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Scalability of resonant motor-driven flapping wing propulsion systems
Mostafa R A Nabawy1,2, Ruta Marcinkeviciute1
1Department of Mechanical, Aerospace and Civil Engineering, The University of Manchester, Manchester M1 3BB, UK.
Royal Society Open Science
|September 27, 2021
Summary
This study presents an integrated design process for resonant motor-driven flapping wing vehicles, optimizing propulsion systems for efficiency and scalability. Peak efficiency reaches 36% with specific motor masses and kinematics.
Area of Science:
- Aerospace Engineering
- Robotics
- Mechanical Engineering
Background:
- Flapping wing vehicles offer potential for efficient aerial locomotion.
- Developing scalable and high-performance propulsion systems remains a challenge.
Purpose of the Study:
- To develop an integrated conceptual design process for resonant motor-driven flapping wing propulsion systems.
- To assess the scalability and performance of these systems by analyzing key design variables.
Main Methods:
- Quasi-steady aerodynamic modeling based on wing geometry and kinematics.
- Second-order dynamic system modeling for mechanics with nonlinear damping.
- Standard motor equations for electrical domain analysis.
- Development of design scaling laws based on current technology.
Main Results:
- The design process integrates electrical, mechanical, and aerodynamic domains.
- Peak system efficiency of 30-36% achieved at motor masses of 0.5-1 g with constant angle of attack kinematics.
- Sinusoidal angle of attack kinematics requires more power but can increase peak efficiency by up to 15%.
Conclusions:
- The integrated design process provides insights into actuator size, mass fraction, and pitching kinematics effects.
- Optimized kinematics and motor mass are crucial for maximizing propulsion system efficiency in flapping wing vehicles.
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