Method for machining a metal component
AssigneeMTU Aero Engines AG
InventorsErwin Bayer, Martin Bussmann, Albin Platz
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AssigneeMTU Aero Engines AG
InventorsErwin Bayer, Martin Bussmann, Albin Platz
Estimating the term…
The invention concerns a method for the machining of a metallic structural component, particularly a structural component of a gas turbine, by means of finishing with a pulsed electrochemical ablation process, whereby the structural component features a pre-contour, to be finished, with different over-measures. The method is characterized by the following processing steps: a) determination of the different over-measures of the pre-contour, and b) bilateral and simultaneous finishing by means of a simultaneous feed of respectively at least one electrode disposed on different sides of the structural component, whereby the feed velocity of the electrode in the area of the largest over-measure of the pre-contour is higher than the feed velocity in the area of the smaller over-measure of the pre-contour.
A method for machining a metallic structural component by finishing with a pulsed electrochemical ablation process, wherein before finishing the structural component has a pre-contour with different over-measures in different areas, the method including the following steps:
A method for machining a metallic structural component having a pre-contour with different over-measures in different areas relative to a predetermined end-contour, the method including the following steps:
A method for machining a metallic structural component having a pre-contour with different over-measures in different areas relative to a predetermined end-contour, the method including the following steps:
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