4.3 Article Proceedings Paper

New Approach to Folding a Thin-Walled Yoshimura Patterned Cylinder

Journal

JOURNAL OF SPACECRAFT AND ROCKETS
Volume 58, Issue 2, Pages 516-530

Publisher

AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.A34784

Keywords

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Funding

  1. Space Core Technology Development Program [NRF-2018M1A3A3A02065888]
  2. High Potential Individuals Global Training Program [2019-001598]
  3. Korean government (Ministry of Science and ICT)

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A new folding approach for the Yoshimura cylinder is proposed in this study, utilizing a mathematical problem and three governing equations to determine a special folding pattern. The proposed folding methodology achieves more efficient folding with no wrinkles in the fully folded state, compared to conventional approaches.
A new approach for folding the Yoshimura cylinder is proposed in this study. The proposed concept is based on a reconfiguration process involving a cylindrical structure with the Yoshimura pattern and the bellows fold pattern. Static analyses are conducted to confirm the effectiveness of the proposed folding methodology. A special case of folding is observed that does not create wrinkles in the fully folded state. A mathematical problem is established and three governing equations are derived from the problem. The special folding pattern is determined by solving the three governing equations. The most geometrically and structurally efficient configuration for the reconfigured cylinder is determined. A geometrical analysis is conducted for various configurations of the cylinder that can be observed in the proposed folding methodology. The proposed folding methodology folds the Yoshimura cylinder much more efficiently in terms of required force and stress compared to the conventional folding approach.

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