A heated floor panel system (1) for an aircraft, said floor panel system (1) comprising a floor panel element (3) including a panel structure (11) and a panel heater device (13), a temperature sensor device (5) for detecting the temperature at the floor panel element (3), and a connector device (7) connected to the floor panel element (3), wherein the connector device (7) comprises a power link (23) for providing an electric power connection between the panel heater device (13) and an electric power supply (27), and a data link (25) for providing a data connection between the temperature sensor device (5) and a control unit (9). The object of the present invention, to provide a floor panel system (1) including a floor panel element (3) which has a possibly simple construction and which can be used independently from the connector device (7), is achieved in that the temperature sensor device (5) is located in the connector device (7) and connected to the floor panel element (3) via a thermal conductor element (29).


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    Title :

    A HEATED FLOOR PANEL SYSTEM FOR AN AIRCRAFT


    Additional title:

    BEHEIZTES BODENPLATTENSYSTEM FÜR EIN FLUGZEUG
    SYSTÈME DE PANNEAU DE PLANCHER CHAUFFANT POUR UN AVION


    Contributors:

    Publication date :

    2018-04-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F24D DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATING SYSTEMS , Haus- oder Raumheizungssysteme, z.B. Zentralheizungssysteme / H05B ELECTRIC HEATING , Elektrische Heizung



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