发明名称 GAS-TURBINE PLANT
摘要 FIELD: mechanical engineering; gas-turbine plants. ^ SUBSTANCE: proposed gas-turbine plant includes low-pressure compressor at input, power turbine at output, intermediate housing with separation of flows between compressors and channels of outer and inner loops. Inner loop contains high-pressure compressor with mixer at output. Input of channel of outer loop is connected with output of low-pressure compressor, and output, with external side of mixer. Ratio of area of channel of outer loop at flow separator in intermediate housing between compressors in gas-turbine plant to area of channel of inner loop at flow separator in intermediate housing between compressors in gas-turbine plant is within 0.1-3. Ratio of area of channel of outer loop at output of mixer to area of channel of inner loop at output of mixer is within 0.1-2.5. Number of stages of free power turbine is 1-3. ^ EFFECT: improved reliability and increased efficiency of plant at minimum cost owing to reduction of vibration stresses of turbine working blades and provision of uniform cooling of outer housings. ^ 3 dwg
申请公布号 RU2305789(C2) 申请公布日期 2007.09.10
申请号 RU20050126567 申请日期 2005.08.22
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 SULIMOV DANIIL DMITRIEVICH;POZHARINSKIJ ALEKSANDR ADOL'FOVICH;TOROPCHIN SERGEJ VALENTINOVICH;KUZNETSOV VALERIJ ALEKSEEVICH
分类号 F02K3/02 主分类号 F02K3/02
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