基于Accordion折纸的异形遮光罩薄膜结构设计与分析

doi:10.3901/JME.2025.17.080

机械工程学报 ›› 2025, Vol. 61 ›› Issue (17): 80-89.doi: 10.3901/JME.2025.17.080

• 机器人及机构学 • 上一篇

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基于Accordion折纸的异形遮光罩薄膜结构设计与分析

田大可¹, 薛景赛², 崔锡赫¹, 史创³, 金路⁴, 张立永¹

1. 沈阳建筑大学机械工程学院沈阳 110168;
2. 上海卫星工程研究所上海 201109;
3. 哈尔滨工业大学宇航空间机构全国重点实验室哈尔滨 150001;
4. 沈阳建筑大学土木工程学院沈阳 110168

收稿日期:2024-10-08 修回日期:2025-01-21 发布日期:2025-10-24
作者简介:田大可，男，1981年出生，教授。主要研究方向为宇航空间折展机构、空天变体飞行器、变胞折纸机构。E-mail：tiandake@sjzu.edu.cn;崔锡赫(通信作者)，男，1999年出生，硕士研究生。主要研究方向为空间大型可展开薄膜遮光罩结构设计与分析。E-mail：cuixihe@stu.sjzu.edu.cn
基金资助:
国家自然科学基金联合基金(U2341237)、东北大学航空动力装备振动及控制教育部重点实验室研究基金(VCAME202207)、宇航空间机构全国重点实验室开放课题和辽宁省教育厅基本科研项目(LJ222410153096, JYTMS20231592)资助项目。

Design and Analysis of Membrane Structure for Special-shaped Sunshield Based on Accordion Origami

TIAN Dake¹, XUE Jingsai², CUI Xihe¹, SHI Chuang³, JIN Lu⁴, ZHANG Liyong¹

1. School of Mechanical Engineering, Shenyang Jianzhu University, Shenyang 110168;
2. Shanghai Institute of Satellite Engineering, Shanghai 201109;
3. National Key Laboratory of Aerospace Machanism, Harbin Institute of Technology, Harbin 150001;
4. School of Civil Engineering, Shenyang Jianzhu University, Shenyang 110168

Received:2024-10-08 Revised:2025-01-21 Published:2025-10-24

摘要/Abstract

摘要： 为满足空间光学系统用遮光罩结构大型化、复杂化、高收纳率的发展需求，提出一种大尺度异形可展开遮光罩薄膜结构。首先，根据光学系统遮光要求，研究了可展开遮光罩结构的总体设计方案。其次，基于Accordion(手风琴)折纸原理，开展了遮光罩薄膜结构折叠方案设计，建立了不规则多边形柱状折叠结构参数化数学模型。再次，采用ABAQUS仿真软件建立了薄膜结构展开过程仿真模型，分析了展开过程中应力的变化规律。最后，研制了缩比原理样机，并进行了展开功能试验。仿真及试验结果表明：所设计的遮光罩结构能够顺利完成展开动作，薄膜与可展开支撑机构无干涉，且展开过程无卡顿，薄膜未发生撕裂破坏现象。研究成果可为其他航天器遮光罩结构设计与研究提供一定的借鉴与参考。

关键词: 异形遮光罩, 薄膜结构, Accordion折纸, 展开过程, 结构设计

Abstract: In order to meet the development needs of large-scale, lightweight and high storage rate of space optical system sunshield structure, a large-scale special-shaped deployable sunshield structure is proposed. Firstly, according to the shading requirements of the optical system, the overall design scheme of the deployable sunshield structure is studied. Secondly, based on the Accordion origami principle, the folding scheme design of the membrane structure of sunshield is carried out, and a parametric mathematical model of irregular polygonal columnar folding structure is established. Thirdly, the ABAQUS simulation software is used to establish the simulation model of the membrane structure deployable process, and the variation law of the stress during the deployable process is analyzed. Finally, a scale-down prototype is developed, and the deployment function test is carried out. The simulation and experimental results show that the designed sunshield structure can complete the deployment action successfully, the membrane has no interference with the deployable support mechanism, and there is no jam in the deployable process, and the membrane does not tear. The research results can provide certain reference for the structural design and research of other spacecraft sunshield.

Key words: special-shaped sunshield, membrane structure, Accordion origami, deployable process, structural design

中图分类号:

V443

田大可, 薛景赛, 崔锡赫, 史创, 金路, 张立永. 基于Accordion折纸的异形遮光罩薄膜结构设计与分析[J]. 机械工程学报, 2025, 61(17): 80-89.

TIAN Dake, XUE Jingsai, CUI Xihe, SHI Chuang, JIN Lu, ZHANG Liyong. Design and Analysis of Membrane Structure for Special-shaped Sunshield Based on Accordion Origami[J]. Journal of Mechanical Engineering, 2025, 61(17): 80-89.

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基于Accordion折纸的异形遮光罩薄膜结构设计与分析

Design and Analysis of Membrane Structure for Special-shaped Sunshield Based on Accordion Origami

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