| 摘要 |
The aerodynamic aircraft roundabout has a mast which is arranged on a platform and on which a central bearing is arranged which can rotate, is adjustable in height and has supporting arms which project like rays and can be freely pivoted with respect to the central bearing between a lower and an upper pivoting angle limit in the vertical plane. Arranged on the free supporting arm ends are aircraft gondolas which can rotate freely about their aircraft longitudinal axis with respect to the supporting arms and are constructed with aerodynamically effective aerofoils whose angle of incidence can be controlled manually, and which additionally have aerofoil ailerons, which can be controlled manually, in order to be able to control the altitude and flying attitude of the aircraft gondolas individually, from the gondola, when the rotation speed of the roundabout produces sufficient lift moments on the aerofoils.
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