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.


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    Title :

    HYBRID INFLATABLE AIRCRAFT OF THE UNMANNED TYPE



    Publication date :

    2024-02-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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