Described and illustrated is a floor panel (1) for an aircraft, said floor panel (1) comprising a panel structure (3) for transmitting forces applied to the floor panel (1), wherein the panel structure (3) includes an upper cover layer (7), a lower cover layer (9), and a core assembly (11) sandwiched between the upper and lower cover layers (7, 9), and a heater layer (5) for heating the floor panel (1), wherein the heater layer (5) is provided between the upper and lower cover layers (7, 9). The object of the present invention, to provide a possibly simple heated floor panel for an aircraft, wherein the risk of overheating and at the same time the risk of local hot spots at the heater layer is reduced, is achieved in that the heater layer (5) is formed as a PTC-layer having a plurality of electric conductor paths (27) interconnected to one another by a plurality of PTC-resistor paths (29) comprising a PTC-material, wherein the electric resistance of said PTC-Material increases with increasing temperature.


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    Titel :

    A floor panel for an aircraft, and an aircraft comprising such a floor panel


    Weitere Titelangaben:

    Bodenplatte für ein Flugzeug und Flugzeug mit solch einer Bodenplatte
    Panneau de plancher pour un aéronef et aéronef comprenant un tel panneau


    Beteiligte:

    Erscheinungsdatum :

    29.05.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / 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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