Generally described, an architecture for an aircraft braking system is provided. The architecture includes a brake having friction members and electromechanical actuators, each electromechanical actuator having an electric motor and a power module; a computer arranged to produce digital control signals; a power unit arranged to produce an electrical power supply for powering the electric motors; and a junction box disposed on the undercarriage. The junction box may be configured to receive and to distribute the electrical power supply. The junction box generally includes an electrical motor control module that produces digital motor command signals from the digital control signals, and an electrical converter module that converts the digital motor command signals into analog motor command signals for the power modules of the electromechanical actuators.
ARCHITECTURE DE SYSTEME DE FREINAGE POUR AERONEF
ARCHITECTURE OF AN AIRCRAFT BRAKING SYSTEM
AUFBAU EINES BREMSSYSTEMS FÜR EIN LUFTFAHRZEUG
2020-11-25
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |