发明名称 |
COUNTERCOOLED TURBINE NOZZLE |
摘要 |
A turbine nozzle (20) includes a mid vane (24) mounted between a pair of e nd vanes (26) in outer and inner bands (28,30). The mid vane (24) includes a first pattern of film cooling holes (56,58,60) configured to discharge more cooling air th an each of the two end vanes having respective second patterns of film cooling holes (56,58).
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申请公布号 |
CA2562584(A1) |
申请公布日期 |
2007.06.19 |
申请号 |
CA20062562584 |
申请日期 |
2006.10.05 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
FLODMAN, DAVID ALLEN;SHAPIRO, JASON DAVID;KULYK, MICHAEL PETER |
分类号 |
F01D9/02;F01D5/18;F01D25/12 |
主分类号 |
F01D9/02 |
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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