions of the invention is within about 10% of R-410A, preferably within about 7% of R-410A, such as within 5% of R-410A. Preferably, the cycle efficiency is equivalent to or higher than R-410A.

    [0097] Conveniently, the compressor discharge temperature of the compositions of the invention is within about 15K of the existing refrigerant fluid it is replacing (e.g. R-410A or R-32), preferably within about 10K or even about 5K. Advantageously, the compressor discharge temperature of the compositions of the invention is lower than that of R-32.

    [0098] Conveniently, the operating pressure in a condenser containing a composition of the invention is lower than that of the condenser containing R-32. In one embodiment, the operating condenser pressure in a condenser containing a composition of the invention is within about 10% of that of the condenser containing R-410A, preferably within about 5%.

    [0099] The compositions of the invention are typically suitable for use in existing designs of equipment, and are compatible with all classes of lubricant currently used with established HFC refrigerants. They may be optionally stabilised or compatibilized with mineral oils by the use of appropriate additives.

    [0100] Preferably, when used in heat transfer equipment, the composition of the invention is combined with a lubricant.

    [0101] Conveniently, the lubricant is selected from the group consisting of mineral oil, silicone oil, polyalkyl benzenes (PABs), polyol esters (POEs), polyalkylene glycols (PAGs), polyalkylene glycol esters (PAG esters), polyvinyl ethers (PVEs), poly (alpha-olefins) and combinations thereof. PAGs and POEs are currently preferred lubricants for the compositions of the invention.

    [0102] Advantageously, the lubricant further comprises a stabiliser.

    [0103] Preferably, the stabiliser is selected from the group consisting of diene-based compounds, phosphates, phenol compounds and epoxides, and mixtures thereof.

    [0104] Conveniently, the composition of the invention may be combined with a flame retardant.

    [0105] Advantageously, the flame retardant is selected from the group consisting of tri-(2-chloroethyl)-phosphate, (chloropropyl) phosphate, tri-(2,3-dibromopropyl)-phosphate, tri-(1,3-dichloropropyl)-phosphate, diammonium phosphate, various halogenated aromatic 25 compounds, antimony oxide, aluminium trihydrate, polyvinyl chloride, a fluorinated iodocarbon, a fluorinated bromocarbon, trifluoro iodomethane, perfluoroalkyl amines, bromo-fluoroakyl amines and mixtures thereof.

    [0106] In one embodiment, the invention provides a heat transfer device comprising a composition of the invention. Preferably, the heat transfer device is a refrigeration device.

    [0107] Conveniently, the heat transfer device is a residential or commercial air conditioning system, a heat pump or a commercial or industrial refrigeration system.

    [0108] The invention also provides the use of a composition of the invention in a heat transfer device, such as a refrigeration system, as herein described.

    [0109] According to another aspect of the invention, there is provided a sprayable composition comprising a material to be sprayed and a propellant comprising a composition of the invention.

    [0110] According to a further aspect of the invention, there is provided a method for cooling an article which comprises condensing a composition of the invention and thereafter evaporating said composition in the vicinity of the article to be cooled.

    [0111] According to another aspect of the invention, there is provided a method for heating an article which comprises condensing a composition of the invention in the vicinity of the article to be heated and thereafter evaporating said composition.

    [0112] According to a further aspect of the invention, there is provided a method for extracting a substance from biomass comprising contacting the biomass with a solvent comprising a composition of the invention, and separating the substance from the solvent.

    [0113] According to another aspect of the invention, there is provided a method of cleaning an article comprising contacting the article with a solvent comprising a composition of the invention.

    [0114] According to a further aspect of the invention, there is provided a method for extracting a material from an aqueous solution comprising contacting the aqueous solution with a solvent comprising a composition of the invention, and separating the material from the solvent.

    [0115] According to another aspect of the invention, there is provided a method for extracting a material from a particulate solid matrix comprising contacting the particulate solid matrix with a solvent comprising a composition of the invention, and separating the material from the solvent.

    [0116] According to a further aspect of the invention, there is provided a mechanical power generation device containing a composition of the invention.

    [0117] Preferably, the mechanical power generation device is adapted to use a Rankine Cycle or modification thereof to generate work from heat.

    [0118] According to another aspect of the invention, there is provided a method of retrofitting a heat transfer device comprising the step of removing an existing heat transfer fluid, and introducing a composition of the invention. Preferably, the heat transfer device is a refrigeration device, such as an ultra-low temperature refrigeration system. Advantageously, the method further comprises the step of obtaining an allocation of greenhouse gas (e.g. carbon dioxide) emission credit.

    [0119] In accordance with the retrofitting method described above, an existing heat transfer fluid can be fully removed from the heat transfer device before introducing a composition of the invention. An existing heat transfer fluid can also be partially removed from a heat transfer device, followed by introducing a composition of the invention.

    [0120] The compositions of the invention may also be prepared simply by mixing the R-1132a, R-32, R-1234yf (and optional components such as R-744, R-1123, hydrocarbons, a lubricant, a stabiliser or an additional flame retardant) in the desired proportions. The compositions can then be added to a heat transfer device (or used in any other way as defined herein).

    [0121] In a further aspect of the invention, there is provided a method for reducing the environmental impact arising from operation of a product comprising an existing compound or composition, the method comprising replacing at least partially the existing compound or composition with a composition of the invention.

    [0122] By environmental impact we include the generation and emission of greenhouse warming gases through operation of the product.

    [0123] As mentioned above, this environmental impact can be considered as including not only those emissions of compounds or compositions having a significant environmental impact from leakage or other losses, but also including the emission of carbon dioxide arising from the energy consumed by the device over its working life. Such environmental impact may be quantified by the measure known as Total Equivalent Warming Impact (TEWI). This measure has been used in quantification of the environmental impact of certain stationary refrigeration and air conditioning equipment, including for example supermarket refrigeration systems.

    [0124] The environmental impact may further be considered as including the emissions of greenhouse gases arising from the synthesis and manufacture of the compounds or compositions. In this case the manufacturing emissions are added to the energy consumption and direct loss effects to yield the measure known as Life-Cycle Carbon Production (LCCP). The use of LCCP is common in assessing environmental impact of automotive air conditioning systems.

    [0125] In a preferred embodiment, the use of the composition of the invention results in the equipment having a lower Total Equivalent Warming Impact, and/or a lower Life-Cycle Carbon Production than that which would be attained by use of the existing compound or composition.

    [0126] These methods may be carried out on any suitable product, for example in the fields of air-conditioning, refrigeration (e.g. low and ultra-low temperature refrigeration), heat transfer, aerosols or sprayable propellants, gaseous dielectrics, flame suppression, solvents (e.g. carriers for flavorings and fragrances), cleaners, topical anesthetics, and expansion applications. Preferably, the field is refrigeration.

    [0127] Examples of suitable products include heat transfer devices, sprayable compositions, solvents and mechanical power generation devices. In a preferred embodiment, the product is a heat transfer device, such as a refrigeration device.

    [0128] The existing compound or composition has an environmental impact as measured by GWP and/or TEWI and/or LCCP that is higher than the composition of the invention which replaces it. The existing compound or composition may comprise a fluorocarbon compound, such as a perfluoro-, hydrofluoro-, chlorofluoro- or hydrochlorofluoro-carbon compound or it may comprise a fluorinated olefin.

    [0129] Preferably, the existing compound or composition is a heat transfer compound or composition such as a refrigerant. Examples of refrigerants that may be replaced include R-410A, R454B, R-452B and R-32, preferably R-410A.

    [0130] Any amount of the existing compound or composition may be replaced so as to reduce the environmental impact. This may depend on the environmental impact of the existing compound or composition being replaced and the environmental impact of the replacement composition of the invention. Preferably, the existing compound or composition in the product is fully replaced by the composition of the invention.

    [0131] The invention is illustrated by the following non-limiting examples.

    EXAMPLES

    [0132] Performance Assessment Two thermodynamic models of the fluid system were constructed, with pure component data and mixture equilibrium data fitted into each of them. The NIST REFPROP 9.1 software was used to build the first model. Mexichem in-house software coded in Matlab was used to build the second model to correlate accurately the vapour-liquid equilibrium properties of the mixture components. The predictions of both models for a typical air-conditioning cycle were checked against each other and were found to be in good agreement. The Mexichem equilibrium model gave more accurate fitting of our experimental mixture equilibrium data. It was therefore used for both performance modelling and derivation of the worst-case composition for flammability. The conditions used for the modelling are shown in Table 1 below; these represent an air-conditioning cycle application.

    TABLE-US-00003 TABLE 1 Modelling conditions used for assessing performance Parameter Units Value Cooling duty kW 14.2 Mean condenser temperature C. 54.4 Mean evaporator temperature C. 7.2 Condenser subcooling K 8.3 Evaporator superheat K 5.6 Evaporator pressure drop bar 0.00 Suction line pressure drop bar 0.00 Condenser pressure drop bar 0.00 Compressor suction superheat K 11.1 Isentropic efficiency 70.0%

    [0133] The measured performance data for the compositions of the present invention is listed in the following tables (Examples 1 to 26).

    [0134] In addition, the Matlab thermodynamic property model for the compositions of the present invention was used to estimate WCFF compositions as the initial vapour in a cylinder filled to 90% maximum at 40 C. The following operating conditions were assumed:

    TABLE-US-00004 Cylinder fill temperature ( C.) 54.4 Cylinder fractionation temperature 40 ( C.) Liquid density model used Quartic VLE model used Peng Robinson/Wong Sandler Matlab workspace file LFR databank Jun. 25th, 2019.mat'

    TABLE-US-00005 Blending tolerances for ASHRAE (% mass) Upper Component bound Lower bound R-1132a 0.5 1 R-744 1 0.5 R-32 1 1 R-1234yf 1.5 1.5

    [0135] The results are outlined in Examples 27 to 40.

    [0136] It can be seen that in nearly all cases the initial vapour composition is less than 35% by volume of R-1132a.

    Example 1 (Ternary Blends of R-1132a/R-32/R-1234yf Comprising 4 Weight % R-1132a)

    [0137]

    TABLE-US-00006 Nominal composition (weight %) R-1132a 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 60 58 56 54 52 50 48 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 106.3% 106.2% 105.9% 105.7% 105.5% 105.3% 105.1% Cooling Capacity relative to reference 100.0% 84.3% 85.7% 87.2% 88.6% 90.1% 91.5% 92.8% Compressor discharge temperature difference K 0.0 4.2 3.4 2.4 1.5 0.6 0.4 1.2 Pressure ratio 3.32 3.49 3.48 3.47 3.46 3.46 3.45 3.44 Volumetric efficiency 94.5% 93.6% 93.7% 93.7% 93.8% 93.9% 94.0% 94.0% Condenser glide K 0.2 5.9 5.4 5.2 4.9 4.7 4.5 4.1 Evaporator glide K 0.1 6.0 5.7 5.5 5.3 5.0 4.8 4.5 Evaporator inlet temperature C. 7.2 4.2 4.4 4.5 4.6 4.7 4.8 5.0 Condenser exit temperature C. 46.0 43.2 43.4 43.5 43.7 43.8 43.9 44.0 Condenser pressure bar 33.7 27.5 27.9 28.4 28.8 29.3 29.7 30.1 Evaporator pressure bar 10.2 7.9 8.0 8.2 8.3 8.5 8.6 8.7 Refrigeration effect kJ/kg 151.2 157.1 159.0 161.2 163.2 165.4 167.6 169.6 Coefficient of Performance (COP) 2.88 3.07 3.06 3.05 3.05 3.04 3.04 3.03 Discharge temperature C. 105.5 101.3 102.1 103.1 104.0 105.0 105.9 106.7 Mass flow rate kg/hr 251 242 239 236 233 230 227 224 Volumetric flow rate m.sup.3/hr 7.28 8.63 8.49 8.34 8.21 8.07 7.95 7.84 Volumetric cooling capacity kJ/m.sup.3 5226 4403 4478 4558 4632 4709 4784 4851 Suction line pressure drop Pa/m 163 189 184 179 174 170 165 161 Suction line gas density kg/m.sup.3 34.6 28.0 28.2 28.3 28.4 28.5 28.5 28.6 Condenser line gas density kg/m.sup.3 155.3 128.6 129.1 130.0 130.5 131.1 131.7 131.8

