An aircraft heated floor panel, comprising a first face sheet (106), a second face sheet (108) opposite the first face sheet, a core (110) with an insulating core portion (124, 126) and a conductive core portion (112), and a lead (102, 104) electrically connected to the conductive core portion, wherein the insulating core portion separates the conductive core portion from the first face sheet, wherein the insulating core portion and the conductive core portion both supporting the first face sheet and the second face sheet, and wherein the conductive core portion is electrically insulated from the external environment by the first and second faces to resistively heat the first face sheet.


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    Titel :

    HEATED AIRCRAFT FLOOR PANELS


    Weitere Titelangaben:

    BEHEIZTES FLUGZEUGDECK
    PANNEAUX DE PLANCHER CHAUFFÉS D'AÉRONEF


    Beteiligte:
    OWENS GEORGE (Autor:in) / ROACH KEVIN E (Autor:in) / MULLEN JAMES (Autor:in) / GIAMATI MICHAEL J (Autor:in) / SHEARER JON (Autor:in) / TWISK JAMES V (Autor:in) / BRITTINGHAM DAVID L (Autor:in) / WILSON TOM (Autor:in) / HU JIN (Autor:in) / VERONESI WILLIAM A (Autor:in)

    Erscheinungsdatum :

    2019-08-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F24D DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATING SYSTEMS , Haus- oder Raumheizungssysteme, z.B. Zentralheizungssysteme



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