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公开(公告)号:US12071237B2
公开(公告)日:2024-08-27
申请号:US17822901
申请日:2022-08-29
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Yumian Deng , Rongming Xiong , Tao Zhao , Yin Tang
CPC classification number: B64C39/024 , B64C1/30 , B64C25/52 , B64U10/10 , B64U10/13 , B64U30/20 , B64U80/00
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.
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公开(公告)号:US11186366B2
公开(公告)日:2021-11-30
申请号:US16119434
申请日:2018-08-31
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Tao Zhao , Guyue Zhou , Ang Liu , Xiao Hu , Litian Zhang
IPC: B64C39/02 , G05D1/00 , G06F3/0488 , G08G5/04 , G08G5/00
Abstract: A method for controlling flight includes displaying prompt information in a picture received from an aerial vehicle, dividing the picture into at least two portions based on the prompt information, obtaining a location of a click operation on the picture, and controlling a flight direction of the aerial vehicle based on the location and the prompt information.
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公开(公告)号:US10797499B2
公开(公告)日:2020-10-06
申请号:US15387395
申请日:2016-12-21
Applicant: SZ DJI TECHNOLOGY Co., Ltd
Inventor: Tao Zhao , Juncheng Zhan , Yuancai Liu , Lei Wang , Wentao Wang
Abstract: Systems, methods, and devices of managing a battery assembly used to power an object are provided to discharge a battery assembly for a safe and long-term storage. A controlled self-discharge of the battery assembly may be initiated when the power to the object is turned off for a certain length of time or the battery assembly is not in use for a threshold length of time. The controlled self-discharge may be terminated if the battery assembly reaches a threshold voltage value or the battery is in use again during the self-discharge.
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公开(公告)号:US10763557B2
公开(公告)日:2020-09-01
申请号:US15455824
申请日:2017-03-10
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Tao Zhao , Wentao Wang , Lei Wang , Juncheng Zhan , Yuancai Liu
IPC: H01M10/655 , H01M10/613 , H01M10/625 , H01M10/6555 , B64D27/24 , B64C39/02
Abstract: A battery, a thermal management device of the battery, and an unmanned aerial vehicle having the battery are provided. The thermal management device comprises a heat conducting housing having a receiving cavity and configured to divide the receiving cavity into a plurality of cell compartments for receiving cells, and a heat conducting shelf mounted within the receiving cavity and configured to be in contact with at least one of the cells to conduct heat generated by the at least one of the cells. The heat conducting shelf is thermally connected with an inner wall of the receiving cavity and configured to conduct heat in the heat conducting shelf to the heat conducting housing.
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公开(公告)号:US10717363B2
公开(公告)日:2020-07-21
申请号:US16111038
申请日:2018-08-23
Applicant: SZ DJI TECHNOLOGY CO., Ltd
Inventor: Tao Zhao
Abstract: The disclosure provides a battery which can include a power supply and power supply circuit, the power supply circuit connected to the power supply. The power supply can discharge through the power supply circuit. An electronic switch can control the power-on or off of the power supply, thereby avoiding the generation of sparks during the power on process and allowing for the normal use of the battery and the safety of the aircraft. The disclosure also provides an aircraft having the battery.
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公开(公告)号:US10681849B2
公开(公告)日:2020-06-09
申请号:US16237984
申请日:2019-01-02
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Yin Tang , Xifeng Zhao , Tao Zhao , Xiaokai Guo , Yanxin Huang
Abstract: An unmanned aerial vehicle (UAV) includes a heat dissipation device, an inertial measurement unit (IMU), and a control module. The heat dissipation device includes an air guiding cover and a heat conduction plate. The air guiding cover includes an air duct configured to guide an airflow, and the heat conduction plate directly constitutes a portion of a sidewall of the air duct. The IMU module is received within the air duct. The control module is located outside the air duct and disposed at a side of the heat conduction plate that faces away from the IMU module. Heat generated by the IMU module is taken away directly by the airflow within the air duct.
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公开(公告)号:US10272994B2
公开(公告)日:2019-04-30
申请号:US16027178
申请日:2018-07-03
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor: Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
IPC: B64C39/02 , B64C27/08 , G01V3/16 , B64C25/06 , B64C27/00 , B64D43/00 , G05D1/00 , B64C27/54 , B64C1/30 , B64C25/32 , B64D31/14 , G01R33/00 , A63H27/00
Abstract: The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.
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公开(公告)号:US20190089871A1
公开(公告)日:2019-03-21
申请号:US16194590
申请日:2018-11-19
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Paul Pan , Xifeng Zhao , Tao Zhao
IPC: H04N5/225 , B64D1/08 , G03B17/56 , B64D47/08 , F16M13/02 , B64C39/02 , F16M11/12 , H04N5/232 , F16M11/22 , F16M11/10 , F16M11/20 , G03B15/00 , F16M11/04 , F16M11/18 , F16M13/04 , A45F5/10
Abstract: An assembly includes a payload configured to obtain sensor data and a mounting platform coupled to the payload via a first coupling and including one or more actuators configured to adjust a spatial disposition of the payload. The assembly is for interchangeably mounting onto a plurality of base supports including a first base support and a second base support. The mounting platform is configured to be releasably coupled via a second coupling to each of the first base support and the second base support. The first base support is configured to control a function of the payload when the mounting platform is coupled to the first base support.
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公开(公告)号:US20190011921A1
公开(公告)日:2019-01-10
申请号:US16067577
申请日:2015-10-30
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Mingyu Wang , Tao Zhao , Yun YU , Guyue Zhao , Ketan Tang , Cong Zhao , Ang Liu , You Zhou , Minjian Pang , Xiao Hu , Litian Zhang
Abstract: A method for controlling a movable object comprise receiving an input indicative of a selected mode, wherein the selected mode is selected from a plurality of modes, and effecting movement of the movable object based on the selected mode. The plurality of modes may comprise at least a target mode and a directional mode. The movable object may be configured to move towards or follow a selected target when the selected mode is the target mode. The movable object may be configured to move in a selected direction when the selected mode is the directional mode. An apparatus, a medium and an UAV system are also provided.
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公开(公告)号:US10160538B2
公开(公告)日:2018-12-25
申请号:US16049768
申请日:2018-07-30
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Tao Wang , Tao Zhao , Zhi Gang Ou
Abstract: Systems, methods, and devices for propelling self-propelled movable objects are provided. In one aspect, a rotor assembly for a self-propelled movable object comprises: a hub comprising a first fastening feature; a drive shaft comprising a second fastening feature and directly coupled to the hub by a mating connection of the first and second fastening features, wherein the drive shaft is configured to cause rotation of the hub such that the mating connection of the first and second fastening features is tightened by the rotation; and a plurality of rotor blades coupled to the hub and configured to rotate therewith to generate a propulsive force.
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