发明名称 Shrink shock strut locking mechanism for retractable aircraft landing gear
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.
申请公布号 US2012056035(A1) 申请公布日期 2012.03.08
申请号 US20100807538 申请日期 2010.09.08
申请人 LUCE WILLIAM E.;GOODRICH CORPORATION 发明人 LUCE WILLIAM E.
分类号 B64C25/26 主分类号 B64C25/26
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