A lever assembly (10) for controlling an aircraft system, comprising: a housing (30) having an outer side (33) and an aperture (35) delimited by a rim (36); and a control rod (20), the control rod (20) extending through the aperture (35) and being movable in the aperture (35); the control rod (20) has an outer cover member (61) arranged to slide over the outer side (33) of the housing (30) and to cover the rim (36) over the entire range of movement of the control rod (20).

    一种用于控制航空器系统的控制杆组合件(10),包括:壳体(30),所述壳体(30)具有外侧(33)和由边沿(36)界定的孔口(35);以及控制杆(20),所述控制杆(20)延伸穿过所述孔口(35)并且能够在所述孔口(35)中移动;所述控制杆(20)具有外覆盖部件(61),所述外覆盖部件(61)被布置成在所述壳体(30)的所述外侧(33)之上滑动并且在所述控制杆(20)的整个移动范围内覆盖所述边沿(36)。


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    Titel :

    Control lever assembly for controlling aircraft system


    Weitere Titelangaben:

    用于控制航空器系统的控制杆组合件


    Beteiligte:
    SOULIER AURELIEN (Autor:in) / MOLENIS PETER (Autor:in)

    Erscheinungsdatum :

    17.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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