- 专利标题: Lead-lag damper integrated inside a blade of a rotor
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申请号: US15728750申请日: 2017-10-10
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公开(公告)号: US11142307B2公开(公告)日: 2021-10-12
- 发明人: Stephane Mazet , Jean-Romain Bihel , Mathias Fournier , Sylvain Berthalon
- 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: FR1601495 20161014
- 主分类号: B64C27/51
- IPC分类号: B64C27/51 ; B64C27/00 ; B64C27/35 ; B64C27/48
摘要:
A lead-lag damper arranged inside a blade of a rotor of a rotary wing aircraft. The lead-lag damper comprises an inner strength member provided with a cage in which a ball-joint connection is arranged, an outer strength member for securing to the blade, and an elastomer material member arranged between the two strength members. The two strength members and the elastomer material member extending beyond the zone around the cage so that the relative movements between two strength members resulting from the movements of the blade are damped by deformations of the elastomer material member, at least a portion of the lead-lag damper being designed to occupy a portion of the inside of the blade that is conventionally filled with foam.
公开/授权文献
- US20180105265A1 LEAD-LAG DAMPER INTEGRATED INSIDE A BLADE OF A ROTOR 公开/授权日:2018-04-19
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