航空学报 > 2009, Vol. 30 Issue (3): 562-569

基于蜻蜓膜翅结构的飞机加强框的仿生设计

马建峰1, 陈五一1, 赵岭1, 赵大海2   

  1. 1. 北京航空航天大学 机械工程及自动化学院 2. 沈阳飞机设计研究所
  • 收稿日期:2007-12-17 修回日期:2008-03-31 出版日期:2009-03-25 发布日期:2009-03-25
  • 通讯作者: 马建峰

Bionic Design of Aircraft Reinforced Frame Based on Structure of Dragonfly Wing

Ma Jianfeng1, Chen Wuyi1, Zhao Ling1, Zhao Dahai2   

  1. 1. School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics 2. Shenyang Aircraft Design and Research Institute
  • Received:2007-12-17 Revised:2008-03-31 Online:2009-03-25 Published:2009-03-25
  • Contact: Ma Jianfeng

摘要: 由于机动性和能耗的要求,飞机设计过程当中轻量化设计是十分重要的。经过亿万年的进化,在承受自身重量及生长环境的载荷过程中,生物体获得了适应环境的最优结构。通过分析蜻蜓膜翅和飞机机身加强框的结构相似性,提取决定蜻蜓膜翅结构优良力学性能的结构特征,将其应用到飞机机身加强框的设计当中,并用有限元工具验证了结构的优化效果。在同样的承载条件下,仿生型结构的比刚度比原型结构提高了2%~6%,比强度提高了1%~8%。同时,仿生型结构的最大应力减小,而最小应力明显增大,因此其应力分布更加均匀,从而体现了仿生结构件材料的优化分布和最大效能。

关键词: 蜻蜓膜翅, 加强框, 结构仿生, 轻量化结构, 比刚度, 比强度, 应力均匀

Abstract: Design for light weight is very important in overall aircraft design because of the need for aircraft mobility and low energy consumption. In nature, after the evolution of hundreds of millions years, the organism obtains the optimal structure to adapt to the living environment based on the effect of gravity and environmental load. After an analysis of the load similarity between an aircraft reinforced frame and a dragonfly wing, some feature structures, which influence the mechanical proprieties of the dragonfly wing, are extracted for use in the design of the aircraft reinforced frame. Meanwhile, the finite element analysis (FEA) tool is used to verify the optimization effect. It is found that, compared with the conventional structure, bionic structures can increase specific stiffness by 2%-6% and specific strength by 1%-8%. The maximum stress decreases while the minimum stress increases, which indicates that the bionic structures result in more uniform stress distribution. Therefore, the study suggests that the bionic structures obtain optimal distribution of material and maximum structural efficiency.

Key words: dragonfly wing, reinforced frame, structural bionics, light weight structures, specific stiffness, specific strength, uniform stress

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