发明名称 Safety catch for aircraft launched missile - has safety pin sheared by cable unwinding to unscrew nut to engage shearing cam
摘要 <p>The safety catch forms part of the missile and comprises a spool (19) storing a predetermined length (17,18) of cable. One end of this is fixed (15) to the aircraft,itsother end rotating the spool on launching the missile. This unscrews a nut (22) down a spindle (23,24). This runs into a cam (3) and a projection (25) on the nut enters an annular recess (8), up to a stop (9). This projection, together with a spring (28), exerts pressure on the cam and causes a safety pin (7) to shear and arm the missile. The cable then breaks.</p>
申请公布号 FR2458460(A1) 申请公布日期 1981.01.02
申请号 FR19790014756 申请日期 1979.06.08
申请人 MULLEMAN MICHEL 发明人
分类号 B64D1/02;F42C14/06;(IPC1-7):64D1/02;42C15/12;64D7/08 主分类号 B64D1/02
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