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用于航空航天技术的浮力膜结构的机械性质分析
Shuhong Xu1, Xiaojiao Yu2, Yue Gao2
1School of Engineering, Applied Technology Collage of Soochow University, Suzhou 215325, China.
Materials (Basel, Switzerland)
|July 13, 2024
概括
由纤维增强聚合物复合材料制成的新的可折叠带弹杆提供了改进的可部署空间结构. 这项研究分析了它们的特性,并为太阳能电池组等大型航天器应用提供了设计指南.
科学领域:
- 航空航天工程 航空航天工程
- 材料科学 材料科学 材料科学
- 结构力学 结构力学
背景情况:
- 传统的可部署托架空间结构在部署面积,折叠比率和重量方面面临限制.
- 对大型航天器的新兴需求需要新的可扩展机制和部署类型.
- 纤维增强聚合物 (FRP) 层叠复合带弹弹是最近的一项进步.
研究的目的:
- 分析可伸缩带弹弹及其相关弹膜结构的部署特性.
- 通过参数研究,为弹杆膜结构提供设计指导.
- 通过实验验证分析模型和部署的属性.
主要方法:
- 为带弹弹和弹膜结构开发分析模型.
- 使用分析模型计算曲刚度,临界曲负荷和基本频率.
- 进行几何和材料参数研究.
- 进行实验调查以验证理论发现.
主要成果:
- 分析模型成功预测了部署的弹杆和膜结构的关键性质.
- 参数研究提供了关于几何和材料参数对性能影响的见解.
- 实验结果证实了分析预测的有效性和结构的可行性.
结论:
- 可折叠的伸缩带弹弹为克服传统空间结构的局限性提供了可行的解决方案.
- 开发的分析框架和实验验证支持大型航天器组件的设计.
- 这些结构特别适合用于天线,太阳能帆和太阳能阵列等应用.
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