- 专利标题: Hydro-elastic damper and an aircraft
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申请号: US16369546申请日: 2019-03-29
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公开(公告)号: US11161601B2公开(公告)日: 2021-11-02
- 发明人: Jean-Romain Bihel , Damien Sequera , Jean-Pierre Jalaguier
- 申请人: AIRBUS HELICOPTERS
- 申请人地址: FR Marignane
- 专利权人: AIRBUS HELICOPTERS
- 当前专利权人: AIRBUS HELICOPTERS
- 当前专利权人地址: FR Marignane
- 代理机构: Brooks Kushman P.C.
- 优先权: FR1870369 20180330
- 主分类号: B64C27/00
- IPC分类号: B64C27/00 ; F16F13/08 ; B64C27/51
摘要:
A hydro-elastic damper comprising at least one elastic assembly comprising an elastic member between two strength members. The elastic assembly including a compression chamber. The hydro-elastic damper includes a damping assembly provided with an expansion chamber that is defined in a transverse direction by an end wall and by a piston. The compression chamber is hydraulically connected to the expansion chamber by three hydraulic connections comprising respectively: a duct; at least one first passage with an overpressure valve; and at least one second passage with a check valve.
公开/授权文献
- US20190300163A1 HYDRO-ELASTIC DAMPER AND AN AIRCRAFT 公开/授权日:2019-10-03
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