Una aeronave de despegue y aterrizaje vertical (VTOL) (100) que tiene: una estructura de ala que tiene alas delanteras derecha e izquierda (20, 22); y alas traseras derecha e izquierda (30, 32), estando cada una de las alas del lado derecho (20, 30) conectadas, y estando cada una de las alas del lado izquierdo (22, 32) conectadas en una configuración de ala en forma de caja; en donde cada ala (20, 22, 30, 32) tiene un borde de ataque fijo (100) y al menos una superficie de control de salida móvil (110), en donde además cada ala (20, 22, 30, 32) tiene al menos un módulo de motor (195), estando el módulo de motor (195) montado de manera pivotante en un lado inferior del borde de ataque fijo (100), y asegurado de manera fija a la superficie de control de salida (110). (Traducción automática con Google Translate, sin valor legal)

    A vertical take-off and landing (VTOL) aircraft (100) having: a wing structure having right and left side forward wings (20, 22); and right and left side rearward wings (30, 32), each of the right side wings (20, 30) being connected, and each of the left side wings (22, 32) being connected in a box wing configuration; wherein each wing (20, 22, 30, 32) has a fixed leading edge (100) and at least one moveable trailing control surface (110), further wherein each wing (20, 22, 30, 32) has at least one motor pod (195), the motor pod (195) being pivotally mounted to an underside of the fixed leading edge (100), and fixedly secured to the trailing control surface (110).


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    Title :

    VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT


    Contributors:

    Publication date :

    2025-02-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Spanish


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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