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
COMMANDE DE SYSTEME D'ACTIONNEUR DU RENVERSEUR DE POUSSEE DE SECOURS
04.05.2023
Patent
Elektronische Ressource
Englisch
Electric Thrust Reverser Actuation Systems
British Library Conference Proceedings | 2002
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