An aircraft insulation system comprising a foil extending at a distance from an inner surface of an aircraft outer shell. An air gap is defined between the foil and the aircraft outer shell. A cabin exhaust air duct is arranged adjacent to an inner surface of the foil and being adapted to have cabin exhaust air flow through the duct.


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    Titel :

    AIRCRAFT INSULATION SYSTEM AND AIRCRAFT AIR CONDITIONING AND INSULATION ARRANGEMENT


    Beteiligte:
    HUMFELDT DIRK (Autor:in)

    Erscheinungsdatum :

    2017-02-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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