The invention discloses a
spinning forming method for a perfect circle aircraft engine lip, and belongs to the technical field of
spinning forming. The
spinning forming method comprises the following steps: S1, designing a spinning process; S2, designing a spinning blank: respectively designing blank sizes required by an inner side wall and an outer side wall according to a product structure; S3, designing a spinning process: S3.1, designing a spinning roller
attack angle and a spinning roller shape, S3.2, designing a spinning roller gap, S3.3, designing a spinning track, S3.4, producing a spinning program, S3.5, designing spinning parameters, S4, spinning forming, and S5,
machining a part. According to the method, the defects of a die spinning process can be overcome, the material performance of the aircraft engine lip is improved through the
machining mode of overall spinning forming of the plate, the problem that microdefects are generated in a
welding seam in a traditional split
welding mode is solved, and the
welding quality of the aircraft engine lip is improved through multi-pass spinning forming and control over the motion trail of a spinning roller in the spinning process. And the temperature in the spinning process is controlled, so that the spinning forming stability is improved, and the product
machining precision is also improved.