发明名称 QUICKLY-DETACHABLE UNIT
摘要 FIELD: rocketry. SUBSTANCE: proposed quickly-detachable unit includes pneumatic pusher mounted inside closed cavity; one end of said pusher is connected with pulling-off unit through sealing members and its other end is connected with locking bush through stroke stop. Locking bush is located inside collet lock. Pneumatic pusher is provided with retainer provided with sealing members. Locking bush is provided with partition for sealing-up the lock cavity which is provided with locking passage relieving pneumatic pressure and filling passage connected with one of filling pipe unions of ground block by means of through pipe line. Pneumatic drive is located inside locking bush. EFFECT: simplified construction; increased payload for spacecraft. 2 dwg
申请公布号 RU2216676(C2) 申请公布日期 2003.11.20
申请号 RU20020103080 申请日期 2002.02.04
申请人 ESKAJA KORPORATSIJA "EHNERGIJA" IM. S.P.KOROLEVA";ESKAJA KORPORATSIJA EHNERGIJA 发明人 MEDVEDEV N.I.;MARTYNOV V.M.;LUZGACHEV M.V.;CHISTOUSOV P.V.
分类号 F16L37/40;(IPC1-7):F16L37/40 主分类号 F16L37/40
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