| 发明名称 |
GAS TURBINE ENGINE COMPONENT HAVING CONTOURED RIB END |
| 摘要 |
A component according to an exemplary aspect of the present disclosure includes, among other things, a wall and at least one rib that protrudes from the wall and extends to a rib end, the rib end having a curved transition portion near a location where the at least one rib meets the wall. |
| 申请公布号 |
EP2948636(A4) |
申请公布日期 |
2016.11.23 |
| 申请号 |
EP20140743391 |
申请日期 |
2014.01.15 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SIMPSON, ALEX J.;NIEZELSKI, DAVID A. |
| 分类号 |
F01D5/18;F01D5/14;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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