针对空间曲柄摇杆机构的优点, 研究分析了将其应用到扑翼飞行器驱动机构上的可行性。基于传统图解法, 建立驱动机构的数学模型, 综合考虑安装方便和结构紧凑, 确定机构尺寸的大小。建立虚拟样机进行仿真分析, 验证理论设计的正确性。结果表明, 该结构可以作为扑翼飞行器的驱动机构。

According to the advantages of the space crank rocker mechanism, the feasibility of applying it to the driving mechanism of the flapping wing aircraft is studied and analyzed. Based on the traditional graphic method, the mathematical model of the drive mechanism is established, and the size of the mechanism is determined by considering the convenient installation and compact structure. The virtual prototype is built for simulation analysis to verify the correctness of the theoretical design. The results show that the drive mechanism can be used as the driving mechanism of the flapping wing aircraft.