• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2024, Vol. 60 ›› Issue (13): 130-140.doi: 10.3901/JME.2024.13.130

• 多学科仿真与优化设计 • 上一篇    下一篇

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考虑惯性载荷的结构热力耦合拓扑优化

郑静1, 荣轩霈1, 姜潮1, 米栋1,2, 李加强2   

  1. 1. 湖南大学特种装备先进设计技术与仿真教育部重点实验室 长沙 410082;
    2. 中国航发湖南动力机械研究所 株洲 412002
  • 收稿日期:2023-10-09 修回日期:2024-01-05 出版日期:2024-07-05 发布日期:2024-08-24
  • 作者简介:郑静,女,1990年出生,博士,助理教授,硕士研究生导师。主要研究方向为结构拓扑优化、可靠性分析与设计。E-mail:jingzheng@hnu.edu.cn;荣轩霈,男,1994年出生,博士研究生。主要研究方向为结构拓扑优化。E-mail:xuanpeirong@hnu.edu.cn;姜潮(通信作者),男,1978年出生,博士,教授,博士研究生导师。主要研究方向为结构优化设计、可靠性分析与设计、结构强度设计。E-mail:jiangc@hnu.edu.cn;米栋,男,1973年出生,硕士,研究员。主要研究方向为结构拓扑优化、结构强度设计。E-mail:capimd@163.com;李加强,男,1993年出生,博士,工程师。主要研究方向为结构拓扑优化、结构强度设计。E-mail:lijq20@tsinghua.org.cn
  • 基金资助:
    国家自然科学基金资助项目(52005172,52235005)。

Thermal-mechanical Coupled Topology Optimization for Structures with Inertial Loads

ZHENG Jing1, RONG Xuanpei1, JIANG Chao1, MI Dong1,2, LI Jiaqiang2   

  1. 1. Key Laboratory of Advanced Design and Simulation Techniques for Special Equipment of Ministry of Education, Hunan University, Changsha 410082;
    2. AECC Hunan Aviation Powerplant Research Institute, Zhuzhou 412002
  • Received:2023-10-09 Revised:2024-01-05 Online:2024-07-05 Published:2024-08-24

摘要: 现代复杂装备结构通常不仅处于热力耦合的复杂环境,而且承受着不可忽视的惯性力作用。针对这一类问题,提出了一种考虑拓扑相关惯性载荷的热力耦合拓扑优化高效求解方法。首先,构建了考虑热载荷、机械载荷以及惯性载荷的热力耦合拓扑优化模型,在体积约束条件下优化结构的柔顺度;其次,给出了惯性载荷的计算方法,针对低密度区域材料分布不收敛的问题提出了一种改进的材料插值惩罚模型,并基于此推导了结构柔顺度关于拓扑设计变量的敏度;最后,采用了基于梯度的移动渐近线法(Method of moving asymptotes, MMA)更新拓扑设计变量。此外,开发了基于MATLAB和ABAQUS的热力耦合拓扑优化平台,可适用于复杂工程中不规则结构设计域的拓扑优化问题。数值算例结果表明,所提出方法可有效避免低密度区域结构分布模糊的现象,具有良好的收敛性。

关键词: 拓扑优化, 热力耦合, 惯性载荷

Abstract: Modern complex equipment structures are usually not only in a complex environment of thermal-mechanical coupling, but also subject to inertial forces that cannot be ignored. A high-efficiency solution method for thermoelastic topology optimization considering topology related inertial loads is proposed for this type of problem. First, a thermoelastic topology optimization model considering thermal, mechanical, and inertial loads is constructed to optimize the compliance of the structure under volume constraints; Secondly, a calculation method for inertial loads is provided, and an improved material interpolation penalty model is proposed to address the issue of non-convergence of material distribution in low density areas. Based on this, the sensitivity of structural compliance to topological variables is derived. Finally, the gradient based Method of Moving Asymptotes is used to update the topology design variables. In addition, a thermal coupling topology optimization platform based on MATLAB and ABAQUS has been developed, which can be applied to topology optimization problems of irregular structural design domains in complex engineering. The numerical example results show that the proposed method can effectively avoid the phenomenon of fuzzy structural distribution in low density areas and has good convergence.

Key words: topology optimization, thermal-mechanical coupled, inertial load

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