A small unmanned aerial vehicle has a fuselage 1 with aerodynamically active surfaces or wings 2 arranged on the fuselage 1. Control surfaces 7 are located to the rear of the wings and are pivotable at right angles to the longitudinal axis X of the small aerial vehicle. At least one propeller 42,52 is arranged to be drivable by a drive motor 40,50. In order to make the aerial vehicle more controllable in strong winds, at least one region of the control surfaces 7 is arranged directly behind the propellers 42,52 in the direction of the air flow produced by them.
Small unmanned aerial vehicle
2017-04-26
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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