An aircraft control surface actuation assembly comprises a first electromechanical actuator assembly (44) driven by two independent motors (48, 50) for redundancy, with a damping assembly (46) provided to mitigate flutter.
CONTROL SURFACE ACTUATION ASSEMBLY
STEUERFLÄCHENBETÄTIGUNGSANORDNUNG
ENSEMBLE D'ACTIONNEMENT DE SURFACE DE COMMANDE
2017-11-08
Patent
Electronic Resource
English