发明名称 TURBINE NOZZLE SEGMENT AND METHOD OF REPAIRING SAME.
摘要 A method for repairing a turbine nozzle segment having at least one vane disposed between outer and inner bands includes separating the inner band from the nozzle segment, and joining the inner band to a newly manufactured replacement casting having an outer band and at least one vane. The replacement casting includes a mounting platform formed on one end of the vane and a boss formed on the mounting platform. A collar is joined to the inner band and has a slot formed therein. The boss is then inserted into the slot, and the mounting platform is received in a recess formed in the inner band. Joining is completed by joining the boss to the collar and the mounting platform to the inner band.
申请公布号 MXPA01011698(A) 申请公布日期 2005.04.19
申请号 MX2001PA11698 申请日期 2001.11.15
申请人 GENERAL ELECTRIC COMPANY 发明人 GLENN HERBERT NICHOLS
分类号 F01D9/02;B23P6/00;F01D5/00;F01D9/04;F02C7/00;(IPC1-7):B23P6/04 主分类号 F01D9/02
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