    Example 2 (Ternary Blends of R-1132a/R-32/R-1234yf Comprising 5 Weight % R-1132a)

    [0138]

    TABLE-US-00007 Nominal composition (weight %) R-1132a 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 59 57 55 53 51 49 47 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 105.9% 105.7% 105.5% 105.3% 105.1% 104.9% 104.7% Cooling Capacity relative to reference 100.0% 85.4% 86.9% 88.4% 89.8% 91.4% 92.7% 94.1% Compressor discharge temperature difference K 0.0 3.8 2.8 1.9 1.1 0.1 0.8 1.7 Pressure ratio 3.32 3.49 3.48 3.47 3.46 3.46 3.45 3.44 Volumetric efficiency 94.5% 93.6% 93.7% 93.8% 93.8% 93.9% 94.0% 94.1% Condenser glide K 0.2 6.0 5.7 5.4 5.0 4.9 4.6 4.3 Evaporator glide K 0.1 6.2 6.0 5.7 5.5 5.2 4.9 4.7 Evaporator inlet temperature C. 7.2 4.1 4.2 4.4 4.5 4.6 4.7 4.9 Condenser exit temperature C. 46.0 43.1 43.3 43.4 43.6 43.7 43.8 44.0 Condenser pressure bar 33.7 28.0 28.4 28.9 29.3 29.8 30.2 30.6 Evaporator pressure bar 10.2 8.0 8.2 8.3 8.5 8.6 8.8 8.9 Refrigeration effect kJ/kg 151.2 157.1 159.1 161.2 163.1 165.4 167.5 169.6 Coefficient of Performance (COP) 2.88 3.05 3.05 3.04 3.04 3.03 3.02 3.02 Discharge temperature C. 105.5 101.8 102.7 103.6 104.4 105.5 106.3 107.2 Mass flow rate kg/hr 251 242 239 236 233 230 227 224 Volumetric flow rate m.sup.3/hr 7.28 8.52 8.37 8.23 8.10 7.96 7.85 7.73 Volumetric cooling capacity kJ/m.sup.3 5226 4463 4543 4622 4695 4775 4844 4915 Suction line pressure drop Pa/m 163 186 181 176 172 167 163 159 Suction line gas density kg/m.sup.3 34.6 28.4 28.6 28.7 28.8 28.9 28.9 29.0 Condenser line gas density kg/m.sup.3 155.3 131.2 132.0 132.7 133.1 134.0 134.2 134.5

    Example 3 (Ternary Blends of R-1132a/R-32/R-1234yf Comprising 6 Weight % R-1132a)

    [0139]

    TABLE-US-00008 Nominal composition (weight %) R-1132a 6 6 6 6 6 6 6 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 58 56 54 52 50 48 46 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 105.5% 105.3% 105.1% 104.9% 104.7% 104.4% 104.3% Cooling Capacity relative to reference 100.0% 86.6% 88.2% 89.6% 91.1% 92.5% 93.8% 95.3% Compressor discharge temperature difference K 0.0 3.3 2.4 1.5 0.6 0.3 1.2 2.1 Pressure ratio 3.32 3.49 3.48 3.47 3.46 3.45 3.44 3.44 Volumetric efficiency 94.5% 93.6% 93.7% 93.8% 93.8% 93.9% 94.0% 94.1% Condenser glide K 0.2 6.1 5.9 5.5 5.3 5.0 4.5 4.4 Evaporator glide K 0.1 6.4 6.2 5.9 5.7 5.4 5.1 4.9 Evaporator inlet temperature C. 7.2 4.0 4.1 4.3 4.4 4.5 4.7 4.8 Condenser exit temperature C. 46.0 43.1 43.2 43.4 43.5 43.6 43.8 43.9 Condenser pressure bar 33.7 28.4 28.9 29.4 29.8 30.3 30.7 31.1 Evaporator pressure bar 10.2 8.2 8.3 8.5 8.6 8.8 8.9 9.0 Refrigeration effect kJ/kg 151.2 157.0 159.1 161.1 163.2 165.3 167.2 169.5 Coefficient of Performance (COP) 2.88 3.04 3.03 3.03 3.02 3.02 3.01 3.01 Discharge temperature C. 105.5 102.2 103.2 104.0 105.0 105.9 106.7 107.6 Mass flow rate kg/hr 251 242 239 236 233 230 227 224 Volumetric flow rate m.sup.3/hr 7.28 8.40 8.25 8.12 7.98 7.86 7.75 7.64 Volumetric cooling capacity kJ/m.sup.3 5226 4524 4607 4683 4761 4836 4903 4979 Suction line pressure drop Pa/m 163 184 179 174 169 165 162 157 Suction line gas density kg/m.sup.3 34.6 28.8 29.0 29.1 29.2 29.3 29.3 29.4 Condenser line gas density kg/m.sup.3 155.3 133.8 134.8 135.4 136.2 136.6 136.9 137.2

    Example 4 (Ternary Blends of R-1132a/R-32/R-1234yf Comprising 7 Weight % R-1132a)

    [0140]

    TABLE-US-00009 Nominal composition (weight %) R-1132a 7 7 7 7 7 7 7 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 57 55 53 51 49 47 45 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 105.1% 104.8% 104.6% 104.5% 104.3% 104.1% 103.9% Cooling Capacity relative to reference 100.0% 87.8% 89.4% 90.8% 92.3% 93.8% 95.1% 96.5% Compressor discharge temperature difference K 0.0 2.9 1.8 1.0 0.1 0.8 1.6 2.5 Pressure ratio 3.32 3.48 3.48 3.47 3.46 3.45 3.44 3.43 Volumetric efficiency 94.5% 93.6% 93.7% 93.8% 93.9% 93.9% 94.0% 94.1% Condenser glide K 0.2 6.3 6.1 5.7 5.4 5.1 4.8 4.6 Evaporator glide K 0.1 6.6 6.4 6.1 5.8 5.6 5.3 5.0 Evaporator inlet temperature C 7.2 3.9 4.0 4.2 4.3 4.4 4.6 4.7 Condenser exit temperature C 46.0 43.0 43.1 43.3 43.4 43.6 43.7 43.8 Condenser pressure bar 33.7 28.9 29.5 29.9 30.4 30.8 31.2 31.6 Evaporator pressure bar 10.2 8.3 8.5 8.6 8.8 8.9 9.1 9.2 Refrigeration effect kJ/kg 151.2 157.0 159.1 161.1 163.1 165.2 167.3 169.4 Coefficient of Performance (COP) 2.88 3.03 3.02 3.02 3.01 3.01 3.00 3.00 Discharge temperature C 105.5 102.7 103.7 104.5 105.4 106.3 107.2 108.0 Mass flow rate kg/hr 251 242 239 236 233 230 227 224 Volumetric flow rate m.sup.3/hr 7.28 8.29 8.14 8.01 7.88 7.76 7.65 7.54 Volumetric cooling capacity kJ/m.sup.3 5226 4588 4672 4747 4824 4899 4971 5042 Suction line pressure drop Pa/m 163 181 176 172 167 163 159 156 Suction line gas density kg/m.sup.3 34.6 29.2 29.4 29.5 29.6 29.7 29.7 29.8 Condenser line gas density kg/m.sup.3 155.3 136.7 137.9 138.4 139.0 139.5 139.8 140.0

    Example 5 (Ternary Blends of R-1132a/R-32/R-1234yf Comprising 8 Weight % of R-1132a)

    [0141]

    TABLE-US-00010 Nominal composition (weight %) R-1132a 8 8 8 8 8 8 8 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 56 54 52 50 48 46 44 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 104.6% 104.4% 104.2% 104.0% 103.9% 103.7% 103.6% Cooling Capacity relative to reference 100.0% 89.0% 90.6% 92.1% 93.5% 94.9% 96.3% 97.6% Compressor discharge temperature difference K 0.0 2.3 1.5 0.6 0.2 1.1 2.0 2.8 Pressure ratio 3.32 3.48 3.47 3.46 3.45 3.44 3.44 3.43 Volumetric efficiency 94.5% 93.7% 93.7% 93.8% 93.9% 94.0% 94.0% 94.1% Condenser glide K 0.2 6.4 6.1 5.8 5.4 5.1 4.8 4.6 Evaporator glide K 0.1 6.8 6.6 6.3 6.0 5.7 5.5 5.2 Evaporator inlet temperature C. 7.2 3.8 3.9 4.1 4.2 4.3 4.5 4.6 Condenser exit temperature C. 46.0 42.9 43.0 43.2 43.4 43.5 43.7 43.8 Condenser pressure bar 33.7 29.5 29.9 30.4 30.8 31.3 31.7 32.1 Evaporator pressure bar 10.2 8.5 8.6 8.8 8.9 9.1 9.2 9.4 Refrigeration effect kJ/kg 151.2 157.0 159.0 161.0 162.9 165.0 167.1 169.2 Coefficient of Performance (COP) 2.88 3.02 3.01 3.00 3.00 2.99 2.99 2.98 Discharge temperature C. 105.5 103.2 104.1 105.0 105.8 106.7 107.5 108.4 Mass flow rate kg/hr 251 242 239 236 233 230 228 225 Volumetric flow rate m.sup.3/hr 7.28 8.17 8.03 7.90 7.78 7.67 7.56 7.45 Volumetric cooling capacity kJ/m.sup.3 5226 4653 4734 4812 4884 4959 5031 5102 Suction line pressure drop Pa/m 163 179 174 169 165 161 158 154 Suction line gas density kg/m.sup.3 34.6 29.6 29.8 29.9 30.0 30.1 30.1 30.1 Condenser line gas density kg/m.sup.3 155.3 139.8 140.6 141.4 141.8 142.2 142.5 142.7

    Example 6 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 4 Weight % of R-1132a and 3 Weight % of CO.SUB.2 .(R-744))

    [0142]

    TABLE-US-00011 Nominal composition (weight %) R-1132a 4 4 4 4 4 4 4 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 57 55 53 51 49 47 45 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 104.3% 104.1% 103.9% 103.7% 103.5% 103.3% 103.1% Cooling Capacity relative to reference 100.0% 91.2% 92.8% 94.2% 95.6% 97.0% 98.4% 99.7% Compressor discharge temperature difference K 0.0 0.3 0.6 1.4 2.3 3.2 4.1 4.9 Pressure ratio 3.32 3.52 3.51 3.50 3.49 3.48 3.48 3.47 Volumetric efficiency 94.5% 93.6% 93.7% 93.8% 93.9% 93.9% 94.0% 94.1% Condenser glide K 0.2 7.9 7.6 7.2 6.8 6.5 6.2 5.9 Evaporator glide K 0.1 7.5 7.2 6.9 6.6 6.4 6.1 5.8 Evaporator inlet temperature C. 7.2 3.5 3.6 3.8 3.9 4.0 4.2 4.3 Condenser exit temperature C. 46.0 42.2 42.3 42.5 42.7 42.9 43.0 43.1 Condenser pressure bar 33.7 30.3 30.8 31.2 31.6 32.1 32.5 32.9 Evaporator pressure bar 10.2 8.6 8.8 8.9 9.1 9.2 9.3 9.5 Refrigeration effect kJ/kg 151.2 160.4 162.4 164.4 166.4 168.5 170.6 172.7 Coefficient of Performance (COP) 2.88 3.01 3.00 2.99 2.99 2.98 2.98 2.97 Discharge temperature C. 105.5 105.2 106.1 107.0 107.8 108.7 109.6 110.5 Mass flow rate kg/hr 251 237 234 231 228 226 223 220 Volumetric flow rate m.sup.3/hr 7.28 7.97 7.84 7.72 7.61 7.50 7.39 7.29 Volumetric cooling capacity kJ/m.sup.3 5226 4768 4849 4922 4997 5070 5142 5212 Suction line pressure drop Pa/m 163 172 167 163 159 155 152 148 Suction line gas density kg/m.sup.3 34.6 29.7 29.8 29.9 30.0 30.1 30.1 30.2 Condenser line gas density kg/m.sup.3 155.3 141.7 142.5 143.0 143.6 144.1 144.4 144.6

