A heated floor panel system for an aircraft, the floor panel system comprising a floor panel element including a panel structure and a panel heater device, a temperature sensor device for detecting the temperature at the floor panel element, and a connector device connected to the floor panel element, wherein the connector device comprises a power link for providing an electric power connection between the panel heater device and an electric power supply, and a data link for providing a data connection between the temperature sensor device and a control unit. An object of the present disclosure, to provide a floor panel system including a floor panel element which has a possibly simple construction and which can be used independently from the connector device, is achieved in that the temperature sensor device is located in the connector device and connected to the floor panel element via a thermal conductor element.


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    Title :

    Heated floor panel system for an aircraft


    Contributors:

    Publication date :

    2020-08-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / 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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