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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    Title :

    AIRCRAFT INSULATION SYSTEM AND AIRCRAFT AIR CONDITIONING AND INSULATION ARRANGEMENT


    Additional title:

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


    Contributors:

    Publication date :

    2019-05-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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