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A method for repairing a component of a gas turbine and a solder alloy are disclosed. In an embodiment, the method includes applying the solder alloy to the component in an area of the component having a punctiform damage or a linear imperfection, where the solder alloy is a mixture of a NiCoCrAlY a

A method for repairing a component of a gas turbine and a solder alloy are disclosed. In an embodiment, the method includes applying the solder alloy to the component in an area of the component having a punctiform damage or a linear imperfection, where the solder alloy is a mixture of a NiCoCrAlY alloy and a Ni-based solder. A molded repair part made of the solder alloy is applied to the component in an area of the component having a planar defect. The component is heat treated to solder the molded repair part on the component and to solder the solder alloy applied to the component in the area of the component having the punctiform damage or the linear imperfection. The component is cooled after the heat treating and, following the cooling, the component is further heat treated.

대표청구항 ▼

1. A method for repairing a component of a gas turbine, comprising the steps of: applying a solder alloy to the component in an area of the component having a punctiform damage or a linear imperfection, wherein the solder alloy is a mixture of a NiCoCrAlY alloy and a Ni-based solder;applying a molde

1. A method for repairing a component of a gas turbine, comprising the steps of: applying a solder alloy to the component in an area of the component having a punctiform damage or a linear imperfection, wherein the solder alloy is a mixture of a NiCoCrAlY alloy and a Ni-based solder;applying a molded repair part made of the solder alloy to the component in an area of the component having a planar defect;heat treating the component to solder the molded repair part on the component and to solder the solder alloy applied to the component in the area of the component having the punctiform damage or the linear imperfection;cooling the component after the heat treating; andfollowing the cooling, further heat treating the component wherein the further heat treating includes three sequences of a cooling and a heating. 2. The method according to claim 1, wherein the cooling of the component cools the component to room temperature. 3. The method according to claim 1, further comprising an additional heat treating step for coating the component in addition to the three sequences of the cooling and heating. 4. The method according to claim 1, wherein the component is formed of a Ni-based or Co-based super alloy. 5. The method according to claim 1, wherein the molded repair part is a green compact. 6. The method according to claim 1, wherein the molded repair part is a sintered molded repair part.