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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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