This invention discloses a composite
machining equipment for aero-engine
turbine guide vanes, belonging to the field of mechanical combination
machining technology. It includes an integrated
electrical control box and a composite
machining table. The composite machining table integrates a turning unit, an electrolytic roughing unit, a
drying and strengthening unit, a finish milling unit, and a closed-loop
conveyor system. The closed-loop
conveyor system enables precise gripping, positioning, and automatic transfer of workpieces between the various machining units. Roughing is completed by combining turning and electrolytic processes, while hot
air drying combined with
laser strengthening improves workpiece performance. Finish milling ensures high precision requirements. This equipment achieves integrated continuous machining of
turbine guide vanes, shortening the process flow, reducing manual intervention, improving
processing efficiency and quality stability, and solving the problems of dispersed
processing steps and large precision fluctuations in traditional machining. It is suitable for
mass production of aero-engine parts.