Un vehículo aéreo no tripulado (UAV) que comprende: un fuselaje; y al menos un estabilizador. La base del estabilizador está configurada para pivotar alrededor de un primer eje y un segundo eje, donde el al menos un estabilizador es configurable en al menos las siguientes disposiciones: una disposición compacta que comprende: el al menos un estabilizador estibado contra el fuselaje, y un disposición desplegada que comprende: el menos un estabilizador desplegado desde el fuselaje alrededor del primer eje. (Traducción automática con Google Translate, sin valor legal)

    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 :

    Vehículo aéreo con componentes desplegables



    Publication date :

    2023-07-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Spanish


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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