| 发明名称 |
TURBINE COMPONENT COATING PROCESSES AND TURBINE COMPONENTS |
| 摘要 |
Turbine component coating processes include applying a malleable masking material to one or more apertures of one or more fluid flow passages within a turbine component surface and then applying a first coating over the malleable masking material and on the turbine component surface. The turbine component coating processes further include locally applying a local masking material to the one or more apertures of the one or more fluid flow passages and then applying a second coating over the local masking material and on the first coating. |
| 申请公布号 |
US2016089692(A1) |
申请公布日期 |
2016.03.31 |
| 申请号 |
US201414501607 |
申请日期 |
2014.09.30 |
| 申请人 |
General Electric Company |
发明人 |
Reid Thomas Robert;Lomas Jonathan Matthew |
| 分类号 |
B05D1/32;B05D1/28;B05D3/12;F01D25/00;B05D5/00;C23C4/12;C23C28/00;F01D5/28;B05D1/36;B05D7/14 |
主分类号 |
B05D1/32 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine component coating process, comprising:
applying a malleable masking material to one or more apertures of one or more fluid flow passages within a turbine component surface; then applying a first coating over the malleable masking material and on the turbine component surface; then locally applying a local masking material to the one or more apertures of the one or more fluid flow passages; and then applying a second coating over the local masking material and on the first coating. |
| 地址 |
Schenectady NY US |
