发明名称 ENGINE COMPONENT
摘要 An engine component for a gas turbine engine includes a film-cooled substrate having a hot surface facing hot combustion gas and a cooling surface facing a cooling fluid flow. The substrate includes one or more film holes that have a passage with an inlet and an outlet, where the passage includes portions that are angled relative to each other.
申请公布号 CA2920563(A1) 申请公布日期 2016.08.24
申请号 CA20162920563 申请日期 2016.02.11
申请人 GENERAL ELECTRIC COMPANY 发明人 BUNKER, RONALD SCOTT;BUCK, FREDERICK ALAN
分类号 F01D25/12;F01D5/18;F02C7/12 主分类号 F01D25/12
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