Aircraft braking system architecture comprising:a brake comprising electromechanical actuators (1, 2);a principal control channel (6) and an alternative control channel (7) comprising electrical components that are at least partly different and adapted to provide respectively a principal braking control function and an alternative braking control function that are at least partly different;power modules (15, 16) comprising electrical components that are at least partly different and adapted to generate electrical power supply currents (I1, I2) on the basis of principal control signals or alternative control signals;a surveillance unit (8) adapted to ensure that in normal operation the principal control signals are used and that in the event of a fault the alternative control signals are used to generate the electrical power supply currents.
ARCHITECTURE DE SYSTÈME DE FREINAGE POUR AÉRONEF
ARCHITECTURE OF AN AIRCRAFT BRAKING SYSTEM
AUFBAU EINES BREMSSYSTEMS FÜR LUFTFAHRZEUG
2024-04-17
Patent
Electronic Resource
French