发明名称 AFT ENGINE MOUNT
摘要 The engine is mounted on a wing strut (10), at a preset spacing from the wing. A low-profile engine mount is attachable to the strut and engine to secure the two, whilst occupying a minium of the engine-wing spacing. The mount accommodates longitudinal growth of the engine due to thermal expansion, but is stiff enough to react against vertical, side and torque loads. The mounting comprises a yoke with two arms (56), mounted on the strut to permit pivoting. The arms are secured to an engine mounting ring (38) on the engine. Links (48, 54) between the engine ring and arms include universal joints. engine.
申请公布号 DE3374545(D1) 申请公布日期 1987.12.23
申请号 DE19833374545 申请日期 1983.12.08
申请人 THE BOEING COMPANY 发明人 CHEE, WAN, TONY
分类号 B64D27/26;F02C7/20;(IPC1-7):B64D27/00 主分类号 B64D27/26
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