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

Author:

Li Yiming123ORCID,Li Keyu123,Fu Fang4,Li Yao123ORCID,Li Bing123ORCID

Affiliation:

1. Guangdong Provincial Key Laboratory of Intelligent Morphing Mechanisms and Adaptive Robots, Harbin Institute of Technology, Shenzhen 518055, China

2. Key University Laboratory of Mechanism & Machine Theory and Intelligent Unmanned Systems of Guangdong, Harbin Institute of Technology, Shenzhen 518055, China

3. School of Mechanical Engineering and Automation, Harbin Institute of Technology, Shenzhen 518055, China

4. College of Art and Design, Shenzhen University, Shenzhen 518060, China

Abstract

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.

Funder

National Natural Science Foundation of China

Guangdong Basic and Applied Basic Research Foundation

State Key Laboratory of Mechanical System and Vibration

Shenzhen Science and Technology Program

Shenzhen Peacock Innovation Team Project

Publisher

MDPI AG

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