The device has a gear rim (104) mounted to rotate on an undercarriage axle (105) and constrained in rotation with a torsion tube (106). Braking actuators (110) i.e. electromechanical actuators, are carried by the rim for selectively pressing a stack of disks (116) together. A drive member (130) carries a secondary winding (120) of a single-phase transformer with a primary winding (121) arranged facing the rim while being stationary in rotation, where the secondary winding is electrically coupled to the actuators and the primary winding is coupled to a non-direct current (DC) voltage source.
Dispositif de freinage/entraînement d'une roue d'aéronef
Device for braking/powering an aircraft wheel.
Vorrichtung zum Bremsen/Antrieb eines Rads eines Luftfahrzeugs
2016-01-27
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
ECRAN THERMIQUE POUR DISPOSITIF DE FREINAGE D'UNE ROUE D'AERONEF
Europäisches Patentamt | 2021
|Ecran thermique pour dispositif de freinage d’une roue d’aéronef
Europäisches Patentamt | 2022
|ECRAN THERMIQUE POUR DISPOSITIF DE FREINAGE D'UNE ROUE D'AERONEF
Europäisches Patentamt | 2023
|