The invention is suitable for the technical field of
aerospace machinery
processing, and provides a preparation method of a high-pressure-bearing
aerospace engine thin-wall cylinder, which mainly comprises the steps of modeling and forming mold production,
decomposition of a digital model into a plane model drawing,
surface plate material treatment, plate material
welding and splicing, blank material treatment, heat treatment and
compression molding, and
electron beam
welding forming. The method comprises the following steps: modeling a cylinder of a water-cooling double-layer structure, decomposing the cylinder into a plane model drawing through a digital model, selecting straight plate materials, carrying out plane milling and flow channel
processing, fully fitting and
welding the two plate materials through vacuum
diffusion welding, and carrying out heat treatment to form a semicircular cylinder. The two semicircular barrels are welded through vacuum variable-focus
electron beam welding, so that rotary body welding is changed into plane welding, the purpose of welding multiple pieces at a time can be achieved, the rate of finished products can be increased, a modular
machining production mode is adopted, the production period can be effectively shortened, the production cost is reduced, and the production efficiency is improved. And the overall production efficiency is improved.