FIELD: aviation.
SUBSTANCE: invention relates to vertical take-off aircraft. Vertical take-off and landing aircraft comprises a control cabin, a fuselage with a vertical channel, having inlet and outlet holes, a tail unit, wings attached to fuselage having pressure nozzles on ends, a power unit and undercarriage. Channel is a slot and is located along fuselage. In channel there is a rotary charger for external air suction and discharge of air vertically downwards.
EFFECT: invention is aimed at widening range of equipment.
4 cl, 5 dwg
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