The invention discloses a reverse construction method and
system for a three-dimensional non-axisymmetric parameterized
nacelle model. The method comprises the following steps: extracting two-dimensional section point coordinates from a plurality of key circumferential positions of a target
nacelle; an L-BFGS-B constrained optimization
algorithm is adopted, the minimization of the average square distance between the generated curve and the target point is taken as the target, and iCST parameterization representation of each section is reversely solved; reconstructing a two-dimensional section by using the obtained parameters and keeping the points consistent; based on the characteristic that a fan surface is a rotating surface, moving and aligning all sections to enable radiuses of the fan to be consistent; interpolating the corresponding points among the key sections to generate a
continuous transition section; arranging all sections along the circumferential direction; and finally, on the basis of all section discrete
point data, a smooth and continuous three-dimensional non-axisymmetric
nacelle parameterized model is constructed through a curved surface generation
algorithm, and a general CAD format file can be output. According to the method, the full-parameterized three-dimensional model is automatically reconstructed from two-dimensional information, and the problems of high cost, low efficiency and poor flexibility in the prior art are solved.