发明名称 Turbine component repair system and method of using thereof
摘要 A system and method for repairing turbine components. The system includes means for obtaining a rapidly solidified material having a means of forming a rapidly solidified repair material and a means for melting the rapidly solidified repair material at a repair site located in a region of the turbine component. The means for obtaining the rapidly solidified material include melt spinning, planar flow, and melt extraction systems. Means for melting the rapidly solidified repair material include a welding torch, an electron beam, a laser beam, a welding torch, a TIG welder, and a plasma torch. A method for using the repair system includes the steps of providing a molten repair material, contacting the molten repair material with a rotating drum, thereby rapidly solidifying the repair material, melting the rapidly solidified repair material and portion of the turbine component at a repair site, and resolidifying the molten repair material and turbine component portion, thereby repairing a defect located at the repair site.
申请公布号 US6626228(B1) 申请公布日期 2003.09.30
申请号 US20000670590 申请日期 2000.09.29
申请人 GENERAL ELECTRIC COMPANY 发明人 BEWLAY BERNARD PATRICK;FRISCHMANN PETER GEORGE
分类号 B22D11/06;B23K9/04;B23K35/02;B23K35/30;C23C26/02;F01D5/00;(IPC1-7):B22D11/00 主分类号 B22D11/06
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