发明授权
US08469165B2 Interconnecting strut for arranging between adjacent landing flaps of an aircraft
失效
互连支柱,用于在飞机的相邻着陆襟翼之间进行排列
- 专利标题: Interconnecting strut for arranging between adjacent landing flaps of an aircraft
- 专利标题(中): 互连支柱,用于在飞机的相邻着陆襟翼之间进行排列
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申请号: US12226622申请日: 2007-04-27
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公开(公告)号: US08469165B2公开(公告)日: 2013-06-25
- 发明人: Susanne Versluis
- 申请人: Susanne Versluis
- 申请人地址: DE Hamburg
- 专利权人: Airbus Deutschland GmbH
- 当前专利权人: Airbus Deutschland GmbH
- 当前专利权人地址: DE Hamburg
- 代理机构: Greer, Burns & Crain, Ltd.
- 优先权: DE102006020554 20060503
- 国际申请: PCT/EP2007/054136 WO 20070427
- 国际公布: WO2007/128708 WO 20071115
- 主分类号: F16F7/12
- IPC分类号: F16F7/12
摘要:
An interconnecting strut includes two coaxially arranged strut elements which may be displaced relative to one another in the longitudinal direction of the interconnecting strut, two end stops defining the mutual displaceability of the two strut elements, as well as damping elements, which when a specific permissible displacement is exceeded, damp the displacement movement of the strut elements before reaching the end stops, in which the damping elements consist of a material which is plastically deformable in the occurring force range, the damping elements being compressed for damping the displacement movement in the longitudinal direction and, at the same time, being subjected to a cross-sectional enlargement transversely to the longitudinal direction, due to the compression.
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