The present invention relates generally to a vertical take-off and landing (VTOL) aircraft and a propulsion system for a vehicle vertical take-off and landing (VTOL), for example, helicopters, others VTOL aircrafts. The claimed VTOL aircraft provides a most effective control of the aircraft equipped with such a propulsion system, performed through the optimal distribution of the airflow generated by the rotor, while maintaining the simplicity, reliability and efficiency of the aircraft design.


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    Title :

    VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT AND A PROPULSION SYSTEM FOR A VEHICLE VERTICAL TAKE-OFF AND LANDING (VTOL)


    Contributors:

    Publication date :

    2019-01-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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