An aircraft winglet light assembly (102) is disclosed. The aircraft winglet light assembly includes an exterior skin coupled to an aircraft winglet of an aircraft. At least one interior surface of the exterior skin defines a cavity within the exterior skin. The aircraft winglet light assembly further includes one or more illumination sources housed within the cavity. The aircraft winglet light assembly further includes one or more sets (110) of holes (200) within the exterior skin. The one or more sets of holes are configured to allow illumination generated by the one or more illumination sources to pass through the exterior skin. The aircraft winglet light assembly further includes one or more protection elements (112) proximate to the one or more sets of holes.


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    Title :

    AIRCRAFT WINGLET LIGHT ASSEMBLY


    Additional title:

    LICHTANORDNUNG FÜR FLUGZEUG-WINGLETS
    ENSEMBLE D'ÉCLAIRAGE D'AILETTE D'AÉRONEF


    Contributors:

    Publication date :

    2024-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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