发明名称 Method for rejuvenating cooling passages within a turbine airfoil
摘要 An electrode (110) for rejuvenating a cooling passage (101) within an airfoil, the electrode including a tip (130), an end (140), a conductive core (116) extending between the tip and the end, and an insulating coating (118) disposed on the conductive core. The insulating coating exposes a number of conductive strips (150) of the conductive core extending between the tip and the end. The insulating coating forms a number of insulating portions (160) and further exposes a number of spacer portions (133) of the conductive core longitudinally positioned between the insulating portions. The insulating portions substantially span a distance between the tip and the end and are positioned between the conductive strips. <IMAGE> <IMAGE>
申请公布号 EP1442817(A2) 申请公布日期 2004.08.04
申请号 EP20030251579 申请日期 2003.03.14
申请人 GENERAL ELECTRIC COMPANY 发明人 LEE, CHING-PANG;WEI, BIN;KOOL, LAWRENCE BERNARD;JOHNSON, ROBERT ALAN;WANG, HSIN-PANG
分类号 F01D5/08;B23H9/10;B23H9/16;C25F1/04;F01D9/02;F01D25/00;F01D25/08;F02C7/00;(IPC1-7):B23H9/10 主分类号 F01D5/08
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