| 发明名称 |
GAS TURBINE ENGINE BLADE SQUEALER POCKETS |
| 摘要 |
A blade for a gas turbine engine includes an airfoil having a tip with a terminal end surface and multiple squealer pockets recessed into the terminal end surface. |
| 申请公布号 |
US2016017719(A1) |
申请公布日期 |
2016.01.21 |
| 申请号 |
US201514696601 |
申请日期 |
2015.04.27 |
| 申请人 |
United Technologies Corporation |
发明人 |
Propheter-Hinckley Tracy A.;Quach San |
| 分类号 |
F01D5/18 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A blade for a gas turbine engine comprising:
an airfoil having a tip with a terminal end surface, and multiple squealer pockets recessed into the terminal end surface. |
| 地址 |
Hartford CT US |
