发明名称 |
ROTATABLE SCARF INLET FOR AN AIRCRAFT ENGINE AND METHOD OF USING THE SAME |
摘要 |
A rotatable scarf inlet for an engine and a method of operating a jet aircraft engine on an aircraft. The rotatable scarf inlet is rotatably supported at a forward end portion of a nacelle of the engine. The rotatable scarf inlet is controllably rotatable relative to the engine nacelle to a plurality of angular positions to inhibit ingestion of foreign object debris or to improve airflow characteristics, depending on whether the aircraft is taxiing, taking off from a runway, or operating in a cruise condition. The method involves controllably rotating the rotatable scarf inlet with respect to the engine nacelle to a corresponding one of the plurality of angular positions.
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申请公布号 |
US2004113014(A1) |
申请公布日期 |
2004.06.17 |
申请号 |
US20020316497 |
申请日期 |
2002.12.11 |
申请人 |
SANKRITHI MITHRA M.K.V.;NELSON PAUL E. |
发明人 |
SANKRITHI MITHRA M.K.V.;NELSON PAUL E. |
分类号 |
B64D33/02;F02C7/042;(IPC1-7):B64C27/22 |
主分类号 |
B64D33/02 |
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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