发明名称 Rear engine redundant mount
摘要 An airframe mounted jet engine has a three point support including a front engine mount located on the longitudinal axis of the engine and lateral inboard and outboard rear engine mounts. A redundant rear mount is provided beneath the engine in the vertical plane including the longitudinal axis of the engine which normally does not contribute any significant support for the engine but which, in the event of failure of either one of the two lateral rear mounts, cooperates with the other rear mount to provide a provisional rear support for the engine.
申请公布号 US3907220(A) 申请公布日期 1975.09.23
申请号 US19740451661 申请日期 1974.03.14
申请人 UNITED AIRCRAFT CORPORATION 发明人 AMELIO, ARMAND FRANCIS
分类号 F02K99/00;B64D27/18;B64D27/26;B64D33/04;F16M7/00;(IPC1-7):B64D27/16 主分类号 F02K99/00
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