A system for inductive heating of an aircraft surface includes a conductive outer layer configured to be located on an outer portion of the aircraft surface. The system further includes a carbon nanotube (CNT) yarn configured to receive and conduct electrical current. The system further includes an insulator located between the conductive outer layer and the CNT yarn such that the electrical current flowing through the CNT yarn generates induction heating on the conductive outer layer.


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    Titel :

    CARBON NANOTUBE (CNT) OR CARBON ALLOTROBE BASED INDUCTION HEATING FOR AIRCRAFT ICE PROTECTION


    Beteiligte:
    HU JIN (Autor:in) / BOTURA GALDEMIR CEZAR (Autor:in) / ATALLA MAURO J (Autor:in)

    Erscheinungsdatum :

    30.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / C01B NON-METALLIC ELEMENTS , Nichtmetallische Elemente / D02G CRIMPING OR CURLING FIBRES, FILAMENTS, YARNS, OR THREADS , Kräuseln oder Texturieren von Fasern, Fäden, Garnen oder Zwirnen / H01B CABLES , Kabel



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