Konstrukce UAV typu křídlo s elektropohonem

Abstract

BIČAN, M. Design of Wing Type UAV with Electric Power Plaint: Master Thesis. Ostrava : VŠB – Technical University of Ostrava, Faculty of Mechanical Engineering, Institute of Transport, 2012, 99 p. Thesis head: Martinec, F. Master thesis deals with Design of Wing Type UAV with Electric Power Plaint. In the introduction is conducted analysis of similar structural solutions. For existing structural solutions are described their advantages and disadvantages, and subsequently selected properties and structural characteristics, that are advantageous for the proposed construction. There is also done conceptual design of the airframe and powerplant of the aircraft, including the selection of parameters of the aircraft, propulsion units and their mutual arrangement. There is also designed specific wing structural solution and propulsion units, choice of materials used, their size, weight and other properties. In the final part of this thesis is processed for the production process of the proposed aircraft. Partial implementation of UAV aircraft design is documented in the enclosure of the master thesis.