AIRCRAFT BASED ON MAGNUS EFFECT Russian patent published in 2024 - IPC B64C23/08 

FIELD: aviation.

SUBSTANCE: invention relates to the field of aviation, in particular to vertical takeoff and landing aircraft. The aircraft based on the Magnus effect consists of a body, in the front and rear parts of which there are air intakes, inside the body, along the perimeter, cylinders with the possibility of rotation are also installed inside the body. In the front and rear parts there is an air intake and thrust distribution zone for the cylinders, in which, above and below, two impellers are located at the exit from the zone. Along the perimeter, above and below, there are flow ducts in the form of tunnels running to the cylinders, the upper and lower flow ducts are independent and not connected to each other. At the same time, the device additionally, is equipped with a cabin with a control system for the device, as well as at least two main engines, which are a nozzle inside which a flow screw with blades twisted around the shaft is mounted on the shaft. In this case, each blade is a ¼ torus and has the shape of a spiral with a variable pitch, and the inner walls of the nozzle have spiral grooves in which the trajectory of the air flow changes from spiral to direct air flow. The objective of the invention is to create an aircraft based on the well-known physical principle of the Magnus effect, to achieve sufficient maneuverability and flight range of the aircraft.

EFFECT: achieved sufficient maneuverability and flight range of the aircraft.

1 cl, 4 dwg