发明名称 GAS TURBINE PLANT BLADES COOLING
摘要 FIELD: engines and pumps.SUBSTANCE: turbine blades are cooled with the help of the cooling circuit. The cooling circuit consists of the electrically conducting circuit. The elements of the latter are arranged on the turbine structural elements to make the cathode by application of thermal emission ply on the blades of electrically conducting material emitting the electrons into working fluid at heating. Besides, the anode is fabricated and secured via the electric insulation ply inside the housing, for example, at the housing inner wall to take up the electrons of emission from the working fluid. Electrically conducting circuit is composed by serial connection of said anode with cathode via electric load, current pickup, shaft, rotor and turbine blade. Anode temperature is kept below the turbine blade emission ply temperature by anode cooling at its seat of the turbine structural element.EFFECT: lower temperature of turbine blades, higher efficiency and reliability of the turbine.1 dwg
申请公布号 RU2573551(C2) 申请公布日期 2016.01.20
申请号 RU20140121444 申请日期 2014.05.27
申请人 FEDERAL'NOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "BALTIJSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET "VOENMEKH" IM. D.F. USTINOVA (BGTU "VOENMEKH");KERNOZHITSKIJ VLADIMIR ANDREEVICH;KOLYCHEV ALEKSEJ VASIL'EVICH 发明人 KERNOZHITSKIJ VLADIMIR ANDREEVICH;KOLYCHEV ALEKSEJ VASIL'EVICH
分类号 F02C7/12 主分类号 F02C7/12
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