The invention relates to a side lever grip with minimum cross axis control coupling. Specifically, a side lever grip is disclosed that minimizes intersecting axis control coupling about three or more control axes, where one of the control axes provides a directional (yaw) input by twisting the grip in a clockwise/counterclockwise direction. Minimizing cross axis control in accordance with the embodiments disclosed herein is achieved primarily by substantially coincidence of a grip reference point (GRP) of the side lever grip (i.e., a theoretical point at which pitch and roll forces are applied) with the yaw axis of rotation. By providing the GRP substantially coincident with the yaw rotation axis, unexpected yaw torque is minimized when control inputs are applied on the side levers on a pitch axis and a roll axis.

    本发明涉及具有最小交叉轴线控制耦合的侧杆握把。具体地,公开了这样的侧杆握把,所述侧杆握把使围绕三个以上控制轴线的交叉轴线控制耦合最小化,其中,所述控制轴线中的一个通过在顺时针/逆时针方向上扭转所述握把来提供方向(偏航)输入。根据本文所公开的实施例最小化交叉轴线控制主要通过使所述侧杆握把的握把基准点(GRP)(即,施加俯仰力和翻滚力的理论点)与偏航旋转轴线基本上重合来实现。通过提供与所述偏航旋转轴线基本上重合的所述GRP,当控制输入在俯仰轴线和翻滚轴线上施加在所述侧杆上时,使意外的偏航扭矩最小化。


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    Titel :

    Side lever grip with minimum cross axis control coupling


    Weitere Titelangaben:

    具有最小交叉轴线控制耦合的侧杆握把



    Erscheinungsdatum :

    13.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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