An exterior aircraft light unit comprises a housing, at least one light source, and a heat sink. The heat sink includes at least one first heat sink portion and at least one second heat sink portion. The at least one light source is thermal connected with the at least one first heat sink portion for transferring heat from the at least one light source to the at least one first heat sink portion; and the at least one second heat sink portion is configured to be selectively attachable to the at least one first heat sink portion.


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    Title :

    Exterior aircraft light unit


    Contributors:

    Publication date :

    2020-03-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F21S Ortsfeste Leuchten , NON-PORTABLE LIGHTING DEVICES / F21V FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF , Funktionsmerkmale oder Einzelheiten von Leuchten oder Beleuchtungssystemen



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