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    AN UNMANNED AERIAL VEHICLE AND A SYSTEM FOR CONTROLLING AN UNMANNED AERIAL VEHICLE
    1.
    发明申请
    AN UNMANNED AERIAL VEHICLE AND A SYSTEM FOR CONTROLLING AN UNMANNED AERIAL VEHICLE 审中-公开
    无人机空中车辆和无人驾驶飞机的控制系统

    公开(公告)号：WO2018027315A1

    公开(公告)日：2018-02-15

    申请号：PCT/CA2017/050940

    申请日：2017-08-08

    Applicant: CLEO ROBOTICS INC.

    Inventor： ELERYAN, Omar ,  CZARNOTA, Szymon

    IPC: B64C39/00 ,  B64C27/08 ,  B64C29/00 ,  B64C39/02

    Abstract: A lightweight, pocket-sized unmanned aerial vehicle (UAV) that can be held in an outstretched hand by a user for take-off and landing of the UAV. The UAV comprises a semi-toroidal or a substantially toroidal hollow body that defines a duct. The UAV further comprises a motor for rotating a fan that directs air into and out of the duct enabling the UAV to take flight. The UAV comprises a flight-control system that comprises at least two flight control surfaces that can alter the directed air as it flows through the duct for controlling the roll and pitch and optionally the yaw of the UAV during flight. The flight control system may be controlled by a microprocessor controller. The UAV further comprises a payload, with at least a wireless transmitter and receiver unit.

    Abstract translation: 一种轻便的口袋大小的无人驾驶飞行器（UAV），可由使用者伸出手握住，用于无人机的起飞和着陆。 该无人飞行器包括限定管道的半环形或大致环形的中空体。 该无人飞行器还包括用于旋转风扇的马达，该风扇引导空气进出导管，使得无人机能够飞行。 该无人飞行器包括飞行控制系统，该飞行控制系统包括至少两个飞行控制表面，所述至少两个飞行控制表面可以在其经过管道流动时改变定向空气，用于在飞行期间控制无人机的侧倾和俯仰以及可选的偏航。 飞行控制系统可以由微处理器控制器控制。 无人机还包括一个有效载荷，至少有一个无线发射器和接收器单元。

    AN UNMANNED AERIAL VEHICLE AND A SYSTEM FOR CONTROLLING AN UNMANNED AERIAL VEHICLE
    2.
    发明公开
    AN UNMANNED AERIAL VEHICLE AND A SYSTEM FOR CONTROLLING AN UNMANNED AERIAL VEHICLE 审中-公开

    公开(公告)号：EP4286273A2

    公开(公告)日：2023-12-06

    申请号：EP23204199.6

    申请日：2017-08-08

    Applicant: Cleo Robotics Inc.

    Inventor： ELERYAN, Omar ,  CZARNOTA, Szymon

    IPC: B64C27/20

    Abstract: A lightweight, pocket-sized unmanned aerial vehicle (UAV) that can be held in an outstretched hand by a user for take-off and landing of the UAV. The UAV comprises a semi-toroidal or a substantially toroidal hollow body that defines a duct. The UAV further comprises a motor for rotating a fan that directs air into and out of the duct enabling the UAV to take flight. The UAV comprises a flight-control system that comprises at least two flight control surfaces that can alter the directed air as it flows through the duct for controlling the roll and pitch and optionally the yaw of the UAV during flight. The flight control system may be controlled by a microprocessor controller. The UAV further comprises a payload, with at least a wireless transmitter and receiver unit.

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