中国航空学报(英文版)2024,Vol.37Issue(6) :425-438.DOI:10.1016/j.cja.2023.10.004

A flat-foldable equiangular spiral folding pattern inspired by sunflowers for deployable structures

Shuangqing YU Jinguo LIU Pengyuan ZHAO Yingying TANG
中国航空学报(英文版)2024,Vol.37Issue(6) :425-438.DOI:10.1016/j.cja.2023.10.004

A flat-foldable equiangular spiral folding pattern inspired by sunflowers for deployable structures

Shuangqing YU 1Jinguo LIU 2Pengyuan ZHAO 1Yingying TANG1
扫码查看

作者信息

  • 1. State Key Laboratory of Robotics,Shenyang Institute of Automation,Chinese Academy of Sciences,Shenyang 110016,China;Institutes for Robotics and Intelligent Manufacturing,Chinese Academy of Sciences,Shenyang 110169,China;University of Chinese Academy of Sciences,Beijing 100049,China
  • 2. State Key Laboratory of Robotics,Shenyang Institute of Automation,Chinese Academy of Sciences,Shenyang 110016,China;Institutes for Robotics and Intelligent Manufacturing,Chinese Academy of Sciences,Shenyang 110169,China
  • 折叠

Abstract

Flasher origami pattern has been widely utilized to improve the stowage efficiency of deployable structures.Nevertheless,flasher origami cannot be folded fully flat,and they still have great potential for optimization in terms of storage volume and folding creases.In this paper,a flat foldable equiangular spiral folding pattern inspired by the sunflower disk is introduced.Then,a parametric design method for this equiangular spiral crease diagram is introduced in detail.Subse-quently,a kinematic model of the equiangular spiral folding pattern is established based on the kinematic equivalence between rigid origami and spherical linkages.A simulation of the developed model demonstrates that the equiangular spiral folding pattern can be folded flat.Using the folded ratio as an evaluation index,the calculated results and experiments show that the equiangular spiral crease pattern can yield fewer creases and improve stowage efficiency in comparison to flasher ori-gami pattern.Equiangular spiral folding pattern can save a considerable amount of space and pro-vide a new approach to spatially deployable structures.

Key words

Flasher origami/Sunflower-inspired/Deployable structures/Flat-foldability/Equiangular spiral folding pattern

引用本文复制引用

基金项目

National Key R&D Program of China(2018YFB1304600)

CAS Interdisciplinary Innovation Team(JCTD-2018-11)

Natural Science Foundation of China(51775541)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量3
段落导航相关论文