An aircraft exterior anti-collision light system (200) comprises a plurality of anti-collision lights (120a, 120b, 128a-128c) and a bus (210), wherein each of the plurality of anti-collision lights (120a, 120b, 128a-128c) is coupled to the bus (210). Each of the plurality of anti-collision lights (120a, 120b, 128a-128c) comprises at least one light source (121a, 121b, 129a-129c) and is configured to emit a sequence of light flashes (R, W). Each of the plurality of anti-collision lights (120a, 120b, 128a-128c) is configured to carry out an initialization routine in response to an activation command. Each of the plurality of anti-collision lights (120a, 120b, 128a-128c) is configured to transmit an activation status message on the bus (210), after the initialization routine has been carried out. Each of the plurality of anti-collision lights (120a, 120b, 128a-128c) is configured to listen on the bus (210) for activation status messages and to log activation status messages received on the bus (210). Each of the plurality of anti-collision lights (120a, 120b, 128a-128c) is configured to set a timing of the sequence of light flashes (R, W) depending on the activation status messages received on the bus (210).
AIRCRAFT EXTERIOR ANTI-COLLISION LIGHT SYSTEM, AIRCRAFT, AND METHOD OF OPERATING AN EXTERIOR ANTI-COLLISION LIGHT SYSTEM
ÄUSSERES ANTIKOLLISIONSLICHTSYSTEM FÜR FLUGZEUGE, FLUGZEUG UND VERFAHREN ZUM BETRIEB EINES ÄUSSEREN ANTIKOLLISIONSLICHTSYSTEMS
SYSTÈME DE FEUX ANTI-COLLISION EXTÉRIEURS D'AVION, AVION, ET PROCÉDÉ DE FONCTIONNEMENT D'UN SYSTÈME DE FEUX ANTI-COLLISION EXTÉRIEURS
2023-10-25
Patent
Electronic Resource
English
European Patent Office | 2023
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