An aircraft fuselage includes at least one space arranged in the aircraft fuselage and at least one wall. The wall resists burnthrough for a period of at least four minutes from outside the aircraft fuselage towards the space, wherein the region of the aircraft fuselage underneath the space does not include burnthrough-resistant insulation. The space may be a cargo compartment of the aircraft or a passenger cabin, while the wall may be designed as a cargo compartment floor, passenger cabin floor or wing/fuselage fairing (belly fairing). The design of the aircraft fuselage results in burnthrough resistance that meets the requirements of FAR §25.856 (b) without any additional burnthrough-resistant insulation in the aircraft fuselage.


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    Titel :

    Aircraft fuselage having burnthrough resistant components


    Beteiligte:

    Erscheinungsdatum :

    2018-01-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Full Scale Fuselage Burnthrough Tests

    Sarkos, G. | British Library Conference Proceedings | 1991


    Burnthrough Resistance of Fuselage and Cabin Structures

    Povey, N. J. / Dodd, D. C. / Marker, T. R. et al. | British Library Conference Proceedings | 1997


    BURNTHROUGH PROTECTION SYSTEM

    FERNANDO JOSEPH A / GARVEY CHAD E / RIOUX ROBERT et al. | Europäisches Patentamt | 2017

    Freier Zugriff


    BURNTHROUGH PROTECTION SYSTEM

    FERNANDO JOSEPH A / GARVEY CHAD E / RIOUX ROBERT et al. | Europäisches Patentamt | 2017

    Freier Zugriff