A comprehensive study of a new cylindrical flexible Miura-Ori origami: Kinematics, FEA, and fatigue assessments

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-09-30 DOI:10.1016/j.ast.2024.109620
Hadi Ebrahimi Fakhari , Habib Eslami , Mojtaba Moshtaghzadeh , Pezhman Mardanpour
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Abstract

In this paper, we introduced a new cylindrical flexible structure incorporating a multi-story origami based on the Miura-Ori pattern and mathematized kinematics. Our experiments validated the finite element simulations as well as the feasibility of the kinematics. We developed a fabrication technique and made a sample to study the feasibility and applicability of the designed structure. Subsequently, we set up a finite element simulation that mirrors the prepared sample. A series of axial folding experiments were carried out to validate the FEM simulation. We have also derived kinematic formulations relating the structure's height, folding angle, and radius. To model and analyze the folding and unfolding mechanisms of this innovative structure, we employed Finite Element Analysis (FEA). In our study, we investigate four main geometric parameters that significantly influence our design's characteristics: crease thickness, number of stories, crease width, and number of vertexes in one story. By varying these design parameters, we systematically examine their impact on key structural attributes such as fatigue life, folding force, and energy absorption. Our findings indicate that reduced crease thickness correlates with lower von-Mises stress and strain, significantly extending the origami design's lifespan. Through our analysis, we identify specific parameter values that maximize fatigue life, ensuring the structural integrity and longevity of the design. Our findings show that increasing the crease width extends the fatigue life dramatically. In conclusion, we summarize the influence of each design parameter on the structure's behavioral characteristics in a comprehensive approach.
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新型圆柱形柔性三浦奥里折纸的综合研究:运动学、有限元分析和疲劳评估
在本文中,我们介绍了一种新型圆柱形柔性结构,它结合了基于三浦-奥里模式的多层折纸和数学化运动学。我们的实验验证了有限元模拟以及运动学的可行性。我们开发了一种制作技术,并制作了一个样品来研究设计结构的可行性和适用性。随后,我们建立了一个与制备的样品相匹配的有限元模拟。为了验证有限元模拟,我们进行了一系列轴向折叠实验。我们还推导出了与结构高度、折叠角度和半径相关的运动学公式。为了模拟和分析这种创新结构的折叠和展开机制,我们采用了有限元分析法(FEA)。在研究中,我们调查了对设计特性有重大影响的四个主要几何参数:折痕厚度、层数、折痕宽度和一层中的顶点数量。通过改变这些设计参数,我们系统地研究了它们对疲劳寿命、折叠力和能量吸收等关键结构属性的影响。我们的研究结果表明,折痕厚度的减少与较低的 von-Mises 应力和应变相关,从而大大延长了折纸设计的使用寿命。通过分析,我们确定了能最大限度延长疲劳寿命的特定参数值,从而确保了设计的结构完整性和使用寿命。我们的研究结果表明,增加折痕宽度可显著延长疲劳寿命。最后,我们总结了每个设计参数对结构行为特征的影响,并提出了一种全面的方法。
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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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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