A fuselage assembly for an aircraft including a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Fuselage assembly for an aircraft



    Erscheinungsdatum :

    2020-12-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aircraft fuselage assembly and aircraft

    HE JIANBING / XU ZHIQIN / XIAO DINGFENG et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Assembly method for assembling aircraft fuselage panel, fuselage part and aircraft

    AGUERA DAMIEN / DE KERGOMMEAUX MATHIEU / DENTESANO JOHN | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT FUSELAGE ASSEMBLY JIG AND METHOD FOR HANDLING AIRCRAFT FUSELAGE PANEL

    KASAHARA KENJI / SEGAWA SHUHEI | Europäisches Patentamt | 2017

    Freier Zugriff

    Camera assembly, aircraft fuselage and aircraft

    LI ZHIGUO / DAI YIN / WANG YANWEI | Europäisches Patentamt | 2023

    Freier Zugriff

    FUSELAGE ASSEMBLY FOR AN AIRCRAFT

    SCHROEDER MATTHIAS / BATANERO BENITO JESUS MIGUEL / SRINIVASAN SRIVATS et al. | Europäisches Patentamt | 2024

    Freier Zugriff