BRAKE ACTUATOR FOR AN AIRCRAFT WHEEL HYDRAULIC BRAKE
    1.
    发明申请
    BRAKE ACTUATOR FOR AN AIRCRAFT WHEEL HYDRAULIC BRAKE 有权
    制动器制动器用于航空轮液压制动

    公开(公告)号:US20150275992A1

    公开(公告)日:2015-10-01

    申请号:US14645792

    申请日:2015-03-12

    Abstract: A brake actuator comprising a sleeve (1), a piston (3) sealingly slidably mounted in the sleeve to apply a braking force, the piston being provided with an internal cage (21), and a wear compensating device (10) which defines a retracted position of the piston in the sleeve by means of an axially mobile stop which is able to be moved forward by the piston during the application of a braking force and/in frictional relationship with a fixed part (12) of the wear compensating device attached to the sleeve. The mobile stop comprises a radially deformable bushing (16) which cooperates with an olive (15) which is attached to a distal end of the fixed part of the wear compensating device. The bushing comprises means for guiding its proximal end (17) against an internal face of the internal cage (21).

    Abstract translation: 一种制动致动器,包括套筒(1),密封地可滑动地安装在套筒中以施加制动力的活塞(3),所述活塞设置有内部保持架(21),以及磨损补偿装置(10) 活塞在套筒中的缩回位置借助于轴向移动的止挡件,该止动件能够在施加制动力期间由活塞向前移动,并且与附接的磨损补偿装置的固定部件(12)成摩擦关系 到袖子。 移动式止动件包括可径向变形的衬套(16),该衬套与附接到磨损补偿装置的固定部分的远端的橄榄(15)配合。 衬套包括用于将其近端(17)引导到内部保持架(21)的内表面的装置。

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