A VTOL (vertical take-off and landing) rotorcraft with distributed propulsion system having the capability to convert to 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 proprotor mounted to the pivotable rotor booms, a plurality of rear lift rotor 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 design. The proprotors in a first configuration and lift rotors provide 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.


    Access

    Download


    Export, share and cite



    Title :

    MULTIROTOR AERIAL VEHICLE WITH TILTABLE ROTOR


    Contributors:
    WANG XI (author)

    Publication date :

    2024-08-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Multirotor aerial vehicle with tiltable rotor

    WANG XI | European Patent Office | 2024

    Free access

    MULTIROTOR AERIAL VEHICLE WITH TILTABLE ROTOR BOOM

    WANG XI | European Patent Office | 2025

    Free access

    Deformation tiltable four-rotor unmanned aerial vehicle

    HU DANDAN / FENG KUNHUI / GUAN RUOQIAO et al. | European Patent Office | 2021

    Free access

    Rotor wing tiltable unmanned aerial vehicle control system

    ZHANG JUNQI | European Patent Office | 2024

    Free access

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

    ZHU HANG / ZHANG JIAKUO / LIN DEKAI et al. | European Patent Office | 2024

    Free access