发明名称 |
Penguin missile folding wing configuration |
摘要 |
An over-center locking mechanism is provided for a guided missile foldable wing structure which ensures stable reliable and non-reversible locking of the foldable wing. A pyrotechnic actuator is connected to the mechanism and, upon firing, quickly operates the mechanism to a deployed condition.
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申请公布号 |
US4717093(A) |
申请公布日期 |
1988.01.05 |
申请号 |
US19850764457 |
申请日期 |
1985.08.12 |
申请人 |
GRUMMAN AEROSPACE CORPORATION |
发明人 |
ROSENBERGER, MARK A.;ETTINGER, JOHN J. |
分类号 |
B64C3/56;F42B10/14;F42B10/16;F42B10/20;F42B15/01;(IPC1-7):B64C3/56 |
主分类号 |
B64C3/56 |
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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