发明名称 PROCESS OF REMOVING A COATING DEPOSIT FROM A THROUGH-HOLE INA COMPONENT AND COMPONENT PROCESSED THEREBY
摘要 <p>A process of removing deposits (22) from through-holes (12) in a component (10), such as metallic bond coat and ceramic materials from cooling holes (12) in an air- cooled gas turbine engine. The process is particularly effective in removing a TBC material deposited in a cooling hole (12) of a component (10) as a result of depositing a coating (20) of the TBC material on a surface (14) of the component (10), in which the deposit (22) is removed from the cooling hole (12) without damaging the cooling hole (12) or the TBC coating (20) surrounding the cooling hole (12) on the coated surface (14) of the component (10). A preferred feature is that the cooling hole (12), including the entrance to the hole (12) at a surface (16) of the component (10) opposite the coated surface (14) and the coating (20) surrounding the exit o f the hole (12) at the coated surface (14), exhibits improved surface characteristics that increase the discharge coefficient of the cooling hole (12), as evidenced by an increase in the effective area of the cooling hole (12).</p>
申请公布号 CA2419361(A1) 申请公布日期 2003.09.01
申请号 CA20032419361 申请日期 2003.02.20
申请人 GENERAL ELECTRIC COMPANY 发明人 FARMER, GILBERT;FEHRENBACH, JEFFREY ARNOLD
分类号 B24C1/00;B23P6/00;B24C11/00;C23C4/00;F01D5/18;F01D5/28;(IPC1-7):B08B9/032;B08B3/02 主分类号 B24C1/00
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