An UAV comprising a fuselage and at least one wing configurable between a stowed configuration, where the at least one wing is stowed against the fuselage, and a deployed configuration, where the at least one wing is deployed from the fuselage. The UAV further comprising at least one stabilizer configurable between a stowed configuration, where the at least one stabilizer is stowed against the fuselage, and a deployed configuration, where the at least one stabilizer is deployed from the fuselage. The UAV is configurable in at least: a compact arrangement comprising the at least one wing and the at least one stabilizer in their respective stowed configurations, a deployed arrangement comprising the at least one wing and the at least one stabilizer in their respective deployed configurations, and an expanded arrangement comprising the at least one wing telescoped to increase its wingspan compared to the deployed arrangement.


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    Titel :

    AERIAL VEHICLE WITH DEPLOYABLE COMPONENTS


    Weitere Titelangaben:

    LUFTFAHRZEUG MIT AUSFAHRBAREN KOMPONENTEN
    AÉRONEF DOTÉ DE ELÉMENTS DÉPLOYABLES



    Erscheinungsdatum :

    07.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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