Design and analysis of an aerial vehicle using Solidworks

Despite the advances that have been made in the design of drones, different configurations are still being built that in many cases are adjusted to many specific situations. Thus, hexacopters with six rotors, octocopters with eight rotors and quadcopters with four rotors are the three most popular types. For the construction of the equipment, the payload, the necessary stability and the desired flight duration are just some of the variables that influence the choice of configuration, this is directly related to the work to be developed by the equipment. Along with the above, it is also essential to take into account, the material used to build it, generally, this material is light but resistant, such as carbon fiber, fiberglass reinforced plastic or aluminum alloys. The assembly of the drone’s motor and propeller, which functions as its propulsion system, is crucial. Depending on the total weight of the drone and the payload it will carry, the motors are chosen. The propellers themselves must be compatible with the motors and have sufficient thrust. Last but not least, the aerodynamic design of a drone is a key factor in ensuring safe and effective flight. This design takes into account aspects such as component protection, weight distribution and body shape. It should be noted that the aerodynamic design may change depending on the size of the drone and the intended use. addresses the continued diversification in drone configuration and design, despite advances in technology. The preeminence of three predominant types is underlined: hexacopters, octocopters and quadcopters, which adapt to particular contexts. In construction, variables such as payload, stability and flight duration, linked to the specific tasks of the drone, influence the choice of configuration. The choice of material, with a focus on lightness and resistance, such as carbon fiber, fiberglass reinforced plastic or aluminum alloys, emerges as an essential aspect. The selection and combination of engines and propellers, vital in the propulsion system, are made considering the total weight and load. Aerodynamic design, encompassing component safeguarding, weight distribution and body morphology, is critical to safe and efficient flight. It is important to note that the aerodynamic design varies depending on the size and intended use of the drone. In essence, this summary focuses on the increasing diversity and fundamental considerations in the design and configuration of drones, with the purpose of achieving optimal and functional flights in various applications.