A braking system architecture for aircraft, the architecture comprising: a brake including friction members and electromechanical actuators for exerting a braking torque on the wheel; a computer situated in the fuselage of the aircraft and arranged to produce first control signals; and a junction box situated on the undercarriage, the junction box being connected to the computer and to the electromechanical actuators, the junction box being configured to receive the first control signals and to use the first control signals to produce second control signals for application to the electromechanical actuators in order to control the electromechanical actuators.
ARCHITECTURE DE SYSTEME DE FREINAGE POUR AERONEF
ARCHITECTURE OF AN AIRCRAFT BRAKING SYSTEM
AUFBAU EINES BREMSSYSTEMS FÜR EIN LUFTFAHRZEUG
27.07.2022
Patent
Elektronische Ressource
Französisch