VERTICAL TAKE-OFF AND LANDING AIRCRAFT
    1.
    发明申请

    公开(公告)号:WO2021236576A1

    公开(公告)日:2021-11-25

    申请号:PCT/US2021/032874

    申请日:2021-05-18

    Abstract: A vertical take-off and landing aircraft (100) includes a fuselage (102), at least one wing (104) connected to the fuselage, a plurality of rotors (112) connected to the at least one wing for providing lift for vertical take-off and landing of the aircraft and a plurality of prop rotors (114) connected to the at least one wing and tiltable between lift configurations for providing lift for vertical take-off and landing of the aircraft and propulsion configurations for providing forward thrust to the aircraft

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