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Design of Multi-Mode Morphing Wings Based on Multi-Stable Beam-Type Metastructures

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Intelligent Robotics and Applications (ICIRA 2024)

Part of the book series: Lecture Notes in Computer Science ((LNAI,volume 15201))

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Abstract

The morphing wing can change its shape through mechanism deformation, to improve the aerodynamic performance of the aircraft and save energy. Based on the multi-stable beam-type metastructures, a morphing wing structure with lightweight, large deformation, multiple stable states is designed in this paper. The overall structure can achieve two different deformation modes and maintain the profile shapes without the need for continuous external driving forces. Additionally, carbon-fiber materials are utilized for the flexible skin and actuation of the morphing structure. Finally, a prototype is constructed to demonstrate the multiple morphing modes, thereby validating the feasibility of the proposed structure.

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Disclosure of Interests

The authors have no competing interests to declare that are relevant to the content of this article.

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Acknowledgments

The authors acknowledge the funding support from the National Natural Science Foundation of China No. 52105002 and The Shanghai Pujiang Programme No. 23PJD069.

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Correspondence to Yinjun Zhao .

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Wang, J., Wang, Y., Tian, Y., Hao, G., Xi, F., Zhao, Y. (2025). Design of Multi-Mode Morphing Wings Based on Multi-Stable Beam-Type Metastructures. In: Lan, X., Mei, X., Jiang, C., Zhao, F., Tian, Z. (eds) Intelligent Robotics and Applications. ICIRA 2024. Lecture Notes in Computer Science(), vol 15201. Springer, Singapore. https://doi.org/10.1007/978-981-96-0771-6_11

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  • DOI: https://doi.org/10.1007/978-981-96-0771-6_11

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-96-0770-9

  • Online ISBN: 978-981-96-0771-6

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