The invention provides aerodynamic lift, or downward thrust for the amphibious environment, by means of two conical frames that are opposed at the bases and counter-rotating, thus cancelling out the opposing torque moment when rotating, being provided with concentric rows of fixed and retractable blades having variable angle of attack, arranged along the generatrix, separated by the fixed central area of the frame, where the power plant and the electro-mechanical elements that enable its operation are located, the cabins being situated in the conoidal hollow space of both, thus forming a body of lenticular geometry. The invention is provided with an electro-aerodynamic stabilisation system (2 and 4) and landing gear (T), propulsion and manoeuvring (19) being provided by pressurised air supplied through variable-area nozzles, and by the thrust due to the tilting of its axis (Y), with a fairing. Its functions and performance are similar to those of a helicopter.


    Access

    Download


    Export, share and cite



    Title :

    Aerodino tripulado lenticular


    Contributors:

    Publication date :

    2021-11-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Spanish


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AERODINO TRIPULADO LENTICULAR

    BERNEDO TORÁN MANUEL | European Patent Office | 2023

    Free access

    Misil no tripulado

    European Patent Office | 2018

    Free access

    Vehículo de superficie no tripulado

    RYDELL ANDERS | European Patent Office | 2019

    Free access

    VEHICULO NO TRIPULADO MULTITAREA

    VILLARRICA VIÑES JORGE / SANDE LAMAS RUBÉN | European Patent Office | 2024

    Free access

    Vehículo submarino no tripulado

    ITEM ERIK F / LANGELIER MARK S / CARLSTEN CURTIS B et al. | European Patent Office | 2018

    Free access