The invention discloses a
titanium alloy skin processing compensation method based on a digital twinning
residual stress prediction model, particularly relates to the field of aeronautical manufacturing, and aims to solve the problems that local resilience is difficult to prejudge and a compensation result is unstable due to inconsistent stress
release time sequences and dispersed compensation basis in a
subunit cutting process of a
titanium alloy skin. A unit stress release state is constructed by collecting a unit contour offset and a unit
cutting sequence, same-chain deduction is carried out by combining preorder unit
residual stress mapping to generate a unit compensation candidate quantity, and execution judgment and a closed-loop updating parameter layer are formed based on playback and re-scanning
consistency analysis. According to the method, compensation decision
traceability,
processing deviation convergence and continuous inheritance between working steps are achieved, the manual repeated trial
cutting and parameter adjustment cost is reduced, and the transition smoothness of adjacent units and the forming consistency of the whole
skin are improved.