发明名称 |
Thermal management system for gas turbine engine |
摘要 |
A thermal management system (68) for a gas turbine engine (20) includes a first heat exchanger (HX1) and a second heat exchanger (HX2) in communication with a bypass flow through an inlet (70). A valve (72) is operable to selectively communicate the bypass flow to either the first heat exchanger or the second heat exchanger through the inlet. |
申请公布号 |
EP2546472(A3) |
申请公布日期 |
2015.12.23 |
申请号 |
EP20120162781 |
申请日期 |
2012.03.30 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
MURPHY, MICHAEL J. |
分类号 |
F02C7/14;F01D17/08;F01D25/12;F02C7/18 |
主分类号 |
F02C7/14 |
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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