The present invention relates to a heating device for an aircraft interior. The heating device has a mechanically loadable support structure, a mechanically loadable and thermally conductive outer structure, and a heater for converting electrical energy into thermal energy, wherein the heater is arranged between the support structure and the outer structure and has a heating layer composed of a resistance material with a positive temperature coefficient.


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    Title :

    HEIZVORRICHTUNG UND VERFAHREN ZUM HERSTELLEN DERSELBEN


    Additional title:

    HEATING DEVICE AND METHOD FOR MANUFACTURING SAME
    DISPOSITIF DE CHAUFFAGE ET PROCÉDÉ DE FABRICATION


    Contributors:

    Publication date :

    2020-02-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    F24D DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATING SYSTEMS , Haus- oder Raumheizungssysteme, z.B. Zentralheizungssysteme / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



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