Preliminary design and analysis of a cubic deployable support structure based on shape memory polymer composite |
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| Authors: | Fengfeng Li Liwu Liu Xin Lan Xiaojun Zhou Wenfeng Bian Yanju Liu |
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| Affiliation: | 1. Department of Astronautical Science and Mechanics, Harbin Institute of Technology (HIT), Harbin, People’s Republic of China;2. Centre for Composite Materials, Science Park of Harbin Institute of Technology (HIT), Harbin, People’s Republic of China;3. Department of Civil Engineering, Harbin Institute of Technology, Weihai, China |
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| Abstract: | The deployable structures based on shape memory polymer composites (SMPCs) have been developed for its unique properties, such as high reliability, low-cost, lightweight, and self-deployment without complex mechanical devices compared with traditional deployable structures. In order to increase the inflatable structure system’s robustness and light the weight of it, a cubic deployable support structure based on SMPC is designed and analyzed preliminarily. The cubic deployable support structure based on SMPC consists of four dependent spatial cages, each spatial cage is composed of 12 three-longeron SMPC truss booms and end connections. The shape recovery of arc-shaped deployable laminates drive the three-longeron SMPC truss booms to unfold, thus realize the expansion of the deployable support structure. The concept and operation of the cubic deployable support structure are described in detail. A series of experiments are performed on the three-longeron deployable laminates unit and the simplified cubic deployable support structure to investigate the shape recovery behavior in the deployment process. Results indicate that the cubic deployable support structure has a high deployment-tgo-stowage volume ratio and can achieve self-deployment, package, and deploy without complex mechanical devices. |
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| Keywords: | Shape memory polymer composites deployable structure shape recovery experiment |
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