多约束的桥梁结构拓扑优化

基于ESO (Evolutionary Structural Optimization)的拓扑优化方法,本文提出了一种适应于桥梁结构的拓扑优化方法。引进了两种性能指标公式来确定最佳拓扑设计。另外,为了更有效地尝试改进最终设计的细节,而又不进行更精细有限元网格的完整分析,这里提出了一种精细网络设计方案。再者,结合细啃技术,完成了考虑应力、位移、频率约束的斜拉桥优化设计。通过几种桥梁的设计优化,表明该方法的可应用性、简洁性和有效性。     

基于改进渐进结构优化方法的结构动力优化研究

在对渐进结构优化方法基本理论分析基础上,根据结构动力学的拓扑优化特点,结合尺寸优化理论,提出了一种新的删除准则。探索了一种改进型渐进结构优化方法,并叙述基本的优化步骤。最后,融入了质量、应力、位移以及频率等动力学约束条件参数,运用该方法进行谐激励力作用下的板结构动力响应拓扑优化。算例表明,改进渐进结构优化方法对结构动力学拓扑优化问题具有一定的适用性,拓展了基本渐进结构优化方法的应用范围。     

一种变频率约束限的结构拓扑优化方法

针对仅频率约束和重量最小的结构拓扑优化问题,基于ICM(独立、连续、映射)方法和渐进结构优化方法的思路,提出了一种变频率约束限的结构拓扑优化方法.在优化迭代循环的每一轮子循环迭代求解开始时,为了控制拓扑设计变量的变化量,依据结构频率和其约束限,形成和引进了新的频率约束限.另外,建立了单元删除阈值和几轮迭代循环的单元删除策略.为了确保优化迭代中结构非奇异和方法具有增添单元的功能,在结构孔洞和边界周围引入了一层人工材料单元.结合拉格朗日乘子法,形成了一种新的连续体结构的拓扑优化方法.给出的算例表明该方法没有目标函数的振荡现象,且验证了该方法的正确性和有效性.     

基于种群动力学模型的连续体结构拓扑优化仿生方法

通过种群动力学模型和有限元方法的耦合建立了骨骼重建数学模型,然后用像素单元的添加和删除准则把骨重建过程转化为材料形成和吸收过程,对连续体结构提出了仿生拓扑优化计算方法。通过对两个连续体结构拓扑优化中被广泛应用的典型数值算例进行拓扑优化计算,并将其结果与其它几种拓扑优化方法进行比较,验证了该方法的有效性。最终在三种不同边界条件下对长悬臂梁模型进行拓扑优化计算,以及在四种不同边界条件下拱桥模型进行拓扑优化计算,获得规则性和对称性的拓扑形式,该结果进一步说明了该仿生方法的合理性和可行性。     

一种包装堆垛机械手的结构优化

目的应用Ansys Workbench软件对一种包装堆垛机械手的结构进行优化,减少结构质量,提高机械手的工作效率和定位精度。方法对机械手进行建模及使用应力分析软件对其进行静力分析、模态分析,并利用拓扑优化方法的变密度法,对机械手结构的关键部位进行拓扑优化。结果机械手在满足整体强度的条件下,改变其质量分布,选择合理的驱动电机,达到减弱振动和轻量化的成效。结论拓扑优化方法的变密度法为机械手的结构优化和提高执行工作频率提供了一种高效可行的途径。     

胶印机滚筒结构的拓扑及尺寸优化设计

胶印机滚筒在印刷压力作用下的挠曲变形是影响印品质量的重要原因。以PZ1740胶印机橡皮滚筒为研究对象,提出了一种基于拓扑优化和尺寸优化的橡皮滚筒结构设计方法。建立了滚筒结构的二维拓扑模型,以应变能最小为目标,体积分数作为约束,得到滚筒结构的拓扑分布;在拓扑构型基础上,建立了滚筒结构的参数化模型,以挠曲变形最小为目标,结构质量作为约束条件进行尺寸优化,得到了滚筒具体的结构。优化分析结果表明,优化后的滚筒结构在质量约束的条件下有效地减小了挠曲变形,提出的方法在胶印机滚筒结构优化设计中可行且有效。     

