The invention relates to an aircraft wing and a method of adjusting an aircraft wing. The invention relates to an aircraft wing comprising: a fixed wing having a tip; a wing tip device rotatably mounted at the hinge at the tip of the fixed wing such that the wing tip device is rotatable about the hinge; and an actuation system for rotating the wing tip device about the hinge wherein the actuation system comprises a motor, at least one geared rotary actuator, a reduction gearbox, a clutch for selectively disconnecting rotation of the motor from rotation of the geared rotary actuator, the geared rotary actuator is drivable by the motor and is arranged to convert a rotary motion into a different rotary motion and to rotate the wing tip device relative to the tip of the fixed wing, the clutch is coupled to the geared rotary actuator by a shaft and the shaft is rotationally fixed to a mass disposed radially outward from the shaft.
本发明涉及飞行器机翼和调整飞行器机翼的方法。该飞行器机翼包括:固定机翼,该固定机翼具有梢部;翼梢装置,该翼梢装置以可旋转的方式安装在位于固定机翼的梢部处的铰接件,使得翼梢装置能够绕铰接件旋转;以及致动系统,该致动系统用于使翼梢装置绕铰接件旋转,其中,致动系统包括马达、至少一个齿轮传动式旋转致动器、减速齿轮箱、用于将马达的旋转与齿轮传动式旋转致动器的旋转选择性地断开接合的离合器,齿轮传动式旋转致动器能够由马达驱动并且布置成将旋转运动转换成不同的旋转运动且布置成使翼梢装置相对于固定机翼的梢部旋转,其中,离合器通过轴联接至齿轮传动式旋转致动器并且轴以旋转的方式固定至从轴径向向外设置的质量块。
Aircraft wing and method of adjusting aircraft wing
飞行器机翼和调整飞行器机翼的方法
2024-12-17
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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