| 摘要 |
<p>A flap actuator system for an airfoil structure (10) including: a flap member (14a) for controlling the airfoil structure; a bearing member (26a) interconnected with the flap member and the airfoil structure; and an actuator device for rotating the flap member about the bearing member relative to the airfoil structure; the actuator device including an electromagnetic motor segment and a drive mechanism driven by the electromagnetic motor to rotate the flap member about the axis of the bearing member relative to the airfoil structure; the electromagnetic motor being integral with the airfoil structure and the drive mechanism; the electromagnetic motor including a field circuit (40) integral with the drive mechanism and an armature circuit (46) integral with the airfoil structure; the field circuit located within the armature circuit.</p> |
