基于拓优化和蜂材料的飞机双关节结构的轻量化设计
Haifeng Ou1, Shumeng Pang1,2, Weijun Tao2,3
1School of Environment and Civil Engineering, Dongguan University of Technology, Dongguan 523808, China.
Materials (Basel, Switzerland)
|December 11, 2025
概括
拓优化与蜂材料相结合,可显著降低飞机组件重量. 这种创新方法可以实现59.7%的重量减轻双关节结构,同时保持强度和安全性.
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
- 机械工程 机械工程
背景情况:
- 结构轻量化是航空航天设计的一个主要目标.
- 传统方法通常在实现复杂元件的最佳硬度与重量比方面存在局限性.
研究的目的:
- 提出一种新的设计方法,将拓优化 (TO) 与蜂巢材料相结合.
- 为了在典型的飞机双关节结构 (DLJS) 中实现显著的减重.
主要方法:
- 使用可变密度方法优化拓,以确定最佳的材料分布.
- 使用3D建模软件重建优化的设计 (SolidWorks 2022).
- 在低压力区域中整合蜂材料或去除材料以提高硬度与重量比率.
主要成果:
- 设计的DLJS实现了38.44公斤的质量,比最初的95.38公斤减少了59.7%.
- 数值强度验证证实,在典型的负载情况下,应力仍然低于材料产率强度.
- 通过缩小DLJS标本的3D打印来证明制造的可行性.
结论:
- TO和蜂材料的结合方法对于轻量化复杂的3D结构是有效的.
- 这种方法为设计复杂的航空航天部件提供了有价值的见解,可以提高度与重量比率.
- 该研究验证了先进的设计技术在航空航天工程中的实际应用和潜力.
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