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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:

  • 飞机机翼需要适应形状,以在各种飞行条件下提供最佳性能.
  • 传统的形状变形系统通常涉及复杂的,重型设计,持续的能源需求,限制效率和有效载荷.

研究的目的:

  • 为飞机机翼结构引入一种新型的增材制造,双可变旋转元件.
  • 为了使机翼几何形状能够发生实质性的,可逆的变化,而无需持续的能源支出.

主要方法:

  • 利用几何非线性来创建双可变的几何结构,用于翼的变形.
  • 设计和制造增材制造的,可变的旋转元件.
  • 进行实验验证,包括风洞测试和有限元分析.

主要成果:

  • 证明了翅膀和弦状几何学的实质性和可逆性变化.
  • 确认了消除在机动期间用于形状维护的连续能源使用.
  • 验证了多稳定的变形翼的机械可靠性和形状保持能力.

结论:

  • 拟议的多台式变形机翼提供可调节的机械和几何性能,以进行精确的调整.
  • 这项技术显著节省能源,减轻重量,提高性能,特别是在无人机 (UAV) 中.
  • 该概念对航空航天应用和在其他工程学科的潜在应用具有前景.