发明名称 UNFOLDING WING OF TWO-STAGE ROCKET
摘要 FIELD: weapons and ammunition.SUBSTANCE: wing and unfolding mechanism are arranged independently at different stages of the rocket. Unfolding mechanism is composed of revolving crank consisting of lever and pin fitted in thrust bearing. Pivot pins of wing and lever are aligned. Said lever is fitted on its pivot pin to revolve thereon and locked by pyro retainer fixed at said lever. Thrusts are fitted on lever pivot pin and on lever proper to accommodate contraction spring there between. Said lever if furnished with pins to interact with seats made in wing rear edge. Wing unfolds behind its rear edge by means of two pins fitted on said lever.EFFECT: reduced unfolding forces, decreased weight.7 dwg
申请公布号 RU2478907(C1) 申请公布日期 2013.04.10
申请号 RU20110150664 申请日期 2011.12.14
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "VOENNO-PROMYSHLENNAJA KORPORATSIJA "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE MASHINOSTROENIJA" 发明人 VOLKOV VLADIMIR ALEKSANDROVICH;ZEMSKOV VJACHESLAV ALEKSANDROVICH;BELJUSTIN LEV VLADIMIROVICH
分类号 F42B10/14 主分类号 F42B10/14
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