发明授权
- 专利标题: Shrink shock strut locking mechanism for retractable aircraft landing gear
- 专利标题(中): 收缩式起落架收缩冲击支柱锁定机构
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申请号: US12807538申请日: 2010-09-08
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公开(公告)号: US08727273B2公开(公告)日: 2014-05-20
- 发明人: William E. Luce
- 申请人: William E. Luce
- 申请人地址: US NC Charlotte
- 专利权人: Goodrich Corporation
- 当前专利权人: Goodrich Corporation
- 当前专利权人地址: US NC Charlotte
- 代理机构: Snell & Wilmer L.L.P.
- 主分类号: B64C25/26
- IPC分类号: B64C25/26
摘要:
A shrink shock strut assembly for retractable aircraft landing gear is disclosed which includes an elongated strut cylinder, an elongated strut piston coaxially mounted for reciprocal movement within the strut cylinder between a shrunk condition when the landing gear is retracted into a wheel well of an aircraft and a fully extended condition when the landing gear is deployed from the wheel well for landing the aircraft, and a blocking mechanism operatively associated with the strut cylinder and mounted for movement into a blocking position with respect to the strut piston, when the landing gear is retracted within the wheel well, to prevent axial movement of the strut piston into the fully extended condition within the wheel well.
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