Design study of a rotorless Unmanned Aerial Vehicle

Abstract

The modeling software Fusion360 was used to design a compact and symmetric rotorless Unmanned Aerial Vehicle (UAV) that aims to address the safety hazards and high noise levels associated with rotor blades rotating at high speeds. The rotorless UAV utilizes four bladeless fans instead of external paddles and places the motors needed to provide power inside the fuselage. The locations of the rotorless UAV's air vents, air inlets, camera, and sled mount structures are analyzed, while the operating parameters of the main structural energy supply module (battery), power module, and control module are studied. The safety and noise problems caused by the rotor blades during the flight of the rotorless UAV and the damage of the motor easily caused by external factors are explored and solved.