Large-Scale Three-Dimensional Anisotropic Topology Optimization of Variable-Axial Composite Structures

Yuqing Zhou, T. Nomura, Enpei Zhao, Wei Zhang, K. Saitou
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Abstract

Variable-axial fiber-reinforced composites allow for local customization of fiber orientation and thicknesses. Despite their significant potential for performance improvement over the conventional multiaxial composites and metals, they pose challenges in design optimization due to the vastly increased design freedom in material orientations. This paper presents an anisotropic topology optimization (TO) method for designing large-scale, 3D variable-axial composite structures. The computational challenge for large-scale 3D TO with extremely low volume fraction is addressed by a tensor-based representation of 3D orientation that would avoid the 2π periodicity of angular representation such as Eular angles, and an adaptive meshing scheme, which, in conjunction with PDE regularization of the density variables, refines the mesh where structural members appear and coarsens where there is void. The proposed method is applied to designing a heavy-duty drone frame subject to complex multi-loading conditions. Finally, the manufacturability gaps between the optimized design and the fabrication-ready design for Tailored Fiber Placement (TFP) is discussed, which motivates future work toward fully-automated design synthesis.
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变轴复合材料结构的大尺度三维各向异性拓扑优化
可变轴向纤维增强复合材料允许纤维取向和厚度的局部定制。尽管与传统的多轴复合材料和金属相比,它们具有显著的性能改进潜力,但由于材料取向的设计自由度大大增加,它们在设计优化方面提出了挑战。提出了一种设计大型三维变轴复合材料结构的各向异性拓扑优化方法。对于具有极低体积分数的大规模3D TO的计算挑战是通过基于张量的3D方向表示来解决的,该表示可以避免角表示(如欧拉角)的2π周期性,以及自适应网格划分方案,该方案与密度变量的PDE正则化相结合,可以细化出现结构成员的网格,并粗糙存在空隙的网格。将该方法应用于复杂多载荷条件下的重型无人机框架设计。最后,讨论了定制纤维放置(TFP)的优化设计与制造就绪设计之间的可制造性差距,这激励了未来全自动设计综合的工作。
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