发明名称 METHOD OF CONVERTING TURBO SHAFT ENGINE INTO GROUND-BASED GAS-TURBINE PLANT
摘要 FIELD: engines.SUBSTANCE: method of aviation turbo shaft engine converting in ground-based gas-turbine plant. Blades are removed from flow parts of compressor last stages and turbine first stages. First stage nozzle assembly (from remaining) of converted turbine is replaced with nozzle assembly of higher performance. Gaseous low-calorie fuel of gas or biogas type product is supplied for combustion to combustion chamber burners. In steady-state operating mode of converted engine temperature of combustion products of gas in chamber maximum of 800 K is set by fuel consumption variation. Degree of compressor full pressure increase is decreased up to 3-4. Mechanical energy is transferred to power consumer through engine output shaft with reduction gear.EFFECT: invention allows to ensure operation of spent engine operating life using low-calorie gaseous fuel from solid household wastes and bio-waste, improves environment, reduce costs for operation of plants and increase their operating life.3 cl, 1 dwg
申请公布号 RU2579526(C2) 申请公布日期 2016.04.10
申请号 RU20140126764 申请日期 2014.07.02
申请人 FEDERALNOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE"TSENTRALNYJ INSTITUT AVIATSIONNOGO MOTOROSTROENIJA IMENI P.I. BARANOVA" 发明人 GUROV VALERIJ IGNATEVICH;SHESTAKOV KONSTANTIN NIKODIMOVICH;KHARKOVSKIJ SERGEJ VALENTINOVICH
分类号 F02C3/04 主分类号 F02C3/04
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