An aircraft rudder and brake pedal assembly includes a rudder arm assembly having a rudder arm with a first upper arm portion and a first lower arm portion and another rudder arm with a second upper arm portion and a second lower arm portion. The rudder arm assembly is fitted to the beam at an intersection of the first upper arm portion and the first lower arm portion and an intersection of the second upper arm portion and the second lower arm portion. The first rudder arm and the second rudder arm are configured to rotate around the beam at the intersection. Rotation of the first and second rudder arms is configured to adjust a control surface that controls a yaw axis of the aircraft. A brake pedal is attached to the first lower arm portion and the second lower arm portion. Rotation of the brake pedal brakes the aircraft. A rotation sensor is fitted to the brake pedal and the lower arm portion, and is configured to determine a degree of rotation of the brake pedal.

    一种飞机方向舵和制动踏板组件,包括舵臂组件,该舵臂组件具有一个带有第一上臂部和第一下臂部的舵臂,以及另一个带有第二上臂部和第二下臂部的舵臂。舵臂组件在第一上臂部和第一下臂部的交叉处以及第二上臂部和第二下臂部的交叉处被装配至梁。第一舵臂和第二舵臂构造为在交叉处围绕梁旋转。第一舵臂和第二舵臂的旋转构造为调整控制飞机的偏航轴的控制表面。制动踏板附接至第一下臂部和第二下臂部。制动踏板的旋转使飞机制动。旋转传感器被装配至制动踏板和下臂部,并且构造为确定制动踏板旋转的程度。


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    Titel :

    Rudder and brake pedal assembly


    Weitere Titelangaben:

    方向舵和制动踏板组件


    Beteiligte:
    WALLS JEFFREY T (Autor:in) / STARKNICK DARRYL S (Autor:in) / ROMANA ROY (Autor:in)

    Erscheinungsdatum :

    2022-06-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05G CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY , Steuer- oder Regelvorrichtungen oder Steuer- oder Regelsysteme gekennzeichnet ausschließlich durch mechanische Einzelheiten



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