发明名称 Rocket motor igniter, arming firing device
摘要 An arming-firing device that provides handling safety in a rocket motor. The arming-firing device provides pyrotechnic (out-of-line) and electrical (open circuit) safety features wherein the arming-firing device is armed by rotating a mechanical rotor by a solenoid that aligns multiple prongs of the barrier with multiple cavities of the rotor and this action simultaneously electrically arms (closes circuits) and mechanically enables the igniter whereupon receiving a firing signal starts the rocket motor. The mating of the barrier prongs with the rotor cavities obviates rebounding, thus affording proper ignition. The mechanical barrier and a solenoid return spring prevents inadvertent firing from any cause.
申请公布号 US4278026(A) 申请公布日期 1981.07.14
申请号 US19790084487 申请日期 1979.10.15
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY 发明人 HIBBS, JOSEPH E.;CHALMERS, GERALD W.;DURRELL, ROBERT L.;SMITH, WALTER C.
分类号 F42C15/31;F42C15/40;F42C21/00;(IPC1-7):F42C15/40 主分类号 F42C15/31
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