    Example 7 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 5 Weight % of R-1132a and 3 Weight % of CO.SUB.2 .(R-744))

    [0143]

    TABLE-US-00012 Nominal composition (weight %) R-1132a 5 5 5 5 5 5 5 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 56 54 52 50 48 46 44 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 103.9% 103.7% 103.4% 103.3% 103.1% 102.9% 102.7% Cooling Capacity relative to reference 100.0% 92.4% 94.0% 95.5% 96.8% 98.2% 99.7% 101.0% Compressor discharge temperature difference K 0.0 0.1 1.0 1.9 2.7 3.6 4.5 5.4 Pressure ratio 3.32 3.51 3.51 3.50 3.49 3.48 3.48 3.47 Volumetric efficiency 94.5% 93.6% 93.7% 93.8% 93.9% 94.0% 94.0% 94.1% Condenser glide K 0.2 8.0 7.7 7.3 6.9 6.6 6.3 6.0 Evaporator glide K 0.1 7.7 7.4 7.1 6.8 6.5 6.2 5.9 Evaporator inlet temperature C. 7.2 3.4 3.5 3.7 3.8 4.0 4.1 4.3 Condenser exit temperature C. 46.0 42.1 42.3 42.5 42.7 42.8 42.9 43.1 Condenser pressure bar 33.7 30.8 31.3 31.7 32.1 32.6 33.0 33.4 Evaporator pressure bar 10.2 8.8 8.9 9.1 9.2 9.4 9.5 9.6 Refrigeration effect kJ/kg 151.2 160.2 162.3 164.3 166.2 168.3 170.5 172.6 Coefficient of Performance (COP) 2.88 2.99 2.99 2.98 2.98 2.97 2.96 2.96 Discharge temperature C. 105.5 105.6 106.6 107.4 108.2 109.1 110.0 110.9 Mass flow rate kg/hr 251 237 234 231 229 226 223 220 Volumetric flow rate m.sup.3/hr 7.28 7.87 7.74 7.62 7.51 7.41 7.30 7.20 Volumetric cooling capacity kJ/m.sup.3 5226 4830 4912 4988 5060 5133 5208 5278 Suction line pressure drop Pa/m 163 169 165 161 157 154 150 147 Suction line gas density kg/m.sup.3 34.6 30.1 30.3 30.4 30.4 30.5 30.5 30.6 Condenser line gas density kg/m.sup.3 155.3 144.4 145.5 146.2 146.6 147.1 147.6 147.8

    Example 8 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 6 Weight % of R-1132a and 3 Weight % of CO.SUB.2 .(R-744))

    [0144]

    TABLE-US-00013 Nominal composition (weight %) R-1132a 6 6 6 6 6 6 6 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 55 53 51 49 47 45 43 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 103.5% 103.2% 103.0% 102.8% 102.6% 102.5% 102.3% Cooling Capacity relative to reference 100.0% 93.7% 95.1% 96.6% 98.0% 99.4% 100.8% 102.2% Compressor discharge temperature difference K 0.0 0.5 1.4 2.2 3.1 4.0 4.8 5.7 Pressure ratio 3.32 3.51 3.50 3.49 3.48 3.48 3.47 3.46 Volumetric efficiency 94.5% 93.7% 93.7% 93.8% 93.9% 94.0% 94.0% 94.1% Condenser glide K 0.2 8.2 7.7 7.3 6.9 6.6 6.3 6.1 Evaporator glide K 0.1 7.9 7.6 7.3 7.0 6.7 6.4 6.1 Evaporator inlet temperature C. 7.2 3.3 3.4 3.6 3.7 3.9 4.0 4.2 Condenser exit temperature C. 46.0 42.0 42.3 42.5 42.6 42.8 43.0 43.1 Condenser pressure bar 33.7 31.3 31.8 32.2 32.7 33.1 33.5 33.9 Evaporator pressure bar 10.2 8.9 9.1 9.2 9.4 9.5 9.7 9.8 Refrigeration effect kJ/kg 151.2 160.2 162.1 164.1 166.1 168.1 170.2 172.4 Coefficient of Performance (COP) 2.88 2.98 2.98 2.97 2.96 2.96 2.95 2.95 Discharge temperature C. 105.5 106.0 106.9 107.8 108.6 109.5 110.4 111.3 Mass flow rate kg/hr 251 237 235 232 229 226 223 221 Volumetric flow rate m.sup.3/hr 7.28 7.76 7.65 7.53 7.42 7.32 7.22 7.12 Volumetric cooling capacity kJ/m.sup.3 5226 4897 4971 5048 5123 5196 5268 5340 Suction line pressure drop Pa/m 163 167 163 159 156 152 148 145 Suction line gas density kg/m.sup.3 34.6 30.6 30.7 30.8 30.8 30.9 31.0 31.0 Condenser line gas density kg/m.sup.3 155.3 147.6 148.4 149.2 149.7 150.2 150.5 150.8

    Example 9 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 7 Weight % of R-1132a and 3 Weight % of CO.SUB.2 .(R-744))

    [0145]

    TABLE-US-00014 Nominal composition (weight %) R-1132a 7 7 7 7 7 7 7 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 54 52 50 48 46 44 42 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 103.0% 102.7% 102.6% 102.4% 102.2% 102.0% 101.9% Cooling Capacity relative to reference 100.0% 94.8% 96.3% 97.8% 99.3% 100.7% 102.1% 103.4% Compressor discharge temperature difference K 0.0 0.9 1.8 2.7 3.5 4.4 5.3 6.1 Pressure ratio 3.32 3.51 3.50 3.49 3.48 3.47 3.47 3.46 Volumetric efficiency 94.5% 93.7% 93.8% 93.8% 93.9% 94.0% 94.1% 94.1% Condenser glide K 0.2 8.1 7.6 7.4 7.0 6.7 6.4 6.1 Evaporator glide K 0.1 8.0 7.7 7.4 7.1 6.8 6.5 6.2 Evaporator inlet temperature C. 7.2 3.2 3.4 3.5 3.7 3.8 4.0 4.1 Condenser exit temperature C. 46.0 42.1 42.3 42.4 42.6 42.8 42.9 43.1 Condenser pressure bar 33.7 31.8 32.3 32.8 33.2 33.6 34.1 34.4 Evaporator pressure bar 10.2 9.1 9.2 9.4 9.5 9.7 9.8 10.0 Refrigeration effect kJ/kg 151.2 159.9 161.8 163.9 165.9 168.0 170.1 172.2 Coefficient of Performance (COP) 2.88 2.97 2.96 2.96 2.95 2.95 2.94 2.94 Discharge temperature C. 105.5 106.4 107.3 108.2 109.1 109.9 110.8 111.6 Mass flow rate kg/hr 251 238 235 232 229 226 224 221 Volumetric flow rate m.sup.3/hr 7.28 7.67 7.56 7.44 7.33 7.23 7.13 7.04 Volumetric cooling capacity kJ/m.sup.3 5226 4954 5030 5113 5188 5262 5334 5403 Suction line pressure drop Pa/m 163 166 162 157 154 150 147 143 Suction line gas density kg/m.sup.3 34.6 31.0 31.1 31.2 31.3 31.3 31.4 31.4 Condenser line gas density kg/m.sup.3 155.3 150.7 151.7 152.6 153.1 153.6 153.9 154.0

    Example 10 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 8 Weight % of R-1132a and 3 Weight % of CO.SUB.2 .(R-744))

    [0146]

    TABLE-US-00015 Nominal composition (weight %) R-1132a 8 8 8 8 8 8 8 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 Results R410A R-1234yf 53 51 49 47 45 43 41 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 102.7% 102.3% 102.1% 101.9% 101.9% 101.6% 101.5% Cooling Capacity relative to reference 100.0% 96.1% 97.5% 99.0% 100.5% 102.0% 103.2% 104.6% Compressor discharge temperature difference K 0.0 1.3 2.2 3.1 3.9 4.8 5.5 6.5 Pressure ratio 3.32 3.50 3.49 3.49 3.48 3.47 3.46 3.45 Volumetric efficiency 94.5% 93.7% 93.8% 93.9% 93.9% 94.0% 94.1% 94.2% Condenser glide K 0.2 8.2 7.7 7.4 7.0 6.9 6.3 6.1 Evaporator glide K 0.1 8.2 7.9 7.6 7.2 7.0 6.6 6.3 Evaporator inlet temperature C. 7.2 3.1 3.3 3.4 3.6 3.7 3.9 4.0 Condenser exit temperature C. 46.0 42.0 42.2 42.4 42.6 42.7 42.9 43.1 Condenser pressure bar 33.7 32.3 32.8 33.3 33.7 34.2 34.5 35.0 Evaporator pressure bar 10.2 9.2 9.4 9.5 9.7 9.8 10.0 10.1 Refrigeration effect kJ/kg 151.2 159.9 161.7 163.7 165.7 167.9 169.7 171.9 Coefficient of Performance (COP) 2.88 2.96 2.95 2.94 2.94 2.94 2.93 2.93 Discharge temperature C. 105.5 106.8 107.7 108.6 109.4 110.3 111.1 112.0 Mass flow rate kg/hr 251 238 235 232 229 226 224 221 Volumetric flow rate m.sup.3/hr 7.28 7.57 7.46 7.35 7.24 7.13 7.05 6.95 Volumetric cooling capacity kJ/m.sup.3 5226 5022 5097 5175 5249 5331 5392 5466 Suction line pressure drop Pa/m 163 163 160 156 152 148 145 142 Suction line gas density kg/m.sup.3 34.6 31.4 31.5 31.6 31.7 31.7 31.8 31.8 Condenser line gas density kg/m.sup.3 155.3 154.0 155.1 155.9 156.5 156.9 157.0 157.3

    Example 11 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 9 Weight % of R-1132a and 3 Weight % of CO.SUB.2 .(R-744))

    [0147]

    TABLE-US-00016 Nominal composition (weight %) R-1132a 9 9 9 9 9 9 9 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 R-1234yf 52 50 48 46 44 42 40 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 102.0% 101.7% 101.7% 101.5% 101.3% 101.2% 101.1% Cooling Capacity relative to reference 100.0% 97.2% 98.6% 100.2% 101.6% 103.1% 104.4% 105.8% Compressor discharge temperature difference K 0.0 1.7 2.6 3.4 4.2 5.1 5.9 6.8 Pressure ratio 3.32 3.50 3.49 3.48 3.47 3.46 3.46 3.45 Volumetric efficiency 94.5% 93.7% 93.8% 93.9% 94.0% 94.0% 94.1% 94.2% Condenser glide K 0.2 8.1 7.7 7.4 7.0 6.7 6.4 6.1 Evaporator glide K 0.1 8.3 8.0 7.7 7.4 7.1 6.8 6.5 Evaporator inlet temperature C. 7.2 3.1 3.2 3.4 3.5 3.7 3.8 4.0 Condenser exit temperature C. 46.0 42.0 42.3 42.4 42.6 42.8 42.9 43.1 Condenser pressure bar 33.7 32.9 33.4 33.8 34.2 34.7 35.1 35.5 Evaporator pressure bar 10.2 9.4 9.6 9.7 9.9 10.0 10.2 10.3 Refrigeration effect kJ/kg 151.2 159.6 161.4 163.4 165.4 167.5 169.6 171.7 Coefficient of Performance (COP) 2.88 2.94 2.93 2.93 2.93 2.92 2.92 2.91 Discharge temperature C. 105.5 107.3 108.2 109.0 109.7 110.7 111.5 112.3 Mass flow rate kg/hr 251 238 236 233 230 227 224 221 Volumetric flow rate m.sup.3/hr 7.28 7.49 7.38 7.26 7.16 7.06 6.97 6.88 Volumetric cooling capacity kJ/m.sup.3 5226 5079 5155 5235 5308 5385 5458 5528 Suction line pressure drop Pa/m 163 162 158 154 151 147 144 141 Suction line gas density kg/m.sup.3 34.6 31.8 31.9 32.0 32.1 32.2 32.2 32.2 Condenser line gas density kg/m.sup.3 155.3 157.6 158.7 159.3 159.7 160.4 160.7 160.7

