A damage recovery system of a fuselage (1) of an aircraft (3), comprising: a tank (8) containing a polyurethane foam; a main duct (10a) fluidically coupled to the tank to receive the foam; secondary ducts (10b) fluidically coupled to the main duct; and distribution means (12) adapted to allow an outflow of the foam from the secondary ducts. Graphene powder can be mixed and added to the polyurethane foam. In flight, a possible leak (crack or hole) in the fuselage is plugged by the polyurethane foam with graphene powder.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    СИСТЕМА ДЛЯ УЛУЧШЕНИЯ ПРОЧНОСТИ КОНСТРУКЦИИ САМОЛЕТА И САМОЛЕТ, СОДЕРЖАЩИЙ ТАКУЮ СИСТЕМУ


    Erscheinungsdatum :

    2020-05-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

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