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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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