An aircraft headlight includes at least one visible light source for emitting a headlight light output; a light transmissive cover, at least partially covering the at least one visible light source; and at least one infrared emitter for emitting infrared radiation. At least 90% of radiation energy, comprised in the infrared radiation emitted by the at least infrared emitter, is emitted within a predefined wavelength range; and the light transmissive cover 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.
AIRCRAFT HEADLIGHT, AIRCRAFT COMPRISING AN AIRCRAFT HEADLIGHT, AND METHOD OF OPERATING AN AIRCRAFT HEADLIGHT
2023-03-02
Patent
Electronic Resource
English
European Patent Office | 2024
|European Patent Office | 2024
|AIRCRAFT HEADLIGHT AND AIRCRAFT COMPRISING AN AIRCRAFT HEADLIGHT
European Patent Office | 2025
|AIRCRAFT HEADLIGHT AND AIRCRAFT COMPRISING AN AIRCRAFT HEADLIGHT
European Patent Office | 2025
|European Patent Office | 2024
|