非传统的翼结构设计与格子填充通过设计增材制造的设计
Numan Khan1, Valerio Acanfora1, Aniello Riccio1
1Department of Engineering, University of Campania "Luigi Vanvitelli", via Roma, 29, 81031 Aversa, Italy.
Materials (Basel, Switzerland)
|April 13, 2024
概括
研究人员探索了用于航空航天应用的格子填充的翼结构. 凯尔文晶格结构提供最佳性能,在轻量级设计中降低重量和翅膀尖端偏移.
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:
- 具有高刚度与重量比的轻质结构对于航空航天减重至关重要.
- 非传统结构,特别是格子结构,越来越多地被用于航空航天应用.
- 增材制造可以创建复杂的格子设计,以提高机械性能.
研究的目的:
- 评估非传统的格子填充翼结构的实用性,以取代传统的肋设计.
- 为了确定航空航天应用的最佳格子充满的翼结构.
- 分析格子单元细胞类型和排列对应力分布的影响.
主要方法:
- 用有限元分析 (FEA) 来评估网格充满的翼结构的性能.
- 使用nTop和ANSYS Workbench的自动代方法,用于获得最佳的格子设计.
- 我们比较了五种不同类型的优化格子填充结构.
主要成果:
- 凯尔文格子结构在评估的设计中表现最好.
- 凯尔文晶格结构导致了最小的翼尖偏移,减轻重量和较低的应力水平.
- 压力分布的明显依赖于格子单元细胞类型和排列被确立.
结论:
- 格子填充结构为轻量级航空航天翼设计提供了一个创新的和可行的替代方案.
- 凯尔文晶格结构被认为是当前航空航天应用中非常合适的选择.
- 优化的格子设计显著提高了机械性能,降低了结构重量.
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