| abstract |
A component for a gas turbine, especially a blisk or a bling, whereby the component includes a rotor base ( 12 ) made of a high temperature-resistant nickel alloy and a plurality of turbine blades ( 14 ) joined to the rotor base, whereby each turbine blade includes a rotor blade ( 16 ) made of a titanium alloy and a blade root. The blade root is configured as an adapter element ( 18 ) that is made of a material that can be welded to the titanium alloy as well as to the high temperature-resistant nickel alloy and that is integrally joined to the rotor base ( 12 ) and to the rotor blade ( 16 ) fusion. A method for the production of the component is also described. |