仿蜻蜓扑动机构改进及气动力/力矩测量  

Improvement of flapping mechanism and measurement of aerodynamic force/moment of bionic dragonfly prototype

作　　者：张锐 胡薇 郑兴 徐礼超[1] 汪超 ZHANG Rui;HU Wei;ZHENG Xing;XU Lichao;WANG Chao(School of Traffic Engineering,Huaiyin Institute of Technology,Huaian Jiangsu 223003,China;School of Mechanical Engineering,Huaiyin Institute of Technology,Huaian Jiangsu 223003,China;School of Mechanical Engineering,Dongguan University of Technology,Dongguan Guangdong 523808,China)

机构地区：[1]淮阴工学院交通工程学院,江苏淮安223003 [2]淮阴工学院机械与材料工程学院,江苏淮安223003 [3]东莞理工学院机械工程学院,广东东莞523808

出　　处：《航空动力学报》2022年第12期2729-2735,共7页Journal of Aerospace Power

基　　金：国家自然科学基金(52005104);淮安市自然科学研究项目(HAB202152);江苏省高校自然科学研究项目(22KJD410001);广东省“创新强校工程”特色创新项目(2020KTSCX149);广东省普通高校机器人与智能装备重点实验室(2017KSYS009);东莞理工学院机器人与智能装备创新中心(KCYCXPT2017006);江苏省大学生创新创业训练计划项目(202211049016Z)。

摘　　要：为进一步提高扑翼微型飞行器的机动性能,对前期提出的可移动铰链曲柄滑块扑动机构进行了改进和小型化。该机构运动学表明:移动铰链后两侧翅膀扑动幅值差值从之前的21.3°增大到51.2°,同时平均扑动幅值降到0°。研制了可快速模块化组装的碳纤维板仿蜻蜓扑翼样机。样机测量和试飞实验表明,通过调节扑动频率可以明显改变样机的升力和推力,有效实现飞行器的快速爬升机动飞行。在较大扑动频率移动铰链可以产生足够的偏航力矩和滚转力矩用于转弯等机动飞行。For further improving the maneuverability of the flapping-wing micro air vehicle,the movable hinge crank slider flapping mechanism proposed earlier was improved and miniaturized.The kinematics of the flapping mechanism indicated that as the hinges moved,the difference of the bilateral flapping amplitudes increased from 21.3°to 51.2°and the bilateral mean flapping amplitudes decreased to 0°.And a modularized and carbon fiber plate bionic dragonfly prototype was designed.The measurement and flight test of the prototype showed that the lift and thrust of the prototype changed obviously by adjusting the flapping frequency,realizing rapid acceleration and climbing maneuvering flight.By moving the hinge,significant yaw moment and roll moment were generated for maneuvering turn at larger flapping frequency.

关 键 词：仿蜻蜓扑翼 扑动机构 移动铰链 曲柄滑块 气动力/力矩 机动转弯 

分 类 号：V211.1[航空宇航科学与技术—航空宇航推进理论与工程]