A process for the preparation of a blisk or a blings of a gas turbine, and then produced component

摘要

A process for the preparation of a blisk (‘ bladed disks ") or a blings (‘ bladed ring ") of a gas turbine or a high - or low pressure compressor, characterized in that the method comprises the steps of:a) preparation of an annular blade ring (12); andb) connecting the annular blade ring (12) with a rotor disk (16) or a rotor ring in a manner such that the blade ring (12) on the outer circumference (18) of the rotor disk (16) or of the rotor ring is arranged, wherein after the connection of the annular blade ring (12) with the rotor disk (16) or the rotor ring recesses (20) in the rotor disk (16) or the rotor ring are formed, where the recesses (20) between each two adjacent individual blades (14) of the blade ring (12) on the outer circumference (18) of the rotor disk (16) or of the rotor ring are arranged peripherally.