发明名称 GAS-TURBINE ENGINE
摘要 FIELD: engine manufacture. SUBSTANCE: engine has stator with bearing supports provided with air cavities communicating at outlet with atmosphere and supporting rotors mounted on common shaft with compressor and turbine. Radial air cavities are made at stator inlet providing compressor communication with air cavities of shaft and bearing supports through holes in hollow shaft. Holes are spaced apart through 4-15 of shaft cavity diameter. EFFECT: improved reliability of engine due to reduced temperature and clean cooling air flowing over bearing supports. 7 dwg
申请公布号 RU2124644(C1) 申请公布日期 1999.01.10
申请号 RU19960100268 申请日期 1996.01.05
申请人 AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 KUZNETSOV V.A.;TUNKIN A.I.;LEZGIN N.A.
分类号 F02C7/06;(IPC1-7):F02C7/06 主分类号 F02C7/06
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