A method of manufacturing a blisk or a bling, component thus prepared and the turbine blade

The present invention relates to a process for the operations department of a blisk ( "bladed disk") or a bling ( "bladed ring") of a gas turbine, the method comprising the steps of: a) producing a turbine blade (10) by joining (by an airfoil 12 ) (to an existing of a melt-weldable metallic material adapter element 16), wherein the adapter element (16) to form a blade root of the turbine blade (10) is used and b) connecting the turbine blade (10) with a group consisting of a melt-weldable metallic material rotor disk (22 ) or a group consisting of a melt-weldable metallic material rotor ring, so that the turbine blade (10) 26) of the rotor disc (22) or of the rotor ring is disposed (on the outer circumference. The invention further relates to a component of a gas turbine or a high or low pressure compressor, in particular a blisk ( "bladed disk") or a bling ( "bladed ring"). According to the invention, the component (30) made of separately produced turbine blades (10) or one of the turbine blades (10) separately prepared annular blade ring (28) and an associated, consisting of a melt-weldable metallic material rotor disc (22) or an associated, from a melt-weldable metallic material existing rotor ring, said turbine blades (10) or the blade ring (28) on the outer periphery ...