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    UNMANNED AERIAL VEHICLE AND WING THEREOF
    2.
    发明公开
    UNMANNED AERIAL VEHICLE AND WING THEREOF 审中-公开

    公开(公告)号：US20240166381A1

    公开(公告)日：2024-05-23

    申请号：US18512399

    申请日：2023-11-17

    申请人： AUTEL ROBOTICS CO., LTD.

    发明人： Zhuanpeng CHENG ,  Feifei YAO ,  Ao HE

    IPC分类号： B64U10/25 ,  B64U20/50 ,  B64U30/10

    CPC分类号： B64U10/25 ,  B64U20/50 ,  B64U30/10

    摘要： The present disclosure discloses an unmanned aerial vehicle and a wing thereof. The wing includes an intermediate wing assembly, configured to connect to a fuselage of an unmanned aerial vehicle; an outer wing, arranged corresponding to the intermediate wing assembly and located on a side of the intermediate wing assembly away from the fuselage when the outer wing is in an unfolded state; and a folding apparatus, including a driver and a first rotating shaft, the driver being connected to the intermediate wing assembly and the first rotating shaft including a first rotating portion and a first fixed portion that are rotatably connected, the first fixed portion being connected to the intermediate wing assembly and the first rotating portion being connected to the outer wing, the first rotating portion being further connected to an output end of the driver, to rotatably connect the outer wing and the intermediate wing assembly.

    MONOCOPTER
    3.
    发明公开
    MONOCOPTER 审中-公开

    公开(公告)号：US20240262541A1

    公开(公告)日：2024-08-08

    申请号：US18682655

    申请日：2022-09-16

    申请人： Singapore University of Technology and Design

    发明人： Luke Soe Thura Win . ,  Shane Kyi Hla WIN ,  Shaohui FOONG

    IPC分类号： B64U10/13 ,  B64U20/50 ,  B64U30/16 ,  B64U50/13

    CPC分类号： B64U10/13 ,  B64U20/50 ,  B64U30/16 ,  B64U50/13

    摘要： According to various embodiments, there may be provided a monocopter. The monocopter may include a body chassis. The monocopter may further include a wing structure extending from the body chassis, the body chassis being at a root of the wing structure. The wing structure may include a plurality of rigid wing segments distributed along a spanwise direction extending between the root and a tip of the wing structure. The wing structure may further include a plurality of flexible wing segments, each flexible wing segment adjoining a pair of adjacent rigid wing segments of the plurality of rigid wing segments. The monocopter may further include a propulsion unit coupled to a rigid wing segment of the plurality of rigid wing segments between a midspan of the wing structure and the tip of the wing structure.

    AERIAL VEHICLE
    10.
    发明公开
    AERIAL VEHICLE 审中-公开

    公开(公告)号：US20240132237A1

    公开(公告)日：2024-04-25

    申请号：US18384498

    申请日：2023-10-26

    申请人： SZ DJI TECHNOLOGY CO., LTD.

    发明人： Xiang XIAO

    IPC分类号： B64U20/50 ,  B64U10/20 ,  B64U101/30

    CPC分类号： B64U20/50 ,  B64U10/20 ,  B64U2101/30

    摘要： An aerial vehicle may include a fuselage; and one or more propellers coupled to the fuselage, wherein the aerial vehicle may have at least a taking off or landing state and a cruise state. In response to the aerial vehicle being in the taking off or landing state, an angle between a longitudinal axis of the fuselage and a horizontal plane may be within a first angular range and in response to the aerial vehicle being in the cruise state, an angle between the longitudinal axis of the fuselage and the horizontal plane may be within a second angular range. A maximum value of the second angular range may be less than a minimum value of the first angular range. In response to the aerial vehicle switching between the takeoff or landing state and the cruise state, the fuselage and the propellers may tilt as a whole.