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。
Considering the flight performance and dynamics of the flapping wing aircraft,this paper designs a dragonfly miniature flapping wing aircraft.The mechanical structure of the flapping wing aircraft is analyzed and designed,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.
作者
王仲文
李振
段瑞珍
WANG Zhong-wen;LI Zhen;DUAN Rui-zhen(Rongcheng Campus, Harbin University of Science and Technology, Weihai 264300, China;School of Mechanical Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074, China)
出处
《哈尔滨理工大学学报》
CAS
北大核心
2020年第6期98-106,共9页
Journal of Harbin University of Science and Technology
基金
国家自然科学基金(51375123)
黑龙江省自然科学基金(E2016040).
关键词
扑翼飞行器
机械结构
有限元分析
蜻蜓
flapping wing aircraft
mechanical structure
finite element analysis
dragonfly
