Abstract: A device for clamping a turbine blade (9) during a welding repair of the blade tip (11). The blade has a peripheral surface that has a suction side (5) and pressure side (7) and has a blade tip. The device has at least one movable clamping structure (1,3) for pressing on the suction side (5) or the pressure side (7) of a turbine blade (9) in the region of the blade tip (11) of the turbine blade, wherein the clamping structure (1,3) is designed to remove heat from the turbine blade (9). The at least one movable clamping structure (1,3) has a plurality of clamping elements (13), which are each individually movably supported in such a way that the clamping elements can be moved toward the peripheral surface of a turbine blade (9) to be clamped and away from the peripheral surface.

Abstract: A method for repairing an airfoil of an axial turbomachine in which material is deposited onto the airfoil by means of deposition welding, the airfoil being cooled during the deposition welding, is provided. A cooling collar including at least one cooling channel which has a coolant inlet and a coolant outlet and through which a coolant flows in the intended state, is also provided. The cooling collar also includes multiple cooling elements which are arranged along an inner circumference of the cooling collar and adjacently to the at least one cooling channel, the cooling elements resting against an object to be cooled, in particular an airfoil to be cooled, in the intended state.

Abstract: A device for clamping a turbine blade (9) during a welding repair of the blade tip (11). The blade has a peripheral surface that has a suction side (5) and pressure side (7) and has a blade tip. The device has at least one movable clamping structure (1,3) for pressing on the suction side (5) or the pressure side (7) of a turbine blade (9) in the region of the blade tip (11) of the turbine blade, wherein the clamping structure (1,3) is designed to remove heat from the turbine blade (9). The at least one movable clamping structure (1,3) has a plurality of clamping elements (13), which are each individually movably supported in such a way that the clamping elements can be moved toward the peripheral surface of a turbine blade (9) to be clamped and away from the peripheral surface.