Keyword: «carrier system»

DETERMINATION OF OPTIMAL BLADE PARAMETERS MAIN ROTOR

Authors:

Urii Onyshkin,

Vyacheslav Polyyahtov,

Vadim Popov

The article considers the results of optimization of the main rotor and determines the flight characteristics of a UAV with an optimized main rotor. To achieve this goal, a mathematical model of the helicopter's hovering main rotor was created, which allows you to find the propeller thrust and power consumption depending on the blade profile, blade shape in plan, geometric twist and fill factor.

Keywords: unmanned aerial vehicle, helicopter, power plant, carrier system, tactical and technical data

SIMULATION OF THE APPROACH OF THE BLADES OF AN UNMANNED AIRCRAFT AIRCRAFT OF THE HELICOPTER TYPE COAXIAL SCHEME AT OPERATING SPEED

Authors:

Urii Onyshkin,

Dmitrii Sizov,

Svyatoslav Kochish

The article considers the results of mathematical modeling of the flywheel motion of a single rotor blade, obtaining integral characteristics of a single rotor, calculation features of the carrier system with coaxial propellers, modeling the approach of helicopter blades of a coaxial scheme.

Keywords: helicopter, power plant, carrier system, tactical and technical data, unmanned aerial vehicle (uav), tactical and technical requirements