| 发明名称 |
GAS TURBINE ENGINE WITH PLURAL ACCESSORY AIR PATHS |
| 摘要 |
A gas turbine engine has a first source of air to be delivered into a core of the engine, and a second source of air, distinct from the first source of air and including separately controlled first and second fans, each delivering air into respective first and second conduits connected to distinct auxiliary applications. |
| 申请公布号 |
EP2929163(A1) |
申请公布日期 |
2015.10.14 |
| 申请号 |
EP20130862641 |
申请日期 |
2013.06.20 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;CHANDLER, JESSE M. |
| 分类号 |
B64D13/06;F01D25/12;F02C6/08;F02C7/18;F02C9/18;F02K3/00 |
主分类号 |
B64D13/06 |
| 代理机构 |
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代理人 |
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