FIELD: aircraft engineering.
SUBSTANCE: claimed method exploits the principle based on revolution of the dynamic bearing elements around their axes and, at the same time, around the central axis perpendicular to their plane of revolution. Dynamic bearing elements used to develop the aircraft lift are composed of the discs integrated into separate sets, each consisting of pairs of discs located in one plane. Said discs of every set run in opposite directions and at different rpm. Note here that for control over aircraft thrust the inclination of discs revolution to horizontal plane is varies from 0 to 45 degrees. To equalise the dynamic loads at the central drive shaft the sets of discs are located concentrically with the central rotational axis and equally spaced apart.
EFFECT: development of combined thrust, reduced airflow friction, higher efficiency of aircraft drive.
2 cl, 3 dwg
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