• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2021, Vol. 57 ›› Issue (2): 121-138.doi: 10.3901/JME.2021.02.121

• 运载工程 • 上一篇    下一篇

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机翼中小尺度主动变形研究进展及关键技术

周文雅1, 张宗宇1, 王晓明2, 吕维梁1, 钱卫1   

  1. 1. 大连理工大学航空航天学院 大连 116024;
    2. 中山大学航空航天学院 广州 510006
  • 收稿日期:2020-01-22 修回日期:2020-08-11 出版日期:2021-01-20 发布日期:2021-03-15
  • 通讯作者: 张宗宇(通信作者),男,1995年出生。主要研究方向为飞行器动力学与控制。E-mail:z18042654126@163.com
  • 作者简介:周文雅,男,1981年出生,博士,副教授。主要研究方向为飞行器动力学与控制。E-mail:zwy@dlut.edu.cn
  • 基金资助:
    装备预研领域基金资助项目(6140206020)。

Research Progress and Key Techniques of Active Morphing Wing at Medium and Small Scales

ZHOU Wenya1, ZHANG Zongyu1, WANG Xiaoming2, Lü Weiliang1, QIAN Wei1   

  1. 1. School of Aeronautics and Astronautics, Dalian University of Technology, Dalian 116024;
    2. School of Aeronautics and Astronautics, Sun Yat-Sen University, Guangzhou 510006
  • Received:2020-01-22 Revised:2020-08-11 Online:2021-01-20 Published:2021-03-15

摘要: 变形机翼能够根据飞行工况的变化,主动调节自身形状以改善飞行器任务适应性,是未来飞行器设计的研究前沿与热点。阐述国内外机翼中小尺度主动变形技术的研究进展,围绕机翼设计中柔顺变形能力与气动承载能力间冲突,对现阶段变翼型弯度、变厚度和扭转变形机翼中的机械变形结构设计方案进行重点分析探讨。对变形机翼设计中变形蒙皮、轻质高输出驱动系统、协调变形控制系统设计等关键技术的研究瓶颈及技术方案进行阐述分析,探讨变形机翼未来发展方向,为变形机翼设计与工程应用提供技术参考。

关键词: 变形机翼, 主动变形, 变翼型弯度, 变厚度, 机翼扭转, 变形蒙皮

Abstract: According to the change of flight conditions, the morphing wing can actively adjust its shape to improve the mission adaptability of the aircraft, which is the research frontier and hotspot of future aircraft design. Based on this background, this paper mainly describes the research progress of small and medium scale active wing deformation technology at home and abroad. Focusing on the conflict between the flexibility deformation capacity and the aerodynamic bearing capacity in the design of the wing, the mechanical deformation structure design of the wing with variable camber, variable thickness and torsional morphing at the present stage is emphatically analyzed and discussed. The research bottleneck and technical scheme of the key technologies such as deformation skin, light and high output driving system and coordinated deformation control system in the design of morphing wing are expounded and analyzed. The future development direction of the morphing wing is discussed, which provides a technical reference for the design and engineering application of the morphing wing.

Key words: morphing wing, active morphing, variable camber, variable thickness, wing twisting, morphing skin

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