| abstract |
The present invention relates to a method for producing a component of a turbomachine, in particular a blade, in which First, a sheath (6) with an internal cavity (7) corresponding to the outer contour of the component is produced from an intermetallic TiAl material and then a Ti alloy in powder form is filled into the cavity and the cavity sealed with the filled Ti alloy powder Subsequently, the sealed shell (6) with the enclosed Ti alloy powder is processed by hot isostatic pressing to the component of the turbomachine. Alternatively, the invention relates to a method for the generative production of a component with a shell of a TiAl alloy and a core of a Ti alloy. Moreover, the invention relates to a correspondingly manufactured component. |