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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    Title :

    AERIAL VEHICLE WITH DEPLOYABLE COMPONENTS


    Additional title:

    LUFTFAHRZEUG MIT EINSETZBAREN KOMPONENTEN
    VÉHICULE AÉRIEN À ÉLÉMENTS DÉPLOYABLES



    Publication date :

    2022-06-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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