FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the structures of vertical take-off and landing aircraft for various purposes. Vertical take-off and landing aircraft consists of a body (1) in the form of a hollow cylinder and two horizontal platforms (2, 3) of a circular shape. On the upper platform (2) there is a power unit (4) and a cabin (5) with the control system of the aircraft, covered by the skin of the upper part of the fuselage (6). Between the upper platform (2) and the lower platform (3), coaxial rotors (7, 8) with blades (9) are installed. On the perimeter of the rotors, the upper (10) and lower (11) fairings are fixed. Between the rotors there is a swash plate (12). Under the lower platform (3) is located the lower part of the fuselage, which rests on the telescopic supports (14) of the aircraft.
EFFECT: provides a free space above the top part of the fuselage.
1 cl, 3 dwg
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