FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed aircraft comprises fuselage, tail structure, landing gear, screw, rudder, vertical rudders, flaps, passenger seats, and control system built around digital processor. Closed wing surfaces with engines attached thereto may turn. Tail structure is equipped with two coaxial screws with independent drives. Aforesaid fuselage is provided with rack to secure seats therein. Said racks displace freely in fuselage guides and are equipped with ejection mechanism for emergent conditions and independent parachute systems. Said racks are arranged inclined in cases with covers at fuselage top, or horizontally, while covers are located at fuselage rear.
EFFECT: possibility of vertical take-off and landing and rescue of passengers in accidents, higher maneuverability.
9 dwg
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