An actuator system for controlling a control surface of an aircraft, which includes a control structure which defines the control surface and the control structure has an axis of rotation about which the control structure can rotate relative to the aircraft. A first actuator assembly has a first actuator arm and a second actuator assembly has a second actuator arm. The first actuator assembly and the second actuator assembly are spaced apart from one another along the axis of rotation. The first actuator arm is connected to a first band member and the first band member is connected to the control structure on a first side of the axis of rotation and the second actuator arm is connected to a second band member and the second band member is connected to the control structure on a second opposing side of the axis of rotation.
HYDRAULIC ACTUATION SYSTEM FOR IMPAIRING ROTATION
HYDRAULISCHES BETÄTIGUNGSSYSTEM ZUR VERMINDERUNG DER ROTATION
SYSTÈME D'ACTIONNEMENT HYDRAULIQUE POUR ALTÉRER LA ROTATION
05.07.2023
Patent
Elektronische Ressource
Englisch