发明名称 ADAPTIVE COMBUSTION CHAMBER
摘要 FIELD: turbomechanical engineering. SUBSTANCE: flow separator is rigidly fixed on front movable part of flame tube and functions to optimally control proportion of primary and secondary air at the same time varying flow section areas of secondary-air supply holes by relative closure of shaping holes in front and rear parts. EFFECT: improved combustion efficiency in combustion chamber within comprehensive operating range of gas-turbine engine; reduced hydraulic loss.
申请公布号 RU94022641(A) 申请公布日期 1996.06.20
申请号 RU19940022641 申请日期 1994.06.10
申请人 STAVROPOL'SKOE VYSSHEE AVIATSIONNOE INZHENERNOE UCHILISHCHE PVO IM.MARSHALA SUDTSA V.A. 发明人 BUGA A.L.;VASIL'TSOV G.L.;KOVALEV V.D.;MURAVLJANNIKOV I.A.;PAKHOL'CHENKO A.A.
分类号 F23R3/26 主分类号 F23R3/26
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