An aircraft winglet light assembly 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 of holes 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 proximate to the one or more sets of holes.


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    Titel :

    Aircraft winglet light assembly


    Beteiligte:

    Erscheinungsdatum :

    22.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F21V FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF , Funktionsmerkmale oder Einzelheiten von Leuchten oder Beleuchtungssystemen / F21Y Index-Schema in Verbindung mit den Unterklassen F21K, F21L, F21S und F21V, betreffend die Form oder die Art der Lichtquellen oder die Farbe des emittierten Lichts , INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO THE FORM OR THE KIND OF THE LIGHT SOURCES OR OF THE COLOUR OF THE LIGHT EMITTED



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