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    PRECISION OPERATOR FOR AN AIRCRAFT AUTOTHROTTLE OR AUTOPILOT SYSTEM
    2.
    发明公开
    PRECISION OPERATOR FOR AN AIRCRAFT AUTOTHROTTLE OR AUTOPILOT SYSTEM 审中-公开
    航空器自动或自动驾驶仪系统的精密操作员

    公开(公告)号：EP3250458A1

    公开(公告)日：2017-12-06

    申请号：EP16862626.5

    申请日：2016-08-01

    申请人： Innovative Solutions & Support, Inc.

    发明人： HEDRICK, Geoffrey, S.M.

    IPC分类号： B64D31/06 ,  B64D31/08 ,  B64D31/02 ,  G05D1/00

    摘要： An autothrottle system for an aircraft includes a motor, actuator assembly, and position sensor operatively connected between the motor and a moving portion of the actuator assembly. An electronic controller is configured to control the motor to move the actuator assembly to actuator positions based at least on position information from the position sensor to move the throttle lever to lever positions. The actuator assembly includes a bearing assembly having a plurality of bearings to contact a surface of a shaft for converting rotational movement of the shaft into linear motion of the bearing assembly along the shaft. The actuator assembly further includes a shuttle arm having at one end a mounting surface to attach to the bearing assembly and at the other end a linkage arm operatively coupled to the attachment end of the lever.

    Control apparatus
    5.
    发明公开
    Control apparatus 失效
    Kontrollvorrichtung。

    公开(公告)号：EP0415467A1

    公开(公告)日：1991-03-06

    申请号：EP90202037.9

    申请日：1990-07-25

    申请人： BRITISH AEROSPACE PUBLIC LIMITED COMPANY

    发明人： Aldersley, Alan, British Aerospace Public Ltd Comp ,  Hayes, Ronald, British Aerospace Public Ltd. Comp.

    IPC分类号： B64D31/02

    CPC分类号： B64D31/04

    摘要： Control apparatus, such as an aircraft throttle box, includes a manual control member 8 linearly movable on a first shaft 2. The position of the control member is sensed by rotation of the shaft 2 to generate an output control signal. In order to balance the apparatus, especially against high g-forces, a second shaft 3 is provided, parallel to the first carrying a counterweight 13 that moves together with the control member 8, but in the opposite direction.

    摘要翻译： 诸如飞行器节气门箱的控制装置包括可在第一轴2上直线移动的手动控制构件8.通过轴2的旋转来感测控制构件的位置，以产生输出控制信号。 为了平衡装置，特别是抵抗高g力，第二轴3设置成平行于第一轴3，第一轴3承载与控制构件8一起移动但沿相反方向运动的配重13。