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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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