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.
AERODYNE HYBRIDE DE TYPE VTOL OU STOL
HYBRID AERODYNE OF THE VTOL OR STOL TYPE
HYBRIDES LUFTFAHRZEUG VOM VTOL- ODER STOL-TYP
14.12.2022
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
AERODYNE HYBRIDE DE TYPE VTOL OU STOL (BASCULEMENT ROTOR)
Europäisches Patentamt | 2022
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