FOLDABLE AND RETRACTABLE MECHANISM, PROPELLER PROTECTION DEVICE, AND ROTOR UNMANNED AERIAL VEHICLE

    公开(公告)号:US20210129979A1

    公开(公告)日:2021-05-06

    申请号:US17144430

    申请日:2021-01-08

    Abstract: A foldable and retractable mechanism includes a first body and a second body. The first body includes a first connection member. The second body is configured to rotate relative to the first body and including a second connection member. The first connection member and the second connection member are assembled in movable manner. The first connection member and the second connection member are configured to be in a retracted state, in which the first connection member and the second connection member at least partially overlap with each other and constraint relative rotation of the first body and the second body. The first connection member and the second connection member are configured to be in an extended state, in which the first connection member is away from the second connection member, and the second body is rotatable and capable of being folded over the first body.

    UNMANNED AERIAL VEHICLE
    2.
    发明申请

    公开(公告)号:US20200290718A1

    公开(公告)日:2020-09-17

    申请号:US16888051

    申请日:2020-05-29

    Abstract: The present disclosure provides an unmanned aerial vehicle. The unmanned aerial vehicle includes a fuselage, a plurality of rotor propulsion assemblies installed on the fuselage, and a fixed-wing propulsion assembly that is detachably installed on the fuselage. The fixed-wing propulsion assembly is able to rotate relative to the fuselage when the fixed-wing propulsion assembly is installed on the fuselage.

    MOVABLE DEVICE
    3.
    发明申请

    公开(公告)号:US20220021106A1

    公开(公告)日:2022-01-20

    申请号:US17490560

    申请日:2021-09-30

    Abstract: An unmanned aerial vehicle (UAV) includes a fuselage including an upper portion and a lower portion, a navigation antenna arranged at head portion and/or a tail portion of the upper portion of the fuselage, a battery compartment arranged at the upper portion of the fuselage and configured to accommodate a battery, and a circuit board arranged in the lower portion of the fuselage below both the navigation antenna and the battery compartment. The circuit board is parallel to a bottom of the battery compartment.

    FOLDABLE MULTI-ROTOR AERIAL VEHICLE
    4.
    发明申请

    公开(公告)号:US20200377212A1

    公开(公告)日:2020-12-03

    申请号:US16849518

    申请日:2020-04-15

    Abstract: An unmanned aerial vehicle includes a central body and a plurality of arms extendable from the central body. Each of the plurality of arms is configured to support one or more propulsion units. Each of the plurality of arms is configured to transform between (1) a flight configuration in which the arm is extending away from the central body and (2) a compact configuration in which the arm is folded against the central body. At least one of the plurality of arms is configured to rotate about a first rotational axis and at least a portion of the at least one of the plurality of arms is configured to rotate about a second rotational axis not parallel to the first rotational axis.

    FOLDABLE MULTI-ROTOR AERIAL VEHICLE

    公开(公告)号:US20220402607A1

    公开(公告)日:2022-12-22

    申请号:US17822901

    申请日:2022-08-29

    Abstract: An unmanned aerial vehicle includes a central body, a plurality of arms extendable from the central body, and one or more joints. Each of the plurality of arms is configured to support one or more propulsion units, and is configured to transform between (1) a flight configuration in which the arm is extending away from the central body and (2) a compact configuration in which the arm is folded against the central body. Each joint is configured to couple one arm to the central body. At least one of the one or more joints includes an elastic element configured to cause at least one of the plurality of arms to automatically retract when the at least one of the plurality of arms is reversibly folded to a first predetermined state, and automatically extend when the at least one of the plurality of arms is reversibly extended to a second predetermined state.

    UAV AND BODY THEREOF, AND GIMBAL CAMERA

    公开(公告)号:US20210271153A1

    公开(公告)日:2021-09-02

    申请号:US17123684

    申请日:2020-12-16

    Abstract: An unmanned aerial vehicle (UAV) includes a body and a gimbal camera. The body includes a housing including an inwardly recessed mounting groove with a notch on one side of the mounting groove, and a protective cover arranged at the housing and configured to open and cover the notch. The gimbal camera includes a mounting frame detachably connected to the housing via the mounting groove; a gimbal arranged at the mounting frame; and a camera arranged at the gimbal. In response to the gimbal camera and the housing being connected via the mounting frame, the gimbal camera is at least partially accommodated in the notch.

    BATTERY ASSEMBLY, AUTONOMOUS MOVABLE PLATFORM, AND AUTONOMOUS MOVABLE PLATFORM SYSTEM

    公开(公告)号:US20210104805A1

    公开(公告)日:2021-04-08

    申请号:US17123733

    申请日:2020-12-16

    Abstract: A battery assembly includes a battery body, a housing, a switch assembly, an output terminal, and a snap clip assembly. The housing includes an accommodation chamber. The battery body is mounted in the accommodation chamber. The switch assembly is fixed at the housing and configured to generate an in-position signal. The output terminal is arranged at the housing and configured to output power of the battery body and the in-position signal. The snap clip assembly is arranged at the housing and configured to cause the switch assembly to be in a first status when no external force is applied to the snap clip assembly, the in-position signal being at a first level in the first status, and when an external force is applied to the snap clip assembly, cause the switch assembly to be in a second status, the in-position signal being at a second level in the second status.

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