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
2023-07-05
Patent
Electronic Resource
English