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


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    CONTROL LEVER ASSEMBLY FOR CONTROLLING AN AIRCRAFT SYSTEM


    Weitere Titelangaben:

    ASSEMBLAGE DE LEVIER DE COMMANDE POUR CONTROLER UN SYSTEME DE BORD D'AERONEF


    Beteiligte:
    SOULIE ARNAUD (Autor:in) / MOULENES PATRICK (Autor:in)

    Erscheinungsdatum :

    13.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16J Kolben , PISTONS / B64C AEROPLANES , Flugzeuge



    Control lever assembly for controlling aircraft system

    SOULIER AURELIEN / MOLENIS PETER | Europäisches Patentamt | 2023

    Freier Zugriff

    CONTROL LEVER ASSEMBLY FOR CONTROLLING AN AIRCRAFT SYSTEM

    SOULIÉ ARNAUD / MOULÈNES PATRICK | Europäisches Patentamt | 2023

    Freier Zugriff

    CONTROL LEVER ASSEMBLY FOR CONTROLLING AN AIRCRAFT SYSTEM

    SOULIE ARNAUD / MOULENES PATRICK | Europäisches Patentamt | 2023

    Freier Zugriff

    Control lever assembly for controlling an aircraft system

    SOULIÉ ARNAUD / MOULÈNES PATRICK | Europäisches Patentamt | 2024

    Freier Zugriff

    Control lever for controlling a rotary wing, a mechanical control system including said control lever, and an aircraft

    COUDERC GÉRARD / BIEST ROMUALD | Europäisches Patentamt | 2015

    Freier Zugriff