The application discloses a kind of
composite material curing after re-perforation deformation prediction method, first use three-
dimensional modeling software to establish the finite
element model of not being perforated, and carry out mesh division;Adopt the method of complete
thermal coupling, respectively through calculation to obtain temperature, curing rate, degree of cure, and stress result before demoulding;By converting the boundary condition of finite
element model, through stress calculation method, the
stress distribution result and displacement deformation result of finite
element model after demoulding are recalculated, obtain the
stress distribution result and displacement deformation result after demoulding;Then again mark the area needing to be perforated, and carry out stiffness reduction, release stress, realize the
simulation to be perforated, through stress calculation method, the
stress distribution result and displacement deformation result of finite element model after perforation are recalculated;Export the back result of component after perforation and the result before curing, with the aid of Geomagic
Control software carries out high-precision fitting, obtains the final curing after perforation deformation result.