An aircraft headlight (2) comprises at least one visible light source (8) for emitting a headlight light output; a light transmissive cover (14), at least partially covering the at least one visible light source (8); and at least one infrared emitter (24) for emitting infrared radiation (28). At least 90 % of radiation energy, comprised in the infrared radiation (28) emitted by the at least infrared emitter (24), is emitted within a predefined wavelength range; and the light transmissive cover (14) allows at least 25 %, in particular at least 30 %, more particularly at least 45 %, of the radiation energy, which is emitted within the predefined wavelength range, to pass through the light transmissive cover (14).
AIRCRAFT HEADLIGHT, AIRCRAFT COMPRISING AN AIRCRAFT HEADLIGHT, AND METHOD OF OPERATING AN AIRCRAFT HEADLIGHT
FLUGZEUGSCHEINWERFER, FLUGZEUG MIT EINEM FLUGZEUGSCHEINWERFER UND VERFAHREN ZUM BETRIEB EINES FLUGZEUGSCHEINWERFERS
PHARE D'AÉRONEF, AÉRONEF COMPRENANT UN PHARE ET PROCÉDÉ DE FONCTIONNEMENT D'UN PHARE D'AÉRONEF
2023-03-01
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Europäisches Patentamt | 2024
|Europäisches Patentamt | 2023
|Europäisches Patentamt | 2024
|Dynamic aircraft headlight and method of operating a dynamic aircraft headlight
Europäisches Patentamt | 2018
|Europäisches Patentamt | 2024
|