| 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 interconnected with the flap member and airfoil structure for rotating the flap member about the axis of the bearing member relative to the airfoil structure and including a field circuit (40) integral with one of the flap member and airfoil structure and an armature circuit (46) integral with the other, the bearing member may be a tension member (26a) which is attached to the airfoil structure at a first point (36) and to the flap member at a second point (32) spaced from the first point.</p> |
