An aircraft light (2) comprises a support board (6); a light source (4), arranged on the support board (6); a first optical element (8), which is at least partially light transmissive, which is arranged over the light source (4), and which is fixed to the support board (6); and a second optical element (10), which is at least partially light transmissive, wherein the first optical element (8) is interposed between the light source (4) and the second optical element (10). The first optical element (8) has a first engagement portion (12) and the second optical element (10) has a second engagement portion (14). The first engagement portion (12) and the second engagement portion (14) establish a positive fit between the first optical element (8) and the second optical element (10). At least a portion of light, which is emitted by the light source (4) in operation, passes through the first optical element (8) and through the second optical element (10).


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    Title :

    AIRCRAFT LIGHT, AIRCRAFT, AND METHOD OF ASSEMBLING AN AIRCRAFT LIGHT


    Additional title:

    FLUGZEUGLICHT, FLUGZEUG UND VERFAHREN ZUR MONTAGE EINES FLUGZEUGLICHTS
    LUMIÈRE D'AÉRONEF, AÉRONEF, ET PROCÉDÉ D'ASSEMBLAGE D'UNE LUMIÈRE D'AÉRONEF



    Publication date :

    2023-08-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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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