发明公开
- 专利标题: HYDRAULIC CYLINDER FOR AIRCRAFT LANDING GEAR
- 专利标题(中): 液压油ZYLINDERFÜRFLUGZEUGFAHRWERK
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申请号: EP16189261.7申请日: 2016-09-16
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公开(公告)号: EP3150863A1公开(公告)日: 2017-04-05
- 发明人: KONDO, Taku , ONISHI, Takaaki , HAGIHARA, Shogo
- 申请人: Sumitomo Precision Products Co., Ltd.
- 申请人地址: 1-10 Fuso-cho Amagasaki -shi Hyogo 660-0891 JP
- 专利权人: Sumitomo Precision Products Co., Ltd.
- 当前专利权人: Sumitomo Precision Products Co., Ltd.
- 当前专利权人地址: 1-10 Fuso-cho Amagasaki -shi Hyogo 660-0891 JP
- 代理机构: BRP Renaud & Partner mbB Rechtsanwälte Patentanwälte Steuerberater
- 优先权: JP2015194249 20150930
- 主分类号: F15B15/22
- 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.
公开/授权文献
- EP3150863B1 HYDRAULIC CYLINDER FOR AIRCRAFT LANDING GEAR 公开/授权日:2021-07-21
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