Моделирование напряженно-деформированного состояния деталей, используемых в современных беспилотных авиационных комплексах в качестве плоских пружин и элементов жесткости

Abstract

The article considers the methods of analytic determining the stress state of the miniature unmanned aerial vehicles and starting systems. The stiffening elements of the wing and the plane elastic elements of the catapult are calculated. Strength computing of the strengthened with tubular longeron wing of the unmanned aerial vehicle and the plane elastic elements of the starting systems are performed with ANSYS software. The strength calculations allow ensuring reliable operation of the miniature unmanned aerial vehicles and starting systems for the given conditions