发明名称 Hybrid cooling system for aircraft applications
摘要 An aircraft cooling system includes a refrigerant cycle (22) including a first heat exchanger (26). A liquid cycle passes a liquid through the first heat exchanger (26), at which it is cooled by a refrigerant in the refrigerant cycle. An air cycle compresses (42) air and delivers the compressed air into a second heat exchanger (48). The liquid passes through the second heat exchanger at a location downstream of the first heat exchanger. The liquid cools the air in the second heat exchanger. Air downstream of the second heat exchanger passes to be utilized by a use (58) on an aircraft.
申请公布号 EP2319761(A2) 申请公布日期 2011.05.11
申请号 EP20100251913 申请日期 2010.11.10
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 BRUNO, LOUIS J.;CHRISTIANS, DOUGLAS L
分类号 B64D13/06 主分类号 B64D13/06
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