    Example 12 (Quaternary Blends of R-1132a/Co.SUB.2./R-32/R-1234yf Comprising 10 Weight % of R-1132a and 3 Weight % of Co.SUB.2 .(R-744))

    [0148]

    TABLE-US-00017 Nominal composition (weight %) R-1132a 10 10 10 10 10 10 10 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 R-1234yf 51 49 47 45 43 41 39 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 101.4% 101.3% 101.2% 101.1% 100.9% 100.8% 100.7% Cooling Capacity relative to reference 100.0% 98.2% 99.8% 101.3% 102.8% 104.2% 105.6% 107.0% Compressor discharge temperature difference K 0.0 2.1 2.9 3.8 4.6 5.4 6.3 7.1 Pressure ratio 3.32 3.50 3.48 3.48 3.47 3.46 3.45 3.44 Volumetric efficiency 94.5% 93.8% 93.8% 93.9% 94.0% 94.1% 94.1% 94.2% Condenser glide K 0.2 7.9 7.6 7.3 7.0 6.7 6.4 6.1 Evaporator glide K 0.1 8.4 8.1 7.8 7.5 7.2 6.9 6.6 Evaporator inlet temperature C. 7.2 3.0 3.2 3.3 3.5 3.6 3.8 3.9 Condenser exit temperature C. 46.0 42.2 42.3 42.4 42.6 42.8 42.9 43.1 Condenser pressure bar 33.7 33.4 33.9 34.3 34.8 35.2 35.6 36.0 Evaporator pressure bar 10.2 9.6 9.7 9.9 10.0 10.2 10.3 10.5 Refrigeration effect kJ/kg 151.2 159.1 161.0 163.2 165.1 167.2 169.3 171.4 Coefficient of Performance (COP) 2.88 2.92 2.92 2.92 2.91 2.91 2.90 2.90 Discharge temperature C. 105.5 107.7 108.5 109.3 110.2 111.0 111.8 112.6 Mass flow rate kg/hr 251 239 236 233 230 227 225 222 Volumetric flow rate m.sup.3/hr 7.28 7.41 7.29 7.18 7.08 6.98 6.89 6.80 Volumetric cooling capacity kJ/m.sup.3 5226 5131 5213 5296 5372 5446 5519 5589 Suction line pressure drop Pa/m 163 160 157 153 149 146 142 139 Suction line gas density kg/m.sup.3 34.6 32.3 32.4 32.5 32.5 32.6 32.6 32.6 Condenser line gas density kg/m.sup.3 155.3 161.2 162.0 162.9 163.5 164.0 164.2 164.3

    Example 13 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 4 Weight % of R-1132a and 4 Weight % of CO.SUB.2 .(R-744))

    [0149]

    TABLE-US-00018 Nominal composition (weight %) R-1132a 4 4 4 4 4 4 4 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 56 54 52 50 48 46 44 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 103.7% 103.4% 103.2% 103.0% 102.8% 102.6% 102.4% Cooling Capacity relative to reference 100.0% 93.6% 95.1% 96.5% 98.0% 99.4% 100.7% 102.0% Compressor discharge temperature difference K 0.0 0.9 1.8 2.6 3.5 4.4 5.3 6.1 Pressure ratio 3.32 3.53 3.52 3.51 3.50 3.49 3.49 3.48 Volumetric efficiency 94.5% 93.6% 93.7% 93.8% 93.9% 93.9% 94.0% 94.1% Condenser glide K 0.2 8.5 8.1 7.7 7.4 7.0 6.7 6.4 Evaporator glide K 0.1 8.0 7.7 7.4 7.1 6.8 6.5 6.2 Evaporator inlet temperature C. 7.2 3.2 3.4 3.5 3.7 3.8 4.0 4.1 Condenser exit temperature C. 46.0 41.9 42.1 42.2 42.4 42.6 42.7 42.9 Condenser pressure bar 33.7 31.2 31.7 32.1 32.6 33.0 33.4 33.8 Evaporator pressure bar 10.2 8.9 9.0 9.2 9.3 9.5 9.6 9.7 Refrigeration effect kJ/kg 151.2 161.4 163.3 165.3 167.3 169.4 171.5 173.6 Coefficient of Performance (COP) 2.88 2.99 2.98 2.97 2.97 2.96 2.96 2.95 Discharge temperature C. 105.5 106.4 107.3 108.2 109.1 109.9 110.8 111.7 Mass flow rate kg/hr 251 236 233 230 227 224 222 219 Volumetric flow rate m.sup.3/hr 7.28 7.77 7.65 7.54 7.43 7.32 7.22 7.13 Volumetric cooling capacity kJ/m.sup.3 5226 4891 4968 5044 5119 5192 5263 5332 Suction line pressure drop Pa/m 163 167 162 159 155 151 148 145 Suction line gas density kg/m.sup.3 34.6 30.3 30.4 30.5 30.6 30.6 30.7 30.7 Condenser line gas density kg/m.sup.3 155.3 146.1 146.9 147.6 148.2 148.7 149.1 149.2

    Example 14 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 5 Weight % of R-1132a and 4 Weight % of CO.SUB.2 .(R-744))

    [0150]

    TABLE-US-00019 Nominal composition (weight %) R-1132a 5 5 5 5 5 5 5 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 55 53 51 49 47 45 43 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 103.2% 103.0% 102.7% 102.5% 102.4% 102.2% 102.0% Cooling Capacity relative to reference 100.0% 94.8% 96.3% 97.8% 99.2% 100.7% 101.9% 103.3% Compressor discharge temperature difference K 0.0 1.4 2.2 3.2 4.0 4.9 5.6 6.6 Pressure ratio 3.32 3.52 3.51 3.51 3.50 3.49 3.48 3.48 Volumetric efficiency 94.5% 93.7% 93.7% 93.8% 93.9% 94.0% 94.0% 94.1% Condenser glide K 0.2 8.6 8.2 7.9 7.5 7.3 6.8 6.5 Evaporator glide K 0.1 8.1 7.8 7.5 7.2 6.9 6.6 6.3 Evaporator inlet temperature C. 7.2 3.2 3.3 3.5 3.6 3.8 3.9 4.1 Condenser exit temperature C. 46.0 41.8 42.0 42.2 42.4 42.5 42.7 42.9 Condenser pressure bar 33.7 31.8 32.2 32.7 33.1 33.6 34.0 34.4 Evaporator pressure bar 10.2 9.0 9.2 9.3 9.5 9.6 9.8 9.9 Refrigeration effect kJ/kg 151.2 161.3 163.2 165.3 167.2 169.4 171.3 173.5 Coefficient of Performance (COP) 2.88 2.97 2.97 2.96 2.96 2.95 2.95 2.94 Discharge temperature C. 105.5 106.9 107.8 108.7 109.5 110.4 111.2 112.1 Mass flow rate kg/hr 251 236 233 230 227 224 222 219 Volumetric flow rate m.sup.3/hr 7.28 7.67 7.55 7.43 7.33 7.22 7.14 7.04 Volumetric cooling capacity kJ/m.sup.3 5226 4955 5033 5113 5185 5263 5326 5398 Suction line pressure drop Pa/m 163 164 160 156 153 149 146 143 Suction line gas density kg/m.sup.3 34.6 30.7 30.8 30.9 31.0 31.1 31.1 31.1 Condenser line gas density kg/m.sup.3 155.3 149.4 150.2 151.2 151.6 152.2 152.2 152.5

    Example 15 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 6 Weight % of R-1132a and 4 Weight % of CO.SUB.2 .(R-744))

    [0151]

    TABLE-US-00020 Nominal composition (weight %) R-1132a 6 6 6 6 6 6 6 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 54 52 50 48 46 44 42 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 102.8% 102.5% 102.3% 102.0% 101.8% 101.7% 101.6% Cooling Capacity relative to reference 100.0% 96.1% 97.5% 98.9% 100.3% 101.7% 103.1% 104.5% Compressor discharge temperature difference K 0.0 1.8 2.6 3.4 4.4 5.2 6.0 6.9 Pressure ratio 3.32 3.52 3.51 3.50 3.49 3.49 3.48 3.47 Volumetric efficiency 94.5% 93.7% 93.8% 93.8% 93.9% 94.0% 94.1% 94.1% Condenser glide K 0.2 8.7 8.2 7.8 7.3 7.0 6.7 6.5 Evaporator glide K 0.1 8.3 8.0 7.7 7.4 7.0 6.7 6.5 Evaporator inlet temperature C. 7.2 3.1 3.2 3.4 3.5 3.7 3.8 4.0 Condenser exit temperature C. 46.0 41.7 42.0 42.2 42.5 42.6 42.8 42.8 Condenser pressure bar 33.7 32.3 32.7 33.2 33.7 34.1 34.5 34.9 Evaporator pressure bar 10.2 9.2 9.3 9.5 9.6 9.8 9.9 10.1 Refrigeration effect kJ/kg 151.2 161.2 163.0 164.9 166.8 168.9 171.0 173.3 Coefficient of Performance (COP) 2.88 2.96 2.95 2.95 2.94 2.93 2.93 2.93 Discharge temperature C. 105.5 107.3 108.2 109.0 109.9 110.7 111.6 112.5 Mass flow rate kg/hr 251 236 233 231 228 225 222 219 Volumetric flow rate m.sup.3/hr 7.28 7.57 7.46 7.36 7.26 7.15 7.06 6.96 Volumetric cooling capacity kJ/m.sup.3 5226 5022 5095 5168 5240 5313 5386 5461 Suction line pressure drop Pa/m 163 162 159 155 152 148 145 141 Suction line gas density kg/m.sup.3 34.6 31.1 31.3 31.3 31.4 31.5 31.5 31.5 Condenser line gas density kg/m.sup.3 155.3 152.7 153.5 154.0 154.9 155.3 155.5 155.7

    Example 16 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 7 Weight % of R-1132a and 4 Weight % of CO.SUB.2 .(R-744))

    [0152]

    TABLE-US-00021 Nominal composition (weight %) R-1132a 7 7 7 7 7 7 7 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 53 51 49 47 45 43 41 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 102.3% 102.0% 101.8% 101.7% 101.4% 101.3% 101.2% Cooling Capacity relative to reference 100.0% 97.2% 98.6% 100.0% 101.6% 102.9% 104.4% 105.7% Compressor discharge temperature difference K 0.0 2.1 3.0 3.8 4.7 5.6 6.4 7.3 Pressure ratio 3.32 3.52 3.50 3.50 3.49 3.48 3.47 3.47 Volumetric efficiency 94.5% 93.7% 93.8% 93.9% 93.9% 94.0% 94.1% 94.2% Condenser glide K 0.2 8.6 8.1 7.7 7.5 7.0 6.8 6.5 Evaporator glide K 0.1 8.4 8.1 7.8 7.5 7.2 6.9 6.6 Evaporator inlet temperature C. 7.2 3.0 3.2 3.3 3.5 3.6 3.8 3.9 Condenser exit temperature C. 46.0 41.8 42.1 42.3 42.4 42.6 42.7 42.8 Condenser pressure bar 33.7 32.8 33.2 33.7 34.2 34.6 35.0 35.4 Evaporator pressure bar 10.2 9.3 9.5 9.6 9.8 9.9 10.1 10.2 Refrigeration effect kJ/kg 151.2 160.9 162.7 164.6 166.8 168.6 170.9 173.0 Coefficient of Performance (COP) 2.88 2.95 2.94 2.93 2.93 2.92 2.92 2.92 Discharge temperature C. 105.5 107.7 108.5 109.4 110.3 111.1 111.9 112.8 Mass flow rate kg/hr 251 236 234 231 228 225 222 220 Volumetric flow rate m.sup.3/hr 7.28 7.49 7.38 7.27 7.16 7.07 6.97 6.88 Volumetric cooling capacity kJ/m.sup.3 5226 5078 5152 5227 5309 5375 5453 5523 Suction line pressure drop Pa/m 163 161 157 154 150 147 143 140 Suction line gas density kg/m.sup.3 34.6 31.6 31.7 31.8 31.8 31.9 31.9 31.9 Condenser line gas density kg/m.sup.3 155.3 155.9 156.7 157.5 158.2 158.7 158.9 159.1

