拍打
翼
运动学
折叠(DSP实现)
仿生学
机制(生物学)
空气动力学
刚度
结构工程
航空航天工程
材料科学
工程类
物理
纳米技术
经典力学
量子力学
作者
Xin Li,Yu Zheng,Huan Shen
标识
DOI:10.1088/1748-3190/adb2cb
摘要
When the beetle lands on the target, the hind wings fold regularly to form smaller wing packages and are hidden on the ventral side of the elytra due to the interaction between the elytra and abdomen. Its complex folding pattern is attributed to the flexibility of the hind wings, the super-elasticity of the folding joints, and the special geometric morphology of the veins. The corrugation and folding pattern of the hind wings can provide new insights for the design of folding anti-collision mechanisms and the improvement of aerodynamic performance of ornithopter. This paper first proposes a beetle-type ornithopter with foldable wings based on the folding mechanism and kinematic characteristics of the beetle's hind wings. Subsequently, a series of numerical simulations were conducted on flapping wing robot to explore its flapping kinematics, folding stability, structural stiffness. Finally, the force generation of flapping wings was tested on the fabricated prototype.
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