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Full Length Article | Open Access

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

Shuangqing YUa,b,c, Jinguo LIUa,b( ), Pengyuan ZHAOa,b,c, Yingying TANGa,b,c
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

Peer review under responsibility of Editorial Committee of CJA.

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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. Subsequently, 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 origami pattern. Equiangular spiral folding pattern can save a considerable amount of space and provide a new approach to spatially deployable structures.

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Chinese Journal of Aeronautics
Pages 425-438

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Cite this article:
YU S, LIU J, ZHAO P, et al. A flat-foldable equiangular spiral folding pattern inspired by sunflowers for deployable structures. Chinese Journal of Aeronautics, 2024, 37(6): 425-438. https://doi.org/10.1016/j.cja.2023.10.004

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Received: 05 June 2023
Revised: 14 July 2023
Accepted: 08 September 2023
Published: 11 October 2023
© 2023 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).