| 发明名称 |
SPLAYED TIP FEATURES FOR GAS TURBINE ENGINE AIRFOIL |
| 摘要 |
A component for a gas turbine engine includes a trailing edge tip corner that at least partially defines a trailing edge cavity and a multiple of corner features within the trailing edge cavity, the multiple of corner features splayed along the trailing edge tip corner. |
| 申请公布号 |
US2016069189(A1) |
申请公布日期 |
2016.03.10 |
| 申请号 |
US201514630814 |
申请日期 |
2015.02.25 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Quach San;Propheter-Hinckley Tracy A;Mongillo, JR. Dominic J;Gautschi Steven Bruce |
| 分类号 |
F01D5/14;F01D5/28 |
主分类号 |
F01D5/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A component for a gas turbine engine, comprising:
a trailing edge tip corner that at least partially defines a trailing edge cavity; and a multiple of corner features within said trailing edge cavity, said multiple of corner features splayed along said trailing edge tip corner. |
| 地址 |
Hartford CT US |
