Bionic Structure Design of a Flapping Wing Robot

摘要：

　　As a new field of research,the flapping wing micro air vehicle has a widely application in civil and defense.This paper analyzes the specific state of the flapping wing in flight,and determines the variation range of the flapping angle and the angle of attack.Then we design a simple double crank and double rocker mechanism,in addition we propose a passive rotation mechanism to meet the requirement of micro flapping wing mechanism.Compared to previous flapping wing structures,the mechanism is technically more simple and practical,which is benefit to minimize the flapping wing micro air vehicle.We design the specific structure of Micro Air Vehicle (MAV) and calculate the dimension of the mechanism.Finally,we use the Solidworks to model it and prove the feasibility and accuracy of this flapping wing structure.

关键词： Flapping wing Micro air vehicle Flapping angle Angle of attack

作者: Wenjuan Zhou Huichao Deng Xilun Ding

作者单位: Robotics Institute, Beijing University of Aeronautics and Astronautics,Beijing 100191, China

会议类型: 国际会议

会议名称: 2016中国机构与机器科学国际会议

会议地点: 广州

会议语种:英文

页码: 101-110

在线出版日期: 2016-12-15（万方平台首次上网日期，不代表论文的发表时间）