- 专利标题: HYDRAULIC CYLINDER FOR AIRCRAFT LANDING GEAR
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申请号: US15244743申请日: 2016-08-23
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公开(公告)号: US20170088256A1公开(公告)日: 2017-03-30
- 发明人: Taku Kondo , Takaaki Onishi , Shogo Hagihara
- 申请人: SUMITOMO PRECISION PRODUCTS CO., LTD.
- 优先权: JP2015-194249 20150930
- 主分类号: B64C25/22
- IPC分类号: B64C25/22 ; F15B15/14 ; F15B15/22
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
- US10214280B2 Hydraulic cylinder for aircraft landing gear 公开/授权日:2019-02-26
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