发明名称 |
Locking mechanisms |
摘要 |
A locking mechanism for aircraft landing gear has a hook (3) displaceable into and out of engagement with the landing gear capture pin (1). A roller (45) on a latch arm (40) engages a part (36) of the hook (3) to prevent it moving from a position where the pin (1) is retained. A linear solenoid (50) and a motor-driven rotatable cam (63) can both be operated independently to move the roller (45) out of engagement with the hook (3) and thereby allow a spring (35) to rotate the hook and release the capture pin (1).
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申请公布号 |
US7883125(B2) |
申请公布日期 |
2011.02.08 |
申请号 |
US20040563602 |
申请日期 |
2004.07.02 |
申请人 |
SMITHS GROUP PLC |
发明人 |
SMITH, III REESE RANDOLPH |
分类号 |
E05C3/06;B64C25/26;E05B47/00;E05B65/12;E05C3/24 |
主分类号 |
E05C3/06 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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