发明名称 |
FLUID HEAT SINK POWERED VAPOR CYCLE SYSTEM |
摘要 |
An aircraft cooling system includes a refrigerant cycle including a first heat exchanger, a second heat exchanger, and a compressor. A component of the aircraft is in thermal communication with the first heat exchanger. A heat sink fluid passes through the second heat exchanger to absorb heat from the refrigerant cycle. A hydraulic motor is mechanically connected with the compressor and powered by the heat sink fluid, which is circulated by a pump.
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申请公布号 |
US2011219786(A1) |
申请公布日期 |
2011.09.15 |
申请号 |
US20100721598 |
申请日期 |
2010.03.11 |
申请人 |
ANDRES MICHAEL J;CAMPBELL KRIS H |
发明人 |
ANDRES MICHAEL J.;CAMPBELL KRIS H. |
分类号 |
B64D13/08;F25B23/00;F25B27/00;F25B41/00 |
主分类号 |
B64D13/08 |
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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