    Example 17 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 8 Weight % of R-1132a and 4 Weight % of CO.SUB.2 .(R-744))

    [0153]

    TABLE-US-00022 Nominal composition (weight %) R-1132a 8 8 8 8 8 8 8 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 52 50 48 46 44 42 40 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 101.8% 101.6% 101.4% 101.3% 101.1% 100.9% 100.7% Cooling Capacity relative to reference 100.0% 98.3% 99.8% 101.3% 102.8% 104.2% 105.5% 106.7% Compressor discharge temperature difference K 0.0 2.5 3.4 4.2 5.0 5.9 6.7 7.6 Pressure ratio 3.32 3.51 3.50 3.49 3.48 3.48 3.47 3.46 Volumetric efficiency 94.5% 93.7% 93.8% 93.9% 94.0% 94.0% 94.1% 94.2% Condenser glide K 0.2 8.6 8.2 7.8 7.5 7.1 6.8 6.3 Evaporator glide K 0.1 8.6 8.3 7.9 7.6 7.3 7.0 6.7 Evaporator inlet temperature C. 7.2 2.9 3.1 3.3 3.4 3.6 3.7 3.9 Condenser exit temperature C. 46.0 41.8 42.0 42.2 42.4 42.6 42.7 42.9 Condenser pressure bar 33.7 33.3 33.8 34.3 34.7 35.1 35.5 35.9 Evaporator pressure bar 10.2 9.5 9.7 9.8 10.0 10.1 10.2 10.4 Refrigeration effect kJ/kg 151.2 160.6 162.5 164.5 166.6 168.5 170.6 172.5 Coefficient of Performance (COP) 2.88 2.93 2.93 2.92 2.92 2.91 2.91 2.90 Discharge temperature C. 105.5 108.1 108.9 109.8 110.6 111.4 112.3 113.1 Mass flow rate kg/hr 251 237 234 231 228 226 223 220 Volumetric flow rate m.sup.3/hr 7.28 7.40 7.29 7.18 7.08 6.98 6.89 6.82 Volumetric cooling capacity kJ/m.sup.3 5226 5139 5218 5295 5372 5443 5515 5578 Suction line pressure drop Pa/m 163 159 155 152 148 145 142 139 Suction line gas density kg/m.sup.3 34.6 32.0 32.1 32.2 32.3 32.3 32.3 32.3 Condenser line gas density kg/m.sup.3 155.3 159.3 160.3 161.1 161.6 162.2 162.4 162.5

    Example 18 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 9 Weight % of R-1132a and 4 Weight % of CO.SUB.2 .(R-744))

    [0154]

    TABLE-US-00023 Nominal composition (weight %) R-1132a 9 9 9 9 9 9 9 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 51 49 47 45 43 41 39 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 101.3% 101.2% 101.0% 100.8% 100.6% 100.5% 100.3% Cooling Capacity relative to reference 100.0% 99.4% 101.1% 102.5% 103.9% 105.3% 106.6% 107.9% Compressor discharge temperature difference K 0.0 2.8 3.7 4.6 5.3 6.2 7.0 7.9 Pressure ratio 3.32 3.50 3.49 3.49 3.47 3.47 3.46 3.45 Volumetric efficiency 94.5% 93.8% 93.8% 93.9% 94.0% 94.1% 94.1% 94.2% Condenser glide K 0.2 8.5 8.2 7.7 7.3 7.1 6.7 6.3 Evaporator glide K 0.1 8.7 8.4 8.1 7.7 7.4 7.1 6.8 Evaporator inlet temperature C. 7.2 2.9 3.0 3.2 3.4 3.5 3.7 3.8 Condenser exit temperature C. 46.0 41.9 42.0 42.2 42.4 42.6 42.8 43.0 Condenser pressure bar 33.7 33.8 34.3 34.8 35.2 35.6 36.0 36.4 Evaporator pressure bar 10.2 9.7 9.8 10.0 10.1 10.3 10.4 10.6 Refrigeration effect kJ/kg 151.2 160.2 162.3 164.2 166.1 168.2 170.2 172.2 Coefficient of Performance (COP) 2.88 2.92 2.92 2.91 2.91 2.90 2.90 2.89 Discharge temperature C. 105.5 108.4 109.2 110.1 110.9 111.8 112.5 113.4 Mass flow rate kg/hr 251 237 234 232 229 226 223 221 Volumetric flow rate m.sup.3/hr 7.28 7.32 7.20 7.10 7.01 6.91 6.82 6.74 Volumetric cooling capacity kJ/m.sup.3 5226 5195 5281 5355 5427 5504 5573 5639 Suction line pressure drop Pa/m 163 158 154 150 147 143 140 138 Suction line gas density kg/m.sup.3 34.6 32.4 32.5 32.6 32.7 32.7 32.7 32.7 Condenser line gas density kg/m.sup.3 155.3 162.6 163.7 164.7 165.0 165.8 165.8 166.0

    Example 19 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 10 Weight % of R-1132a and 4 Weight % of CO.SUB.2 .(R-744))

    [0155]

    TABLE-US-00024 Nominal composition (weight %) R-1132a 10 10 10 10 10 10 10 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 50 48 46 44 42 40 38 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 100.8% 100.7% 100.6% 100.3% 100.2% 100.1% 100.0% Cooling Capacity relative to reference 100.0% 100.6% 102.1% 103.7% 105.1% 106.4% 107.9% 109.2% Compressor discharge temperature difference K 0.0 3.3 4.1 4.9 5.7 6.5 7.4 8.2 Pressure ratio 3.32 3.50 3.49 3.48 3.47 3.46 3.46 3.45 Volumetric efficiency 94.5% 93.8% 93.9% 93.9% 94.0% 94.1% 94.2% 94.2% Condenser glide K 0.2 8.5 8.1 7.8 7.3 6.9 6.7 6.4 Evaporator glide K 0.1 8.8 8.5 8.2 7.8 7.5 7.2 6.9 Evaporator inlet temperature C. 7.2 2.8 3.0 3.1 3.3 3.5 3.6 3.8 Condenser exit temperature C. 46.0 41.9 42.1 42.2 42.4 42.6 42.8 42.9 Condenser pressure bar 33.7 34.4 34.8 35.3 35.7 36.1 36.6 37.0 Evaporator pressure bar 10.2 9.8 10.0 10.1 10.3 10.4 10.6 10.7 Refrigeration effect kJ/kg 151.2 160.0 161.9 163.9 165.8 167.8 169.9 172.1 Coefficient of Performance (COP) 2.88 2.91 2.90 2.90 2.89 2.89 2.88 2.88 Discharge temperature C. 105.5 108.8 109.6 110.4 111.3 112.0 112.9 113.7 Mass flow rate kg/hr 251 238 235 232 229 227 224 221 Volumetric flow rate m.sup.3/hr 7.28 7.23 7.12 7.02 6.92 6.84 6.74 6.66 Volumetric cooling capacity kJ/m.sup.3 5226 5258 5338 5418 5490 5561 5637 5707 Suction line pressure drop Pa/m 163 156 152 149 145 142 139 136 Suction line gas density kg/m.sup.3 34.6 32.9 33.0 33.1 33.1 33.1 33.2 33.2 Condenser line gas density kg/m.sup.3 155.3 166.6 167.7 168.3 169.1 169.3 169.8 169.9

    Example 20 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 4 Weight % of R-1132a and 5 Weight % of CO.SUB.2 .(R-744))

    [0156]

    TABLE-US-00025 Nominal composition (weight %) R-1132a 4 4 4 4 4 4 4 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 55 53 51 49 47 45 43 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 103.0% 102.7% 102.5% 102.3% 102.1% 101.9% 101.7% Cooling Capacity relative to reference 100.0% 96.0% 97.5% 98.9% 100.3% 101.7% 103.1% 104.4% Compressor discharge temperature difference K 0.0 2.2 3.0 3.9 4.8 5.6 6.5 7.4 Pressure ratio 3.32 3.54 3.53 3.52 3.51 3.50 3.49 3.49 Volumetric efficiency 94.5% 93.7% 93.7% 93.8% 93.9% 94.0% 94.0% 94.1% Condenser glide K 0.2 9.1 8.7 8.3 7.9 7.5 7.3 6.9 Evaporator glide K 0.1 8.4 8.1 7.8 7.5 7.2 6.9 6.6 Evaporator inlet temperature C. 7.2 3.0 3.2 3.3 3.5 3.6 3.8 3.9 Condenser exit temperature C. 46.0 41.6 41.8 42.0 42.1 42.4 42.5 42.6 Condenser pressure bar 33.7 32.2 32.7 33.1 33.6 34.0 34.4 34.8 Evaporator pressure bar 10.2 9.1 9.3 9.4 9.6 9.7 9.9 10.0 Refrigeration effect kJ/kg 151.2 162.4 164.3 166.3 168.3 170.3 172.5 174.6 Coefficient of Performance (COP) 2.88 2.97 2.96 2.95 2.95 2.94 2.94 2.93 Discharge temperature C. 105.5 107.7 108.6 109.4 110.3 111.1 112.1 112.9 Mass flow rate kg/hr 251 234 231 229 226 223 220 218 Volumetric flow rate m.sup.3/hr 7.28 7.58 7.46 7.35 7.25 7.16 7.06 6.97 Volumetric cooling capacity kJ/m.sup.3 5226 5016 5093 5169 5244 5313 5387 5455 Suction line pressure drop Pa/m 163 162 158 154 150 147 144 141 Suction line gas density kg/m.sup.3 34.6 30.9 31.0 31.1 31.2 31.2 31.2 31.3 Condenser line gas density kg/m.sup.3 155.3 151.0 151.9 152.6 153.3 153.5 154.0 154.2

    Example 21 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 5 Weight % of R-1132a and 5 Weight % of CO.SUB.2 .(R-744))

    [0157]

    TABLE-US-00026 Nominal composition (weight %) R-1132a 5 5 5 5 5 5 5 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 54 52 50 48 46 44 42 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 102.5% 102.3% 102.1% 101.9% 101.7% 101.5% 101.3% Cooling Capacity relative to reference 100.0% 97.2% 98.6% 100.1% 101.6% 102.9% 104.3% 105.6% Compressor discharge temperature difference K 0.0 2.5 3.4 4.3 5.1 6.0 6.9 7.7 Pressure ratio 3.32 3.53 3.52 3.51 3.50 3.49 3.49 3.48 Volumetric efficiency 94.5% 93.7% 93.8% 93.8% 93.9% 94.0% 94.1% 94.1% Condenser glide K 0.2 9.1 8.6 8.3 8.0 7.5 7.3 6.9 Evaporator glide K 0.1 8.6 8.2 7.9 7.6 7.3 7.0 6.7 Evaporator inlet temperature C. 7.2 2.9 3.1 3.3 3.4 3.6 3.7 3.9 Condenser exit temperature C. 46.0 41.6 41.8 42.0 42.1 42.4 42.5 42.6 Condenser pressure bar 33.7 32.7 33.2 33.7 34.1 34.5 34.9 35.3 Evaporator pressure bar 10.2 9.3 9.4 9.6 9.7 9.9 10.0 10.2 Refrigeration effect kJ/kg 151.2 162.2 164.0 166.1 168.1 170.0 172.2 174.3 Coefficient of Performance (COP) 2.88 2.95 2.95 2.94 2.94 2.93 2.92 2.92 Discharge temperature C. 105.5 108.1 108.9 109.8 110.7 111.5 112.4 113.3 Mass flow rate kg/hr 251 234 232 229 226 224 221 218 Volumetric flow rate m.sup.3/hr 7.28 7.49 7.38 7.27 7.16 7.07 6.98 6.89 Volumetric cooling capacity kJ/m.sup.3 5226 5077 5153 5231 5307 5375 5449 5519 Suction line pressure drop Pa/m 163 160 156 152 149 146 142 139 Suction line gas density kg/m.sup.3 34.6 31.3 31.4 31.5 31.6 31.6 31.6 31.7 Condenser line gas density kg/m.sup.3 155.3 154.2 155.0 155.9 156.5 156.8 157.3 157.4

