| 发明名称 |
GAS TURBINE ENGINE COMPONENT EXTERNAL SURFACE MICRO-CHANNEL COOLING |
| 摘要 |
A gas turbine engine component that includes a structure having a surface which includes multiple cooling channels having a width of 20-30 μm and a depth of 25-50 μm. |
| 申请公布号 |
US2015377034(A1) |
申请公布日期 |
2015.12.31 |
| 申请号 |
US201414767922 |
申请日期 |
2014.02.26 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Quitter John |
| 分类号 |
F01D5/18 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine component comprising:
a structure having a surface, the surface including multiple cooling channels having a width of 20-30 μm and a depth of 25-50 μm. |
| 地址 |
Hartford CT US |
