A system architecture for a backup thrust reverser actuation system control is provided. The system architecture includes an AC power supply (101, 201) of an aircraft, a power supply (102, 202) and a motor control (103, 203) adapted to control an electric motor (M) of a thrust reverser actuation system. The system architecture further includes a backup power supply (105, 212) adapted to provide power to the electric motor in the event that the power supply fails
BACK-UP THRUST REVERSER ACTUATION SYSTEM CONTROL
BETÄTIGUNGSSYSTEMSTEUERUNG EINER STÜTZSCHUBUMKEHRVORRICHTUNG
COMMANDE DE SYSTÈME D'ACTIONNEMENT D'INVERSEUR DE POUSSÉE DE SECOURS
15.01.2025
Patent
Elektronische Ressource
Englisch
Electric Thrust Reverser Actuation Systems
British Library Conference Proceedings | 2002
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