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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    КОНСТРУКЦИЯ ДЛЯ ИЗОЛЯЦИИ ВОЗДУШНОГО СУДНА, СИСТЕМА КОНДИЦИОНИРОВАНИЯ ВОЗДУХА И ИЗОЛЯЦИИ ВОЗДУШНОГО СУДНА И СПОСОБ РАБОТЫ ТАКОЙ СИСТЕМЫ


    Erscheinungsdatum :

    23.01.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

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