The present invention relates to a device for directly controlling a blade which comprises a stator (1), at least one blade carrier (7) composed of at least one curved magnet (6), the blade carrier (7) being secured to at least one blade (3) and pivotally coupled to the rotor (8) for varying the alpha angle of said blades with the excitation of the stator (1). The stator (1) is a partially spherical stator, the stator core (1) being the intersection of the blade axis (22) and the rotor axis (20), said stator being radially close to the magnets (3) to control the rotation of the blades (3) around the blade axis (22). A magnetic ring (5) holds the blades (3) in a neutral position, the system can be compared to a cyclically controlled mechanical oscillator, the frequency, phase and amplitude of the oscillation being controlled by said stator. Device providing a compact, lightweight and robust solution for controlling the direction of an aircraft.
DISPOSITIF DE COMMANDE DIRECTE DE PALE PAR ACTIONNEUR ÉLECTROMÉCANIQUE
DEVICE FOR DIRECT CONTROL OF BLADE BY ELECTROMECHANICAL ACTUATOR
VORRICHTUNG ZUR DIREKTEN BLATTKONTROLLE MIT ELEKTROMECHANISCHEM AKTUATOR
2021-07-14
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
DISPOSITIF DE COMMANDE DIRECTE DE PALE PAR ACTIONNEUR ELECTROMECANIQUE
European Patent Office | 2019
|DISPOSITIF DE COMMANDE DIRECTE DE PALE PAR ACTIONNEUR LECTROMÉCANIQUE
European Patent Office | 2019
|Actionneur électromécanique comprenant une unité de commande électronique
European Patent Office | 2024
|ACTIONNEUR ÉLECTROMÉCANIQUE COMPRENANT UNE UNITÉ DE COMMANDE ÉLECTRONIQUE
European Patent Office | 2023
|