An airship comprises a main body having a rigid structure surrounding a plurality of containers for a lighter-than-air gas, a plurality of propeller units mechanically connected to the rigid structure and each comprising one or more electric motors for driving a thrust propeller, and one or more power-generating units for powering the electric motors. The airship also comprises two nacelles symmetrically arranged on either side of the main body and each configured to receive one or more of the power-generating units, each ducted nacelle comprising a mechanical structure connected to the rigid structure of the main body by a joint, a “fail safe” interface, and at least one rod or stay cable between a first point of attachment on the rigid structure of the main body and a second point of attachment on the mechanical structure of the nacelle.


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    Titel :

    DIRIGEABLE DE STRUCTURE RIGIDE A PROPULSION ELECTRIQUE ET NACELLE DE PRODUCTION D'ENERGIE ELECTRIQUE EQUIPANT CE DIRIGEABLE


    Weitere Titelangaben:

    ELECTRICALLY POWERED, RIGID-STRUCTURE AIRSHIP AND ELECTRIC-POWER-GENERATING NACELLE EQUIPPING SAID AIRSHIP
    ELEKTRISCH ANGETRIEBENES LUFTSCHIFF MIT STARRER STRUKTUR UND STROMERZEUGENDE GONDEL ZUR AUSRÜSTUNG DIESES LUFTSCHIFFS


    Beteiligte:

    Erscheinungsdatum :

    29.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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