| 摘要 |
<p>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.</p> |
