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一个可变的Camber翼的概念设计
Spencer Troy P Cortez1, Seksan Winyangkul2, Suwin Sleesongsom1
1Department of Aeronautical Engineering, International Academy of Aviation Industry, King Mongkut's Institute of Technology Ladkrabang, Bangkok 10520, Thailand.
Biomimetics (Basel, Switzerland)
|June 25, 2025
概括
本研究介绍了可变翼 (VCW) 的新三步设计,以提高无人机 (UAV) 的性能. 该方法整合了空气动力学分析,机制合成和先进的变形飞机的结构测试.
科学领域:
- 航空航天工程 航空航天工程
- 机械工程 机械工程
- 材料科学 材料科学 材料科学
背景情况:
- 可变翼 (VCW) 通过持续的形状调整为无人机 (UAV) 提供了增强的性能.
- 目前用于VCW的集成技术在开发中滞后,特别是在概念设计阶段.
- 现有的高起重装置缺乏通过持续的形状变化可以实现的平滑空气流.
研究的目的:
- 提出和验证一个新的三步设计方法,用于结构集成的可变翼 (VCW).
- 为了解决变形飞机的VCW集成技术的发展差距.
- 为了在变形翼设计中提高空气动力学效率和结构完整性.
主要方法:
- 空气动力学分析,以定义在各种飞行条件下最佳的翅膀形状适应.
- 使用基于教学学习的优化变体的机制合成,设计用于尾行边缘偏移的四条链接.
- 结构分析以评估皮肤承载能力和整体VCW系统完整性.
主要成果:
- 一个VCW机制的成功合成满足了定义的空气动力学和结构性目标.
- 实现了9.1764°的实际偏移.
- 经过验证的结构完整性,最大Von Mises应力为81.5MPa,最大屈曲率为0.073m.
结论:
- 拟议的三步设计方法有效地整合了VCW的空气动力学和结构要求.
- 这种方法促进了变形飞机技术的进步.
- 经过验证的VCW设计显示了提高飞机整体性能的巨大潜力.
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