流体力学、飞行力学与发动机

主动变形扑翼飞行器的设计和风洞试验研究

  • 段文博 昂海松 肖天航
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  • 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

  网络出版日期: 2012-12-24

Design and Wind Tunnel Testing of an Active Morphing Wing Ornithopter

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Received date: 2012-03-20

  Revised date: 2012-12-21

  Online published: 2012-12-24

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。

本文引用格式

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, 0 , 0(0) : 0 -0 . DOI: 10.7527/S1000-6893.2013.0083

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.

参考文献

[1] KING, A. S., AND MCLELLAND, J. Form and Func-tion in Birds, 1985, vol. 3. Academic Press, Inc. ISBN 0124075010.
[2] TOBALSKE, B. W., AND DIAL, K. P. Flight kinemat-ics of blackbilled magpies and pigeons over a wide range of speeds. Journal of Experimental Biology, 1996, 199: 263–280.
[3] Bret W. Tobalske. Biomechanics of bird flight. The Journal of Experimental Biology, 2007, 210:3135–3146
[4] Ulla M. Lindhe Norberg, York Winter. Wing beat kine-matics of a nectar-feeding bat, Glossophaga soricina, flying at different flight speeds and Strouhal numbers. The Journal of Experimental Biology, 2006, 209:3887–3897
[5] ANG H S, ZENG R, DUAN W B. Aerodynamic expe-rimental investigation for mechanism of lift and thrust of flexible flapping-wing MAV.Journal of Aerospace Power.2007, 22(11):1938-1845.(in Chinese)
昂海松,曾锐,段文博等.柔性扑翼微型飞行器升力和推力机理的风洞试验和飞行试验.航空动力学报.2007, 22(11):1938-1845
[6] ZHANG Y F,SONG B F,YUAN C S. Lift characte-ristic of the flapping wing micro air Vehicle. Acta Aero-dynamica Sinica, 2008, Vol.26,No.4:519–522. (in Chi-nese)
张亚峰,宋笔峰,袁昌盛等.微型扑翼飞行器升力特性研究.空气动力学学报. 2008, Vol.26, No.4:519–522
[7] Lin C S, Hwu C, Young W B. The thrust and lift of an ornithopter’s membrane wings with simple flapping motion. Aerospace Science and Technology, 2006,10: 111–119
[8] Ramiro Chavez-Alarcon, SHU F J. Lift, Drag and Flow-field Measurements around a Small Ornithopter. Orlando: AIAA, 2011
[9] Billingsley D, Slipher G, Grauer J. Testing of a Passively Morphing Ornithopter Wing. Washington: AIAA, 2009
[10] Mueller D, Gerdes J W, Gupta S K.INCORPORATION OF PASSIVE WING FOLDING IN FLAPPING WING MINIATURE AIR VEHICLES. San Diego: ASME Mechanism and Robotics Conference, 2009
[11] Demetgul M, Pino W, Tansel L N. MORPHING WING DESIGN FOR ORNITHOPTERS. Miami: ECTC, 2008
[12] Li Bing. A Preliminary Study on the Microstructure of Bird Primaries and Their Significance for Flight. Harbin: Northeast Forestry University, 2008.(in Chinese)
李冰.鸟类初级飞羽微观结构与飞行性能相关性的初步研究.哈尔滨:东北林业大学,2008
[13] NORBERG, U. M. Vertebrate Flight. Springer-Verlag. ISBN 0387513701. 1990.
[14] Wu J C, Zoran Popovi′c. Realistic Modeling of Bird Flight Animations. ACM Transactions on Graphics,July 2003,Volume 22 Issue 3:888-895
[15] Pennycuick C. J. Speeds and wingbeat frequencies of migrating birds compared with calculated benchmarks. The Journal of Experimental Biology, 2001, 204:3283–3294
[16] SHAO L M, SONG B F, SONG W P. Experimental research of flapping—wing propulsion for micro air ve-hicles. Journal of Experiments in Fluid Mechanics, 2009, Vol.23,No.1:1–6. (in Chinese)
邵立民,宋笔锋,宋文萍.微型扑翼的推进特性实验研究.实验流体力学. 2009, Vol.23,No.1:1–6.
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