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
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