发明名称 GAS TURBINE PLANT
摘要 FIELD: mechanical engineering; turbines. SUBSTANCE: proposed gas turbine plant with gas generator comprises low-and high-pressure compressors. Ring slot fund behind first blade of low-pressure compressor communicates at inlet with periphery of compressor setting and at outlet, with atmosphere. Ring space found at outlet of low-pressure compressor communicates at inlet with periphery of passage channel between compressors, and at outlet, with atmosphere through housing blow-out system. Ratio of area of ring slot section to area of setting behind first working blade of low-pressure compressor is within 0.005 and 1. EFFECT: improved reliability and efficiency of gas turbine plant owing to two-stage cleaning of air delivered to high-pressure compressor. 3 dwg
申请公布号 RU2198311(C2) 申请公布日期 2003.02.10
申请号 RU20010100249 申请日期 2001.01.03
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 INOZEMTSEV A.A.;GUZACHEV E.T.;TOROPCHIN S.V.;KUZNETSOV V.A.
分类号 F02C7/052 主分类号 F02C7/052
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