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    SYSTEM AND METHOD FOR LANDING A MOBILE PLATFORM VIA A MAGNETIC FIELD
    14.
    发明申请
    SYSTEM AND METHOD FOR LANDING A MOBILE PLATFORM VIA A MAGNETIC FIELD 审中-公开
    用于通过磁场来移动移动平台的系统和方法

    公开(公告)号：US20170038778A1

    公开(公告)日：2017-02-09

    申请号：US15299341

    申请日：2016-10-20

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： Mingxi WANG

    IPC: G05D1/10 ,  B64F1/02 ,  B64C25/00 ,  B64C39/02 ,  G01S19/42

    CPC classification number: G05D1/101 ,  B64C25/001 ,  B64C39/024 ,  B64C2201/145 ,  B64C2201/18 ,  B64F1/02 ,  G01S19/42 ,  G05D1/0676

    Abstract: A system for landing a mobile platform, such as an Unmanned Aerial Vehicle (“UAV”) and methods for making and using the same. The system can land the UAV by applying a magnetic levitation force upon the UAV and adjusting the applied magnetic levitation force. The system can initiate a landing process to a designated docking station and can guide the UAV to an adjacency of the designated docking station. Once the UAV has entered the adjacency, the magnetic levitation forces can take control of the landing process. During the landing process, certain magnetic sensitive devices installed on the UAV and/or on the designated docking station can be protected by turning them off or by shielding them. The system overcomes disadvantages of currently-available landing systems by restricting a size and weight of the landing arrangements, as well as, avoiding potential damage to the UAV and the designated docking station.

    Abstract translation: 用于登陆移动平台的系统，例如无人机（“UAV”）及其制造和使用方法。 该系统可以通过在无人机上施加磁悬浮力并调整所施加的磁悬浮力来降落无人机。 该系统可以启动对指定坞站的着陆过程，并且可以将UAV引导到指定对接站的邻接处。 一旦无人机进入邻近，磁悬浮力就可以控制着陆过程。 在着陆过程中，安装在UAV和/或指定对接站上的某些磁敏装置可以通过关闭或屏蔽它们来保护。 该系统通过限制着陆装置的尺寸和重量来克服目前可用的着陆系统的缺点，以及避免对无人机和指定坞站的潜在损坏。

    FOLDABLE UAV
    15.
    发明申请
    FOLDABLE UAV 有权

    公开(公告)号：US20220001982A1

    公开(公告)日：2022-01-06

    申请号：US17479109

    申请日：2021-09-20

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： Hanping CHEN ,  Mingxi WANG ,  Xiangyu CHEN ,  Qi ZHOU ,  Yuwei WU

    IPC: B64C39/02 ,  B64C3/56

    Abstract: An unmanned aerial vehicle (UAV) includes a central body having a first side and a second side opposite to the first side, and a first arm and a second arm extendable from the central body and respectively disposed on the first side and the second side. Each arm of the first arm and the second arm includes a plurality of sections and holds a set of rotor blades via a rotor shaft, and the plurality of sections includes a first section and a second section rotatably connected to the first section. The each arm of the first arm and the second arm is configured to transform between a flight configuration in which the second section of the each arm is extended away from the central body and a compact configuration in which the plurality of sections of the each arm are located at a corresponding side of the central body.

    UNMANNED AERIAL VEHICLE DOCK AND BATTERY REPLACEMENT DEVICE THEREOF
    16.
    发明申请
    UNMANNED AERIAL VEHICLE DOCK AND BATTERY REPLACEMENT DEVICE THEREOF 审中-公开

    公开(公告)号：US20190210482A1

    公开(公告)日：2019-07-11

    申请号：US16356312

    申请日：2019-03-18

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： Yuan LIN ,  Mingxi WANG ,  Hongju LI

    IPC: B60L53/80 ,  B25J9/00 ,  B64F5/00 ,  B64F1/22 ,  B64F1/36 ,  B60L53/36 ,  B64C39/02 ,  B60L53/14 ,  B60L53/12

    Abstract: A battery replacement device including a first linear motion mechanism, a second linear motion mechanism mounted on the first linear motion mechanism, a third linear motion mechanism mounted on the second linear motion mechanism, and a clamp mechanism mounted on one of the first, second, and third linear motion mechanisms. Each of the first, second, and third linear motion mechanisms includes a carrying member and a driving member configured to drive the carrying member to move translationally in one of a first axis direction, a second axis direction, and a third axis direction that build a three-dimensional Cartesian coordinate system. A coordinate position of the clamp mechanism in the three-dimensional Cartesian coordinate system is adjusted by the first driving member, the second driving member, and the third driving member.

    MULT-FUNCTIONAL COMPARTMENT
    17.
    发明申请
    MULT-FUNCTIONAL COMPARTMENT 审中-公开

    公开(公告)号：US20190144115A1

    公开(公告)日：2019-05-16

    申请号：US16245590

    申请日：2019-01-11

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： Hanping CHEN ,  Xiangyu CHEN ,  Mingxi WANG ,  Qi ZHOU

    IPC: B64C39/02

    Abstract: A method for operating a vehicle chassis includes providing the vehicle chassis including a main body and at least one compartment arranged on the vehicle chassis, selectively receiving one or more components in the compartment, and effecting an operational state of a vehicle comprising the vehicle chassis based on a type of at least one of the one or more components that are selectively received in the compartment. The one or more components is selected from a plurality of components of different types.

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