发明名称 AIRFOIL FOR A TURBINE ENGINE
摘要 An airfoil for a turbine engine includes a cooling cavity and a cooling fluid supply cavity which supplies cooling fluid to the cooling cavity through a passage. The cooling cavity can be provided with a swirl feature for imparting a swirling motion to the cool ing fluid.
申请公布号 CA2910691(A1) 申请公布日期 2016.04.30
申请号 CA20152910691 申请日期 2015.10.29
申请人 GENERAL ELECTRIC COMPANY 发明人 BUNKER, RONALD SCOTT;BERGHOLZ, ROBERT FREDERICK;BRIGGS, ROBERT DAVID;FELDMANN, KEVIN ROBERT
分类号 F01D5/18 主分类号 F01D5/18
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