发明申请
- 专利标题: GAS TURBINE HOT GAS COMPONENT REPAIR METHOD
- 专利标题(中): 燃气涡轮机燃气元件维修方法
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申请号: US12420578申请日: 2009-04-08
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公开(公告)号: US20090255117A1公开(公告)日: 2009-10-15
- 发明人: Simone Hovel , Alexander Stankowski , Gunter Ambrosy , Matthias Hoebel , Alexander Schnell , Hans Bissig , Rainer Kurtz
- 申请人: Simone Hovel , Alexander Stankowski , Gunter Ambrosy , Matthias Hoebel , Alexander Schnell , Hans Bissig , Rainer Kurtz
- 申请人地址: CH Baden
- 专利权人: ALSTOM Technology Ltd.
- 当前专利权人: ALSTOM Technology Ltd.
- 当前专利权人地址: CH Baden
- 优先权: EP08154234.2 20080409
- 主分类号: B23P6/00
- IPC分类号: B23P6/00
摘要:
A gas turbine engine hot gas component repair method for defects that do not extend through the thickness of the component is provided. First defects are removed by machining a cavity in the surface of a component. Coupons, fittable within the cavities are manufactured, are for example coated with brazing medium on an inner surface and then joined to the component by joining means such as laser metal forming. The joint holds the coupon during later heat treatment, thereby eliminating a need for holding aids. Before heat treatment, a further brazing medium can be applied to the surface of the coupon overlapping onto the component. A single heat treatment, brazing the coupon to the component and, brazing the brazing medium to the outer surface of the coupon can, then be used to complete the repair.
公开/授权文献
- US08156649B2 Gas turbine hot gas component repair method 公开/授权日:2012-04-17