Method for producing a plate of a turbomachine
AssigneeMTU Aero Engines AG
InventorsAlbin Platz, Martin Bussmann, Steffen Gerloff, Nicole Feiling, Anna Carina Kuepper, Norbert Huber, Hermann Klingels
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AssigneeMTU Aero Engines AG
InventorsAlbin Platz, Martin Bussmann, Steffen Gerloff, Nicole Feiling, Anna Carina Kuepper, Norbert Huber, Hermann Klingels
Estimating the term…
The present invention relates to a method for manufacturing a plate of a turbomachine having a plurality of receiving grooves, which are formed on the cylindrical peripheral surface of the plate in order to receive blade roots of blades of the turbomachine. The receiving grooves extend in a straight line from one face of the plate to the other face of the plate, such that a straight line delimits the receiving groove from each point on the cross section of the receiving groove on one of the faces to the corresponding point on the cross section on the other face. A circular plate is provided and a plurality of receiving grooves are introduced into the plate simultaneously on opposing regions relative to a central axis of rotation of the plate.
A method for producing a plate or disk of a turbomachine having an axis of rotation and receiving grooves to respectively receive blade roots of the turbomachine, comprising the steps of:
Dependencies are inferred from the claim text.