The invention provides a high-precision
spinning forming process method for a ribbed cylinder section, and aims to solve the problems of
diameter expansion, unevenness in deformation and the like in the traditional
spinning process. The process comprises the following steps: performing double-sided turning on a prefabricated cylinder blank to ensure the inclination, mounting a
spinning mold with a rib structure, heating the cylinder blank, and sleeving the heated cylinder blank on a mold with an inner cross groove to realize
interference fit. And then, a three-spinning-roller spinning
machine is started for spinning, the
plasticity of the material is improved through
induction heating, and the material flows into a cross groove of the mold. And after spinning is completed, the spinning roller is replaced with a turning tool, the outer surface is turned, and finally the part is taken out. According to the method, the inner
diameter is controlled through material
thermal expansion coefficient difference and
diameter compensation, and boundary dimension homogenization is achieved through the
induction heating and in-situ turning technology. The process is suitable for materials such as aluminum
alloy and high-strength steel, the size precision of the cylinder section is remarkably improved, and
technical support is provided for overall near-net forming of aircraft cylinder sections such as tactical projectiles. The spinning process is optimized, and the quality and performance of a final product are improved.