Abstract: The present technology relates to the field of aircraft construction, and more specifically to vertical take-off and landing aircraft. The aircraft includes a bearing frame of a spatial structure, a seat, controls, moto-units, a control system, and a remote control system. The bearing frame is designed with a central portion and with at least two peripheral clusters. The central portion and the peripheral clusters of the frame are designed as a spatial structure. Each peripheral cluster is designed as a truss structure of at least three segments of the same type, which are interconnected. Inside each segment there is a moto-unit, which has at least one motor and at least one horizontal-rotation propeller.

Abstract: There is disclosed a multicopter vertical takeoff and landing (VTOL) aircraft. The aircraft comprises am airframe with spatial design, a pilot seat, a cockpit, controls, engine units, engine compartment, control system, remote control system. The airframe consists of a central section and, at least, two peripheral sections, wherein peripheral sections can be folded up or down, or be retracted under the central section. The central section and peripheral sections of the airframe have spatial design. Each of the peripheral sections comprises at least three standard engine compartments which are connected to each other. Inside each engine compartment there is an engine unit which comprises at least one engine and at least one horizontally rotating propeller together with the control hardware. Each engine unit is an autonomous member of the distributed control system (DCS).

Abstract: There is disclosed a multicopter vertical takeoff and landing (VTOL) aircraft. The aircraft comprises am airframe with spatial design, a pilot seat, a cockpit, controls, engine units, engine compartment, control system, remote control system. The airframe consists of a central section and, at least, two peripheral sections, wherein peripheral sections can be folded up or down, or be retracted under the central section. The central section and peripheral sections of the airframe have spatial design. Each of the peripheral sections comprises at least three standard engine compartments which are connected to each other. Inside each engine compartment there is an engine unit which comprises at least one engine and at least one horizontally rotating propeller together with the control hardware. Each engine unit is an autonomous member of the distributed control system (DCS).

Abstract: The present technology relates to the field of aircraft construction, and more specifically to vertical take-off and landing aircraft. The aircraft includes a bearing frame of a spatial structure, a seat, controls, moto-units, a control system, and a remote control system. The bearing frame is designed with a central portion and with at least two peripheral clusters. The central portion and the peripheral clusters of the frame are designed as a spatial structure. Each peripheral cluster is designed as a truss structure of at least three segments of the same type, which are interconnected. Inside each segment there is a moto-unit, which has at least one motor and at least one horizontal-rotation propeller.