发明名称 Flap actuator system
摘要 A flap actuator system for an airfoil structure including: a flap member for controlling the airfoil structure; a bearing member 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 integral with the drive mechanism and an armature circuit integral with the airfoil structure; the field circuit located within the armature circuit.
申请公布号 US2001035477(A1) 申请公布日期 2001.11.01
申请号 US20000730308 申请日期 2000.12.05
申请人 FINK DAVID ALLAN;GAUDREAU MARCEL PIERRE JOSEPH 发明人 FINK DAVID ALLAN;GAUDREAU MARCEL PIERRE JOSEPH
分类号 B64C3/50;B64C27/615;(IPC1-7):B64C3/50 主分类号 B64C3/50
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