An internal cladding part for cladding a fuselage structure of an aircraft is disclosed having a first cover layer that extends in a planar manner, a second cover layer that extends in a planar manner, a core layer which is disposed between the first and the second cover layer and is connected to the first and the second cover layer and defines a receptacle cavity, and an insulation structure having a porous insulation core and an evacuated film sheath that encases the insulation core in a gas-tight manner. The insulation structure is disposed in the receptacle cavity between the first and the second cover layer.


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    Title :

    INNENVERKLEIDUNGSTEIL ZUR VERKLEIDUNG EINER RUMPFSTRUKTUR EINES LUFTFAHRZEUGS


    Additional title:

    INTERIOR CLADDING SECTION FOR COVERING A FUSELAGE STRUCTURE OF AN AIRCRAFT
    PARTIE DE REVÊTEMENT INTÉRIEUR DESTINÉ AU REVÊTEMENT D'UNE STRUCTURE DE FUSELAGE D'UN AÉRONEF


    Contributors:

    Publication date :

    2021-10-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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