| 摘要 |
A method for manufacturing and/or machining components, in particular gas turbine components such as blades, blade segments or integrally bladed rotors for an aircraft engine, is disclosed. In an embodiment, the method for manufacturing components, in particular gas turbine components, includes at least the following steps: a) providing a workpiece; b) milling the workpiece to provide a component to be manufactured; c) rounding the edges of the component and/or smoothing the surface of the component and/or hardening the surface of the component by a hydraulic method using a lubricant and/or coolant required for the milling.
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