发明名称 Engine attachment pylon
摘要 An engine attachment pylon for mounting an aircraft engine to an aircraft structure while minimizing vibrations induced into the engine attachment pylon during flight and operation of the engine. The engine attachment pylon comprises a rigid box like structure housing a resonator which is tuned to attenuate tension and compression vibrations experienced by the engine attachment pylon. The engine attachment pylon is primarily used in combination within another identical engine attachment pylon, both being linked together on a vertical plane within the fuselage by a hinge like junction, and each engine attachment pylon being raised approximately 30° from the horizontal axis of the fuselage.
申请公布号 US8910904(B2) 申请公布日期 2014.12.16
申请号 US201313777514 申请日期 2013.02.26
申请人 Airbus Operations (SAS) 发明人 Antypas Jerome
分类号 B64D27/02;B64D29/04;B64D27/26;B64D27/10;B64D27/14;B64D27/00 主分类号 B64D27/02
代理机构 Greer Burns & Crain, Ltd. 代理人 Greer Burns & Crain, Ltd.
主权项 1. An engine attachment pylon, for mounting an aircraft engine to an aircraft structure, comprising: a structure forming a box and comprising a first attachment member to connect to the engine and a second attachment member to connect to the fuselage; and, a dynamic mass absorber which is tuned to absorb vibrations of the aircraft engine, the dynamic mass absorber housed in the box and comprising a damping member suspended inside the structure and a lever, wherein the lever is pivotally mounted around a pivot, and connected at one end to a first end of the damping member and at the other end to a fitting mounted on one of the first attachment member or the second attachment member and wherein a second end of the damping member is attached to the other of the first attachment member or the second attachment member.
地址 Toulouse FR