FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the structures and methods of flight of manned aircraft (AC). Individual aircraft contains an X-shaped body, two sliding wings provided with flaps and fixed to the front ends of the body with the ability to rotate along an axis perpendicular to the plane of the body, or four folding wings fixed to the front and rear ends of the body. Four wings are designed to be folded into the plane of the body from a position perpendicular to the plane of the body. AC contains a vertical stabilizer, hand and foot controls located in the front and back of the body, respectively. Four power units are rotatable and are paired on the ends of the body. Each power unit is a motor with air screws in a protective casing. Body is configured to receive a pilot thereon in a position in which the pilot's front plane is parallel to the plane of the body.
EFFECT: provided increase in aerodynamic characteristics due to a reduction in drag.
8 cl, 8 dwg
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Authors
Dates
2018-10-31—Published
2017-12-01—Filed