几何非线性臂架结构稳定拓扑优化

臂架结构是臂架起重机的关键部件,实现结构稳定的拓扑优化对其轻量化设计至关重要。基于敏度分析的结构优化方法耗时耗力,不适用于大型工程结构。在杆系结构SKO （soft kill option）法的基础上,定义了臂架结构整体稳定性和局部压杆稳定性的定量化指标,分析臂架结构抗失稳机制,给出了关联腹杆“冻结”顺序,提出了一种保证结构稳定的臂架结构拓扑优化方法,即SSKO （stability-ensured soft kill option）法。将该方法应用于刚架柱和环轨起重机组合臂架的拓扑优化中,结果表明SSKO法可实现结构的稳定拓扑,优化速度快,效果显著。     

基于映射的拓扑优化最大尺寸控制方法

拓扑优化方法经过几十年的发展,已成功应用于机械工程、航空航天、电磁等领域的构型设计中。然而,由于制造工艺的限制,拓扑优化结果通常无法直接应用,需根据工艺要求进行修改,因此在拓扑优化模型中考虑制造约束成为重要的研究方向。其中,尺寸控制广泛存在于大部分制造工艺中,主要包括最小尺寸控制与最大尺寸控制。该文提出了一种基于映射的拓扑优化最大尺寸控制方法,构造了一种新的映射模型,对结构中不满足最大尺寸约束的中心单元密度进行惩罚,在不引入任何约束条件的情况下实现了对结构最大尺寸的控制。此外,该文将该方法中的惩罚转变为一个全局约束条件后与具有最小尺寸控制功能的拓扑优化鲁棒列式相结合,实现了对构件的最大最小尺寸协同控制。数值算例表明了该方法的有效性。     

一种基于非概率可靠性的结构水平集拓扑优化

该文在研究水平集拓扑优化方法的基础上,对具有区间参数的不确定性结构的非概率可靠性约束进行了分析,经对有限元公式的推导、变换,提出了包涵非概率可靠度信息的拟安全系数形式,从而将非概率可靠性约束问题显式化处理,使得优化过程形式简单、便于计算,避免了复杂的迭代运算。通过对算例中数据及拓扑图形的对比研究,表明该文中模型的合理性和方法的有效性。     

基于ICM法的高层建筑大型支撑体系拓扑优化

提出应用连续体结构拓扑优化ICM法对高层建筑大型支撑体系进行拓扑优化。针对高层建筑规范对结构刚度限值是以层间相对位移差形式给出、并结合结构拓扑优化特点,推导了相对位移差敏度分析的伴随法公式,有效提高了计算效率。应用ICM法建立位移约束下结构重量极小化的优化模型,与高层建筑规范对结构刚度限值要求的提法更符合,得到的最优拓扑完全满足规范要求。所提方法应用在概念设计阶段,提供了一种自动化的分析计算及优化设计工具,可以有效地弥补基于经验设计的不足。     

考虑位移要求的大型三维连续体结构拓扑优化数值技术研究

大型复杂三维结构拓扑优化设计既具有理论意义,又具有重要的应用价值。基于等效转换的非奇异的结构优化模型,研究结构位移要求的最小结构重量设计问题。首先,介绍了位移约束的三维结构优化准则和公式。而后,为了提高拥有数万个单元以上的三维结构的计算效率,结合结构位移计算的迭代方法,在分析用于结构特性参数计算模型的基础上,建立了一套三维结构拓扑优化的求解策略和算法。最后,给出了几个典型和复杂的三维结构的拓扑优化设计算例。算例表明求解策略和算法是正确和有效的,且具有广泛的工程应用前景。     

Topology optimization of energy absorbing structures with maximum damage constraint

A novel density‐based topology optimization framework for plastic energy absorbing structural designs with maximum damage constraint is proposed. This framework enables topologies to absorb large amount of energy via plastic work before failure occurs. To account for the plasticity and damage during the energy absorption, a coupled elastoplastic ductile damage model is incorporated with topology optimization. Appropriate material interpolation schemes are proposed to relax the damage in the low‐density regions while still ensuring the convergence of Newton‐Raphson solution process in the nonlinear finite element analyses. An effective method for obtaining path‐dependent sensitivities of the plastic work and maximum damage via adjoint method is presented, and the sensitivities are verified by the central difference method. The effectiveness of the proposed methodology is demonstrated through a series of numerical examples. Copyright © 2017 John Wiley & Sons, Ltd.     

