Aircraft e.g. helicopter, has radial blower with adjustable driving power assigned to each cylinder for generating air flow that flows transversely against cylinder, where rotor of blower concentrically surrounds cylinder with distance

摘要

The aircraft has a payload body (30) at which a closed cylinder drivable around a transverse axis with controllable number of revolutions is arranged for generation of lift and/or propulsion after a magnus effect. A radial blower having adjustable driving power is assigned to each of the cylinders for generating air flow that flows transversely against the cylinder. A wing profile of the radial blower has rotor blades that are pivotable around an aligned axis parallel to a rotation axis (19), where a rotor of the radial blower concentrically surrounds the cylinder with a distance.