Three-dimensional finite element model trimming method capable of embodying manufacture geometric defects

Abstract

The invention belongs to the technical field of the design of the main force-bearing component of an aerospace structure, and relates to a three-dimensional finite element model trimming method capable of embodying manufacture geometric defects. The method comprises the following steps of: 1) adopting an optical measurement method to carry out measurement to obtain three-dimensional point cloud information; 2) carrying out filtering processing on the three-dimensional point cloud information to eliminate noise; 3) establishing a perfect structure three-dimensional finite element model which does not consider the three-dimensional point cloud information; and 4) on the basis of the three-dimensional point cloud information, or after the obtained three-dimensional point cloud information is subjected to amplification and reduction processing, adopting an interpolation method to trim the perfect structure three-dimensional finite element model, and embodying the manufacture geometric defects. By use of the method, the authenticity of a finite element prediction model can be enhanced, furthermore, the accuracy of finite element prediction can be improved, meanwhile, an existing finite element model can be guaranteed to be fully utilized to realize adaptive defect amplitude scaling and position selection, a workload is extremely low, and the method is expected to become one of the key technologies of finite element model correction in an aerospace field.

Description

technical field [0001] The invention belongs to the technical field of design of main load-bearing components of aerospace structures, and relates to a three-dimensional finite element model modification method for the purpose of reflecting manufacturing geometric defects. Background technique [0002] It is well known that axially compressed thin-walled cylindrical shell structures are very sensitive to initial geometrical imperfections. In the 1940s, in the rocket technology research group led by von Karman, Mr. Qian Xuesen’s very important research work was the research on the stability reduction factor of thin-walled light shells, and found that the reduction factor varies with the structure form and size. And change. Generally speaking, the larger the "diameter-thickness ratio" (radius R of the shell divided by the equivalent thickness t of the shell) of the axially compressed shell structure, the higher the defect sensitivity and the smaller the reduction factor. The...

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Problems solved by technology

[0005] The present invention mainly solves the problem that the existing numerical analysis model of the axially compressed grid-reinforced shell structure is difficult to consider the measured manufacturing geometric defects, and proposes a three-dimensional finite element model modification method for the purpose of reflecting the manufacturing geometric defects. On the basis of the element model, through the actual mea...

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