发明名称 GAS TURBINE ENGINE SUPPORT
摘要 FIELD: engines and pumps. ^ SUBSTANCE: turbine support relates to aircraft engine production. Gas turbine support comprises inner housing with bearing, radial spokes attached to inner housing and passing through turbine nozzle vane inner spaces, flexible elements and outer support made integral from closed hollow ring with brackets arranged along turbine lengthwise axis. Note here that aforesaid brackets are pivoted to aforesaid spokes via adjusting elements. ^ EFFECT: more or less equal tightening of spokes in turbine assembly. ^ 2 cl, 1 dwg
申请公布号 RU2375596(C1) 申请公布日期 2009.12.10
申请号 RU20080116278 申请日期 2008.04.28
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "SATURN" (OAO "NPO "SATURN") 发明人 RAJKOV JURIJ VASIL'EVICH;ABASHKIN SERGEJ BORISOVICH;POLUBOJARINOVA SVETLANA ANATOL'EVNA
分类号 F02C7/20 主分类号 F02C7/20
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