OPTIMIZATION OF UNMANNED AERIAL VEHICLE STRUCTURES USING CARBON PLASTIC MATERIALS

This project investigates the application of carbon plastic composite materials for enhancing the structural integrity and performance of unmanned aerial vehicles (UAVs). The primary objective is to achieve significant weight reduction while simultaneously improving structural strength and aerodynamic stability. Research indicates that carbon composites exhibit a specific strength of 1500 MPa/g/cm³, which is three times greater than that of conventional aerospace materials. Furthermore, the implementation of these composites can lead to a 25-30% increase in structural vibration resistance and a 25% reduction in overall UAV weight. These improvements are attributed to the material's low density, ranging from 1.55 to 1.65 g/cm³, and its capacity for optimal stress distribution within the

structure. The methodology involves utilizing CAD modeling for design and numerical simulations for performance evaluation. The study also assesses the efficiency of advanced manufacturing techniques such as 3D printing and Out-of-Autoclave processes, highlighting their industrial viability. The findings are instrumental for developing lightweight, reliable, and energy-efficient drones suitable for diverse applications, including military operations, agricultural monitoring, and emergency rescue systems, particularly in environments with moderate temperatures and vibrational loads.

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