In an embodiment, a layer material (10, 30, 40) configured to be arranged on a rotor blade tip of a helicopter (6) comprises at least one light emitting section (11) that emits light after absorption of photons directed onto the layer material by a remote light source (71-74). According to another embodiment, a layer material (20, 30, 40) configured to be arranged on a rotor blade tip of a helicopter (6) comprises at least one light reflecting section (21) that reflects light directed onto the layer material by a remote light source (71-74). A helicopter light system (1) for arranging on a helicopter comprises at least one such layer material (10, 20, 30, 40) which is configured to be arranged on a side of a rotor blade tip (632) of the helicopter facing the helicopter body, and at least one light source (71-74) that is configured to be arranged on the helicopter body and to direct light onto the layer material for emitting and/or reflecting visible light by the at least one layer material during rotation of the rotor blade (63) of the helicopter.


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    Titel :

    HELICOPTER LIGHT SYSTEM WITH LAYER MATERIAL ARRANGED ON A ROTOR BLADE TIP OF THE HELICOPTER AND HELICOPTER COMPRISING THE SAME


    Weitere Titelangaben:

    HUBSCHRAUBERBELEUCHTUNGSSYSTEM MIT EINEM SCHICHTMATERIAL ZUR ANORDNUNG AUF EINER ROTORBLATTSPITZE DES HUBSCHRAUBERS SOWIE HUBSCHRAUBER DAMIT
    SYSTÈME LUMINEUX D'HÉLICOPTÈRE AVEC UN MATÉRIAU EN COUCHE DESTINÉ À ÊTRE DISPOSÉ SUR UNE POINTE DE PALE DE ROTOR DUDIT HÉLICOPTÈRE ET HÉLICOPTÈRE COMPRENANT CELUI-CI


    Beteiligte:

    Erscheinungsdatum :

    2020-01-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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