发明名称 Cooled turbine blade platform
摘要 A turbine blade assembly (100) is provided. The turbine blade assembly (100) comprises a turbine blade comprising a cavity (138), and a blade platform (120) supporting the turbine blade, the cavity (138) extending into the blade platform (120). The blade platform (120) comprises an upper surface (128) adjacent the turbine blade and a lower surface (130) comprising a first rib (200), the cavity (138) extending into the first rib (200), the first rib (200) coupled to the lower surface (130), tapering as it extends away from the turbine blade, and comprising a first port (132) extending from the cavity (138) to the upper surface (128).
申请公布号 EP2228518(A2) 申请公布日期 2010.09.15
申请号 EP20100153390 申请日期 2010.02.11
申请人 HONEYWELL INTERNATIONAL INC. 发明人 MORRIS, MARK C.;SMOKE, JASON;HOWE, JEFF;MITLIN, BOB
分类号 F01D5/30;F01D5/18 主分类号 F01D5/30
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