A VTOL (vertical take-off and landing) rotorcraft with distributed propulsion system having the capability to convert between VTOL (vertical take-off and landing) flight and airplane flight. The rotorcraft includes a fuselage, a tail boom or tail fin, a pair of wings, a pair of transversally extended forward pivotable rotor booms, a plurality of forward proprotors mounted to the pivotable rotor booms, a plurality of rear lift rotors mounted to the tail boom, and a stabilizer mounted on the tail boom or tail fin. The proprotor and lift rotor can be open rotor or ducted rotor. The proprotors in a first configuration and lift rotors provide the thrust vector for VTOL (vertical take-off and landing) flight. Moreover, the proprotors in a second configuration provide the forward propulsive thrust in airplane flight.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Multirotor aerial vehicle with tiltable rotor


    Beteiligte:
    WANG XI (Autor:in)

    Erscheinungsdatum :

    10.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    MULTIROTOR AERIAL VEHICLE WITH TILTABLE ROTOR

    WANG XI | Europäisches Patentamt | 2024

    Freier Zugriff

    MULTIROTOR AERIAL VEHICLE WITH TILTABLE ROTOR BOOM

    WANG XI | Europäisches Patentamt | 2025

    Freier Zugriff

    Deformation tiltable four-rotor unmanned aerial vehicle

    HU DANDAN / FENG KUNHUI / GUAN RUOQIAO et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Rotor wing tiltable unmanned aerial vehicle control system

    ZHANG JUNQI | Europäisches Patentamt | 2024

    Freier Zugriff

    Four-shaft eight-rotor unmanned aerial vehicle with tiltable rotor shafts

    ZHU HANG / ZHANG JIAKUO / LIN DEKAI et al. | Europäisches Patentamt | 2024

    Freier Zugriff