仿生扑翼飞行机器人柔性翅试验研究及其理论解释  

Experimental Research on the Flexible Wing and Its Theoretical Explanation for the Bionics Flapping Aerocraft

作　　者：金晓怡[1] 颜景平[1] 周建华 

机构地区：[1]东南大学 [2]扬州大学,扬州225009

出　　处：《中国机械工程》2007年第9期1028-1032,共5页China Mechanical Engineering

基　　金：211工程振兴行动计划资助项目(3008002102)

摘　　要：以柔性翅为研究对象,在自行研制的气动力测量试验平台上进行升力试验研究,旨在为柔性翅的理论研究提供依据。试验结果表明,柔性翅能产生较之刚性翅更大的升力,说明柔性翅将更适合仿生飞行。针对翅变形对昆虫飞行高升力有贡献的试验结果,给出了一种基于柔性楔形效应的升力机制的理论解释。In order to study the flexible wing, the lift force experimental research was put up on the aerodynamic force measurement experimental platform which was designed and developed by authors. The purpose of this study was to provide the basis of the theoretical research on the flexible wing. The experimental result indicates that the flexible wing has more strong lift force than that of the rigid wing. To some extent, this results illuminate that the flexible wing fits bionics flying better. According to the experimental results that the wing distortion has contribution to the higher lift force of the flying insect, a theoretical explanation for the lift force mechanism based on the flexible wedge -effect was put forward.

关 键 词：仿生扑翼飞行机器人 柔性翅 升力 柔性楔形效应 

分 类 号：TB17[生物学—生物工程] TP242[自动化与计算机技术—检测技术与自动化装置]