摘要
采用曲柄摇杆扑翼机构,通过UG实体建模和动力学仿真验证了这一设计的可行性。通过MATLAB和ADAMS建立了微型直流电机和曲柄摇杆扑翼机构的耦合模型,分析了不同定负载条件下齿轮传动机构减速比和曲柄摇杆的参数变化对扑动频率的影响,它为曲柄摇杆扑翼机构的实物快速制造提供了理论依据,也对进一步优化设计具有借鉴意义。
Crank rocker flapping wing mechanism was adopted. UG solid modeling and kinematical simulating were performed to validate the feasibility of this mechanism. Moreover, the coupling model of this structure with a DC micro motor was established through MATLAB and ADAMS. Effects of various crank rocker parameters and gearbox ratios on flapping frequency in different constant loads were analyzed. These optimized results shorten the period of manufacturing of crank rocker flapping wing mechanism. It is also a reference for further study of optimization design.
出处
《系统仿真学报》
EI
CAS
CSCD
北大核心
2007年第8期1758-1761,共4页
Journal of System Simulation
基金
基金:国家自然科学基金(60375033)。
