The invention belongs to the related technical field of aero-engine manufacturing and precision repair, and discloses a blade repair path follow-up compensation method and device based on non-rigid matching, and the method comprises the steps: S1, reconstructing a
machining error reference
point cloud curved surface based on a scanning
data point set and a repair region design model; s2, performing unified modeling on the static deviation of the
machining error of the to-be-compensated blade to obtain an error
transfer model, and simplifying the corresponding nonlinear comprehensive
machining error into a calculation equation of linear
pose deviation of a local workpiece coordinate
system; s3, establishing a tangent contact approximation cost function based on non-rigid matching so as to register and approach a target curved surface under the constraint of retaining
tool path features, and meanwhile, solving a calculation equation by adopting a least square method so as to obtain a linear
pose deviation of a local workpiece coordinate
system, solving to obtain a
pose deviation of each tangent contact coordinate
system so as to obtain a linear pose deviation of each tangent contact coordinate system; and furthermore, each
cutting contact and each
cutter location point are updated, and the shape follow-up compensation of the blade is realized. The compensation precision is improved.