The invention relates to a temperature-control device (100) for an aircraft (102), which device has a first layer (104) and a second layer (106) opposite the first layer (104), a heating layer (108), which is arranged between the first layer (104) and the second layer (106), and a separating layer (110), which is arranged between the heating layer (108) and the second layer (106). The separating layer (110) is shaped so as to allow a relative movement between the heating layer (108) and the second layer (106).


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    Title :

    TEMPERIERVORRICHTUNG FÜR EIN LUFTFAHRZEUG UND VERFAHREN ZUM HERSTELLEN EINER TEMPERIERVORRICHTUNG


    Additional title:

    TEMPERATURE-CONTROL DEVICE FOR AN AIRCRAFT AND METHOD FOR PRODUCING A TEMPERATURE-CONTROL DEVICE
    DISPOSITIF DE RÉGULATION THERMIQUE POUR UN AÉRONEF ET PROCÉDÉ DE FABRICATION D'UN DISPOSITIF DE RÉGULATION THERMIQUE


    Contributors:
    THRON KAI (author)

    Publication date :

    2022-04-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    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 / H05B ELECTRIC HEATING , Elektrische Heizung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT