发明名称 Aircraft engine mounting structure, assembly comprising this structure and associated aircraft
摘要 An engine is suspended from a main linear portion of a structure mounted on a fuselage or a wing surface of an aircraft. A connection includes flat symmetrical wings at an angle to one another, to support an attaching flange on which the engine is mounted, directly or through a mounting element. The flat shape of the wings makes them easy to manufacture, and enables them to resist the forces satisfactorily. The intermediate element resists overhang forces of the mounting satisfactorily. Flexible connections filter the engine's vibrations and prevent irregular forces being transmitted.
申请公布号 US8640987(B2) 申请公布日期 2014.02.04
申请号 US201013496102 申请日期 2010.09.20
申请人 JOURNADE FREDERIC;LAFONT LAURENT;AGOSTINI LAURENT;RENAUD ERIC;JALBERT DELPHINE;AIRBUS OPERATIONS S.A.S. 发明人 JOURNADE FREDERIC;LAFONT LAURENT;AGOSTINI LAURENT;RENAUD ERIC;JALBERT DELPHINE
分类号 B64D27/00 主分类号 B64D27/00
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