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 :

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


    Publication date :

    2018-01-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

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