A drone comprising a carrier structure, at least three lift propulsion rotors and a control system delivering at least one electrical power supply to at least three electric motors driving said at least three rotors, said at least three rotors being spaced apart longitudinally and transversely beside one another, wherein said drone includes a wing carrying two half-wings symmetrically about an anteroposterior plane of symmetry P of said drone, serving at least to increase the lift of said drone, each of said two half-wings including at least one movable portion suitable for moving relative to said carrier structure of said drone with at least a first degree of freedom to move in rotation about a first pivot axis parallel to a longitudinal direction X of said drone; and two first electric actuators respectively enabling each of said movable portions of one of said two half-wings.
DRONE COMPORTANT AU MOINS TROIS ROTORS DE SUSTENTATION ET DE PROPULSION
A DRONE HAVING AT LEAST THREE LIFT AND PROPULSION ROTORS
DROHNE, DIE MINDESTENS DREI ROTOREN ALS HUB- UND FLUGANTRIEBSSYSTEM UMFASST
07.11.2018
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
DRONE COMPORTANT AU MOINS TROIS ROTORS DE SUSTENTATION ET DE PROPULSION
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