The Kinematic Analysis and Bistable Characteristics of the Winding Origami Structure

Peng Liu, Jiayao Ma, Yan Chen, Lin Yuan, Haifeng Zhao, Ke Wang
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Abstract

In the military and aerospace fields, bistable structures with adjustable or adaptive stiffness have been widely applied. Origami structures can be used to design bistable systems due to their unique geometrical characteristics. In this paper, we investigate a special design of winding origami, which consists of a square hub in the center and compactly folded panels around it. This delicate design provides the structure a bistable property. According to its motion characteristics, the folding process of the winding origami can be divided into two stages: the mechanism motion stage and the structural deformation stage. The D-H matrix method and truss transformation method were combined to analyze the kinematic relations, and the winding origami pattern was found to have one degree of freedom. At the structural deformation stage, the mechanical response and the local panel deformation were carefully studied via both experiments and finite element simulations, and a reasonable agreement was reached. It was observed that four creases exhibited a non-uniform folding pattern during the deformation process; that is, a portion of the crease was totally flattened while the rest remained folded. The origami structure’s unique kinematic and bistable features could possibly help provide some new ideas in designing a bistable system in the future.
卷绕折纸结构的运动学分析及双稳态特性
在军事和航空航天领域,具有可调或自适应刚度的双稳结构得到了广泛的应用。折纸结构由于其独特的几何特性,可用于设计双稳系统。在本文中,我们研究了一种特殊的卷绕折纸设计,它由中心的方形轮毂和周围紧密折叠的面板组成。这种精巧的设计使结构具有双稳态特性。根据其运动特性,卷绕折纸的折叠过程可分为两个阶段:机构运动阶段和结构变形阶段。结合D-H矩阵法和桁架变换法分析了卷绕折纸图案的运动关系,发现卷绕折纸图案具有一个自由度。在结构变形阶段,通过试验和有限元模拟对结构的力学响应和局部板变形进行了仔细研究,得出了合理的一致结论。观察到,在变形过程中,4条折痕呈现出不均匀的折叠模式;也就是说,折痕的一部分完全变平,而其余部分保持折叠。折纸结构独特的运动学和双稳态特性可能有助于为未来设计双稳态系统提供一些新的思路。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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