MOUNT MECHANISM FOR ACCESSORY GEARBOX
    1.
    发明公开
    MOUNT MECHANISM FOR ACCESSORY GEARBOX 审中-公开
    附件齿轮箱的安装机构

    公开(公告)号:EP3296215A1

    公开(公告)日:2018-03-21

    申请号:EP15891748.4

    申请日:2015-05-08

    IPC分类号: B64D41/00 B64D27/26 F02C7/32

    摘要: A mount mechanism used to mount an accessory gear box on an engine case in an aircraft engine, includes a pair of first brackets fastened to one of the engine case and the accessory gear box, the pair of first brackets being apart from each other in a circumferential direction of the engine case; a link extending in such a manner that the pair of first brackets are connected to each other via the link, both end portions of the link being coupled to the pair of first brackets by a pair of first pins, respectively; an annular anti-vibration element penetrated by each of the pair of first pins, the annular anti-vibration element being retained by at least one of each of the pair of first brackets and the end portion of the link; and a second bracket fastened to the other of the engine case and the accessory gear box, the second bracket box being coupled to the link by a second pin at a location between the pair of first brackets.

    摘要翻译: 一种用于将附件齿轮箱安装在飞机发动机的发动机箱上的安装机构,包括:一对第一支架,所述一对第一支架紧固到所述发动机箱和所述附件齿轮箱中的一个,所述一对第一支架彼此分开 发动机壳体的周向; 所述连杆以所述一对第一托架经由所述连杆彼此连接的方式延伸,所述连杆的两个端部分别通过一对第一销连接至所述一对第一托架; 所述一对第一销中的每一个穿过所述环形抗振元件,所述环形抗振元件由所述一对第一支架中的每一个和所述连杆的所述端部中的至少一个保持; 以及固定到发动机壳体和附件齿轮箱中的另一个上的第二托架,第二托架箱通过第二销在一对第一托架之间的位置处连接到连杆。