发明名称 Aircraft engine mounting
摘要 An aircraft engine mounting assembly comprising a bracket arrangement with two plates located either side of an opening in the structural bypass duct. The bracket arrangement mounts two inclined links which connect to the engine. In normal usage, tension/compression from the links will be passed by the bracket arrangement into the airframe. Upon failure of one of the links the bracket arrangement will engage with the structural bypass duct to transmit engine loads into the airframe via the duct.
申请公布号 US2005230532(A1) 申请公布日期 2005.10.20
申请号 US20040001122 申请日期 2004.12.02
申请人 STRETTON RICHARD G;THOMPSON EWAN F 发明人 STRETTON RICHARD G.;THOMPSON EWAN F.
分类号 B64D27/26;(IPC1-7):B64D27/12 主分类号 B64D27/26
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