A flight control device for an aircraft

The invention relates to a flight control device (1) for an aircraft, the device comprising a mount (2), a lever (3) pivotally mounted on the mount, and mechanical means for generating a return force for the lever, said means including a spring (6) and a first motor member (13) that are arranged so that a first end of the spring is constrained to move in rotation with the lever and a second end of the spring is constrained to move in rotation with an outlet shaft of the first motor member. According to the invention, the flight control device includes an electrical assistance system (18) for assisting said mechanical means for generating a return force. 本发明涉及种用于飞行器的飞行控制装置(1)，该装置包括底座(2)、枢转地安装在底座上的操作杆(3)以及用于产生操作杆的回复力的机械工具，所述工具包括弹簧(6)和第电机构件(13)，弹簧(6)和第电机构件(13)布置成使得弹簧的第端被约束成随操作杆旋转运动，而弹簧的第二端被约束成随第电机构件的输出轴旋转运动。根据本发明，飞行控制装置包括电辅助系统(18)，电辅助系统(18)用来辅助用于产生回复力的所述机械工具。