An aerodyne comprises a fuselage, a fixed wing , a thruster for cruising flight, and a rotary wing for stages of vertical flight and held stationary during cruising flight. The rotary wing includes at least two contrarotating single-blades disposed at the top of the fuselage and hinged about respective axes perpendicular to the rotor axes of rotation. A maneuvering procedure for maneuvering the aerodyne includes a transition stage between a stage of vertical flight and a stage of cruising flight, wherein in the transition stage, when the speed of each single-blade is less than a threshold speed of rotation, the pitch of each single-blade is such that it no longer provides any lift force and the transverse hinge of the single-blade to its rotor axis is held locked in a position such that the single-blade is perpendicular to the rotor shaft.
VEHICULE AERIEN COMPRENANT AU MOINS DEUX VOILURES TOURNANTES ALIGNEES SELON SON AXE DE ROULIS
AERIAL VEHICLE COMPRISING AT LEAST TWO ROTARY WINGS ALIGNED ALONG ITS ROLL AXIS
LUFTFAHRZEUG MIT MINDESTENS ZWEI ENTLANG SEINER WALZENACHSE AUSGERICHTETEN DREHFLÜGELN
2021-01-20
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
VEHICULE AERIEN COMPRENANT AU MOINS DEUX VOILURES TOURNANTES ALIGNEES SELON SON AXE DE ROULIS
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