FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to structures of aircrafts of vertical takeoff and landing. The aircraft includes front and rear bearing propellers or groups of front and rear bearing propellers, an undercarriage pushing propeller or a group of undercarriage pushing propellers. Each bearing and pushing screw is connected to an independently operating electric engine. Bearing propellers are installed in an equal number, at a certain distance from each other, front and back of the aircraft in a direction of movement of the aircraft in a horizontal plane, symmetrically to the longitudinal axis of the aircraft. At the same time, pushing propellers are installed at a certain distance from each other in a horizontal plane, symmetrically to each other and the longitudinal axis of the aircraft. Independently operating electric engines of front, rear, and undercarriage pushing propellers are installed inside open bearing spatial tubular frames-shields in such a way that they are visible from all outer sides and accessible.
EFFECT: reduction in energy consumption for a horizontal straight-line flight, improvement of controllability and maneuverability of a flight, increase in environmental friendliness.
36 cl, 5 dwg
