| 发明名称 |
HOT SECTION REPAIR OF METALLIC COATINGS |
| 摘要 |
Aspects of the disclosure are directed to a servicing of an airfoil of an aircraft engine. A first portion of a first bondcoat layer may be removed from the airfoil while leaving a second portion of the first bondcoat layer intact on the airfoil. A second bondcoat layer may be applied to the airfoil using a coating technique subsequent to the removal of the first portion of the first bondcoat layer. |
| 申请公布号 |
US2016230557(A1) |
申请公布日期 |
2016.08.11 |
| 申请号 |
US201514617628 |
申请日期 |
2015.02.09 |
| 申请人 |
United Technologies Corporation |
发明人 |
Ucasz Mark T.;Saxton Bruce R.;Bales Daniel A.;Brindley William J. |
| 分类号 |
F01D5/00;C23C14/32;F01D5/28 |
主分类号 |
F01D5/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method for servicing an airfoil of an aircraft engine, comprising:
removing a first portion of a first bondcoat layer from the airfoil while leaving a second portion of the first bondcoat layer intact on the airfoil; and applying a second bondcoat layer to the airfoil using a coating technique subsequent to the removal of the first portion of the first bondcoat layer. |
| 地址 |
Hartford CT US |
