| 发明名称 |
INTERNALLY COOLED GAS TURBINE AIRFOIL AND METHOD |
| 摘要 |
An internally cooled airfoil for a gas turbine engine, wherein a plurality of elongated cooling fins are provided inside the concave sidewall between two crossovers.
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| 申请公布号 |
CA2528098(C) |
申请公布日期 |
2011.12.20 |
| 申请号 |
CA20052528098 |
申请日期 |
2005.11.28 |
| 申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
PAPPLE, MICHAEL |
| 分类号 |
F01D5/18;F02C7/12 |
主分类号 |
F01D5/18 |
| 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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