填充结构拓扑优化的连续与离散变量法OA
Continuous and discrete variable methods for topology optimization of infill structures
针对填充结构拓扑优化问题,对比研究了连续与离散变量设计方法的性能差异.基于局部体积约束,构建了基于最优准则的固体各向同性材料惩罚模型(solid isotropic material with penalization,SIMP)连续变量优化模型和基于正则松弛算法的序列近似整数规划(sequential approximate integer programming,SAIP)离散变量优化模型.首先,通过理论推导介绍了两类方法应用于填充结构拓扑优化的基本列式.然后,利用数值算例从优化结果的性能、结构拓扑设计的清晰程度和计算效率三方面开展对比研究.最后,通过引入相同初始化策略、移动限制策略与收敛准则,消除算法外因干扰.结果表明,基于SIMP法的优化耗时约为基于SAIP法的50%,但其生成的拓扑设计结构边界存在灰度区域;SAIP法能够获得边界清晰、结构形态更优的拓扑设计,其优化结果目标函数值降低了4.2%.研究结果为填充结构拓扑设计优化提供了理论参考和依据.
The performance differences between continuous and discrete variable design methods for topology optimization of infill structures were investigated.Based on local volume constraints,two optimization models were established:a continuous variable model using the SIMP method with the optimality criterion and a discrete variable model using the SAIP method with the canonical relaxation algorithm.Firstly,the fundamental formulations of these methods for topology optimization of infill structures were derived theoretically.Subsequently,numerical examples were utilized to conduct comparative studies from three aspects:optimization performance,clarity of structural topology design,and computational efficiency.Finally,by implementing identical initialization strategies,move limit strategies,and convergence criteria,the external interference in the algorithm was eliminated.The results demonstrate that the optimization time using the SIMP method is approximately 50%of that using the SAIP method;however,the topological designs generated by SIMP exhibit grayscale regions at structural boundaries.In contrast,the SAIP method yields topological designs with clearer boundaries and superior structural configurations,achieving about a 4%reduction in the objective function value.A theoretical reference and basis for the topology optimization design of infill structures is provided.
兰鹏伟;刘宏亮
沈阳航空航天大学 辽宁省飞行器复合材料结构分析与仿真重点实验室,沈阳 110136沈阳航空航天大学 辽宁省飞行器复合材料结构分析与仿真重点实验室,沈阳 110136||大连理工大学工业装备结构分析优化与CAE软件全国重点实验室,辽宁 大连 116023
航空航天
填充结构拓扑优化固体各向同性材料惩罚模型序列近似整数规划离散变量法正则松弛算法
infill structurestopology optimizationSIMPSAIPdiscrete variable methodcanonical relaxation algorithm
《沈阳航空航天大学学报》 2026 (3)
53-60,8
国家自然科学基金(项目编号:12002218)辽宁省高校基本科研业务费项目(项目编号:LJ212410143080)工业装备结构分析优化与CAE软件全国重点实验室项目(项目编号:GZ22108).
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