An aircraft insulation system (10) comprises a foil (42) extending at a distance from an inner surface (44) of an aircraft outer shell (32), an air gap (50) defined between the foil (42) and the aircraft outer shell (32), and a cabin exhaust air duct (28) arranged adjacent to an inner surface (43) of the foil (42) and being adapted to be flown through with cabin exhaust air.


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    Titel :

    AIRCRAFT INSULATION SYSTEM AND AIRCRAFT AIR CONDITIONING AND INSULATION ARRANGEMENT


    Weitere Titelangaben:

    FLUGZEUGISOLIERUNGSSYSTEM UND FLUGZEUGKLIMATISIERUNGS- UND -ISOLIERUNGSANORDNUNG
    SYSTÈME D'ISOLATION D'AÉRONEF, CLIMATISATION D'AÉRONEF ET AGENCEMENT D'ISOLATION


    Beteiligte:
    HUMFELDT DIRK (Autor:in)

    Erscheinungsdatum :

    01.05.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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