UNMANNED AERIAL VEHICLE
    1.
    发明申请

    公开(公告)号:US20190256215A1

    公开(公告)日:2019-08-22

    申请号:US16401854

    申请日:2019-05-02

    摘要: An unmanned aerial vehicle (UAV) includes a fuselage, an electrical component, and an adapter arranged at the fuselage. The fuselage includes a battery compartment for accommodating a battery. The battery compartment includes an electrical connector for electrically coupling to the battery. The adapter is electrically coupled to the electrical connector and includes an access unit electrically coupled to the electrical connector and an adapting unit detachably coupled to the access unit. The adapting unit is configured to be electrically connected to the access unit when the adapting unit is coupled to the access unit. The adapting unit is electrically coupled to the electrical component through an adapting conductive wire to conduct power from the battery to the electrical component.

    ELECTRICAL CONNECTOR
    3.
    发明申请

    公开(公告)号:US20210309171A1

    公开(公告)日:2021-10-07

    申请号:US17352238

    申请日:2021-06-18

    摘要: A movable object includes a body, one or more propulsion units carried by the body and configured to effect movement of the movable object, and an electrical plug for power and signal transmission. The electrical plug includes at least one signal pin configured to communicate signal, a plurality of power pins configured to transmit electrical power, and a plug substrate configured to support the at least one signal pin and the plurality of power pins. The plurality of power pins include at least one power pin having a first polarity and at least one power pin having a second polarity opposite to the first polarity. The one or more propulsion units are provided with electrical energy via the electrical plug. The plurality of power pins and the at least one signal pin include a first set of power pins and signal pins, and a second set of power pins and signal pins. The first set and the second set are disposed symmetrically opposite to each other on the plug substrate, and the second set is provided in a row with the first set.

    DIAL STRUCTURE, REMOTE CONTROLLER EMPLOYING THE SAME, AND CONTROLLING METHOD

    公开(公告)号:US20200257286A1

    公开(公告)日:2020-08-13

    申请号:US16856750

    申请日:2020-04-23

    发明人: Tao PENG Yin TANG

    摘要: Disclosed is a controlling method for an unmanned aerial vehicle (UAV) that includes an image device. The controlling method includes transmitting, by a remote controller when a dial of a dial structure of the remote controller is rotated, a first control signal for changing imaging device information of an imaging device of the UAV via a signal transmitting device of the remote controller. The imaging device information comprises at least one of an operating mode of the imaging device, a shutter speed of the imaging device, an aperture size of the imaging device, a light sensitivity of the imaging device, or a preview image of the imaging device. The controlling method further includes transmitting a second control signal for confirming imaging device information via the signal transmitting device by the controller when the dial is slid with a displacement,?

    ROTOR-WING ASSEMBLY AND UNMANNED AERIAL VEHICLE

    公开(公告)号:US20190256204A1

    公开(公告)日:2019-08-22

    申请号:US16401930

    申请日:2019-05-02

    IPC分类号: B64C27/473 B64C39/02

    摘要: A rotor-wing assembly includes a motor, a propeller, and a connection assembly connecting the propeller to the motor. The motor includes a rotating portion. The connection assembly includes a locking member and a reinforcing member arranged between the propeller and the motor. The locking member locks the propeller to the rotating portion. A first end of the reinforcing member is mounted at the rotating portion. A second end of the reinforcing member opposite to the first end is engaged with the locking member, to reinforce the locking member to lock the propeller to the rotating portion.