| 发明名称 |
GAS TURBINE ENGINE BUFFER SYSTEM PROVIDING ZONED VENTILATION |
| 摘要 |
A gas turbine engine includes a first zone and a second zone downstream from the first zone. A buffer system can communicate a buffer cooling air to at least the first zone. A bleed source can communicate a bleed air to the second zone. |
| 申请公布号 |
EP2809909(A4) |
申请公布日期 |
2015.10.07 |
| 申请号 |
EP20130775635 |
申请日期 |
2013.01.16 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
ACKERMANN, WILLIAM K.;STRIPINIS, PHILIP S. |
| 分类号 |
F02C6/08;F01D5/08;F01D25/18;F02C7/18 |
主分类号 |
F02C6/08 |
| 代理机构 |
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代理人 |
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