Clapping-wing micro air vehicle of insect size

被引:21
作者
Kawamura, Yoshiyuki [1 ]
Souda, Satoshi [1 ]
Nishimoto, Satoshi [1 ]
Ellington, Charles P. [2 ]
机构
[1] Fukuoka Inst Technol, Fac Engn, Dept Intelligent Mech Engn, Fukuoka, Japan
[2] Univ Cambridge, Dept Zool, Cambridge CB2 1TN, England
来源
BIO-MECHANISMS OF SWIMMING AND FLYING: FLUID DYNAMICS, BIOMIMETIC ROBOTS, AND SPORTS SCIENCE | 2008年
关键词
MAV; micro air vehicle; flapping; clapping; insect; hawkmoth;
D O I
10.1007/978-4-431-73380-5_26
中图分类号
R318 [生物医学工程];
学科分类号
0831 ;
摘要
The efficiencies for generating the axial thrust and the lift of a flapping wing micro air vehicle (MAV) were increased by clapping the wings together, using the "Weis Fogh clap and fling mechanism" from Studies on the aerodynamics of the insect flight. Making use of this effect, we have succeeded in the development and the flight of an insect-size clapping wing MAV. The span and the weight were 10cm and 2.3g, respectively, which are very close to those of the hawkmoth (Manduca sexta), and amongst the smallest and the lightest ever built. The flight characteristics of the clapping MAV were similar to those of the hawkmoth. These results are the first step towards MAVs that mimic insects at lower Reynolds numbers.
引用
收藏
页码:319 / +
页数:2
相关论文
共 11 条
[1]   Wing rotation and the aerodynamic basis of insect flight [J].
Dickinson, MH ;
Lehmann, FO ;
Sane, SP .
SCIENCE, 1999, 284 (5422) :1954-1960
[2]   Leading-edge vortices in insect flight [J].
Ellington, CP ;
vandenBerg, C ;
Willmott, AP ;
Thomas, ALR .
NATURE, 1996, 384 (6610) :626-630
[3]  
Ellington CP, 1999, J EXP BIOL, V202, P3439
[4]  
FRY SN, 2002, AERODYNAMICS FREE FL, V300, P495
[5]   Effects of dynamic stall on propulsive efficiency and thrust of flapping airfoil [J].
Isogai, K ;
Shinmoto, Y ;
Watanabe, Y .
AIAA JOURNAL, 1999, 37 (10) :1145-1151
[6]   Delta-wing function of webbed feet gives hydrodynamic lift for swimming propulsion in birds [J].
Johansson, LC ;
Norberg, RÅ .
NATURE, 2003, 424 (6944) :65-68
[7]   Numerical simulations of membrane wing aerodynamics for micro air vehicle applications [J].
Lian, YS ;
Shyy, W .
JOURNAL OF AIRCRAFT, 2005, 42 (04) :865-873
[8]  
MARDEN JH, 1987, J EXP BIOL, V130, P235
[9]  
WEISFOGH T, 1973, J EXP BIOL, V59, P169
[10]  
Willmott AP, 1997, J EXP BIOL, V200, P2705