FOLDABLE UAV
    11.
    发明申请

    公开(公告)号:US20210009269A1

    公开(公告)日:2021-01-14

    申请号:US17035266

    申请日:2020-09-28

    Abstract: An unmanned aerial vehicle (UAV) includes a central body and a plurality of arms extendable from the central body using one or more actuators. Each of the plurality of arms is configured to support one or more propulsion units. One arm of the plurality of arms is configured to connect to one of the one or more actuators via a linkage mechanism. The one of the one or more actuators is configured to actuate the linkage mechanism between (1) a first dead center position for securing the one arm when the one arm is extended away from the central body in a flight configuration and (2) a second dead center position for securing the one arm when the one arm is folded substantially parallel to the central body in a compact configuration.

    MOBILE PLATFORM SYSTEM AND MOBILE PLATFORM PAYLOAD SYSTEM

    公开(公告)号:US20210003979A1

    公开(公告)日:2021-01-07

    申请号:US17024379

    申请日:2020-09-17

    Abstract: The present disclosure provides a mobile platform system. The system includes a mobile platform; a payload controller connected to the mobile platform through a first communication link for generating a payload control signal; a payload connected to the payload controller and configured to receive the payload control signal generated by the payload controller; and a gimbal carried by the mobile platform, the gimbal including a gimbal controller and a gimbal driver, the gimbal controller being communicatively connected to the payload controller through a second communication link to control the gimbal driver.

    VEHICLE BODY AND UNMANNED AERIAL VEHICLE
    14.
    发明申请

    公开(公告)号:US20200010200A1

    公开(公告)日:2020-01-09

    申请号:US16549353

    申请日:2019-08-23

    Abstract: An unmanned aerial vehicle (UAV) includes a vehicle body and a flight control circuit. The vehicle body includes a housing and a fan. The housing includes two vents arranged at two ends of the housing and in communication with an internal space of the housing. The two vents and the internal space form a heat dissipation air passage. The fan is arranged at one of the two vents, and is configure to drive external air into the heat dissipation air passage and expel internal air from the heat dissipation air passage. The flight control circuit is arranged inside the housing and is configured to control flight parameters of the UAV. The heat dissipation air passage is configured to dissipate heat generated by the flight control circuit.

    SYSTEMS AND METHODS OF AIRCRAFT WALKING SYSTEMS

    公开(公告)号:US20190127052A1

    公开(公告)日:2019-05-02

    申请号:US16226140

    申请日:2018-12-19

    Abstract: An unmanned aerial vehicle (UAV) includes a central body and a plurality of landing gears that are extendable from and movable relative to the central body. The plurality of landing gears are configured to transform between a flight configuration and a surface configuration. In the flight configuration, the landing gears are extending laterally away from the central body and not in contact with a surface below the central body. In the surface configuration, the landing gears are extending towards the surface below the central body. When the landing gears are in the surface configuration, the landing gears are configured to support a weight of the central body on the surface and transport the UAV over the surface by moving one or more of the landing gears relative to the surface.

    FOLDABLE UAV
    16.
    发明申请
    FOLDABLE UAV 审中-公开

    公开(公告)号:US20190084673A1

    公开(公告)日:2019-03-21

    申请号:US16192316

    申请日:2018-11-15

    CPC classification number: B64C39/024 B64C3/56 B64C2201/027 B64C2201/108

    Abstract: An unmanned aerial vehicle (UAV) includes a central body having a plurality of sides and a plurality of arms extendable from the central body. Each arm of the plurality of arms comprises a plurality of foldable sections. Each arm of the plurality of arms is configured to transform between a flight configuration and a compact configuration. When an arm is in the flight configuration, the plurality of foldable sections of the arm are extended away from the central body. When an arm is in the compact configuration, the plurality of foldable sections of the arm are folded toward a corresponding side of the central body such that the plurality of foldable sections are substantially parallel to one another.

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