The invention relates to a multirotor drone (1) comprising a fuselage and a plurality of engine units driving a plurality of rotors (4), each rotor comprising two blades (5) mounted in a facing arrangement on either side of a blade tilting axis BP, such that each of the blades (5) has one rotational degree of freedom about said blade tilting axis BP.
DRONE AVEC ROTOR COMPRENANT DES PALES ARTICULEES
2018-04-13
Patent
Electronic Resource
French
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