发明名称 GAS TURBINE ENGINE WITH AFT FAN
摘要 FIELD: engines and pumps. ^ SUBSTANCE: proposed engine comprises gas generator arranged at compressor inlet, compressor shell fairing connected by inlet posts with air intake and, further, with engine nacelle. Compressor shell fairing and air intake have annular slotted spaces with airflow about. Heated rotary inlet distributor is arranged between said posts and compressor rotor. Distributor vane inner cavities communicate at inlet via vane outer pins with compressor intermediate stage and, at outlet, with fairing slotted annular space of compressor shell communicated via hollow inlet posts with air intake slotted space communicated with atmosphere at outlet. ^ EFFECT: higher engine reliability due to ruling out of icing. ^ 5 dwg
申请公布号 RU2439347(C1) 申请公布日期 2012.01.10
申请号 RU20100123297 申请日期 2010.06.07
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 KUZNETSOV VALERIJ ALEKSEEVICH
分类号 F02C7/047 主分类号 F02C7/047
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