| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a component repairing method capable of improving the quality of a brazed part of a damaged part of a gas turbine component, and improving the efficiency of the repair work by the brazing, and to provide a repaired component. <P>SOLUTION: A gas turbine component 1 includes an opening part 12 formed in a body 11 by reducing the thickness of a material of a part including a ridge 13 in the body 11 of the gas turbine component 1, a side wall part 15 provided along other surface (YZ surface) except one surface (XY surface) in the surfaces with the ridge 13 as a boundary in the opening part 12, and a brazing filler metal 16 which is provided in the opening part 12 to connect the body 11 to the side wall part 15. <P>COPYRIGHT: (C)2013,JPO&INPIT |
