A rotorcraft having at least one stabilizer device of the tail plane and/or of the tail fin type. At least one stabilizer device is a variable wing area stabilizer device comprising an airfoil member provided with a stationary airfoil surface and a movable airfoil surface. A control system is connected to a mover system for moving the movable airfoil surface in translation between a refracted position for occupying when the rotorcraft has a forward speed less than a first speed threshold, and an extended position for occupying when the rotorcraft has a forward air speed greater than a second speed threshold greater than the first speed threshold.
GIRAVION MUNI D'UN DISPOSITIF STABILISATEUR
A ROTORCRAFT HAVING A STABILIZER DEVICE
DREHFLÜGELFLUGZEUG, DAS MIT EINER STABILISATORVORRICHTUNG AUSGESTATTET IST
2016-12-21
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
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