An aircraft beacon light (120, 120a, 120b) comprises a plurality of primary light sources (6) for emitting light into at least two spatial sectors (12-18), wherein the at least two spatial sectors (12-18) include a forward sector (12) and at least one of an aft sector (14), a starboard lateral sector (16), and a portside lateral sector (18); and a light transmissive cover (4), which covers the plurality of primary light sources (6). The plurality of primary light sources (6) are arranged and configured for providing an FAR-compliant aircraft beacon light output of the aircraft beacon light (120, 120a, 120b), in case of the light transmissive cover (4) being in a non-eroded state. The aircraft beacon light (120, 120a, 120b) further comprises at least one booster light source (20) for selectively emitting a booster light output into the forward sector (12). The at least one booster light source (20) is controllable independently of the plurality of primary light sources.
AIRCRAFT BEACON LIGHT, AIRCRAFT WITH AN AIRCRAFT BEACON LIGHT AND METHOD OF OPERATING AN AIRCRAFT BEACON LIGHT
FLUGZEUGBAKENLEUCHTE, FLUGZEUG MIT EINER FLUGZEUGBAKENLEUCHTE UND VERFAHREN ZUM BETRIEB EINER FLUGZEUGBAKENLEUCHTE
BALISE LUMINEUSE D'AÉRONEF, AÉRONEF COMPRENANT UNE BALISE LUMINEUSE D'AÉRONEF ET PROCÉDÉ DE FONCTIONNEMENT D'UNE BALISE LUMINEUSE D'AÉRONEF
2024-03-20
Patent
Elektronische Ressource
Englisch
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