主动变形扑翼飞行器的设计和风洞试验研究

doi:10.7527/S1000-6893.2013.0083

流体力学、飞行力学与发动机

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主动变形扑翼飞行器的设计和风洞试验研究

段文博¹,昂海松²,肖天航³

1. 南京航空航天大学
2. 南京航空航天大学南
3. 南京航空航天大学航空宇航学院

收稿日期:2012-03-20 修回日期:2012-12-21 出版日期:2012-12-24 发布日期:2012-12-24
通讯作者: 段文博

Design and Wind Tunnel Testing of an Active Morphing Wing Ornithopter

Received:2012-03-20 Revised:2012-12-21 Online:2012-12-24 Published:2012-12-24
Contact: Wen-Bo DUAN

摘要/Abstract

摘要： 主动变形扑翼可以模仿鸟翼飞行时的复杂运动。为了了解主动变形扑翼飞行器的气动特性，在对鸟类骨骼结构和翅膀及尾翼运动规律研究的基础上，设计并制造了一种基于机器人技术的主动变形扑翼飞行器；给出了主动变形扑翼飞行器的机构运动规律函数，设计出机构运动控制系统；在低速风洞中对此飞行器进行了一系列测力试验，研究了主动变形扑翼的升力、推力特性和气动机理，以及风速、扑动频率、扑动幅度、伸展相位等参数对升力、推力的影响，并与常规扑翼进行了对比分析。试验结果表明，较之常规扑翼在相同情况下主动变形扑翼可以显著提高升力和对不同飞行状态的适应能力。

Abstract: The active morphing flapping wing can mimic the complex movement of a flying bird’s wings. In order to understand the aerodynamics of the active morphing wing ornithopter, the bird’s bone structure, the laws of motion of wing and tail were studied, an active morphing wing ornithopter was designed and built base on robotics. The laws of motion of the ornithopter were presented, a control system was designed and built. Wind tunnel tests of the ornithopter were performed in a low-speed wind tunnel. The lift, thrust characteristics and aerodynamic mechanism were studied, also the influence of wind velocity, flapping frequency, amplitude, stretch phase was investigated. The conventional flapping wing was tested as contrast. The test result shows that the active morphing wing can increase the lift and enhance ability to adapt to flight status.

中图分类号:

V211.7

段文博昂海松肖天航. 主动变形扑翼飞行器的设计和风洞试验研究[J]. 航空学报, doi: 10.7527/S1000-6893.2013.0083.

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E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

主动变形扑翼飞行器的设计和风洞试验研究

Design and Wind Tunnel Testing of an Active Morphing Wing Ornithopter

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