Abstract: A magnet arrangement for a magnetically impelled arc butt welding system, wherein the system is used to weld an airfoil to a platform of a gas turbine. The magnet arrangement includes a first plurality of magnets wherein the magnets are located adjacent a first curved airfoil surface and arranged in a first curved shape corresponding to a shape of the first curved airfoil surface. The magnet arrangement also includes a second plurality of magnets wherein the magnets are located adjacent a second curved airfoil surface and arranged in a second curved shape corresponding to a shape of the second curved airfoil surface such that the first plurality of magnets has a different curvature than the second plurality of magnets. The first and second plurality of magnets guide an electric arc of the system along mating surfaces to heat the mating surfaces to enable the airfoil and platform to be forged together.

Abstract: A magnet arrangement for a magnetically impelled arc butt welding system, wherein the system is used to weld an airfoil to a platform of a gas turbine. The magnet arrangement includes a first plurality of magnets wherein the magnets are located adjacent a first curved airfoil surface and arranged in a first curved shape corresponding to a shape of the first curved airfoil surface. The magnet arrangement also includes a second plurality of magnets wherein the magnets are located adjacent a second curved airfoil surface and arranged in a second curved shape corresponding to a shape of the second curved airfoil surface such that the first plurality of magnets has a different curvature than the second plurality of magnets. The first and second plurality of magnets guide an electric arc of the system along mating surfaces to heat the mating surfaces to enable the airfoil and platform to be forged together.

Abstract: A crack repair method for a turbine component using spark plasma sintering: Applying filler material on a cracked portion of the turbine component. Applying joining pressure on the cracked portion of the turbine component by punches pressing on the component. Simultaneously heating the filler material by an application of electric current. Then cooling the heated filler material to form a joint at the cracked portion.