发明名称 DURABLE TURBINE VANE
摘要 A durable nozzle vane includes a leading edge(50) where hot combustion gas impinges on the vane, a pressure side (52) extending from the leading edge to a trailing edge (58) and a suction side (54) extending from the leading edge to the trailing edge, a blunt region (74) along the suction side between the leading edge and a high curvature region (72), the blunt region having small curvature in the length between the leading edge and the high curvature region allowing for at least two rows of cooling apertures (66).
申请公布号 CA2870612(A1) 申请公布日期 2013.10.31
申请号 CA20132870612 申请日期 2013.04.05
申请人 GENERAL ELECTRIC COMPANY 发明人 BUBNICK, JOSEPH STEVEN;BARTZ, ROBERT JOSEPH;DEMERS, DANIEL EDWARD;FREDERICK, ROBERT ALAN;HEFFRON, TODD STEPHEN;MOLLESON, SEAN MICHAEL
分类号 F01D5/18 主分类号 F01D5/18
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