发明名称 Fin erection mechanism
摘要 A plurality of fins for a missile which are capable of being folded to conform to the general cylindrical contour of the missile body and which are biased to unfold to an erect position and which includes an interconnection mechanism for connecting all the fins together to ensure simultaneous erection and for distributing the erection moment of individual fins to all fins; said interconnection means further being capable of acting without interfering with the movement of the fins for flight control without need for disengagement after erection.
申请公布号 US4296895(A) 申请公布日期 1981.10.27
申请号 US19790003358 申请日期 1979.01.15
申请人 GENERAL DYNAMICS CORPORATION 发明人 PAZMANY, LADISLAO
分类号 F42B10/16;F42B10/64 主分类号 F42B10/16
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