发明名称 Method and apparatus for cooling gas turbine engine rotor blades
摘要 A method for fabricating a turbine rotor blade includes casting a turbine rotor blade including a dovetail, a platform having an outer surface, an inner surface, and a cast-in plenum defined between the outer surface and the inner surface, and an airfoil, and forming a plurality of openings between the platform inner surface and the platform outer surface to facilitate cooling an exterior surface of the platform.
申请公布号 US7198467(B2) 申请公布日期 2007.04.03
申请号 US20040909199 申请日期 2004.07.30
申请人 GENERAL ELECTRIC COMPANY 发明人 KEITH SEAN ROBERT;DANOWSKI MICHAEL JOSEPH;LEEKE, JR. LESLIE EUGENE
分类号 F01S5/18 主分类号 F01S5/18
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