    Example 22 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 6 Weight % of R-1132a and 5 Weight % of CO.SUB.2 .(R-744))

    [0158]

    TABLE-US-00027 Nominal composition (weight %) R-1132a 6 6 6 6 6 6 6 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 53 51 49 47 45 43 41 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 102.0% 101.7% 101.5% 101.5% 101.2% 100.9% 101.0% Cooling Capacity relative to reference 100.0% 98.3% 99.7% 101.2% 102.8% 104.0% 105.3% 106.8% Compressor discharge temperature difference K 0.0 2.9 3.8 4.7 5.5 6.3 7.2 8.1 Pressure ratio 3.32 3.53 3.52 3.51 3.50 3.49 3.48 3.48 Volumetric efficiency 94.5% 93.7% 93.8% 93.9% 93.9% 94.0% 94.1% 94.2% Condenser glide K 0.2 9.1 8.5 8.1 8.1 7.5 7.1 7.0 Evaporator glide K 0.1 8.7 8.4 8.1 7.8 7.4 7.1 6.8 Evaporator inlet temperature C. 7.2 2.9 3.0 3.2 3.3 3.5 3.7 3.8 Condenser exit temperature C. 46.0 41.6 41.9 42.1 42.1 42.4 42.6 42.6 Condenser pressure bar 33.7 33.2 33.7 34.2 34.6 35.0 35.5 35.9 Evaporator pressure bar 10.2 9.4 9.6 9.7 9.9 10.0 10.2 10.3 Refrigeration effect kJ/kg 151.2 161.9 163.7 165.6 168.0 169.8 171.7 174.1 Coefficient of Performance (COP) 2.88 2.94 2.93 2.93 2.93 2.92 2.91 2.91 Discharge temperature C. 105.5 108.5 109.3 110.2 111.0 111.8 112.8 113.6 Mass flow rate kg/hr 251 235 232 230 226 224 221 218 Volumetric flow rate m.sup.3/hr 7.28 7.40 7.30 7.19 7.07 6.99 6.91 6.81 Volumetric cooling capacity kJ/m.sup.3 5226 5138 5210 5286 5374 5437 5504 5582 Suction line pressure drop Pa/m 163 158 155 151 147 144 141 138 Suction line gas density kg/m.sup.3 34.6 31.7 31.8 31.9 32.0 32.0 32.0 32.1 Condenser line gas density kg/m.sup.3 155.3 157.6 158.5 159.3 159.9 160.1 160.7 160.7

    Example 23 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 7 Weight % of R-1132a and 5 Weight % of CO.SUB.2 .(R-744))

    [0159]

    TABLE-US-00028 Nominal composition (weight %) R-1132a 7 7 7 7 7 7 7 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 52 50 48 46 44 42 40 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 101.6% 101.3% 101.1% 101.0% 100.8% 100.7% 100.6% Cooling Capacity relative to reference 100.0% 99.5% 101.0% 102.5% 103.9% 105.2% 106.6% 108.0% Compressor discharge temperature difference K 0.0 3.3 4.2 5.0 5.9 6.6 7.5 8.4 Pressure ratio 3.32 3.52 3.51 3.50 3.49 3.48 3.48 3.47 Volumetric efficiency 94.5% 93.7% 93.8% 93.9% 94.0% 94.0% 94.1% 94.2% Condenser glide K 0.2 9.0 8.6 8.2 7.9 7.4 7.1 7.0 Evaporator glide K 0.1 8.8 8.5 8.2 7.9 7.5 7.2 6.9 Evaporator inlet temperature C. 7.2 2.8 3.0 3.1 3.3 3.5 3.6 3.8 Condenser exit temperature C. 46.0 41.6 41.8 42.0 42.2 42.4 42.6 42.6 Condenser pressure bar 33.7 33.8 34.2 34.7 35.2 35.5 36.0 36.4 Evaporator pressure bar 10.2 9.6 9.8 9.9 10.1 10.2 10.3 10.5 Refrigeration effect kJ/kg 151.2 161.6 163.6 165.5 167.5 169.5 171.5 173.8 Coefficient of Performance (COP) 2.88 2.93 2.92 2.92 2.91 2.91 2.90 2.90 Discharge temperature C. 105.5 108.8 109.7 110.6 111.4 112.2 113.0 113.9 Mass flow rate kg/hr 251 235 232 230 227 224 222 219 Volumetric flow rate m.sup.3/hr 7.28 7.31 7.20 7.10 7.00 6.91 6.83 6.73 Volumetric cooling capacity kJ/m.sup.3 5226 5199 5277 5354 5429 5498 5569 5645 Suction line pressure drop Pa/m 163 157 153 149 146 143 140 136 Suction line gas density kg/m.sup.3 34.6 32.2 32.3 32.3 32.4 32.4 32.5 32.5 Condenser line gas density kg/m.sup.3 155.3 161.0 162.0 162.8 163.5 163.6 163.9 164.1

    Example 24 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 8 Weight % of R-1132a and 5 Weight % of CO.SUB.2 .(R-744))

    [0160]

    TABLE-US-00029 Nominal composition (weight %) R-1132a 8 8 8 8 8 8 8 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 51 49 47 45 43 41 39 Results R410A GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 101.1% 100.9% 100.8% 100.6% 100.5% 100.2% 100.1% Cooling Capacity relative to reference 100.0% 100.6% 102.1% 103.8% 105.1% 106.5% 107.8% 109.1% Compressor discharge temperature difference K 0.0 3.7 4.5 5.3 6.2 7.0 7.9 8.7 Pressure ratio 3.32 3.51 3.50 3.50 3.49 3.48 3.47 3.46 Volumetric efficiency 94.5% 93.8% 93.8% 93.9% 94.0% 94.1% 94.1% 94.2% Condenser glide K 0.2 9.0 8.5 8.4 7.9 7.6 7.1 6.8 Evaporator glide K 0.1 9.0 8.6 8.3 8.0 7.6 7.3 7.0 Evaporator inlet temperature C. 7.2 2.7 2.9 3.1 3.2 3.4 3.6 3.7 Condenser exit temperature C. 46.0 41.6 41.9 41.9 42.2 42.3 42.5 42.7 Condenser pressure bar 33.7 34.3 34.7 35.2 35.7 36.1 36.5 36.9 Evaporator pressure bar 10.2 9.8 9.9 10.1 10.2 10.4 10.5 10.6 Refrigeration effect kJ/kg 151.2 161.3 163.2 165.4 167.3 169.3 171.3 173.4 Coefficient of Performance (COP) 2.88 2.91 2.91 2.91 2.90 2.90 2.89 2.88 Discharge temperature C. 105.5 109.2 110.0 110.9 111.7 112.5 113.4 114.2 Mass flow rate kg/hr 251 236 233 230 227 225 222 219 Volumetric flow rate m.sup.3/hr 7.28 7.23 7.13 7.01 6.92 6.83 6.75 6.67 Volumetric cooling capacity kJ/m.sup.3 5226 5259 5334 5422 5491 5566 5634 5703 Suction line pressure drop Pa/m 163 155 151 147 144 141 138 135 Suction line gas density kg/m.sup.3 34.6 32.6 32.7 32.8 32.8 32.9 32.9 32.9 Condenser line gas density kg/m.sup.3 155.3 164.6 165.4 166.5 167.0 167.4 167.9 167.9

    Example 25 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 9 Weight % of R-1132a and 5 Weight % of CO.SUB.2 .(R-744))

    [0161]

    TABLE-US-00030 Nominal composition (weight %) R-1132a 9 9 9 9 9 9 9 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf Results R410A 50 48 46 44 42 40 38 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 100.7% 100.5% 100.3% 100.2% 99.8% 99.8% 99.6% Cooling Capacity relative to reference 100.0% 101.8% 103.4% 104.8% 106.3% 107.5% 109.0% 110.2% Compressor discharge temperature difference K 0.0 4.0 4.9 5.6 6.4 7.3 8.2 9.0 Pressure ratio 3.32 3.51 3.50 3.49 3.48 3.47 3.47 3.46 Volumetric efficiency 94.5% 93.8% 93.9% 93.9% 94.0% 94.1% 94.2% 94.2% Condenser glide K 0.2 9.0 8.7 8.2 7.8 7.2 7.1 6.6 Evaporator glide K 0.1 9.1 8.7 8.4 8.1 7.7 7.4 7.1 Evaporator inlet temperature C. 7.2 2.7 2.8 3.0 3.2 3.4 3.5 3.7 Condenser exit temperature C. 46.0 41.6 41.8 42.0 42.2 42.5 42.6 42.8 Condenser pressure bar 33.7 34.8 35.3 35.7 36.2 36.6 37.0 37.4 Evaporator pressure bar 10.2 9.9 10.1 10.2 10.4 10.5 10.7 10.8 Refrigeration effect kJ/kg 151.2 161.1 163.1 164.9 167.0 168.7 170.9 172.9 Coefficient of Performance (COP) 2.88 2.90 2.90 2.89 2.89 2.88 2.88 2.87 Discharge temperature C. 105.5 109.5 110.4 111.2 112.0 112.9 113.7 114.5 Mass flow rate kg/hr 251 236 233 230 228 225 222 220 Volumetric flow rate m.sup.3/hr 7.28 7.14 7.03 6.94 6.85 6.77 6.68 6.60 Volumetric cooling capacity kJ/m.sup.3 5226 5322 5404 5477 5554 5615 5694 5758 Suction line pressure drop Pa/m 163 153 150 146 143 140 137 134 Suction line gas density kg/m.sup.3 34.6 33.0 33.1 33.2 33.3 33.3 33.3 33.3 Condenser line gas density kg/m.sup.3 155.3 168.2 169.4 170.2 170.7 171.4 171.7 171.5

    Example 26 (Quaternary Blends of R-1132a/CO.SUB.2./R-32/R-1234yf Comprising 10 Weight % of R-1132a and 5 Weight % of CO.SUB.2 .(R-744))

    [0162]

    TABLE-US-00031 Nominal composition (weight %) R-1132a 10 10 10 10 10 10 10 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf R410A 49 47 45 43 41 39 37 GWP (AR4 basis) 2107 244 257 271 284 298 311 325 Cooling COP relative to reference 100.0% 100.1% 99.9% 99.8% 99.6% 99.5% 99.4% 99.3% Cooling Capacity relative to reference 100.0% 102.9% 104.3% 105.9% 107.3% 108.7% 110.1% 111.4% Compressor discharge K 0.0 4.4 5.1 6.0 6.8 7.6 8.4 9.3 temperature difference Pressure ratio 3.32 3.50 3.49 3.49 3.47 3.47 3.46 3.45 Volumetric efficiency 94.5% 93.8% 93.9% 94.0% 94.0% 94.1% 94.2% 94.3% Condenser glide K 0.2 8.8 8.3 8.0 7.6 7.3 7.0 6.7 Evaporator glide K 0.1 9.2 8.8 8.5 8.1 7.8 7.5 7.2 Evaporator inlet temperature C. 7.2 2.6 2.8 3.0 3.1 3.3 3.5 3.6 Condenser exit temperature C. 46.0 41.7 42.0 42.1 42.3 42.5 42.6 42.8 Condenser pressure bar 33.7 35.4 35.8 36.3 36.7 37.1 37.5 37.9 Evaporator pressure bar 10.2 10.1 10.3 10.4 10.6 10.7 10.9 11.0 Refrigeration effect kJ/kg 151.2 160.6 162.5 164.5 166.4 168.5 170.5 172.7 Coefficient of Performance (COP) 2.88 2.89 2.88 2.88 2.87 2.87 2.86 2.86 Discharge temperature C. 105.5 109.9 110.7 111.5 112.3 113.2 114.0 114.8 Mass flow rate kg/hr 251 237 234 231 229 226 223 220 Volumetric flow rate m.sup.3/hr 7.28 7.07 6.97 6.87 6.78 6.69 6.61 6.53 Volumetric cooling capacity kJ/m.sup.3 5226 5377 5452 5533 5605 5682 5753 5824 Suction line pressure drop Pa/m 163 152 149 145 142 139 136 133 Suction line gas density kg/m.sup.3 34.6 33.5 33.6 33.6 33.7 33.7 33.7 33.7 Condenser line gas density kg/m.sup.3 155.3 172.3 173.1 174.3 174.7 175.4 175.6 175.6