Topology optimization of geometrically nonlinear structures using an evolutionary optimization method

The topology optimization using isolines/isosurfaces and extended finite element method (Iso-XFEM) is an evolutionary optimization method developed in previous studies to enable the generation of high-resolution topology optimized designs suitable for additive manufacture. Conventional approaches for topology optimization require additional post-processing after optimization to generate a manufacturable topology with clearly defined smooth boundaries. Iso-XFEM aims to eliminate this time-consuming post-processing stage by defining the boundaries using isovalues of a structural performance criterion and an extended finite element method (XFEM) scheme. In this article, the Iso-XFEM method is further developed to enable the topology optimization of geometrically nonlinear structures undergoing large deformations. This is achieved by implementing a total Lagrangian finite element formulation and defining a structural performance criterion appropriate for the objective function of the optimization problem. The Iso-XFEM solutions for geometrically nonlinear test cases implementing linear and nonlinear modelling are compared, and the suitability of nonlinear modelling for the topology optimization of geometrically nonlinear structures is investigated.     

Nonlinear response topology optimization using equivalent static loads—case studies

Nonlinear structural optimization is fairly expensive and difficult, because a large number of nonlinear analyses is required due to the large number of design variables involved in topology optimization. In element density based topology optimization, the low density elements create mesh distortion and the updating of finite element material with low density elements has a severe effect on the optimization results in the next cycles. In order to overcome these difficulties, the equivalent static loads method for nonlinear response structural optimization (ESLSO) primarily used for size and shape optimization has been applied to topology optimization. The nonlinear analysis is performed with the given loading conditions to calculate equivalent static loads (ESLs) and these ESLs are used to perform linear response optimization. In this paper, the authors have presented the results of five case studies with material, geometric and contact nonlinearities showing good agreement and providing justification of the proposed method.     

基于应变能的预应力平面实体结构拓扑优化设计

研究了预应力平面实体钢结构拓扑优化设计问题。建立了以索力值和结构拓扑为设计变量,以结构储存应变能为约束条件,以结构重量最小为目标函数的数学优化模型。在求解方法上,首先以结构储存应变能最小(刚度最大)确定施加在结构上的索力值,然后采用渐进结构优化法(ESO方法)删除低应变能的单元实现结构的拓扑优化并减轻结构重量。算例结果与相应体系受力性能的结论相吻合,表明本文所提出的优化方法是可行的。     

A scaled boundary finite element based explicit topology optimization approach for three-dimensional structures

This article proposes an efficient approach for solving three-dimensional (3D) topology optimization problem. In this approach, the number of design variables in optimization as well as the number of degrees of freedom in structural response analysis can be reduced significantly. This is accomplished through the use of scaled boundary finite element method (SBFEM) for structural analysis under the moving morphable component (MMC)-based topology optimization framework. In the proposed method, accurate response analysis in the boundary region dictates the accuracy of the entire analysis. In this regard, an adaptive refinement scheme is developed where the refined mesh is only used in the boundary region while relating coarse mesh is used away from the boundary. Numerical examples demonstrate that the computational efficiency of 3D topology optimization can be improved effectively by the proposed approach.     

Microstructural topology optimization for minimizing the sound pressure level of structural–acoustic coupled systems with multi-scale random parameters

The main aim of this article is to present a robust microstructural topology optimization methodology for structural–acoustic coupled systems with multi-scale random parameters. During the microstructural topology optimization, both the uncertainty at the macro-scale, which comes from the physical parameters of the acoustic medium or the external load, and the uncertainty existing in the constituent material properties of the microstructure at the micro-scale are considered as random parameters. A homogenization-based probabilistic finite element method (HPFEM) is first developed for quantifying the structural–acoustic system with multi-scale random parameters. The use of the HPFEM transforms the problem of microstructural topology optimization with multi-scale random parameters to an augmented deterministic microstructural topology optimization problem. This provides a computationally cheap alternative to Monte Carlo-based optimization algorithms. A numerical example of a hexahedral box is given to demonstrate the efficiency of the proposed method.     

Simultaneous partial topology and size optimization of a wing structure using ant colony and gradient based methods

This article presents a methodology and process for a combined wing configuration partial topology and structure size optimization. It is aimed at achieving a minimum structural weight by optimizing the structure layout and structural component size simultaneously. This design optimization process contains two types of design variables and hence was divided into two sub-problems. One is structure layout topology to obtain an optimal number and location of spars with discrete integer design variables. Another is component size optimization with continuous design variables in the structure FE model. A multi city-layer ant colony optimization (MCLACO) method is proposed and applied to the topology sub-problem. A gradient based optimization method (GBOM) built in the MSC.NASTRAN SOL-200 module was employed in the component size optimization sub-problem. For each selected layout of the wing structure, a size optimization process is performed to obtain the optimum result and feedback to the layout topology process. The numerical example shows that the proposed MCLACO method and a combination with the GBOM are effective for solving such a wing structure optimization problem. The results also indicate that significant structural weight saving can be achieved.