AIRCRAFT BASED ON THE MAGNUS EFFECT AND METHOD OF ITS WORK Russian patent published in 2021 - IPC B64C29/00 B64C23/08 

FIELD: aircrafts.

SUBSTANCE: inventions group relates to the field of vertical take-off and landing aircraft. The aircraft is a multifaceted rectangular body, along the perimeter of which cylinders (1) are installed with the possibility of rotation. To supply air to the inside of the housing, inlets (2) are made, leading to the gas intake and supply zone, located inside the housing, in which centrifugal impellers (3) are installed above and below, creating a forced gas flow. At the outlet of the gas intake and supply zone along the perimeter, above and below, there are streams, representing cells (4), passing into a tunnel (5), narrowing at the outlet directly in front of the cylinder (1). The upstream and downstream streams are independent and not interconnected. Impellers (3) and cylinders (1) are driven by motors (6). The method is implemented as follows. Gas enters the housing through inlets (2). When the impellers (3) rotate, gas is drawn in and supplied. The forced oncoming gas flow created during the rotation of centrifugal impellers (3) passes through the cells (4) of the flow duct, which allows one continuous flow to be split into several small ones, and makes its supply uniform over the entire length of the cylinders (1). After the cells, the flows pass through a tunnel (5), in which they narrow and fall on rotating cylinders (1). The narrowing of gas flows increases its speed, but decreases its effect on the area of ​​the cylinders (1). The forced flow on the rotating cylinders (1) creates the Magnus effect. The torque of the upper impeller (3) is compensated by the torque of the lower one.

EFFECT: increasing the carrying capacity.

2 cl, 3 dwg