发明名称 TURBINE NOZZLE AND METHOD FOR COOLING TURBINE NOZZLE OF GAS TURBINE ENGINE
摘要 PROBLEM TO BE SOLVED: To provide a turbine nozzle for a gas turbine engine.SOLUTION: The turbine nozzle may include a first nozzle vane, a second nozzle vane, and a platform connecting the first nozzle vane and the second nozzle vane. The platform may include a first cooling passage and a separate second cooling passage defined therein. The first cooling passage may be configured to direct a first flow of cooling fluid in a first direction, and the second cooling passage may be configured to direct a second flow of cooling fluid in a second direction substantially opposite the first direction. The present application and the resultant patent further provide a method for cooling a turbine nozzle of a gas turbine engine.
申请公布号 JP2015127538(A) 申请公布日期 2015.07.09
申请号 JP20140261430 申请日期 2014.12.25
申请人 GENERAL ELECTRIC CO <GE> 发明人 MICHELLE JESSICA IDUATE;FOSTER GREGORY THOMAS;DAVID WAYNE WEBER
分类号 F01D9/02;F02C7/18 主分类号 F01D9/02
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