A Method for Optimizing Structural Parameters Based on Sparse Matrix Symbolic Operation Results

A sparse matrix and symbolic operation technology, applied in multi-objective optimization, design optimization/simulation, CAD numerical modeling, etc., can solve the problems of low design efficiency and optimization efficiency, and achieve the effect of improving the efficiency of optimization design

Active Publication Date: 2021-11-19
CHINA AIRPLANT STRENGTH RES INST
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Problems solved by technology

At present, with the improvement of computer hardware technology, finely divided finite element grids are often used for increasingly complex structural design forms. The finite element model of millions of nodes in the design is quite common, and the finite element model of this scale is repeatedly called for optimization. The design efficiency is relatively low
refer to figure 2 , the analysis process in the traditional optimization design is used as a black box call, and the response is obtained by repeatedly calling the solver, and the optimization efficiency is low

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  • A Method for Optimizing Structural Parameters Based on Sparse Matrix Symbolic Operation Results
  • A Method for Optimizing Structural Parameters Based on Sparse Matrix Symbolic Operation Results
  • A Method for Optimizing Structural Parameters Based on Sparse Matrix Symbolic Operation Results

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[0022] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a method for optimizing structural parameters based on sparse matrix symbolic operation results, and belongs to the technical field of aircraft structure strength analysis. The method mainly includes firstly generating the stiffness matrix through the finite element analysis method; secondly, performing matrix transformation on the stiffness matrix with the goal of minimizing the filling element, and establishing a mapping relationship; and then performing numerical decomposition on the right-hand side of the load by using the above transformation , form the triangular decomposition matrix of the sparse matrix of the linear equation system; and use the matrix decomposition results to conduct finite element analysis and perform optimization calculations, and the updated design variables use the above mapping relationship to perform numerical item replacement operations; finally repeat the optimization process until the optimization converges . The present invention makes full use of the result of the first symbolic operation to carry out the numerical decomposition operation, and only one symbolic operation is required in the whole design process. Compared with the traditional design process, the method will shorten the design time by about 50% in theory.

Description

technical field [0001] The invention belongs to the technical field of aircraft structural strength analysis, and in particular relates to a method for optimizing structural parameters based on sparse matrix symbolic operation results. Background technique [0002] In order to complete the research and development design of the structure with high quality under the limited time and funds, it is an inevitable choice to design by means of optimization. Optimal design is increasingly becoming an effective means for people to solve the contradictions of safety, performance, time and cost. After decades of hard work, the development of optimization techniques has made great progress in theory and application. [0003] Due to historical reasons, in the traditional optimization design process, the finite element analyzer is artificially isolated from the optimization process, and the results of the optimizer after numerical optimization must be returned to the analyzer for a comple...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/15G06F30/23G06F111/06
CPCG06F30/15G06F30/23G06F2111/10
Inventor 王立凯聂小华郭瑜超罗利龙张生贵
Owner CHINA AIRPLANT STRENGTH RES INST
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