剪切合规边界在空间膜结构中的配置设计和验证
Anbo Cao1, Zhiquan Liu1, Qiuhong Lin1
1Beijing Institute of Spacecraft System Engineering, Beijing 100094, China.
Polymers
|April 13, 2024
概括
新的剪切合规边界提高了空间膜结构中的应力均性. 这种设计方法减少了35.6%的压力,并提高了平坦度,为航空航天工程提供了宝贵的参考.
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:
- 空间膜结构经常遭受不均的应力分布.
- 对于符合剪切边界的现有设计方法是不够的.
研究的目的:
- 设计,优化和验证空间膜结构的剪切合规边界.
- 为这些边界开发配置设计方法.
主要方法:
- 使用希尔和克里斯森-洛复合材料模型开发了一个正方形模型.
- 采用有限元形状寻找方法与混合坐标系统.
- 进行模拟和膜延伸实验.
主要成果:
- 实现了与时分系统 (0.23%的影响力) 的边界兼容性.
- 最大应力减少了35.6%,应力均性提高了30.5%.
- 在剪切应力下降了58.1%的平度增速.
结论:
- 剪切合规边界有效地减轻了剪切应力传播,并提高了应力均性.
- 拟议的设计方法为空间膜结构的压力均设计提供了一种可行的方法.
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