| 发明名称 |
COATED GAS TURBINE ENGINE COMPONENTS |
| 摘要 |
A gas turbine engine component may include a coating adapted to protect the component during use. The coating may be applied by sintering metallic particles to form a metallic matrix fused to the component. |
| 申请公布号 |
US2015377039(A1) |
申请公布日期 |
2015.12.31 |
| 申请号 |
US201514734834 |
申请日期 |
2015.06.09 |
| 申请人 |
Rolls-Royce Corporation |
发明人 |
Shuck Quinlan Y. |
| 分类号 |
F01D5/28;C23C24/08;F01D11/00 |
主分类号 |
F01D5/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of making a coated gas turbine engine component comprising:
depositing a layer of powder including metallic particles and abrasive particles on a gas turbine engine component; and applying microwaves to the layer of powder to heat the metallic particles in order to sinter the metallic particles into a metallic matrix joined to the gas turbine engine component. |
| 地址 |
Indianapolis IN US |
