A cover (62) for an exterior aircraft light (6) includes a lens cover structure (70), attachable to an exterior aircraft light housing (60) and configured to close the exterior aircraft light housing (60), wherein the lens cover structure (70) has an inside and an outside and is at least partially made of transparent material; and a wear indicator (80), attached to the inside of the lens cover structure (70), the wear indicator (80) having a contrasted pattern (90) visible from the outside of the lens cover structure (70) through the transparent material.
COVER FOR AN EXTERIOR AIRCRAFT LIGHT, EXTERIOR AIRCRAFT LIGHT, AND METHOD OF DETERMINING A WEAR STATE OF A LENS COVER STRUCTURE
ABDECKUNG FÜR EIN ÄUSSERES FLUGZEUGLICHT, ÄUSSERES FLUGZEUGLICHT UND VERFAHREN ZUR BESTIMMUNG EINES VERSCHLEISSZUSTANDS EINER LINSENABDECKUNGSSTRUKTUR
COUVERCLE POUR LUMIÈRE D'AÉRONEF EXTÉRIEURE, LUMIÈRE D'AÉRONEF EXTÉRIEURE ET PROCÉDÉ DE DÉTERMINATION D'UN ÉTAT D'USURE D'UNE STRUCTURE DE COUVERCLE DE LENTILLE
2021-08-11
Patent
Elektronische Ressource
Englisch
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