发明名称 FLAT NOZZLE OF JET TURBINE ENGINE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: flat nozzle of jet turbine engine includes body, subsonic doors hinged to it, supersonic doors, external doors, brackets and hydraulic cylinders connected to levers rigidly attached to subsonic doors, which are installed outside side walls of the nozzle body. Supersonic doors are hinged to subsonic doors. One end of external doors is attached to the housing and the other end is attached to supersonic doors. Brackets are arranged on longitudinal axes of side walls of nozzle body on their external side and hinged to subsonic door turning hydraulic cylinders. Each bracket is provided on its front and rear ends with rollers taken to the guides rigidly attached to the body and with two transverse eye lugs connected by means of rods to levers of subsonic doors. To each lever there hinged is additional rod that is equipped on the other end with rollers taken to the guides provided on external doors. On side walls of nozzle body there installed are additional hydraulic cylinders the stocks of which are hinged to additional rods for turning of external doors. ^ EFFECT: invention allows improving operating reliability and efficiency coefficient of jet turbine engine. ^ 3 dwg
申请公布号 RU2462609(C1) 申请公布日期 2012.09.27
申请号 RU20110106167 申请日期 2011.02.18
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "SATURN" (OAO "NPO "SATURN") 发明人 PYRKOV SERGEJ NIKOLAEVICH;DEMCHENKO ALEKSANDR VALER'EVICH;KIRJUKHIN VLADIMIR VALENTINOVICH;MARCHUKOV EVGENIJ JUVENAL'EVICH
分类号 F02K1/12 主分类号 F02K1/12
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