发明名称 JET ENGINE TELESCOPING NOZZLE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: invention relates to missilery and can be used in development of telescoping nozzles of jet engines, primarily, with major expansion. Proposed nozzle comprises fixed cowl, extendable nozzle arranged on guide cylinder, nozzle folded position retainer with catches and power drive with pyrotechnical device. Ledges of retainers interact with aforesaid fixed cowl and are enveloped by binding tape with lock. Aforesaid power drive is arranged on fixed coal and linked up with binding tape lock clamping link. Linkage represents a rod passed through the cylinder opening. Lock clamping link represents a sleeve inserted in holes of binding tape lock mating parts and oriented opposite aforesaid cylinder opening. ^ EFFECT: reduced weight and higher reliability. ^ 2 cl, 4 dwg
申请公布号 RU2366824(C1) 申请公布日期 2009.09.10
申请号 RU20080103970 申请日期 2008.02.01
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "ISKRA" 发明人 SOKOLOVSKIJ MIKHAIL IVANOVICH;GOROZHANTSEV VLADIMIR VLADIMIROVICH;FLORINSKAJA ZULJA MUBAREKOVNA
分类号 F02K9/97 主分类号 F02K9/97
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