HYDRAULIC CYLINDER FOR AIRCRAFT LANDING GEAR
    1.
    发明公开
    HYDRAULIC CYLINDER FOR AIRCRAFT LANDING GEAR 审中-公开
    液压油ZYLINDERFÜRFLUGZEUGFAHRWERK

    公开(公告)号:EP3150863A1

    公开(公告)日:2017-04-05

    申请号:EP16189261.7

    申请日:2016-09-16

    IPC分类号: F15B15/22 B64C25/22

    摘要: A hydraulic cylinder includes: a cylinder tube; a piston; a piston rod; a pair of end covers; and a snubbing mechanism configured to reduce the moving speed of the piston after the piston reaches the vicinity of the end of its stroke. The snubbing mechanism includes: a supply/discharge port formed in an associated one of the end covers; a valve configured to open and close the supply/discharge port; a connector configured to connect the valve and the piston together; and at least one recess extending from the edge of the supply/discharge port. When the piston approaches the end of its stroke, the valve closes the supply/discharge port to form a throttle oil passage, and hydraulic oil is discharged through the throttle oil passage to reduce the moving speed of the piston.

    摘要翻译: 液压缸包括:缸筒; 活塞 活塞杆 一对端盖; 以及缓冲机构,其构造成在活塞到达其行程结束的附近之后减小活塞的移动速度。 缓冲机构包括:形成在相关一个端盖中的供给/排出口; 构造成打开和关闭供给/排出口的阀; 连接器,其构造成将所述阀和所述活塞连接在一起; 以及从供给/排出口的边缘延伸的至少一个凹部。 当活塞接近行程结束时,阀关闭供油/排出口,形成节流油通道,液压油通过节流油通道排出,以降低活塞的移动速度。