The fuselage of an aircraft comprises a floor structure, a roof structure, a first lateral side structure, a second lateral side structure, and a middle structure. The floor structure, the roof structure, the first lateral side structure, and the second lateral side structure define a fuselage space between them. The middle structure spans at least part way between the floor structure and the roof structure, and runs between the first lateral side structure and the second lateral side structure such that the middle structure partitions the fuselage space into an occupant space and a cargo space. A seat for a pilot is disposed in the occupant space lateral to a portion of the middle structure and a portion of the cargo space.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT ADAPTED FOR TRANSPORTING CARGO


    Beteiligte:

    Erscheinungsdatum :

    2016-08-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT ADAPTED FOR TRANSPORTING CARGO

    PAUL JOHN-CURTISS / RAEDER JAMES D | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft adapted for transporting cargo

    PAUL JOHN-CURTISS / RAEDER JAMES D | Europäisches Patentamt | 2016

    Freier Zugriff

    Cargo transporting systems for tailsitter aircraft

    IVANS STEVEN RAY / ROSS BRENT CHADWICK | Europäisches Patentamt | 2023

    Freier Zugriff

    Cargo Transporting Systems for Tailsitter Aircraft

    IVANS STEVEN RAY / ROSS BRENT CHADWICK | Europäisches Patentamt | 2021

    Freier Zugriff

    CARGO TRANSPORTING CART

    SAITO AKIHIRO / MIYASAKA MAHO / TAZAWA KOKI | Europäisches Patentamt | 2017

    Freier Zugriff