Static and structural dynamic analysis of thick panel kirigami deployable structures

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-11-19 DOI:10.1016/j.ast.2024.109753
Junlan Li , Cheng Wang , Yucheng Yan , Peng Wang , Jieliang Zhao , Dawei Zhang
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Abstract

Thick panel origami and kirigami concepts have been wildly used to design novel deployable structures in various engineering applications. However, these novel folding methods usually involve complex connected topologies, which may lead to unclear and intricate characterized relationships between system properties and structural parameters, e.g., the position of cutting creases, design parameters and hinge stiffness arrangement, etc. In this paper, we propose theoretical models to describe the static and dynamic properties of thick panel kirigami structure in the fully deployed configuration. Firstly, the connected topology of the origami and kirigami structure is analysed, and the internal coupling topology of the structure is obtained. Based on the compliant matrix method, the static model of the structure is presented, and the different crease cutting modes of origami and kirigami arrays are discussed. Then, the motion modes of slight oscillation of structure are discussed and the structural dynamic model is obtained based on the Lagrange equation and validated by simulation. On this basis, the sensitivity analysis of the parameters is carried out, and the optimization model is given based on the comprehensive performance evaluation function. A physical prototype is optimized and tested, which indicates that our model is valid. This paper provides models for the structural static and dynamic properties of thick panel kirigami structures with complex connected topology, and the findings have a potential to be developed in other thick panel structures with origami and kirigami folding concepts.
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厚板叽里呱啦可展开结构的静态和结构动态分析
厚板折纸和叽里格米概念已被广泛用于设计各种工程应用中的新型可部署结构。然而,这些新颖的折叠方法通常涉及复杂的连接拓扑结构,这可能导致系统特性与结构参数(如裁剪折痕位置、设计参数和铰链刚度布置等)之间的关系不明确且错综复杂。在本文中,我们提出了理论模型来描述厚板叽里咕噜结构在完全展开配置下的静态和动态特性。首先,分析了折纸和叽里格米结构的连接拓扑,得到了结构的内部耦合拓扑。基于顺应矩阵法,提出了结构的静态模型,并讨论了折纸和气泡纸阵列的不同折痕切割模式。然后,讨论了结构轻微摆动的运动模式,基于拉格朗日方程得到了结构动态模型,并通过仿真进行了验证。在此基础上,对参数进行了敏感性分析,并给出了基于综合性能评价函数的优化模型。物理原型经过优化和测试,表明我们的模型是有效的。本文提供了具有复杂连接拓扑结构的厚板叽里格纸结构的静态和动态性能模型,其研究成果有望应用于其他具有折纸和叽里格纸折叠概念的厚板结构。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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