MONOCOPTER
    5.
    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

    CPC classification number: B64U10/13 B64U20/50 B64U30/16 B64U50/13

    Abstract: 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.

    MONO-WING AERIAL DEVICE AND METHOD OF FORMING THE MONO-WING AERIAL DEVICE

    公开(公告)号:US20230312142A1

    公开(公告)日:2023-10-05

    申请号:US18004454

    申请日:2021-07-07

    CPC classification number: B64U10/10 B64U20/80 B64U30/10 B64U30/294

    Abstract: There is provided a mono-wing aerial device which includes a housing member having disposed thereon electronic components and a power source, including a controller configured to control a thrust unit; a wing member coupled to the housing member, the wing member configured to produce aerodynamic forces for autorotation of the aerial device, the wing member comprising a first edge portion proximal to the housing member and a second edge portion distal to the housing member, wherein the wing member is coupled to the housing member at the first edge portion; and the thrust unit coupled to the wing member at the second edge portion, wherein the thrust unit is configured to generate thrust in a direction substantially tangential to a rotational plane of the wing member. There is also provided a method of forming the mono-wing aerial device.

    AIRCRAFT
    10.
    发明申请
    AIRCRAFT 审中-公开

    公开(公告)号:US20190382104A1

    公开(公告)日:2019-12-19

    申请号:US16484830

    申请日:2018-02-12

    Abstract: An aircraft including: a pair of wings rotatably coupled to opposing lateral sides of the fuselage and being rotatable relative to each other; a pair of servo motors, each connected to a corresponding wing and configured to rotate the corresponding wing in two rotational directions; a pair of thrust motors, each of which mounted on a corresponding wing; and a flight controller connected to the servo motors and to the thrust motors, and configured to control each servo motor and each thrust motor, such that the aircraft can be selectively operated in a cruising mode, such that the pair of wings are in a non-permanent-rotation-state about a yawing axis which extends at least substantially through the center of gravity, and a monocopter mode, in which the pair of thrust motors provide thrust in opposite directions so that the pair of wings are in a permanent-rotation-state about the yawing axis.

Patent Agency Ranking