发明名称 SEAL OF GAS TURBINE ENGINE COMBUSTION CHAMBER-TO-STATOR JOINT
摘要 FIELD: engines and pumps.SUBSTANCE: proposed joint comprises combustion chamber seal ring and nozzle diaphragm lip. Said lip is secured at inner housing furnished with lock ring with floating ring. Seal ring and nozzle diaphragm lip form an annular clearance for air feed for film cooling of channel surfaces. Said floating ring has thrust collar. Nozzle diaphragm lip is equipped with guide ring to make annular clearance with nozzle diaphragm lip inner surface. Lip end abuts on flowing ring collar.EFFECT: stabilised clearance, reliable cooling of nozzle guide and operating vanes.2 cl, 2 dwg
申请公布号 RU2493388(C1) 申请公布日期 2013.09.20
申请号 RU20120111911 申请日期 2012.03.27
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO KONSTRUKTORSKO-PROIZVODSTVENNOE PREDPRIJATIE "AVIAMOTOR" 发明人 KHABIBULLIN MIDKHAT GUBAJDULLOVICH;ZHIL'TSOV EVGENIJ IZOSIMOVICH;KHUSNULLIN VJACHESLAV KHAZIEVICH;MERKUSHIN VALENTIN KONSTANTINOVICH;VIL'GEMSKAJA ELENA VIKTOROVNA
分类号 F02C7/28;F01D11/00;F16J15/46 主分类号 F02C7/28
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