Abstract: A locking and fixing device for a heat shield element, which heat shield element can be arranged along a heat shield row axially directly next to at least one blade provided in a blade row and has, axially facing the blade, at least two projections of rib-like design which are spaced apart in the circular circumferential direction, are raised above a side wall section facing the blade and define a clear intermediate space which extends in the circular circumferential direction and into which a locking lug provided on the blade can be fitted. Further disclosed is at least one rib-like projection, on its side facing away from the clear intermediate space, providing an extension which extends in the circular circumferential direction, is connected to the projection and the side wall section and rises above the side wall section at most up to the rib height of the projection.

Abstract: A gas turbine blade, a gas turbine blade airfoil repair method, and an airfoil corresponding to the product of the method are disclosed. The airfoil extends radially from a platform and includes a tip having a tip edge radially distant from the platform; a trailing edge; and a leading edge. The method includes forming a joining plane extending from the leading edge to the tip edge, wherein the joining plane forms at least one arc; forming a replacement tip fittable on the joining plane; and bonding the replacement tip to the airfoil.

Abstract: A locking and fixing device for a heat shield element which can be connected to a rotor unit of an axial-flow turbomachine is described, which heat shield element can be arranged along a heat shield row axially directly next to at least one blade provided in a blade row and has, axially facing the blade, at least two projections of rib-like design which are spaced apart in the circular circumferential direction, are raised above a side wall section facing the blade and define a clear intermediate space which extends in the circular circumferential direction and into which a locking lug provided on the blade can be fitted. A method for producing a device in this respect is also described.