DE-ICING LIGHT SYSTEMS, ASSEMBLIES, AND METHODS FOR AIRCRAFTS

A de-icing light assembly (100) may comprise: a housing (120); a plurality of lights (110) coupled to the housing; a lens assembly (130) coupled to the housing, the lens assembly comprising: a lens material (132); an indium tin oxide (ITO) film (134) disposed on the lens material; and a silicon oxid...

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Bibliographic Details
Main Authors RAO, Sreekanth Koti Ananda, REDDY, Chana Kesava, AGARWAL, Ashish Kumar, SUBRAMANIAN, Petchi
Format Patent
LanguageEnglish
French
German
Published 25.10.2023
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HEATING
LIGHTING
MECHANICAL ENGINEERING
NON-PORTABLE LIGHTING DEVICES
PARACHUTES
PERFORMING OPERATIONS
SYSTEMS THEREOF
TRANSPORTING
VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLEEXTERIORS
WEAPONS
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Summary:A de-icing light assembly (100) may comprise: a housing (120); a plurality of lights (110) coupled to the housing; a lens assembly (130) coupled to the housing, the lens assembly comprising: a lens material (132); an indium tin oxide (ITO) film (134) disposed on the lens material; and a silicon oxide coating (136) disposed on the ITO film.
Bibliography:Application Number: EP20230154053