    Example 27 (Ternary Compositions Comprising 4, 5 and 6 Weight % of R-1132a)

    [0163]

    TABLE-US-00032 Nominal composition (% mass) R-1132a 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 60 58 56 54 52 50 48 Worst-Case Formulation (% mass) R-1132a 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-32 35 37 39 41 43 45 47 R-1234yf 60.5 58.5 56.5 54.5 52.5 50.5 48.5 Worst-Case Flammable Formulation (% volume) R-1132a 22.8% 22.2% 21.7% 21.1% 20.6% 20.0% 19.6% R-32 59.9% 61.6% 63.2% 64.7% 66.1% 67.5% 68.8% R-1234yf 17.3% 16.2% 15.2% 14.2% 13.3% 12.4% 11.6% Nominal composition (% mass) R-1132a 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 59 57 55 53 51 49 47 Worst-Case Formulation (% mass) R-1132a 5.5 5.5 5.5 5.5 5.5 5.5 5.5 R-32 35 37 39 41 43 45 47 R-1234yf 59.5 57.5 55.5 53.5 51.5 49.5 47.5 Worst-Case Flammable Formulation (% volume) R-1132a 26.6% 25.9% 25.3% 24.6% 24.0% 23.5% 23.0% R-32 57.2% 58.9% 60.5% 62.0% 63.4% 64.8% 66.1% R-1234yf 16.2% 15.2% 14.3% 13.4% 12.5% 11.7% 10.9% Nominal composition (% mass) R-1132a 6 6 6 6 6 6 6 R-32 36 38 40 42 44 46 48 R-1234yf 58 56 54 52 50 48 46 Worst-Case Formulation (% mass) R-1132a 6.5 6.5 6.5 6.5 6.5 6.5 6.5 R-32 35 37 39 41 43 45 47 R-1234yf 58.5 56.5 54.5 52.5 50.5 48.5 46.5 Worst-Case Flammable Formulation (% volume) R-1132a 30.1% 29.3% 28.6% 28.0% 27.2% 26.7% 26.1% R-32 54.7% 56.4% 58.0% 59.5% 61.0% 62.3% 63.6% R-1234yf 15.3% 14.3% 13.4% 12.6% 11.8% 11.0% 10.3%

    Example 28 (Ternary Compositions Comprising 7 and 8 Weight % of R-1132a)

    [0164]

    TABLE-US-00033 Nominal composition (% mass) R-1132a 7 7 7 7 7 7 7 R-32 36 38 40 42 44 46 48 R-1234yf 57 55 53 51 49 47 45 Worst-Case Formulation (% mass) R-1132a 7.5 7.5 7.5 7.5 7.5 7.5 7.5 R-32 35 37 39 41 43 45 47 R-1234yf 57.5 55.5 53.5 51.5 49.5 47.5 45.5 Worst-Case Flammable Formulation (% volume) R-1132a 33.2% 32.3% 31.6% 30.9% 30.3% 29.6% 29.0% R-32 52.5% 54.1% 55.7% 57.2% 58.7% 60.0% 61.3% R-1234yf 14.4% 13.5% 12.7% 11.9% 11.1% 10.4% 9.7% Nominal composition (% mass) R-1132a 8 8 8 8 8 8 8 R-32 36 38 40 42 44 46 48 R-1234yf 56 54 52 50 48 46 44 Worst-Case Formulation (% mass) R-1132a 8.5 8.5 8.5 8.5 8.5 8.5 8.5 R-32 35 37 39 41 43 45 47 R-1234yf 56.5 54.5 52.5 50.5 48.5 46.5 44.5 Worst-Case Flammable Formulation (% volume) R-1132a 36.1% 35.3% 34.4% 33.8% 33.0% 32.3% 31.7% R-32 50.4% 52.0% 53.6% 55.1% 56.5% 57.9% 59.2% R-1234yf 13.6% 12.7% 11.9% 11.2% 10.5% 9.8% 9.1%

    Example 29 (Quaternary Compositions Comprising 3 Weight % CO.SUB.2.)

    [0165]

    TABLE-US-00034 Nominal composition (% mass) R-1132a 4 4 4 4 4 4 4 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 R-1234yf 57 55 53 51 49 47 45 Worst-Case Formulation (% mass) R-1132a 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-744 2.5 2.5 2.5 2.5 2.5 2.5 2.5 R-32 35 37 39 41 43 45 47 R-1234yf 58 56 54 52 50 48 46 Worst-Case Flammable Formulation (% volume) R-1132a 18.2% 17.8% 17.4% 17.0% 16.6% 16.3% 16.0% R-744 20.5% 20.2% 19.8% 19.5% 19.2% 18.9% 18.6% R-32 48.1% 49.7% 51.2% 52.6% 54.0% 55.3% 56.5% R-1234yf 13.1% 12.3% 11.6% 10.9% 10.2% 9.5% 8.9% Nominal composition (% mass) R-1132a 5 5 5 5 5 5 5 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 R-1234yf 56 54 52 50 48 46 44 Worst-Case Formulation (% mass) R-1132a 5.5 5.5 5.5 5.5 5.5 5.5 5.5 R-744 2.5 2.5 2.5 2.5 2.5 2.5 2.5 R-32 35 37 39 41 43 45 47 R-1234yf 57 55 53 51 49 47 45 Worst-Case Flammable Formulation (% volume) R-1132a 21.4% 20.9% 20.5% 20.1% 19.6% 19.2% 18.8% R-744 19.7% 19.4% 19.1% 18.8% 18.6% 18.3% 18.0% R-32 46.4% 47.9% 49.4% 50.8% 52.2% 53.5% 54.7% R-1234yf 12.4% 11.7% 11.0% 10.3% 9.6% 9.0% 8.4%

    Example 30 (Quaternary Compositions Comprising 3 Weight % CO.SUB.2.)

    [0166]

    TABLE-US-00035 Nominal composition (% mass) R-1132a 6 6 6 6 6 6 6 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 R-1234yf 55 53 51 49 47 45 43 Worst-Case Formulation (% mass) R-1132a 6.5 6.5 6.5 6.5 6.5 6.5 6.5 R-744 2.5 2.5 2.5 2.5 2.5 2.5 2.5 R-32 35 37 39 41 43 45 47 R-1234yf 56 54 52 50 48 46 44 Worst-Case Flammable Formulation (% volume) R-1132a 24.4% 23.9% 23.4% 22.9% 22.4% 22.0% 21.5% R-744 19.0% 18.8% 18.5% 18.2% 18.0% 17.7% 17.5% R-32 44.8% 46.3% 47.8% 49.2% 50.5% 51.8% 53.0% R-1234yf 11.8% 11.1% 10.4% 9.8% 9.1% 8.6% 8.0% Nominal composition (% mass) R-1132a 7 7 7 7 7 7 7 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 R-1234yf 54 52 50 48 46 44 42 Worst-Case Formulation (% mass) R-1132a 7.5 7.5 7.5 7.5 7.5 7.5 7.5 R-744 2.5 2.5 2.5 2.5 2.5 2.5 2.5 R-32 35 37 39 41 43 45 47 R-1234yf 55 53 51 49 47 45 43 Worst-Case Flammable Formulation (% volume) R-1132a 27.2% 26.6% 26.1% 25.5% 25.0% 24.5% 24.1% R-744 18.4% 18.1% 17.9% 17.6% 17.4% 17.2% 17.0% R-32 43.3% 44.8% 46.2% 47.6% 48.9% 50.2% 51.4% R-1234yf 11.2% 10.5% 9.9% 9.3% 8.7% 8.1% 7.6%

    Example 31 (Quaternary Compositions Comprising 3 Weight % CO.SUB.2.)

    [0167]

    TABLE-US-00036 Nominal composition (% mass) R-1132a 8 8 8 8 8 8 8 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 R-1234yf 53 51 49 47 45 43 41 Worst-Case Formulation (% mass) R-1132a 8.5 8.5 8.5 8.5 8.5 8.5 8.5 R-744 2.5 2.5 2.5 2.5 2.5 2.5 2.5 R-32 35 37 39 41 43 45 47 R-1234yf 54 52 50 48 46 44 42 Worst-Case Flammable Formulation (% volume) R-1132a 29.7% 29.1% 28.6% 28.0% 27.5% 27.0% 26.5% R-744 17.8% 17.6% 17.3% 17.1% 16.9% 16.7% 16.5% R-32 41.9% 43.4% 44.8% 46.2% 47.5% 48.7% 49.9% R-1234yf 10.6% 10.0% 9.4% 8.8% 8.2% 7.7% 7.2% Nominal composition (% mass) R-1132a 9 9 9 9 9 9 9 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 R-1234yf 52 50 48 46 44 42 40 Worst-Case Formulation (% mass) R-1132a 9.5 9.5 9.5 9.5 9.5 9.5 9.5 R-744 2.5 2.5 2.5 2.5 2.5 2.5 2.5 R-32 35 37 39 41 43 45 47 R-1234yf 53 51 49 47 45 43 41 Worst-Case Flammable Formulation (% volume) R-1132a 32.1% 31.5% 30.9% 30.3% 29.7% 29.2% 28.7% R-744 17.2% 17.0% 16.8% 16.5% 16.3% 16.1% 16.0% R-32 40.6% 42.1% 43.4% 44.8% 46.1% 47.3% 48.5% R-1234yf 10.1% 9.5% 8.9% 8.3% 7.8% 7.3% 6.8%

    Example 32 (Quaternary Compositions Comprising 3 Weight % CO.SUB.2.)

    [0168]

    TABLE-US-00037 Nominal composition (% mass) R-1132a 10 10 10 10 10 10 10 R-744 3 3 3 3 3 3 3 R-32 36 38 40 42 44 46 48 R-1234yf 51 49 47 45 43 41 39 Worst-Case Formulation (% mass) R-1132a 10.5 10.5 10.5 10.5 10.5 10.5 10.5 R-744 2.5 2.5 2.5 2.5 2.5 2.5 2.5 R-32 35 37 39 41 43 45 47 R-1234yf 52 50 48 46 44 42 40 Worst-Case Flammable Formulation (% volume) R-1132a 34.4% 33.7% 33.1% 32.5% 31.9% 31.3% 30.8% R-744 16.7% 16.5% 16.3% 16.1% 15.9% 15.7% 15.6% R-32 39.3% 40.8% 42.2% 43.5% 44.8% 46.0% 47.2% R-1234yf 9.6% 9.0% 8.4% 7.9% 7.4% 6.9% 6.4%

    Example 33 (Quaternary Compositions Comprising 4 Weight % CO.SUB.2 .(R-744)

    [0169]

    TABLE-US-00038 Nominal composition (% mass) R-1132a 4 4 4 4 4 4 4 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 56 54 52 50 48 46 44 Worst-Case Formulation (% mass) R-1132a 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-744 3.5 3.5 3.5 3.5 3.5 3.5 3.5 R-32 35 37 39 41 43 45 47 R-1234yf 57 55 53 51 49 47 45 Worst-Case Flammable Formulation (% volume) R-1132a 16.8% 16.5% 16.1% 15.8% 15.4% 15.1% 14.8% R-744 26.6% 26.2% 25.8% 25.4% 25.1% 24.7% 24.4% R-32 44.6% 46.1% 47.6% 48.9% 50.3% 51.5% 52.7% R-1234yf 11.9% 11.2% 10.5% 9.9% 9.2% 8.7% 8.1%

    Example 34 (Quaternary Compositions Comprising 4 Weight % CO.SUB.2.)

