发明名称 |
Gas turbine engine with active tip clearance control device and corresponding operating method |
摘要 |
<p>An active tip clearance control (ATCC) apparatus (38) of an aircraft gas turbine engine is situated within a pressurized core case (13) of the engine. First and second portions (34,42) of bypass air flow passing through a compressed core compartment (30) and the ATCC apparatus (38), are isolated from one another in order to improve both the ATCC performance and bypass air duct performance.</p> |
申请公布号 |
EP2236772(A2) |
申请公布日期 |
2010.10.06 |
申请号 |
EP20100250560 |
申请日期 |
2010.03.24 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
LEGARE, PIERRE-YVES;MAH, STEPHEN |
分类号 |
F01D11/24;F01D25/12;F02C6/08;F02K3/02 |
主分类号 |
F01D11/24 |
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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