An aircraft fuselage including an outer skin that is stiffened by way of a backing structure and that delimits at least one passenger cabin and one cargo hold. In the vertical direction of the fuselage, the cargo hold is arranged below the passenger cabin. The backing structure in the cargo hold above a cargo-hold floor framework comprises at least two lateral quasi-joints, and below the cargo-hold floor framework comprises at least one further quasi-joint. In the cargo hold, in the longitudinal direction of the fuselage, a multitude of energy absorption devices, arranged one behind the other and acting in the transverse direction of the fuselage, are arranged for absorbing tensile loads.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft fuselage


    Contributors:

    Publication date :

    2016-06-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft fuselage section, aircraft fuselage and aircraft

    LINDE PETER / MATTHIAS HEGENBART | European Patent Office | 2023

    Free access

    Aircraft fuselage

    MARGULL LARS / WAIMER MATTHIAS / SCHATROW PAUL et al. | European Patent Office | 2015

    Free access

    FUSELAGE SECTION OF AN AIRCRAFT, AIRCRAFT FUSELAGE, AND AIRCRAFT

    LINDE PETER / HEGENBART MATTHIAS | European Patent Office | 2023

    Free access

    FUSELAGE SECTION OF AN AIRCRAFT, AIRCRAFT FUSELAGE, AND AIRCRAFT

    LINDE PETER / HEGENBART MATTHIAS | European Patent Office | 2022

    Free access

    AIRCRAFT FUSELAGE

    BRUTYAN MURAD ABRAMOVICH / VOLKOV ANDREJ VIKTOROVICH / POTAPCHIK ALEKSANDR VLADIMIROVICH | European Patent Office | 2020

    Free access