Abstract
The study proposes the use of a new generation of aircraft based on the use of cylindrical rotating blade propellers as a means of transportation. The results of research and development work carried out on several dimensions of cylindrical rotating blade propellers are considered. The results obtained allow us to lay down a certain basis for the theory and practice of the operation of cylindrical rotating blade propellers. In the process of scientific research, an understanding of the role of geometric ratios of rotor elements and the number of blades is obtained. The limits of the angle of attack and thrust vector deflection are defined. The requirements for structural strength and stiffness of the rotating blade propeller parts are formed. The solution of the kinematic mechanisms for controlling the angles of attack of the blades and flaps, and the thrust vector in general, etc., was formed. A conceptual image of a two-seat aircraft using cylindrical rotating blade propellers is proposed. Bench tests of the cylindrical rotating blade propellers allowed the formation of tactical and technical requirements for the two-seat aircraft. It is suggested that further research be considered to determine design solutions for promising aircraft of greater payload and capacity.
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