发明名称 ADJUSTABLE NOZZLE OF JET TURBINE ENGINE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: adjustable nozzle of jet turbine engine refers to aircraft engine building industry, and namely to design of adjustable nozzle of jet turbine engine. Adjustable nozzle of jet turbine engine includes housing with hinged flaps equipped with transverse ribs forming slots and sealing inserts located between them. Sealing inserts are suspended on flaps by means of yokes with lugs taken to slots of flaps. Each flap is provided at slot location point on the side of its outer surface at least with one plate connected to flap by means of longitudinal ribs forming cooling air channels. ^ EFFECT: invention allows improving reliability and service life of nozzle of jet turbine engine owing to decreasing the temperature of nozzle elements and wear of their friction surfaces. ^ 2 dwg
申请公布号 RU2426905(C1) 申请公布日期 2011.08.20
申请号 RU20090145486 申请日期 2009.12.09
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "SATURN" (OAO "NPO "SATURN") 发明人 PYRKOV SERGEJ NIKOLAEVICH;DEMCHENKO ALEKSANDR VALER'EVICH
分类号 F02K1/12 主分类号 F02K1/12
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