An aerial vehicle includes at least one wing, a plurality of thrust producing elements on the at least one wing, a plurality of electric motors equal to the number of thrust producing elements for individually driving each of the thrust producing elements, at least one battery for providing power to the motors, and a flight control system to control the operation of the vehicle. The aerial vehicle may include a fuselage configuration to facilitate takeoffs and landings in horizontal, vertical and transient orientations, redundant control and thrust elements to improve reliability and means of controlling the orientation stability of the vehicle in low power and multiple loss of propulsion system situations. Method of flying an aerial vehicle includes the variation of the rotational speed of the thrust producing elements to achieve active vehicle control.


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    Titel :

    ELECTRICALLY POWERED AERIAL VEHICLES AND FLIGHT CONTROL METHODS


    Weitere Titelangaben:

    ELEKTRISCH ANGETRIEBENE LUFTFAHRZEUGE UND FLUGSTEUERUNGSVERFAHREN
    VÉHICULES AÉRIENS À MOTORISATION ÉLECTRIQUE ET PROCÉDÉS DE COMMANDES DE VOL


    Beteiligte:
    LENG MARCUS (Autor:in)

    Erscheinungsdatum :

    2020-01-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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