The Functions of Phasic Wing-Tip Folding on Flapping-Wing Aerodynamics

被引:0
作者
Li, Yiming [1 ,2 ,3 ]
Li, Keyu [1 ,2 ,3 ]
Fu, Fang [4 ]
Li, Yao [1 ,2 ,3 ]
Li, Bing [1 ,2 ,3 ]
机构
[1] Harbin Inst Technol, Guangdong Prov Key Lab Intelligent Morphing Mech &, Shenzhen 518055, Peoples R China
[2] Key Univ Lab Mech & Machine Theory & Intelligent U, Harbin Inst Technol, Shenzhen 518055, Peoples R China
[3] Harbin Inst Technol, Sch Mech Engn & Automat, Shenzhen 518055, Peoples R China
[4] Shenzhen Univ, Coll Art & Design, Shenzhen 518060, Peoples R China
基金
中国国家自然科学基金;
关键词
flapping-wing flight; wing-tip folding; insect flight aerodynamics; bioinspired flapping mechanism; INSECT; FLIGHT; MECHANISMS;
D O I
10.3390/biomimetics9030183
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Insects produce a variety of highly acrobatic maneuvers in flight owing to their ability to achieve various wing-stroke trajectories. Among them, beetles can quickly change their flight velocities and make agile turns. In this work, we report a newly discovered phasic wing-tip-folding phenomenon and its aerodynamic basis in beetles. The wings' flapping trajectories and aerodynamic forces of the tethered flying beetles were recorded simultaneously via motion capture cameras and a force sensor, respectively. The results verified that phasic active spanwise-folding and deployment (PASFD) can exist during flapping flight. The folding of the wing-tips of beetles significantly decreased aerodynamic forces without any changes in flapping frequency. Specifically, compared with no-folding-and-deployment wings, the lift and forward thrust generated by bilateral-folding-and-deployment wings reduced by 52.2% and 63.0%, respectively. Moreover, unilateral-folding-and-deployment flapping flight was found, which produced a lateral force (8.65 mN). Therefore, a micro-flapping-wing mechanism with PASFD was then designed, fabricated, and tested in a motion capture and force measurement system to validate its phasic folding functions and aerodynamic performance under different operating frequencies. The results successfully demonstrated a significant decrease in flight forces. This work provides valuable insights for the development of flapping-wing micro-air-vehicles with high maneuverability.
引用
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页数:15
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