发明名称 |
Repair Method For TBC Coated Turbine Components |
摘要 |
<p>A method is provided for repairing a metallic turbine component which includes a thermal barrier coating system including a metallic bond coat (22) and a ceramic top coat (24). The method includes: (a) removing the top coat (24) using a mechanical process; (b) partially stripping the metallic bond coat (22) from the component, such that substantially no material of the component is removed; (c) repairing at least one defect in the turbine component; (d) applying a new metallic bond coat (26', 28') to the turbine component; and (e) applying a new ceramic top coat (24) over the metallic bond coat (26', 28').</p> |
申请公布号 |
EP2191930(A2) |
申请公布日期 |
2010.06.02 |
申请号 |
EP20090176677 |
申请日期 |
2009.11.20 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
GUPTA, BHUPENDRA KUMAR;GRADY, WAYNE RAY;GARCIA, ANTOINE FREITAS |
分类号 |
B23P6/00;C23C4/02;F01D5/00 |
主分类号 |
B23P6/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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