| 发明名称 |
THERMAL MANAGEMENT SYSTEM FOR GAS TURBINE ENGINE |
| 摘要 |
A method of thermal management for a gas turbine engine comprising selectively positioning a valve to communicate a bypass flow into either an Environmental Control System (ECS) pre-cooler or an Air Oil Cooler (AOC) “peaker” through a common inlet. |
| 申请公布号 |
US2015052907(A1) |
申请公布日期 |
2015.02.26 |
| 申请号 |
US201414533611 |
申请日期 |
2014.11.05 |
| 申请人 |
United Technologies Corporation |
发明人 |
Murphy Michael Joseph |
| 分类号 |
F02C7/14;F01D25/12 |
主分类号 |
F02C7/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of thermal management for a gas turbine engine comprising:
selectively positioning a valve to communicate a bypass flow into either an Environmental Control System (ECS) pre-cooler or an Air Oil Cooler (AOC) “peaker” through a common inlet. |
| 地址 |
Hartford CT US |
