Manufacturing of Vertical Takeoff And Landing Drone
DOI:
https://doi.org/10.51976/zxcwyx85Keywords:
UAV, Electronic Speed Controller(ESC), Brushless DC Motor(BLDC)Abstract
Based on VTOL DRONE UAV technology, this project. Although UAVs are mostly utilized for military activities, they also have qualities that make them useful to regular people. This project contains new aerodynamically designed vehicle parts for the wing, fuselage, driving system, advances in take-off and landing, ease of use, operating range, and study of parts affected by wind disturbance, altitude, and power needs. to maximize the use of torque for lift generation and reduce wind disturbance loss by optimizing the angle of attack of the wings and the tilt angle of the propeller. Calculations take into account factors such as the amount of thrust needed to provide the required lift force, how much power is lost as a result of drag and weight, the type of drive system needed, and the maximum flying time per charge. Software utilized for both design and analysis is CAD (Solid Works) and CAE (Ansys). The major goals of the project are to shorten the runway, make it simple for UAVs to take off and land on any surface, and maximize the use of torque. VTOL DRONE, UAV, Autocad, Ansys, Solidworks, Airfoil, Flow analysis are some of the keywords.
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