Invention Grant
- Patent Title: Shrink shock strut locking mechanism for retractable aircraft landing gear
- Patent Title (中): 收缩式起落架收缩冲击支柱锁定机构
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Application No.: US12807538Application Date: 2010-09-08
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Publication No.: US08727273B2Publication Date: 2014-05-20
- Inventor: William E. Luce
- Applicant: William E. Luce
- Applicant Address: US NC Charlotte
- Assignee: Goodrich Corporation
- Current Assignee: Goodrich Corporation
- Current Assignee Address: US NC Charlotte
- Agency: Snell & Wilmer L.L.P.
- Main IPC: B64C25/26
- IPC: B64C25/26

Abstract:
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.
Public/Granted literature
- US20120056035A1 Shrink shock strut locking mechanism for retractable aircraft landing gear Public/Granted day:2012-03-08
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