中国航空学报(英文版)2024,Vol.37Issue(8) :460-469.DOI:10.1016/j.cja.2023.05.021

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

Tianwei LIU Jiangbo BAI Nicholas FANTUZZI
中国航空学报(英文版)2024,Vol.37Issue(8) :460-469.DOI:10.1016/j.cja.2023.05.021

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

Tianwei LIU 1Jiangbo BAI 2Nicholas FANTUZZI3
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作者信息

  • 1. 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
  • 2. School of Transportation Science and Engineering,Beihang University,Beijing 100191,China;Jingdezhen Research Institute of Beihang University,Jingdezhen 333000,China
  • 3. DICAM Department,University of Bologna,Bologna 40136,Italy
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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 Archi-medes'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 predic-tion accuracy.Finally,the effect of geometric parameters on folding stable state of Bi-DCB was fur-ther investigated with the aid of the proposed model.

Key words

Bistable/Deployable composite boom/Solar arrays/Antennas/Archimedes'helix/Folding/Failure analysis

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基金项目

National Natural Science Foundation of China(52275231)

National Defense Basic Scientific Research Program of China(JCKY2019205C002)

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
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