An exterior lamp for an aircraft including a housing defining an interior volume, a heat source disposed within the interior volume of the housing, a light source disposed within the housing configured to emit a light therefrom, a protective lens coupled to the housing proximate the light source, wherein the protective lens is configured to transmit the light, and a capillary transport apparatus having a first end and a second end wherein the first end is coupled to the heat source and the second end is disposed in a catchment basin.


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    Titel :

    SYSTEMS AND METHODS FOR MITIGATING CONDENSATION IN AIRCRAFT LIGHTING


    Beteiligte:
    PHIFER VAN I (Autor:in)

    Erscheinungsdatum :

    22.07.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F21V FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF , Funktionsmerkmale oder Einzelheiten von Leuchten oder Beleuchtungssystemen



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