A heated composite structure and a method for forming a heated composite structure. The structure includes carbon fibers embedded within a thermoplastic matrix. The carbon fibers are connected with first and second electrodes that are configured to be connected with an electric source such that applying current to the electrodes causes current to flow through the embedded carbon fibers to provide resistive heating sufficient to heat the composite structure to impede formation of ice on the composite structure.


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    Titel :

    COMPOSITE AEROSTRUCTURE WITH INTEGRATED HEATING ELEMENT


    Beteiligte:
    HARDMAN KYLE B (Autor:in) / CALDER MARK A (Autor:in) / DERX IAN C (Autor:in)

    Erscheinungsdatum :

    2019-10-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / H05B ELECTRIC HEATING , Elektrische Heizung



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