发明名称 Transcritical fluid cooling for aerospace applications
摘要 A cooling system includes a compressor for compressing a refrigerant from a subcritical state to a supercritical state, a cooler for transferring heat from the refrigerant, an expander for expanding the refrigerant in the supercritical state, an expansion valve for expanding the refrigerant from the supercritical state to the subcritical state and an evaporator for transferring heat from a cooling fluid to the refrigerant in the subcritical state. Work extracted by the expander provides power to the compressor. A method for cooling a vehicle includes compressing a refrigerant from a subcritical state to a supercritical state, cooling the refrigerant, expanding the refrigerant in the supercritical state where work produced by expanding the refrigerant is used to compress the refrigerant, expanding the refrigerant from the supercritical state to the subcritical state, cooling a cooling fluid with the refrigerant in the subcritical state and cooling vehicle components with the cooling fluid.
申请公布号 US8327651(B2) 申请公布日期 2012.12.11
申请号 US20090498744 申请日期 2009.07.07
申请人 FINNEY ADAM M.;PARK YOUNG K.;KASLUSKY SCOTT F.;SABATINO DANIEL R.;HAMILTON SUNDSTRAND CORPORATION 发明人 FINNEY ADAM M.;PARK YOUNG K.;KASLUSKY SCOTT F.;SABATINO DANIEL R.
分类号 F25B9/00 主分类号 F25B9/00
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