发明名称 FUZE SAFETY MECHANISM
摘要 FIELD: military equipment, in particular, fuses and safety-actuating mechanisms for war members, stabilized in flight, for example, parachute. SUBSTANCE: the safety mechanism has a body, cocking shackle, rigid safety device and a sleeve and a spring-loaded rod positioned coaxially, a damping, for example, rubber gasket is introduced, and the sleeve is spring- loaded, and its end, facing the rigid safety device, has a spherical shape. The rigid safety device is installed on the cocking shackle and has lugs, at least 3, squeezed in the spherical part of the sleeve, the rod is spring-loaded up to the stop against the rigid safety device and can move together with the cocking shackle and rigid safety device. EFFECT: enhanced reliability and safety at an extraction of the cocking shackle by the joining device of the parachute of the war member. 6 cl, 2 dwg
申请公布号 RU2207496(C1) 申请公布日期 2003.06.27
申请号 RU20020125656 申请日期 2002.09.26
申请人 "NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT "POISK";FEDERALNOE GUP 发明人 EGORENKOV L.S.;OS'KIN I.A.;PLATONOV N.A.;SEVEROV V.JU.
分类号 F42C15/20;(IPC1-7):F42C15/20 主分类号 F42C15/20
代理机构 代理人
主权项
地址