The invention discloses an aero-engine part
fatigue crack propagation identification method based on
machine vision. The method comprises the following steps: S1, obtaining an image block sequence; s2, inputting each image block into a pseudo
stress estimation network to generate an image block pseudo stress diagram; s3, inputting the image block and the image block pseudo-stress diagram into an image feature decoupling coding module, and outputting a fusion
feature vector; s4, inputting the fusion
feature vector into an improved fox
algorithm, and generating a crack path guide map and a
direction vector field; s5, inputting the image block pseudo-stress diagram, the crack path guide diagram, the
direction vector field and the fusion
feature vector into a crack
mask generation module, and outputting an image block crack
mask; s6, splicing the image block crack masks according to the positions of the image blocks in the surface image to generate a complete crack
structure diagram; and S7, outputting a crack propagation result based on the complete crack
structure chart. According to the method,
machine vision and an evolutionary path optimization method are fused, and accurate recognition of aero-engine crack propagation is achieved.