An aircraft navigation light, configured to be usable as any of a left forward navigation light (8), a right forward navigation light (8), and a tail navigation light (9) of an aircraft (2), comprises a common support plate (80) which is substantially vertical in the aircraft frame of reference; a first light source (81) arranged on the common support plate (80) for emitting red light; a second light source (82) arranged on the common support plate (80) for emitting green light; a third light source (83) arranged on the common support plate (80) for emitting white light; a driving circuit (110) coupled to the first light source (81), the second light source (82) and the third light source (83) and configured to supply power to a selected one of the first light source (81), the second light source (82), and the third light source (83); and a blocking element (85) arranged to limit the light output of the aircraft navigation light to one lateral side; wherein the first light source (81) and the second light source (82) are arranged asymmetrically with respect to a horizontal reference plane (A) through the common support plate (80), and/or wherein the third light source (83) is arranged farther from the blocking element (85) than the first and second light sources (81, 82).
AIRCRAFT NAVIGATION LIGHT AND AIRCRAFT COMPRISING THE SAME
FLUGZEUGNAVIGATIONSLICHT UND FLUGZEUG DAMIT
LUMIÈRE DE NAVIGATION D'AÉRONEF ET AÉRONEF LA COMPRENANT
2023-08-30
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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