The application proposes a
turbine blade
precision casting whole process inverse deformation method based on grid nodes, divides the design model into multiple prt files, simultaneously imports HyperMesh, performs Boolean operation on the mutual contact bodies, divides the grid, then imports the
casting special
finite element software ProCAST to perform solidification stage
simulation, then performs de-constraint stage
simulation through extraction mapping operation, sets Vacant to ensure the consistency of the
precision casting process grid nodes, replaces the solidification stage surface grid node P L (x, y, z) with the de-constraint stage deformed grid node P C (x, y, z) into the inverse deformation formula, and obtains the optimized mold cavity data through multiple inverse deformation iterations, which can effectively control the
size change amount of the
turbine blade in the
precision casting process. Compared with the prior art, the application has the advantages that the
turbine blade solidification stage and de-constraint stage, i.e. the
turbine blade precision
casting process, are considered simultaneously, the direct inverse deformation of the two stages of solidification + de-constraint is realized by ensuring the consistency of the nodes, so that the
turbine blade size △D i meets the design requirements △D max , and the blade qualification rate is improved.