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Research on Deployable Wings for MAVs Bioinspired by the Hind Wings of the Beetle Protaetia brevitarsis
by
Sun, Jiyu
, Wang, Wenzhe
, Zhang, Zhijun
, Li, Pengpeng
in
Aerodynamics
/ Analysis
/ beetle
/ Beetles
/ Behavior
/ bionic deployable wing (BD-W)
/ Bionics
/ Design
/ Energy consumption
/ Environmental aspects
/ Fluid dynamics
/ hind wing
/ Insects
/ Laboratory animals
/ Mechanical properties
/ Methods
/ micro aerial vehicles (MAVs)
/ Observations
/ Protaetia brevitarsis
/ Research methodology
/ Researchers
/ Simulation
/ Structure
/ Velocity
/ wind tunnel
/ Wings (Animal)
2024
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Research on Deployable Wings for MAVs Bioinspired by the Hind Wings of the Beetle Protaetia brevitarsis
by
Sun, Jiyu
, Wang, Wenzhe
, Zhang, Zhijun
, Li, Pengpeng
in
Aerodynamics
/ Analysis
/ beetle
/ Beetles
/ Behavior
/ bionic deployable wing (BD-W)
/ Bionics
/ Design
/ Energy consumption
/ Environmental aspects
/ Fluid dynamics
/ hind wing
/ Insects
/ Laboratory animals
/ Mechanical properties
/ Methods
/ micro aerial vehicles (MAVs)
/ Observations
/ Protaetia brevitarsis
/ Research methodology
/ Researchers
/ Simulation
/ Structure
/ Velocity
/ wind tunnel
/ Wings (Animal)
2024
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Research on Deployable Wings for MAVs Bioinspired by the Hind Wings of the Beetle Protaetia brevitarsis
by
Sun, Jiyu
, Wang, Wenzhe
, Zhang, Zhijun
, Li, Pengpeng
in
Aerodynamics
/ Analysis
/ beetle
/ Beetles
/ Behavior
/ bionic deployable wing (BD-W)
/ Bionics
/ Design
/ Energy consumption
/ Environmental aspects
/ Fluid dynamics
/ hind wing
/ Insects
/ Laboratory animals
/ Mechanical properties
/ Methods
/ micro aerial vehicles (MAVs)
/ Observations
/ Protaetia brevitarsis
/ Research methodology
/ Researchers
/ Simulation
/ Structure
/ Velocity
/ wind tunnel
/ Wings (Animal)
2024
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Research on Deployable Wings for MAVs Bioinspired by the Hind Wings of the Beetle Protaetia brevitarsis
Journal Article
Research on Deployable Wings for MAVs Bioinspired by the Hind Wings of the Beetle Protaetia brevitarsis
2024
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Overview
Deployable hind wings of beetles led to a bio-inspired idea to design deployable micro aerial vehicles (MAVs) to meet the requirement of miniaturization. In this paper, a bionic deployable wing (BD-W) model is designed based on the folding mechanism and elliptical wing vein structure of the Protaetia brevitarsis hindwing, and its structural static and aerodynamic characteristics are analyzed by using ANSYS Workbench. Finally, the 3D-printed bionic deployable wing was tested in a wind tunnel and compared with simulation experiments to explore the effects of different incoming velocity, flapping frequency, and angle of attack on its aerodynamic characteristics, which resulted in the optimal combination of the tested parameters, among which, the incoming velocity is 3 m/s, the flapping frequency is 10 Hz, the angle of attack is 15°, and the lift-to-drag ratio of this parameter combination is 4.91. The results provide a theoretical basis and technical reference for the further development of bionic flapping wing for MAV applications.
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