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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.
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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.
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公开(公告)号：US09650155B2
公开(公告)日：2017-05-16
申请号：US14020939
申请日：2013-09-09
Applicant: SZ DJI TECHNOLOGY CO., LTD.
CPC classification number: G05D1/0016 , A63H27/12 , A63H30/04 , B64C13/20 , B64C39/024 , B64C2201/127 , B64C2201/146 , B64D47/08 , G05D1/0033
Abstract: An aircraft control apparatus, control system, and control method are disclosed. A control apparatus includes: a first control rod configured to have a movement in a first movement direction controlling a motion of an aircraft in a first motion direction, wherein after an external force on the first control rod in the first movement direction is removed, the first control rod automatically returns to a preset position in the first movement direction; wherein the preset position which the first control rod automatically returns to corresponds to the aircraft in the first motion direction maintaining a state of flight; wherein the maintaining state of flight depends on control signals received by the aircraft generated resulting from changes in the external force applied to the control rod in the first movement direction and state signals measured by state measurement sensors carried by the aircraft.
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公开(公告)号：US20170104353A1
公开(公告)日：2017-04-13
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：US20170096210A1
公开(公告)日：2017-04-06
申请号：US15294517
申请日：2016-10-14
Applicant: SZ DJI TECHNOLOGY Co., LTD
Inventor： Tao Wang , Tao Zhao , Hao Du , Mingxi Wang
CPC classification number: B64C1/063 , A63H27/12 , B64C1/00 , B64C1/061 , B64C25/32 , B64C27/08 , B64C39/024 , B64C39/028 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/14 , B64C2201/146 , B64C2201/165 , B64D47/00 , B64D47/08 , G05D1/042
Abstract: Systems, devices, and methods for a transformable aerial vehicle are provided. In one aspect, a transformable aerial vehicle includes: a central body and at least two transformable frames assemblies respectively disposed on the central body, each of the at least two transformable frame assemblies having a proximal portion pivotally coupled to the central body and a distal portion; an actuation assembly mounted on the central body and configured to pivot the at least two frame assemblies to a plurality of different vertical angles relative to the central body; and a plurality of propulsion units mounted on the at least two transformable frame assemblies and operable to move the transformable aerial vehicle.
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Patent Agency Ranking
公开(公告)号：US20160096614A1
公开(公告)日：2016-04-07
申请号：US14944042
申请日：2015-11-17
Applicant: SZ DJI TECHNOLOGY CO., Ltd
Inventor： Tao Wang , Tao Zhao , Hao Du , Mingxi Wang
CPC classification number: B64C1/063 , A63H27/12 , B64C1/00 , B64C1/061 , B64C25/32 , B64C27/08 , B64C39/024 , B64C39/028 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/14 , B64C2201/146 , B64C2201/165 , B64D47/00 , B64D47/08 , G05D1/042
Abstract: Systems, devices, and methods for a transformable aerial vehicle are provided. In one aspect, a transformable aerial vehicle includes: a central body and at least two transformable frames assemblies respectively disposed on the central body, each of the at least two transformable frame assemblies having a proximal portion pivotally coupled to the central body and a distal portion; an actuation assembly mounted on the central body and configured to pivot the at least two frame assemblies to a plurality of different vertical angles relative to the central body; and a plurality of propulsion units mounted on the at least two transformable frame assemblies and operable to move the transformable aerial vehicle.
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公开(公告)号：US20160083084A1
公开(公告)日：2016-03-24
申请号：US14954427
申请日：2015-11-30
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor： Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
CPC classification number: B64C27/08 , A63H27/12 , B64C1/30 , B64C25/06 , B64C25/32 , B64C27/00 , B64C27/54 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/14 , B64C2201/141 , B64C2201/20 , B64D31/14 , B64D43/00 , G01R33/0047 , G01V3/16 , G05D1/00 , Y10T29/49117
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：US09284040B2
公开(公告)日：2016-03-15
申请号：US14718021
申请日：2015-05-20
Applicant: SZ DJI TECHNOLOGY CO., Ltd
Inventor： Tao Wang , Tao Zhao , Zhi Gang Ou
CPC classification number: B64C27/32 , A63H27/001 , A63H27/02 , B64C11/02 , B64C11/04 , B64C27/08 , B64C27/14 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , F01D5/025
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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公开(公告)号：US09242714B2
公开(公告)日：2016-01-26
申请号：US14565119
申请日：2014-12-09
Applicant: SZ DJI TECHNOLOGY CO., Ltd
Inventor： Tao Wang , Tao Zhao , Hao Du , Mingxi Wang
CPC classification number: B64C1/063 , A63H27/12 , B64C1/00 , B64C1/061 , B64C25/32 , B64C27/08 , B64C39/024 , B64C39/028 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/14 , B64C2201/146 , B64C2201/165 , B64D47/00 , B64D47/08 , G05D1/042
Abstract: Systems, devices, and methods for a transformable aerial vehicle are provided. In one aspect, a transformable aerial vehicle includes: a central body and at least two transformable frames assemblies respectively disposed on the central body, each of the at least two transformable frame assemblies having a proximal portion pivotally coupled to the central body and a distal portion; an actuation assembly mounted on the central body and configured to pivot the at least two frame assemblies to a plurality of different vertical angles relative to the central body; and a plurality of propulsion units mounted on the at least two transformable frame assemblies and operable to move the transformable aerial vehicle.
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公开(公告)号：US09221536B2
公开(公告)日：2015-12-29
申请号：US14515357
申请日：2014-10-15
Applicant: SZ DJI Technology Co., Ltd
Inventor： Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
CPC classification number: B64C27/08 , A63H27/12 , B64C1/30 , B64C25/06 , B64C25/32 , B64C27/00 , B64C27/54 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/14 , B64C2201/141 , B64C2201/20 , B64D31/14 , B64D43/00 , G01R33/0047 , G01V3/16 , G05D1/00 , Y10T29/49117
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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