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A topology optimization method based on matlab and cfx joint solution platform

A topology optimization and platform technology, applied in multi-objective optimization, design optimization/simulation, geometric CAD, etc., can solve the problems of slow calculation speed, difficult to use, and inconvenient data transmission, etc., and achieve light weight and small energy dissipation , the effect of reducing the optimization solution time

Active Publication Date: 2021-11-12
SHAANXI AVIATION ELECTRICAL
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Problems solved by technology

[0010] Special software for topology optimization (such as Freefem++, Optistruc, Tosca, etc.) is slow in calculation speed and time-consuming when dealing with complex optimization problems (such as aviation motors), and it is not widely used software, which is not easy to use, and it is not easy to use commonly used software. data transmission
How to solve the fluid topology optimization problem with commonly used software in the aviation field is the starting point for the present invention to consider

Method used

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  • A topology optimization method based on matlab and cfx joint solution platform
  • A topology optimization method based on matlab and cfx joint solution platform
  • A topology optimization method based on matlab and cfx joint solution platform

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Embodiment Construction

[0028] The embodiments of the present invention are described in detail below, and the embodiments are exemplary and intended to explain the present invention, but should not be construed as a limitation of the present invention.

[0029] like figure 1 As shown, when the present invention performs structure and shape optimization, the objective to be optimal is listed as the objective function, and the relevant constraint equation is determined. Matlab first initializes the relevant constraint equation, reads the initial field information without the source term, and performs the Calculation of term coefficients, then Matlab outputs the calculation results of the source term coefficients for the Fortran program to read, and then input them into CFX, then CFX solves the flow field, and outputs the solution results in the required format to the required path, Matlab Read the CFX result file for subsequent objective function calculation, conjugate equation solution, sensitivity a...

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Abstract

The present invention proposes a topology optimization method based on Matlab and CFX joint solution platform, which mainly relies on three parts to realize: (1) Matlab transfers CFX solver to automatically perform fluid simulation calculation; (2) establishes a dynamic link library to make the application program It can call functions that do not belong to its executable code, which solves the problem that the Fortran program cannot be directly recognized by CFX, and the source item information can be smoothly transferred to CFX; (3) Matlab calls the CFX post-processing module to convert the calculation results in the specified format and specified The path is exported for Matlab to read and perform subsequent calculations. The invention combines two commonly used software Matlab and CFX, Matlab performs topology optimization algorithm control, CFX performs flow field solution, and establishes an interface to create a joint solution platform, so that the two can call each other and transfer data, each taking two The director of the software can not only solve multi-objective optimization, but also greatly reduce the optimization solution time.

Description

technical field [0001] The invention belongs to the field of shape optimization and topology optimization, and relates to a novel joint solution platform and a novel shape optimization design method for aero-generators. The platform combines Matlab and CFX to perform mutual calling and data transfer to solve complex shape optimization or multi-objective shape optimization. Optimized design. Background technique [0002] Aeronautical generators have the characteristics of small size, high power density and high speed, and the temperature rises significantly during operation, which directly affects the life of the motor, the safety and reliability of operation. The heat dissipation problem caused by the large unit volume loss and small heat dissipation area of ​​aviation generators often becomes a bottleneck restricting the development of motors. In order to reduce the flow resistance, increase the heat dissipation, and optimize the heat dissipation capacity of the motor, it ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/28G06F30/15G06F113/08G06F111/06
CPCG06F30/15G06F30/20
Inventor 张卓飒刘磊姚勋段晓丽张昌盛
Owner SHAANXI AVIATION ELECTRICAL
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