发明名称 |
Nacelle with porous surfaces |
摘要 |
A fan nacelle (34) for a gas turbine engine includes a leading edge region (40) with a flow path (42) between an intake region (48) in a nacelle outer surface (44) and an exhaust region (50) in a nacelle inner surface (46) to locally modify a flow around the leading edge region (40) during a predefined off-design condition. |
申请公布号 |
EP2434095(A2) |
申请公布日期 |
2012.03.28 |
申请号 |
EP20110182894 |
申请日期 |
2011.09.27 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
ATASSI, OLIVER V. |
分类号 |
F01D5/14;B64D33/02;F01D5/28;F02C7/04;F02K3/04;F02K3/06 |
主分类号 |
F01D5/14 |
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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