Rhombic Bistable Composites with Integrated Pneumatic Actuation and Cylindrical Curved Shapes

This study proposes a novel pneumatically driven mechanically prestressed rhombic bistable composite laminate with asymmetric cylindrical curvature, which exhibits two weakly-coupled cylindrical shapes where each shape is influenced by planform and geometry parameters. A reduced-order analytical model is developed to predict the laminate’s quasi-static equilibrium shapes and snap-through transitions of the laminate under pneumatic work loading, which is triggered by the internal pressure applied to the fluidic channels. A sensitivity study based on the model investigates the influence of key planform and geometric parameters (the internal angle α and aspect ratio E) on the laminate’s out-of-plane deflection and snap-through pressure. The results show that increasing α reduces the critical prestrain required to achieve bistability and amplifies the out-of-plane deflection, while excessive α may lead to monostable curvature. Variations in aspect ratio modify the coupling stiffness between orthogonal PEMC layers, thereby influencing the bistable domain and critical snap-through pressure. These findings provide methods for the design of bistable composite structures.

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Publication Details

Journal
Journal of Composites Science
Published
2026-04-27
DOI
https://doi.org/10.3390/jcs10050234
Primary Topic
Aeroelasticity and Vibration Control
Type
article
Field-Weighted Citation Impact
0.00

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article

Rhombic Bistable Composites with Integrated Pneumatic Actuation and Cylindrical Curved Shapes

Tao Tao, Qicai Ren, Xinran Guo, Jiaqiao Liang et al.
Journal of Composites Science
Aeroelasticity and Vibration Control
article

Rhombic Bistable Composites with Integrated Pneumatic Actuation and Cylindrical Curved Shapes

Tao Tao, Qicai Ren, Xinran Guo, Jiaqiao Liang, Shi Liu, Zefeng Xu, Peiyu Liu, Yi Yang, Yitong Zhou
article en

Abstract

This study proposes a novel pneumatically driven mechanically prestressed rhombic bistable composite laminate with asymmetric cylindrical curvature, which exhibits two weakly-coupled cylindrical shapes where each shape is influenced by planform and geometry parameters. A reduced-order analytical model is developed to predict the laminate’s quasi-static equilibrium shapes and snap-through transitions of the laminate under pneumatic work loading, which is triggered by the internal pressure applied to the fluidic channels. A sensitivity study based on the model investigates the influence of key planform and geometric parameters (the internal angle α and aspect ratio E) on the laminate’s out-of-plane deflection and snap-through pressure. The results show that increasing α reduces the critical prestrain required to achieve bistability and amplifies the out-of-plane deflection, while excessive α may lead to monostable curvature. Variations in aspect ratio modify the coupling stiffness between orthogonal PEMC layers, thereby influencing the bistable domain and critical snap-through pressure. These findings provide methods for the design of bistable composite structures.

Journal of Composites ScienceVol. 10(5)
China Southern Power Grid (China) (CN), South China University of Technology (CN)
China Postdoctoral Science Foundation, China Southern Power Grid, National Key Research and Development Program of China
Sustainable cities and communities
Openalex Percentile: Top 2%
Aeroelasticity and Vibration Control
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