The invention relates to a hybrid vertical take-off and landing drone comprising at least two substantially parallel fixed wings (12, 14) each comprising at least two fins (16a, 16b, 18a, 18b) distributed on either side of a roll axis (200) of the drone and individually controlled, characterized in that it comprises at least two counter-rotating rotors (20a, 20b) with a collective pitch system (24a, 24b) and a swashplate (26a, 26b), which are arranged between two wings on either side of the roll axis (200a), individually controlled and articulated so as to allow independent tilting of each rotor on a tilt axis (22a, 22b) substantially parallel to the pitch axis of the drone, the rotational axis of the blades of each rotor being substantially perpendicular to said tilt axis.
DRONE HYBRIDE À DÉCOLLAGE ET ATTERRISSAGE VERTICAL ADAPTÉ AU VOL EN CONDITIONS VENTEUSES
VERTICAL TAKEOFF AND LANDING HYBRID DRONE SUITABLE FOR FLYING IN WINDY CONDITIONS
HYBRIDDROHNE MIT VERTIKALEM START UND VERTIKALER LANDUNG ZUM FLIEGEN UNTER WINDIGEN BEDINGUNGEN
2024-01-10
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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