A system for inductive heating of an aircraft surface includes a conductive outer layer (108) configured to be located on an outer portion (106) of the aircraft surface (104). The system further includes a carbon nanotube (CNT) yarn (110) configured to receive and conduct electrical current. The system further includes an insulator (118) 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


    Weitere Titelangaben:

    KOHLENSTOFFNANORÖHREN- ODER KOHLENSTOFFALLOTROP-BASIERTE INDUKTIONSHEIZUNG FÜR DEN EISSCHUTZ VON FLUGZEUGEN
    CHAUFFAGE PAR INDUCTION BASÉ SUR NANOTUBE (CNT) OU ALLOTROBE À BASE DE CARBONE POUR PROTECTION ANTIGIVRE D'AÉRONEF


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

    Erscheinungsdatum :

    04.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



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