发明名称 PROP-FAN ENGINE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: proposed engine comprises gas generator with compressor and rear prop fan coupled with power turbine 8 via reduction gear 13 surrounded by acicular air and gas chambers. Radial and axial deflectors 21, 22 are arranged in air chambers 19 of posts 16 and air chamber 20 of housing 15 to make oil chamber 23 of reduction gear 13. Ring reflector 30 is arranged on housing ahead of rear support housing flange joint 24 with deflector 22 and reduction gear housing 25. Said ring deflector 30 makes annular slot-like cavity 31 with its outlet communicated with compressor. Ring deflector outlet is provided with nozzle 32 to blow flange joint 24. ^ EFFECT: higher engine reliability due to minimised heat flows onto reduction gear components. ^ 3 dwg
申请公布号 RU2430250(C1) 申请公布日期 2011.09.27
申请号 RU20100100427 申请日期 2010.01.11
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 KUZNETSOV VALERIJ ALEKSEEVICH
分类号 F02C7/12;F02K3/062 主分类号 F02C7/12
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