| 发明名称 |
LEADING EDGE AIRFOIL-TO-PLATFORM FILLET COOLING TUBE |
| 摘要 |
A turbine engine component includes an airfoil portion having a leading edge, a platform, a leading edge airfoil to platform fillet, and a cooling tube located within said fillet. The cooling tube has a flared entrance end and a flared exit end.
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| 申请公布号 |
US2012163993(A1) |
申请公布日期 |
2012.06.28 |
| 申请号 |
US20100977418 |
申请日期 |
2010.12.23 |
| 申请人 |
LEVINE JEFFREY R.;DONNELL BRANDON S.;UNITED TECHNOLOGIES CORPORATION |
发明人 |
LEVINE JEFFREY R.;DONNELL BRANDON S. |
| 分类号 |
F01D5/18 |
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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