发明名称 GAS-TURBINE ENGINE COMPRESSOR
摘要 FIELD: mechanical engineering; gas-turbine engines. ^ SUBSTANCE: invention relates to compressors of gas-turbine engines, including engines of ground application. Novelty is that in compressor with turnable vanes of guide-vane assemblies and with ring closed spaces on periphery of compressor stator connected through channels with compressor passage part, said ring closed spaces on periphery of compressor stator and turnable vanes of guide-vane assemblies are made alternating. ^ EFFECT: improved reliability and increased efficiency of compressor by eliminating irregularity of air pressure along circumference at inlet of working blades. ^ 1 dwg
申请公布号 RU2235919(C2) 申请公布日期 2004.09.10
申请号 RU20020118543 申请日期 2002.07.09
申请人 发明人 KRJUCHKOV JU.A.;TUNKIN A.I.;KUZNETSOV V.A.
分类号 F04D29/00;F04D29/26 主分类号 F04D29/00
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