公开(公告)号：US10753532B2

公开(公告)日：2020-08-25

申请号：US16525052

申请日：2019-07-29

Applicant: SZ DJI TECHNOLOGY CO., LTD.

Inventor： Xin Yan ,  Xifeng Zhao ,  Rongjian Sun ,  Zhuo Guo

IPC: F16M11/00 ,  F16M11/12 ,  F16M13/00 ,  G03B17/56 ,  F16M13/02 ,  F16M11/18 ,  F16M11/04 ,  F16M11/16

Abstract: A gimbal includes a yaw-axis structure, a roll-axis structure connected to the yaw-axis structure and configured to be rotated by the yaw-axis structure, and a pitch-axis structure connected to the roll-axis structure and configured to be rotated by the roll-axis structure. The yaw-axis structure includes a locking structure, a rotating member including a rotor of a motor or a member fixedly connected to the rotor, and a bearing member rotatably connected to the rotating member and including a stator of the motor or a member fixedly connected to the stator. The pitch-axis structure is configured to support a load and drive the load to rotate. The yaw-axis structure is configured to be locked by the locking structure when the yaw-axis structure rotates to a preset position in a non-operational state of the gimbal.

公开(公告)号：US09781313B2

公开(公告)日：2017-10-03

申请号：US15154740

申请日：2016-05-13

Applicant: SZ DJI TECHNOLOGY CO., LTD

Inventor： Paul Pan ,  Xifeng Zhao ,  Tao Zhao

IPC: H04N5/225 ,  F16M13/04 ,  G03B17/56 ,  B64D47/08 ,  B64C39/02 ,  F16M11/12 ,  H04N5/232 ,  F16M13/02 ,  F16M11/20 ,  A45F5/10 ,  B64D1/08 ,  F16M11/10 ,  G03B15/00

CPC classification number: H04N5/2251 ,  A45F5/10 ,  B64C39/024 ,  B64C2201/127 ,  B64D1/08 ,  B64D47/08 ,  F16M11/041 ,  F16M11/105 ,  F16M11/12 ,  F16M11/123 ,  F16M11/18 ,  F16M11/2064 ,  F16M11/22 ,  F16M13/022 ,  F16M13/04 ,  G03B15/006 ,  G03B17/561 ,  G03B17/566 ,  H04N5/2253 ,  H04N5/23203 ,  H04N5/23216

Abstract: A platform for interchangeably mounting a payload to a base support is provided. In one aspect, the platform comprises: a support assembly configured to be releasably coupled to a payload via a first coupling and configured to control a spatial disposition of the payload; and a mounting assembly configured to be releasably coupled via a second coupling to a plurality of types of base supports selected from at least two of the following: an aerial vehicle, a handheld support, or a base adapter mounted onto a movable object.

公开(公告)号：US09781312B2

公开(公告)日：2017-10-03

申请号：US15012210

申请日：2016-02-01

Applicant: SZ DJI TECHNOLOGY Co., LTD

Inventor： Paul Pan ,  Xifeng Zhao ,  Tao Zhao

IPC: H04N5/225 ,  G03B17/56 ,  B64D47/08 ,  F16M13/04 ,  F16M13/02 ,  B64C39/02 ,  F16M11/12 ,  H04N5/232 ,  A45F5/10 ,  B64D1/08 ,  F16M11/10 ,  F16M11/20 ,  G03B15/00

CPC classification number: H04N5/2251 ,  A45F5/10 ,  B64C39/024 ,  B64C2201/127 ,  B64D1/08 ,  B64D47/08 ,  F16M11/041 ,  F16M11/105 ,  F16M11/12 ,  F16M11/123 ,  F16M11/18 ,  F16M11/2064 ,  F16M11/22 ,  F16M13/022 ,  F16M13/04 ,  G03B15/006 ,  G03B17/561 ,  G03B17/566 ,  H04N5/2253 ,  H04N5/23203 ,  H04N5/23216

Abstract: A platform for interchangeably mounting a payload to a base support is provided. In one aspect, the platform comprises: a support assembly configured to be releasably coupled to a payload via a first coupling and configured to control a spatial disposition of the payload; and a mounting assembly configured to be releasably coupled via a second coupling to a plurality of types of base supports selected from at least two of the following: an aerial vehicle, a handheld support, or a base adapter mounted onto a movable object.

公开(公告)号：US11852282B2

公开(公告)日：2023-12-26

申请号：US17651786

申请日：2022-02-18

Applicant: SZ DJI TECHNOLOGY CO., LTD.

Inventor： Xin Yan ,  Xifeng Zhao ,  Rongjian Sun ,  Zhuo Guo

IPC: F16M11/00 ,  F16M11/12 ,  F16M13/00 ,  G03B17/56 ,  F16M13/02 ,  F16M11/18 ,  F16M11/04 ,  F16M11/16

CPC classification number: F16M11/123 ,  F16M11/04 ,  F16M11/16 ,  F16M11/18 ,  F16M13/00 ,  F16M13/02 ,  G03B17/56 ,  F16M2200/022

Abstract: A gimbal includes an axis structure including a rotating member, a bearing member rotatably connected to the rotating member, and a locking structure. The rotating member includes a rotor of a motor or a member fixedly connected to a rotor. The bearing member includes a stator of the motor or a member fixedly connected to a stator. The locking structure includes a positioning snap member movably provided on one of the rotating member and the bearing member and configured to engage with another one of the rotating member and the bearing member. The axis structure is a yaw-axis structure, a roll-axis structure or a pitch-axis structure. The motor is configured to control a movement about a pitch axis, a movement about a yaw axis, or a movement about a roll axis. A rotational position of the rotating member relative to the bearing member is locked by the locking structure when the rotating member rotates to a preset position.

