FIELD: aircrafts.
SUBSTANCE: invention relates to the field of vertical take-off and landing aircraft. The aircraft based on the Magnus effect is a rectangular body, along the perimeter of which cylinders (1) are installed, with the possibility of rotation. Inside the body there is a gas intake and supply zone, in which, above and below, centrifugal discs (2) are installed, gas to which is supplied through the inlet/outlet openings (3) in the body. Discs 2 allow the device to rotate around its axis. Inside the housing, at the top and bottom of each cylinder (1), there is a centrifugal cylindrical fan (4), each impeller (5) of which is made in the entire length of the cylinder (1). The fan casing (4) on one side has an outward inlet (6) for gas intake and supply to the impeller (5), and on the other side it has an outlet (7) for a forced gas flow passing into a stream that includes cells (8) passing into the tunnel (9), which narrows at the outlet directly in front of the cylinder (1). The upstream and downstream streams are independent and not interconnected. All rotating parts of the structure are driven by motors (10).
EFFECT: invention is aimed at increasing the carrying capacity.
1 cl, 3 dwg
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Authors
Dates
2021-12-23—Published
2021-08-25—Filed