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Invited Paper | Open Access

Analytical model for predicting folding stable state of bistable deployable composite boom

Tianwei LIUa,b,c,Jiangbo BAIa,b( )Nicholas FANTUZZIc
School of Transportation Science and Engineering, Beihang University, Beijing 100191, China
Jingdezhen Research Institute of Beihang University, Jingdezhen 333000, China
DICAM Department, University of Bologna, Bologna 40136, Italy

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Bistable Deployable Composite Boom (Bi-DCB) can achieve bistable function by storing and releasing strain energy, which has a good application prospect in space field. For example, it serves as the main support section of deployable structures (e.g., solar arrays and antennas). This paper investigates folding stable state of Bi-DCB through the analytical method. Based on Archimedes’ helix and energy principle, an analytical model for predicting folding stable state of Bi-DCB was presented. The failure index of Bi-DCB in folding stable state were analyzed using the Tsai‐Hill criterion and the maximum stress criterion. Then, a 2400 mm long Bi-DCB was fabricated using autoclave method. The prediction results of the proposed model were compared with experiments and results of two other analytical models. It is shown that the proposed model shows good prediction accuracy. Finally, the effect of geometric parameters on folding stable state of Bi-DCB was further investigated with the aid of the proposed model.

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Chinese Journal of Aeronautics
Pages 460-469
Cite this article:
LIU T, BAI J, FANTUZZI N. Analytical model for predicting folding stable state of bistable deployable composite boom. Chinese Journal of Aeronautics, 2024, 37(8): 460-469. https://doi.org/10.1016/j.cja.2023.05.021

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Received: 18 April 2023
Revised: 08 May 2023
Accepted: 16 May 2023
Published: 27 May 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/).

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