An aircraft navigation light with integrated redundancy having at least a selected minimum light output, comprises a first light source; a second light source; and a common optical element, which is configured for shaping an output light intensity distribution of the aircraft navigation light. The light emitted by each of the first light source and the second light source is modified by the common optical element. Each of the first and second light sources has an individual light output capacity, wherein the individual light output capacity of each of the first and second light sources alone is sufficient for providing the selected minimum light output of the aircraft navigation light.
AIRCRAFT NAVIGATION LIGHT AND AIRCRAFT COMPRISING THE SAME
2019-05-16
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F21V FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF , Funktionsmerkmale oder Einzelheiten von Leuchten oder Beleuchtungssystemen / H05B ELECTRIC HEATING , Elektrische Heizung / H05K PRINTED CIRCUITS , Gedruckte Schaltungen |
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