Design and Ｒesearch of a Dragonfly Flapping Wing Aircraft

WANG Zhong-wen; LI Zhen; DUAN Ｒui-zhen

doi:10.15938/j.jhust.2020.06.014

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Design and Ｒesearch of a Dragonfly Flapping Wing Aircraft

更新时间：2026-08-31

- Design and Ｒesearch of a Dragonfly Flapping Wing Aircraft
- Vol. 25, Issue 6, Pages: 98-106(2020)
- 作者机构：
  
  1. 1．哈尔滨理工大学荣成学院,山东,威海,264300
  2. 2．华中科技大学机械科学与工程学院,武汉,430074
- 作者简介：
- 基金信息：
- DOI：10.15938/j.jhust.2020.06.014
  CLC： TP242
- Published：2020
- 稿件说明：
移动端阅览
WANG Zhong-wen, LI Zhen, DUAN Ｒui-zhen. Design and Ｒesearch of a Dragonfly Flapping Wing Aircraft[J]. 2020, 25(6): 98-106.
DOI：

WANG Zhong-wen, LI Zhen, DUAN Ｒui-zhen. Design and Ｒesearch of a Dragonfly Flapping Wing Aircraft[J]. 2020, 25(6): 98-106. DOI： 10.15938/j.jhust.2020.06.014.

摘要

在考虑扑翼飞行器飞行性能与动力学特性的基础上，提出了一种仿蜻蜓微型扑翼飞行器，对扑翼飞行器的机械结构进行了理论分析与设计，确定了相关机构参数与运动数值。利用 SolidWorks 对设计的仿蜻蜓扑翼飞行器机械结构进行三维建模和运动仿真分析，并采用 ANSYS 与 ADAMS 对所提出的扑翼飞行器开展动力学性能分析。在相关研究基础上进行仿真实验分析，结果表明，所设计的机械结构满足仿蜻蜓微型扑翼飞行器基本功能的要求，具有可行性，可为仿蜻蜓扑翼飞行器的研究提供理论参考。

Abstract

Considering the flight performance and dynamics of the flapping wing aircraft，this paper designs adesigned，and the relevant mechanism parameters and motion parameters are determined． Using SolidWorks to carry out three-dimensional modeling and dynamic simulation analysis of the designed mechanical structure，and adopt ANSYS and ADAMS to carry out force analysis of flapping wing aircraft． On the basis of relevant research， simulation experiment analysis is carried out． The simulation results show that the designed mechanical structure meet the basic function requirements of dragonfly miniature flapping wing aircraft，and it is feasible． It can provide a theoretical reference for the research of dragonfly flapping aircraft．

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