| 发明名称 |
THERMAL BARRIER COATING REPAIR |
| 摘要 |
A method of repairing a gas turbine engine component includes the steps of providing a component with a damaged thermal barrier coating surface, preparing the damaged thermal barrier coating surface to provide a repair area, and suspension plasma spraying a ceramic material onto the repair area to produce a repaired area. |
| 申请公布号 |
US2016281204(A1) |
申请公布日期 |
2016.09.29 |
| 申请号 |
US201415034744 |
申请日期 |
2014.10.27 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Ucasz Mark T. |
| 分类号 |
C23C4/134;F01D5/28;F23R3/00;F01D11/08;F01D25/30;C23C4/06;F01D9/02 |
主分类号 |
C23C4/134 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of repairing a gas turbine engine component, comprising the steps of:
providing a component with a damaged thermal barrier coating surface; preparing the damaged thermal barrier coating surface to provide a repair area; and suspension plasma spraying a ceramic material onto the repair area to produce a repaired area. |
| 地址 |
Hartford CT US |
