Fuselage rear end of an aircraft, comprising: - a structural part (1) comprising a skin and longitudinal (30) and transversal reinforcing members (31, 32), and - a fairing (5). The structural part (1) longitudinally spans over the whole rear end and comprises a first portion (2) in which the transversal reinforcing members (32) occupy the whole perimeter of the corresponding fuselage section and at least a second portion (3) in which the transversal reinforcing members (31) occupy only a portion of the perimeter of the corresponding fuselage section, the fairing (5) being located below the second portion (3) of the structural part (1).


    Access

    Download


    Export, share and cite



    Title :

    Fuselage rear end of an aircraft


    Additional title:

    Rumpfheckende eines Flugzeugs
    Extrémité arrière du fuselage d'un aéronef



    Publication date :

    2018-07-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Aircraft fuselage configuration with upwardly deflected rear fuselage

    REWERTS STEPHEN D / BELL JEFFERY C / LUNDSTROM MICHAEL E | European Patent Office | 2023

    Free access

    Rear fuselage of an aircraft

    GARCIA PATINO MARIA ARÁNZAZU / POSTIGO RODRIGUEZ ANGEL / LÓPEZ FERNÁNDEZ DAVID | European Patent Office | 2018

    Free access

    Rear pressure bulkhead for aircraft, rear fuselage of aircraft, and aircraft

    PARTOUCHE LAURE / JONES JOHN ARTHUR / HOLMES CHRISTOPHER et al. | European Patent Office | 2021

    Free access

    Fuselage rear end of an aircraft

    ARÉVALO RODRÍGUEZ ELENA / CRUZ DOMÍNGUEZ FRANCISCO JOSÉ / MONEO PEÑACOBA ANA REYES | European Patent Office | 2020

    Free access

    Rear fuselage section of an aircraft

    GONZALEZ GOZALBO ALFONSO / LLAMAS SANDIN RAUL CARLOS | European Patent Office | 2016

    Free access