    [0170]

    TABLE-US-00039 Nominal composition (% mass) R-1132a 5 5 5 5 5 5 5 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 55 53 51 49 47 45 43 Worst-Case Formulation (% mass) R-1132a 5.5 5.5 5.5 5.5 5.5 5.5 5.5 R-744 3.5 3.5 3.5 3.5 3.5 3.5 3.5 R-32 35 37 39 41 43 45 47 R-1234yf 56 54 52 50 48 46 44 Worst-Case Flammable Formulation (% volume) R-1132a 19.9% 19.4% 19.0% 18.6% 18.3% 17.9% 17.6% R-744 25.7% 25.3% 25.0% 24.6% 24.3% 23.9% 23.6% R-32 43.2% 44.6% 46.0% 47.4% 48.7% 50.0% 51.2% R-1234yf 11.3% 10.6% 10.0% 9.4% 8.8% 8.2% 7.7% Nominal composition (% mass) R-1132a 6 6 6 6 6 6 6 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 54 52 50 48 46 44 42 Worst-Case Formulation (% mass) R-1132a 6.5 6.5 6.5 6.5 6.5 6.5 6.5 R-744 3.5 3.5 3.5 3.5 3.5 3.5 3.5 R-32 35 37 39 41 43 45 47 R-1234yf 55 53 51 49 47 45 43 Worst-Case Flammable Formulation (% volume) R-1132a 22.7% 22.2% 21.8% 21.3% 20.9% 20.5% 20.1% R-744 24.9% 24.5% 24.2% 23.9% 23.5% 23.2% 22.9% R-32 41.8% 43.2% 44.6% 46.0% 47.3% 48.5% 49.7% R-1234yf 10.7% 10.1% 9.5% 8.9% 8.3% 7.8% 7.3%

    Example 35 (Quaternary Compositions Comprising 4 Weight % CO.SUB.2.)

    [0171]

    TABLE-US-00040 Nominal composition (% mass) R-1132a 7 7 7 7 7 7 7 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 53 51 49 47 45 43 41 Worst-Case Formulation (% mass) R-1132a 7.5 7.5 7.5 7.5 7.5 7.5 7.5 R-744 3.5 3.5 3.5 3.5 3.5 3.5 3.5 R-32 35 37 39 41 43 45 47 R-1234yf 54 52 50 48 46 44 42 Worst-Case Flammable Formulation (% volume) R-1132a 25.3% 24.8% 24.3% 23.8% 23.4% 23.0% 22.5% R-744 24.1% 23.8% 23.4% 23.1% 22.8% 22.6% 22.3% R-32 40.5% 41.9% 43.3% 44.6% 45.9% 47.1% 48.3% R-1234yf 10.2% 9.6% 9.0% 8.4% 7.9% 7.4% 6.9% Nominal composition (% mass) R-1132a 8 8 8 8 8 8 8 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 52 50 48 46 44 42 40 Worst-Case Formulation (% mass) R-1132a 8.5 8.5 8.5 8.5 8.5 8.5 8.5 R-744 3.5 3.5 3.5 3.5 3.5 3.5 3.5 R-32 35 37 39 41 43 45 47 R-1234yf 53 51 49 47 45 43 41 Worst-Case Flammable Formulation (% volume) R-1132a 27.8% 27.2% 26.7% 26.2% 25.7% 25.2% 24.8% R-744 23.3% 23.0% 22.7% 22.5% 22.1% 21.9% 21.6% R-32 39.2% 40.7% 42.0% 43.3% 44.6% 45.8% 47.0% R-1234yf 9.7% 9.1% 8.6% 8.0% 7.5% 7.0% 6.6%

    Example 36 (Quaternary Compositions Comprising 4 Weight % CO.SUB.2.)

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    TABLE-US-00041 Nominal composition (% mass) R-1132a 9 9 9 9 9 9 9 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 51 49 47 45 43 41 39 Worst-Case Formulation (% mass) R-1132a 9.5 9.5 9.5 9.5 9.5 9.5 9.5 R-744 3.5 3.5 3.5 3.5 3.5 3.5 3.5 R-32 35 37 39 41 43 45 47 R-1234yf 52 50 48 46 44 42 40 Worst-Case Flammable Formulation (% volume) R-1132a 30.1% 29.5% 29.0% 28.4% 27.9% 27.4% 26.9% R-744 22.7% 22.3% 22.1% 21.8% 21.6% 21.3% 21.1% R-32 38.1% 39.5% 40.8% 42.1% 43.4% 44.6% 45.7% R-1234yf 9.2% 8.7% 8.1% 7.6% 7.1% 6.7% 6.2% Nominal composition (% mass) R-1132a 10 10 10 10 10 10 10 R-744 4 4 4 4 4 4 4 R-32 36 38 40 42 44 46 48 R-1234yf 50 48 46 44 42 40 38 Worst-Case Formulation (% mass) R-1132a 10.5 10.5 10.5 10.5 10.5 10.5 10.5 R-744 3.5 3.5 3.5 3.5 3.5 3.5 3.5 R-32 35 37 39 41 43 45 47 R-1234yf 51 49 47 45 43 41 39 Worst-Case Flammable Formulation (% volume) R-1132a 32.3% 31.6% 31.1% 30.6% 30.0% 29.5% 29.0% R-744 22.0% 21.7% 21.5% 21.3% 21.0% 20.8% 20.5% R-32 37.0% 38.4% 39.7% 41.0% 42.2% 43.4% 44.6% R-1234yf 8.8% 8.3% 7.7% 7.3% 6.8% 6.3% 5.9%

    Example 37 (Quaternary Compositions Comprising 5 Weight % CO.SUB.2.)

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    TABLE-US-00042 Nominal composition (% mass) R-1132a 4 4 4 4 4 4 4 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 55 53 51 49 47 45 43 Worst-Case Formulation (% mass) R-1132a 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-744 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-32 35 37 39 41 43 45 47 R-1234yf 56 54 52 50 48 46 44 Worst-Case Flammable Formulation (% volume) R-1132a 15.6% 15.3% 15.0% 14.7% 14.4% 14.1% 13.9% R-744 31.9% 31.4% 31.0% 30.6% 30.2% 29.8% 29.4% R-32 41.6% 43.1% 44.4% 45.8% 47.0% 48.2% 49.4% R-1234yf 10.8% 10.2% 9.6% 9.0% 8.4% 7.9% 7.4% Nominal composition (% mass) R-1132a 5 5 5 5 5 5 5 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 54 52 50 48 46 44 42 Worst-Case Formulation (% mass) R-1132a 5.5 5.5 5.5 5.5 5.5 5.5 5.5 R-744 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-32 35 37 39 41 43 45 47 R-1234yf 55 53 51 49 47 45 43 Worst-Case Flammable Formulation (% volume) R-1132a 18.5% 18.1% 17.8% 17.4% 17.1% 16.8% 16.4% R-744 30.9% 30.5% 30.1% 29.7% 29.3% 28.9% 28.5% R-32 40.3% 41.7% 43.1% 44.4% 45.7% 46.9% 48.0% R-1234yf 10.3% 9.7% 9.1% 8.5% 8.0% 7.5% 7.0%

    Example 38 (Quaternary Compositions Comprising 5 Weight % CO.SUB.2.)

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    TABLE-US-00043 Nominal composition (% mass) R-1132a 6 6 6 6 6 6 6 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 53 51 49 47 45 43 41 Worst-Case Formulation (% mass) R-1132a 6.5 6.5 6.5 6.5 6.5 6.5 6.5 R-744 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-32 35 37 39 41 43 45 47 R-1234yf 54 52 50 48 46 44 42 Worst-Case Flammable Formulation (% volume) R-1132a 21.2% 20.7% 20.3% 20.0% 19.6% 19.2% 18.9% R-744 29.9% 29.5% 29.2% 28.8% 28.4% 28.1% 27.8% R-32 39.1% 40.5% 41.9% 43.2% 44.4% 45.6% 46.7% R-1234yf 9.8% 9.2% 8.7% 8.1% 7.6% 7.1% 6.6% Nominal composition (% mass) R-1132a 7 7 7 7 7 7 7 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 52 50 48 46 44 42 40 Worst-Case Formulation (% mass) R-1132a 7.5 7.5 7.5 7.5 7.5 7.5 7.5 R-744 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-32 35 37 39 41 43 45 47 R-1234yf 53 51 49 47 45 43 41 Worst-Case Flammable Formulation (% volume) R-1132a 23.7% 23.2% 22.8% 22.4% 21.9% 21.6% 21.2% R-744 29.1% 28.7% 28.3% 28.0% 27.7% 27.3% 27.0% R-32 38.0% 39.4% 40.7% 42.0% 43.2% 44.4% 45.5% R-1234yf 9.3% 8.8% 8.2% 7.7% 7.2% 6.8% 6.3%

    Example 39 (Quaternary Compositions Comprising 5 Weight % CO.SUB.2.)

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    TABLE-US-00044 Nominal composition (% mass) R-1132a 8 8 8 8 8 8 8 R-744 5 5 5 5 5 5 5 R-32 36 38 40 42 44 46 48 R-1234yf 51 49 47 45 43 41 39 Worst-Case Formulation (% mass) R-1132a 8.5 8.5 8.5 8.5 8.5 8.5 8.5 R-744 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-32 35 37 39 41 43 45 47 R-1234yf 52 50 48 46 44 42 40 Worst-Case Flammable Formulation (% volume) R-1132a 26.0% 25.5% 25.0% 24.6% 24.2% 23.8% 23.4% R-744 28.1% 27.9% 27.5% 27.2% 26.9% 26.6% 26.3% R-32 36.9% 38.3% 39.6% 40.8% 42.0% 43.2% 44.3% R-1234yf 8.9% 8.4% 7.9% 7.4% 6.9% 6.4% 6.0% Nominal composition (% mass) R-1132a 9 9 9 9 9 9 9 R-744 5 5 5 5 5 5 5 R-32 46 46 46 46 46 46 46 R-1234yf 40 40 40 40 40 40 40 Worst-Case Formulation (% mass) R-1132a 9.5 9.5 9.5 9.5 9.5 9.5 9.5 R-744 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-32 45 45 45 45 45 45 45 R-1234yf 41 41 41 41 41 41 41 Worst-Case Flammable Formulation (% volume) R-1132a 25.9% 25.9% 25.9% 25.9% 25.9% 25.9% 25.9% R-744 26.0% 26.0% 26.0% 26.0% 26.0% 26.0% 26.0% R-32 42.1% 42.1% 42.1% 42.1% 42.1% 42.1% 42.1% R-1234yf 6.1% 6.1% 6.1% 6.1% 6.1% 6.1% 6.1%

    Example 40 (Quaternary Compositions Comprising 5 Weight % CO.SUB.2.)

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    TABLE-US-00045 Nominal composition (% mass) R-1132a 10 10 10 10 10 10 10 R-744 5 5 5 5 5 5 5 R-32 46 46 46 46 46 46 46 R-1234yf 39 39 39 39 39 39 39 Worst-Case Formulation (% mass) R-1132a 10.5 10.5 10.5 10.5 10.5 10.5 10.5 R-744 4.5 4.5 4.5 4.5 4.5 4.5 4.5 R-32 45 45 45 45 45 45 45 R-1234yf 40 40 40 40 40 40 40 Worst-Case Flammable Formulation (% volume) R-1132a 27.8% 27.8% 27.8% 27.8% 27.8% 27.8% 27.8% R-744 25.3% 25.3% 25.3% 25.3% 25.3% 25.3% 25.3% R-32 41.1% 41.1% 41.1% 41.1% 41.1% 41.1% 41.1% R-1234yf 5.8% 5.8% 5.8% 5.8% 5.8% 5.8% 5.8%