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).


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    Title :

    CONTROL LEVER ASSEMBLY FOR CONTROLLING AN AIRCRAFT SYSTEM


    Additional title:

    STEUERHEBELANORDNUNG ZUR STEUERUNG EINES FLUGZEUGSYSTEMS
    ENSEMBLE LEVIER DE COMMANDE POUR COMMANDER UN SYSTÈME D'AÉRONEF


    Contributors:

    Publication date :

    2023-03-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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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