| 摘要 |
<p>The present invention relates to a process for producing integrally bladed rotors (10), especially rotors of a gas turbine, characterized in that the process comprises the following steps: a) The defining of and making available a blade profile of a blade to be manufactured with a pre-contour and theoretical contour, b) The production of at least two sectional planes of the blade profile, which sectional planes run vertically to a threading axis of the blade profile and of the blade to be produced, c) The determining of a point of rotation (14, 16) per sectional plane in such a manner that the interval between the pre-contour and the theoretical contour is approximately the same circumferentially, which points of rotation (14, 16) are located on a connecting line running parallel to the threading axis, and d) Making available a base rotor body and the electrochemical working of the base rotor body in order to produce a raw blade (12) with a blade pre-contour by a lowering of a hollow electrode into the base rotor body, during which an advance movement of the hollow electrode, that is superposed by rotation, takes place along the connection line determined in process step c), and during which the hollow electrode has an inner contour adapted to the pre-contour of the raw blade (12) at least in an end area that is lowered onto the base rotor body.</p> |
