| 发明名称 |
TURBOMACHINERY COMPONENT COOLING SCHEME |
| 摘要 |
A turbomachinery component includes a surface exposed to hot working fluid flow. The surface has an undulating contour formed from a series of alternating protuberances and troughs. A set of three cooling outlets is associated with each trough. |
| 申请公布号 |
US2013323079(A1) |
申请公布日期 |
2013.12.05 |
| 申请号 |
US201213488831 |
申请日期 |
2012.06.05 |
| 申请人 |
MARTIN THOMAS J.;STAROSELSKY ALEXANDER;ZELESKY MARK F.;SLAVENS THOMAS N.;UNITED TECHNOLOGIES CORPORATION |
发明人 |
MARTIN THOMAS J.;STAROSELSKY ALEXANDER;ZELESKY MARK F.;SLAVENS THOMAS N. |
| 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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