| 发明名称 |
GAS TURBINE ENGINE BUFFER SYSTEM |
| 摘要 |
<p>A gas turbine engine includes a buffer system. The buffer system can include a first bleed air supply and a conditioning device that conditions the first bleed air supply to render the buffer supply air at an acceptable temperature to anti-ice the hardware of said fan section.</p> |
| 申请公布号 |
EP2809910(A1) |
申请公布日期 |
2014.12.10 |
| 申请号 |
EP20130775763 |
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;F02C7/06;F02C7/141 |
主分类号 |
F02C6/08 |
| 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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