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.
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
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