Integrated Aircraft Flight Control Units
    11.
    发明申请
    Integrated Aircraft Flight Control Units 有权
    综合飞机飞行控制单元

    公开(公告)号:US20130211631A1

    公开(公告)日:2013-08-15

    申请号:US13736156

    申请日:2013-01-08

    CPC classification number: B64C13/04 B64C13/08 B64C13/12 B64C19/00 B64C27/57

    Abstract: According to one embodiment, an integrated aircraft trim assembly features a shaft, a mechanical stop, a trim motor, a clutch, and a measurement device. The mechanical stop device is operable to at least partially prevent rotation of the shaft outside of an allowable range of motion. The trim motor has an output component in mechanical communication with the shaft. The clutch separates the trim motor from the shaft. The measurement device is proximate to the shaft and operable to measure a position of the shaft and communicate the measured position to a flight control computer operable to change a position of a flight control device.

    Abstract translation: 根据一个实施例,集成飞行器装配组件具有轴,机械止动件,调整马达,离合器和测量装置。 机械停止装置可操作以至少部分地防止轴在允许的运动范围之外的旋转。 微调电机具有与轴机械连通的输出部件。 离合器将调整电机与轴分离。 测量装置靠近轴并且可操作以测量轴的位置并将测量位置传递到可操作以改变飞行控制装置的位置的飞行控制计算机。

    Pilot Control System with Pendent Grip
    12.
    发明申请
    Pilot Control System with Pendent Grip 有权
    带吊杆的先导控制系统

    公开(公告)号:US20130206898A1

    公开(公告)日:2013-08-15

    申请号:US13736135

    申请日:2013-01-08

    CPC classification number: B64C13/04 B64C27/56

    Abstract: According to one embodiment, a control assembly includes a post, a grip, and a shaft. The post has a top, a bottom, and a body joining the top to the bottom. The shaft havs a first end coupled proximate to the body below the top and a second end opposite the first end coupled to the grip. The shaft positions at least part of the grip directly over the top of the post.

    Abstract translation: 根据一个实施例,控制组件包括柱,手柄和轴。 该柱具有顶部,底部和与顶部连接的底部。 所述轴具有靠近所述主体的顶部附近的第一端和与所述把手相连的所述第一端相对的第二端。 轴将夹具的至少一部分直接定位在柱的顶部上。

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