A hybrid aircraft of the unmanned type configured for joint and optimized use of aerostatic and aerodynamic force is provided. The hybrid aircraft has an inflatable body having an outer shell and a load-bearing structure inside the outer shell, the inflatable body being adapted to assume a closed wing operating configuration.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE


    Beteiligte:

    Erscheinungsdatum :

    2024-02-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64C AEROPLANES , Flugzeuge



    Unmanned hybrid inflatable aircraft

    PERSECCHINO GIUSEPPE / BALANIERO VINCENZO ROSARIO / BORSA ROBERTO | Europäisches Patentamt | 2023

    Freier Zugriff

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE

    PERSECHINO GIUSEPPE / BARANIELLO VINCENZO ROSARIO / BORSA ROBERTO | Europäisches Patentamt | 2023

    Freier Zugriff

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE

    PERSECHINO GIUSEPPE / BARANIELLO VINCENZO ROSARIO / BORSA ROBERTO | Europäisches Patentamt | 2023

    Freier Zugriff

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE

    PERSECHINO GIUSEPPE / BARANIELLO VINCENZO ROSARIO / BORSA ROBERTO | Europäisches Patentamt | 2022

    Freier Zugriff

    UNMANNED INFLATABLE AIRCRAFT

    SCHALLA JAMES | Europäisches Patentamt | 2017

    Freier Zugriff