Aircraft fuselages (102; 602; 702; 802) are disclosed herein. An example apparatus includes a fuselage (102; 602; 702; 802) of an aircraft having a first section (300; 604; 704; 804) and a second section (302; 606; 706; 806) to which a tail assembly (122; 610; 710; 810) is to be coupled. The second section (302; 606; 706; 806) is aft of the first section (300; 604; 704; 804) and is to extend to at least a trailing edge (308; 618; 718; 818) of a horizontal stabilizer (124; 612; 712; 812) of the tail assembly (122; 610; 710; 810). A first width of the first section (300; 604; 704; 804) decreases from a front to a rear of the first section (300; 604; 704; 804), and a second width of the second section (302; 606; 706; 806) is substantially constant. (Fig. 1)


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft fuselages


    Weitere Titelangaben:

    Flugzeugrümpfe
    Fuselages d'avion


    Beteiligte:

    Erscheinungsdatum :

    2020-12-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT FUSELAGES

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT FUSELAGES

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft fuselages

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft fuselages

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft fuselages

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2017

    Freier Zugriff