1. 北京航空航天大学,北京,100191
2. 中国航天科技体系与创新研究院,北京,100088
纸质出版:2026
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郭祥宇, 朱楠, 徐元铭, 等. 离散组装力学超结构的晶格融合设计及性能调控研究[J]. 航空制造技术, 2026,69(1/2).
GUO Xiangyu, ZHU Nan, XU Yuanming, et al. Hybrid Design and Performance Modulation of Discrete-Assembled Mechanical Metastructures[J]. Aeronautical Manufacturing Technology, 2026, 69(1/2).
郭祥宇, 朱楠, 徐元铭, 等. 离散组装力学超结构的晶格融合设计及性能调控研究[J]. 航空制造技术, 2026,69(1/2). DOI: 10.16080/j.issn1671-833x.25010153.
GUO Xiangyu, ZHU Nan, XU Yuanming, et al. Hybrid Design and Performance Modulation of Discrete-Assembled Mechanical Metastructures[J]. Aeronautical Manufacturing Technology, 2026, 69(1/2). DOI: 10.16080/j.issn1671-833x.25010153.
力学超结构凭借其优异的力学性能,在航空航天等领域应用前景广阔。然而,当前力学超结构的制备普遍依赖于增材制造技术,导致其性能固化、调控手段受限。为解决这些问题,本文提出一种基于L 形组件的可编程离散组装方法。该组件具备几何兼容特性,通过改变空间排布,可实现Octet、FCC、Cuboctahedra 3 类典型晶格的通用组装与拓扑互换,突破传统组装方法构型单一的限制。制备上采用3D打印与机械连接相结合的混合工艺,实现了无支撑打印,同时兼顾高制备效率与低成本效益。本研究通过有限元仿真系统探究了3 类离散组装超结构的力学特性,明确了晶格拓扑与刚度、强度及能量吸收性能的内在关联;进一步提出软– 硬层混杂与局部硬化两种性能调控策略,并深入分析了不同杂化布局对力学特性的影响。本研究为超结构力学性能调控提供了新路径,有望为航空航天等领 域大尺度结构的性能定制与轻量化设计提供新思路。
Mechanical metastructures
owing to their exceptional mechanical performance and structural adaptability
have shown broad application potential in fields such as aerospace and advanced engineering. However
most existing metastructures are fabricated using additive manufacturing (AM)
which often results in fixed mechanical properties and limited tunability. To overcome these limitations
this study proposes a programmable discrete assembly approach based on L-shaped modular elements. The proposed module exhibits geometric compatibility
allowing the construction and topological transformation of three representative lattice architectures—Octet
FCC
and Cuboctahedra—through variations in spatial configuration
thereby overcoming the structural singularity inherent in conventional assembly methods. A hybrid fabrication process combining 3D printing and mechanical fastening was adopted
achieving support-free printing while maintaining high fabrication efficiency and cost-effectiveness for metastructures. Finite element simulations were employed to systematically investigate the mechanical responses of the three discretely assembled lattices
elucidating the intrinsic relationships between lattice topology
stiffness
strength
and energy absorption characteristics. Furthermore
two performance modulation strategies—soft-hard layered hybridization and local lattice hardening—were proposed to enable programmable control of global and local mechanical properties. This study establishes a new design framework for tunable mechanical metastructures
providing an effective pathway for customized performance and lightweight design in large-scale aerospace and multifunctional structural applications.
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