An exterior aircraft light (101, 201, 301, 401) includes a housing (2) having a length (L), a width (W), and a height (H), the length (L) being greater than the width (W) and the height (H) and the housing (2) having a front end region (30) and a rear end region (32), wherein the housing (2) is configured to be mounted on a tail portion (105) of a fuselage (100) of an aircraft (110); at least one first light source (10), arranged in the rear end region (32) of the housing (2), for providing aircraft rearward signal lighting; and a plurality of second light sources (20), which are arranged spaced along the length (L) of the housing (2) for a distributed illumination of a stabilizer (102, 202, 104) of the aircraft (110).
EXTERIOR AIRCRAFT LIGHT, AIRCRAFT COMPRISING THE SAME, AND METHOD OF OPERATING AN EXTERIOR AIRCRAFT LIGHT
FLUGZEUGAUSSENLEUCHTE, FLUGZEUG MIT SOLCH EINER LEUCHTE UND VERFAHREN ZUM BETRIEB EINER FLUGZEUGAUSSENLEUCHTE
UNITÉ D'ÉCLAIRAGE EXTÉRIEUR D'AÉRONEF, AÉRONEF LA COMPRENANT ET PROCÉDÉ DE FONCTIONNEMENT D'UNE UNITÉ D'ÉCLAIRAGE EXTÉRIEUR D'AÉRONEF
2021-08-18
Patent
Elektronische Ressource
Englisch
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