发明公开
- 专利标题： Hybrid cooling system for aircraft applications
- 专利标题（中）： 混合散热系统为飞机的应用
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申请号： EP10251913.9申请日： 2010-11-10
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公开(公告)号： EP2319761A3公开(公告)日： 2014-05-14
- 发明人: Bruno, Louis J. , Christians, Douglas L
- 申请人： Hamilton Sundstrand Corporation
- 申请人地址： One Hamilton Road Windsor Locks, CT 06096 US
- 专利权人： Hamilton Sundstrand Corporation
- 当前专利权人： Hamilton Sundstrand Corporation
- 当前专利权人地址： One Hamilton Road Windsor Locks, CT 06096 US
- 代理机构： Tomlinson, Kerry John
- 优先权： US615656 20091110
- 主分类号： B64D13/06
- IPC分类号： B64D13/06
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.
公开/授权文献
- EP2319761B1 Hybrid cooling system for aircraft applications 公开/授权日：2016-08-31
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