Design of Bionic Deployable Wings

Jiyu Sun, Chao Liu, Ruijuan Du, Zhijun Zhang
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Abstract

Flapping wing micro air vehicles (MAVs) take inspiration from natural insects and small birds. Reducing its size is a trend in development. Bioinspired from hindwings of the Asian ladybeetle, a design scheme of bionic deployable wings is put forward in this paper. The deployable movement is achieved by the mechanical structure of two four-bar-linkages, which learn from the behaviors of the folded motion of the beetle’s hindwings. The links are hollow structures bioinspired by hollow tubular structural of vein of the beetle hindwings, which can reduce the mass and improve the maneuverability in flight. Under uniform load and bending moment, the total deformation, equivalent stress and strain of deployable wings are investigated by the finite element analysis (FEA). The simulation shows that their mechanical properties can have beneficial effect on the flight.
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仿生可展开机翼的设计
扑翼微型飞行器(MAVs)的灵感来自于天然昆虫和小鸟。缩小规模是一种发展趋势。以亚洲瓢虫后翅为灵感,提出了一种可展开仿生翅膀的设计方案。这种可展开的运动是由两个四杆连杆的机械结构实现的,它们学习了甲虫后翅折叠运动的行为。连接部分是由甲虫后翅静脉的空心管状结构启发而成的空心结构,可以减轻重量,提高飞行的机动性。在均布荷载和弯矩作用下,采用有限元分析方法研究了可展开机翼的总变形、等效应力和应变。仿真结果表明,它们的力学性能对飞机的飞行有良好的影响。
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