Exterior aircraft light (2), comprising a light source (4) having a first electrode (6a) and a second electrode (6b) and a light source support (8) for supporting the light source (4), wherein the light source support (8) comprises conductive traces (9a, 9b) for supplying electric energy to the light source (4); and wherein the light source support (8) comprises a first group (16) of electric contact areas (10a), which are spaced from each other and which are electrically connected with each other, and a second group (18) of electric contact areas (10b), which are spaced from each other and which are electrically connected with each other. The first group (16) of electric contact areas (10a) and the second group (18) of electric contact areas (10b) form an extended electric contact structure that allows for the light source (4) to be positioned on the light source support (8) in a plurality of different positions. The first electrode (6a) of the light source (4) is soldered to a subset of the first group (16) of electric contact areas (10a) and the second electrode (6b) of the light source (4) is soldered to a subset of the second group (18) of electric contact areas (10b).
EXTERIOR AIRCRAFT LIGHT, AIRCRAFT COMPRISING AN EXTERIOR AIRCRAFT LIGHT, AND METHOD OF ASSEMBLING AN EXTERIOR AIRCRAFT LIGHT
FLUGZEUGAUSSENLEUCHTE, FLUGZEUG MIT EINER FLUGZEUGAUSSENLEUCHTE UND VERFAHREN ZUR MONTAGE EINER FLUGZEUGAUSSENLEUCHTE
LUMIÈRE EXTÉRIEURE D'AÉRONEF, AÉRONEF COMPRENANT UNE LUMIÈRE EXTÉRIEURE D'AÉRONEF ET PROCÉDÉ D'ASSEMBLAGE D'UNE LUMIÈRE EXTÉRIEURE D'AÉRONEF
2024-06-26
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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