公开(公告)号：US11092771B2

公开(公告)日：2021-08-17

申请号：US16122307

申请日：2018-09-05

Applicant: SZ DJI TECHNOLOGY CO., LTD.

Inventor： Ran Liao ,  Peng Bin ,  Hao Liu ,  Xifeng Zhao

IPC: G02B7/02 ,  G02B7/04 ,  G03B17/12 ,  G03B15/00 ,  G03B5/00

Abstract: A lens locking apparatus is configured to be coupled to a lens module. The lens module is configured to focus on an object by translating along an optical axis of the lens module. The lens locking apparatus is configured to fix a position of the lens module by applying a compressive force on the lens module when the lens module is at a focused position.

公开(公告)号：US10647409B2

公开(公告)日：2020-05-12

申请号：US15584643

申请日：2017-05-02

Applicant: SZ DJI TECHNOLOGY CO., LTD.

Inventor： Weidong Li ,  Xifeng Zhao

IPC: B64C11/02 ,  B64C11/00 ,  B64C39/02 ,  A63H27/00 ,  F02B75/34

Abstract: Locking device, propeller, and aerial vehicle are provided. An exemplary propeller includes a blade; and a locking part, configured for locking the blade to a driving shaft. The locking part includes a fastening portion and a pressing portion. The pressing portion includes a pressing end, an abutting end including an accommodating hole, and an abutting part configured within the accommodating hole for abutting against the fastening portion. The fastening portion is accommodable within the accommodating hole of the pressing portion. The pressing portion of the locking part is slidably connected with the blade. A portion of the driving shaft protrudes into the accommodating hole of the pressing portion. The fastening portion is abutted against the abutting part of the pressing portion and engaged with the driving shaft to lock the driving shaft on the blade.

公开(公告)号：USD805017S1

公开(公告)日：2017-12-12

申请号：US29569817

申请日：2016-06-30

Applicant: SZ DJI Technology Co., Ltd.

Designer： Zhen Wang ,  Xifeng Zhao ,  Ping Wang

公开(公告)号：US20160255249A1

公开(公告)日：2016-09-01

申请号：US15154740

申请日：2016-05-13

Applicant: SZ DJI TECHNOLOGY CO., LTD

Inventor： Paul Pan ,  Xifeng Zhao ,  Tao Zhao

IPC: H04N5/225 ,  F16M11/10 ,  F16M11/20 ,  B64C39/02 ,  F16M13/02

CPC classification number: H04N5/2251 ,  A45F5/10 ,  B64C39/024 ,  B64C2201/127 ,  B64D1/08 ,  B64D47/08 ,  F16M11/041 ,  F16M11/105 ,  F16M11/12 ,  F16M11/123 ,  F16M11/18 ,  F16M11/2064 ,  F16M11/22 ,  F16M13/022 ,  F16M13/04 ,  G03B15/006 ,  G03B17/561 ,  G03B17/566 ,  H04N5/2253 ,  H04N5/23203 ,  H04N5/23216

Abstract: A platform for interchangeably mounting a payload to a base support is provided. In one aspect, the platform comprises: a support assembly configured to be releasably coupled to a payload via a first coupling and configured to control a spatial disposition of the payload; and a mounting assembly configured to be releasably coupled via a second coupling to a plurality of types of base supports selected from at least two of the following: an aerial vehicle, a handheld support, or a base adapter mounted onto a movable object.

公开(公告)号：US20160083110A1

公开(公告)日：2016-03-24

申请号：US14463558

申请日：2014-08-19

Applicant: SZ DJI TECHNOLOGY Co., Ltd.

Inventor： Paul Pan ,  Xifeng Zhao ,  Tao Zhao

IPC: B64D47/08 ,  H04N5/232 ,  H04N5/225 ,  F16M11/12 ,  B64C39/02

CPC classification number: H04N5/2251 ,  A45F5/10 ,  B64C39/024 ,  B64C2201/127 ,  B64D1/08 ,  B64D47/08 ,  F16M11/041 ,  F16M11/105 ,  F16M11/12 ,  F16M11/123 ,  F16M11/18 ,  F16M11/2064 ,  F16M11/22 ,  F16M13/022 ,  F16M13/04 ,  G03B15/006 ,  G03B17/561 ,  G03B17/566 ,  H04N5/2253 ,  H04N5/23203 ,  H04N5/23216

Abstract: A platform for interchangeably mounting a payload to a base support is provided. In one aspect, the platform comprises: a support assembly configured to be releasably coupled to a payload via a first coupling and configured to control a spatial disposition of the payload; and a mounting assembly configured to be releasably coupled via a second coupling to a plurality of types of base supports selected from at least two of the following: an aerial vehicle, a handheld support, or a base adapter mounted onto a movable object.

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

IPC: H05K7/20 ,  B64C39/02

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.