| 发明名称 |
PROTECTIVE COATING SYSTEMS FOR GAS TURBINE ENGINE APPLICATIONS AND METHODS FOR FABRICATING THE SAME |
| 摘要 |
Protective coating systems for gas turbine engine applications and methods for fabricating such protective coating systems are provided. An exemplary method of manufacturing a turbine engine component includes providing a substrate in the form of the turbine engine component and forming a bond coating on and over the substrate. The method further includes forming a thermal barrier coating or an environmental barrier coating on and over the bond coating and forming a magnetoplumbite structure ceramic top coating on an over the thermal barrier coating or the environmental barrier coating. |
| 申请公布号 |
US2015247245(A1) |
申请公布日期 |
2015.09.03 |
| 申请号 |
US201314042323 |
申请日期 |
2013.09.30 |
| 申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
Wali Natalie |
| 分类号 |
C23C30/00;F01D25/00;F01D5/28;C23C28/04 |
主分类号 |
C23C30/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of manufacturing a turbine engine component comprising:
providing a substrate in the form of the turbine engine component; forming a bond coating on and over the substrate; forming a thermal barrier coating or an environmental barrier coating on and over the bond coating; and forming a magnetoplumbite structure ceramic top coating on and over the thermal barrier coating or the environmental barrier coating. |
| 地址 |
Morristown NJ US |
