Polymer based flapping-wing robotic insect: Progress in design, fabrication and characterization

被引:0
作者
Bontemps, A. [1 ]
Vanneste, T. [1 ]
Soyer, C. [1 ]
Paquet, J. B. [2 ]
Grondel, S. [1 ]
Cattan, E. [1 ]
机构
[1] Univ Lille Nord France, IEMN, CNRS UMR 8520, UVHC, F-59313 Valenciennes, France
[2] Off Natl Etud & Rech Aerosp, F-59000 Lille, France
来源
BIOINSPIRATION, BIOMIMETICS, AND BIOREPLICATION 2014 | 2014年 / 9055卷
关键词
Bioinspiration; MEMS; nano air vehicle; SU-8; compliant link; electromagnetic actuator; FLIGHT; AERODYNAMICS; MECHANISM; DYNAMICS; FORCES; LIFT; AIR;
D O I
10.1117/12.2044650
中图分类号
R318 [生物医学工程];
学科分类号
0831 ;
摘要
In the last decade, many researchers pursued the development of tiny flying robots inspired by natural flyers destined for the exploration of confined spaces, for example. Within this context, our main objective is to devise a flying robot bioinspired from insect in terms of size and wing kinematics using MEMS technologies. For this purpose, an original design has been developed around resonant thorax and wings by the way of an indirect actuation and a concise transmission whereas the all-polymer prototypes are obtained using a micromachining SU-8 photoresist process. This paper reports our recent progress on the design of a flapping-wing robotic insect as well as on the characterization of its performance. Prototypes with a wingspan of 3 cm and a mass of 22 mg are achieved. Due to the introduction of an innovative compliant link, large and symmetrical bending angles of 70 degrees are obtained at a flapping frequency of 30 Hz along with passive wing torsion while minimizing its energy expenditure. Furthermore, it leads to a mean lift force representing up to 75 % of the prototype weight as measured by an in-house force sensor. Different improvements are currently underway to increase the power-to-weight ratio of the prototype and to obtain an airborne prototype.
引用
收藏
页数:12
相关论文
共 35 条
[1]  
[Anonymous], 2010, P INT MICR VEH C MAY
[2]  
Bacher J, 2003, THESIS
[3]   Design and fabrication of insect-inspired composite wings for MAV application using MEMS technology [J].
Bao, X. Q. ;
Bontemps, A. ;
Grondel, S. ;
Cattan, E. .
JOURNAL OF MICROMECHANICS AND MICROENGINEERING, 2011, 21 (12)
[4]   Design Overview of a Resonant Wing Actuation Mechanism for Application in Flapping Wing MAVs [J].
Bolsman, C. T. ;
Goosen, J. F. L. ;
van Keulen, F. .
INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES, 2009, 1 (04) :263-272
[5]   Design and performance of an insect-inspired nano air vehicle [J].
Bontemps, A. ;
Vanneste, T. ;
Paquet, J-B ;
Dietsch, T. ;
Grondel, S. ;
Cattan, E. .
SMART MATERIALS AND STRUCTURES, 2013, 22 (01)
[6]  
Chang S., 2000, MIICROSCHALE SYST ME
[7]  
Coleman N., 2009, THESIS
[8]   Into thin air:: contributions of aerodynamic and inertial-elastic forces to wing bending in the hawkmoth Manduca sexta [J].
Combes, SA ;
Daniel, TL .
JOURNAL OF EXPERIMENTAL BIOLOGY, 2003, 206 (17) :2999-3006
[9]   Flexural stiffness in insect wings I. Scaling and the influence of wing venation [J].
Combes, SA ;
Daniel, TL .
JOURNAL OF EXPERIMENTAL BIOLOGY, 2003, 206 (17) :2979-2987
[10]  
Dabral S., 1992, J ELECT, V21