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References in periodicals archive ?
The impact on refrigerant temperatures resulted in increases of compressor discharge temperature of 32.3[degrees]C.
It should be noted that the high pressure ratios associated with simple-cycle (i.e., no intercooler or recuperator), aircraft-derivative engines can lead to compressor discharge temperatures almost as high as the gas temperatures exiting the low pressure turbine.
However, these alternatives, especially R32, are subject to significant increases in compressor discharge temperature.
The compressor discharge temperature is the temperature of the superheated refrigerant at the exit of the compressor.
It can also be seen from Figure 4 that intercooling is only possible when the intermediate pressure is high enough so that the first-stage compressor discharge temperature is higher than the outdoor, i.e., gas cooler, exit temperature.
The test results show R32 compared to R410A was superior in regards to cooling and heating capacities, L41A compared to R410A was superior in regards to COP, D2Y60 compared to R410A was superior in regards to compressor discharge temperature, L41A was superior in terms of SEER and HSPF values compared to other alternative refrigerants.
They found that this compressor technology increases both the heating capacity and the COP of the system whereas it reduces the compressor discharge temperature. Moreover, the authors stated that these improvements are negligible when the evaporating temperature becomes higher than -10[degrees]C.
Finally, it should be noted that compressor discharge temperatures with R-516A ran about 10[degrees]Fd (6[degrees]Cd) lower than those with R-134a.
"Our customers have found Forane[R] 427A refrigerant to match R-22's capacity and efficiency closely, while reducing compressor discharge temperatures."
According to O'Shea, the HFC and ISCEON refrigerants have lower compressor discharge temperatures than HCFC refrigerants like R22.
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