发明名称 METHOD OF CONTROLLING FUEL FEED TO GAS TURBINE ENGINE
摘要 FIELD: transport.SUBSTANCE: invention relates to aircraft engineering, particularly, to gas turbine fuel feed systems. Fuel feed at starting after log outage at low temperature consists in fuel warming up before fuel feed to fuel filter. Note here that prior to feeding, ice is separated from fuel and heated to breakup. Thereafter, water resulted from breakup is added to warmed up fuel. Said water is additionally heated to warmed-up fuel temperature, preferably, to that approximating to boiling point. Note that ice and water are heated by air bled from gas turbine compressor.EFFECT: reliable takeoff after long stay at low temperatures.2 cl, 2 dwg
申请公布号 RU2514522(C2) 申请公布日期 2014.04.27
申请号 RU20120103791 申请日期 2012.02.03
申请人 FEDERAL'NOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "VORONEZHSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET" 发明人 CHERNICHENKO VLADIMIR VIKTOROVICH;SOLZHENIKIN PAVEL ANATOL'EVICH;STOGNEJ VLADIMIR GRIGOR'EVICH
分类号 F02C7/22 主分类号 F02C7/22
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