发明名称 TURBINE COOLING SYSTEM AND METHOD OF COOLING TURBINE SECTION WITH INTERMEDIATE PRESSURE
摘要 FIELD: machine building.SUBSTANCE: turbine cooling system with the first and the second sections comprises the first line to run off the first flow from the first section of the first temperature, the second line to run off the second flow from the first section of the second temperature below the first one, and a common line to send the united flow consisting of the first and the second flows to the second section. The united flow is formed when the second flow exceeds the specified temperature Method of cooling the turbine section with intermediate pressure by a leakage flow from the turbine section with high pressure includes stages at which the leakage flow from the turbine section with high pressure is supplied to it. Afterwards the leakage flow is united with reheat flow from the turbine section with high pressure to form a united flow and the latter flow is sent to the turbine section with intermediate pressure; the united flow is formed when the second flow exceeds the specified temperature.EFFECT: improved efficiency of a turbine cooling system.9 cl, 2 dwg
申请公布号 RU2498098(C2) 申请公布日期 2013.11.10
申请号 RU20080130528 申请日期 2008.07.23
申请人 DZHENERAL EHLEKTRIK KOMPANI 发明人 EHRNANDES NESTOR;GAZZILLO KLEMENT;BOSS MAJKL DZH.;PERRI UILL'JAM;TAJLER KAREN DZH.
分类号 F02C7/12 主分类号 F02C7/12
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