An aircraft light (2) comprises a light source support board (4), having a light source side (4a) and a back side (4b); and a light source (6), arranged on the light source side (4a) of the light source support board (4); wherein the light source support board (4) comprises a first metallic layer (61), the first metallic layer (61) forming conductive traces on the light source side (4a) of the light source support board (4); an isolating layer (8); a second metallic layer (62), wherein the isolating layer (8) is arranged between the first metallic layer (61) and the second metallic layer (62) and isolates the second metallic layer (62) from the first metallic layer (61); and a support board core layer (10). A cavity (12) is provided in the support board core layer (10). The aircraft light (2) further comprises a metallic body (14), which is arranged within the cavity (12) of the light source support board (4), and the metallic body (14) has an inner end face (14a), which is soldered to the second metallic layer (62), and an outer end face (14b), which is substantially flush with the back side (4b) of the light source support board (4).


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    Title :

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


    Additional title:

    FLUGZEUGLEUCHTE, FLUGZEUG MIT EINER FLUGZEUGLEUCHTE UND VERFAHREN ZUR MONTAGE EINER FLUGZEUGLEUCHTE
    FEU D'AÉRONEF, AÉRONEF COMPRENANT UN FEU D'AÉRONEF ET PROCÉDÉ D'ASSEMBLAGE D'UN FEU D'AÉRONEF


    Contributors:

    Publication date :

    2025-04-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05K PRINTED CIRCUITS , Gedruckte Schaltungen



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