COMPONENT FOR A GAS TURBINE AND METHOD FOR PRODUCING THE COMPONENT

摘要

The invention relates to a component of a gas turbine, particularly a blisk or a bling, wherein the component comprises a main rotor body (12) comprising a high temperature resistant nickel alloy and a plurality of turbine blades (14) attached to the main rotor body, wherein each turbine blade (14) comprises an airfoil (16) made of a titanium alloy and a blade footing. The component is characterized in that the blade footing is designed as an adapter element (18), which comprises a material which can be welded both to the titanium alloy and to the high temperature resistant nickel alloy and is integrally connected both the main rotor body (12) and to the airfoil (16) by joining. The invention further describes a method for producing the component.