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公开(公告)号：US09663245B2
公开(公告)日：2017-05-30
申请号：US14877435
申请日：2015-10-07
Applicant: SZ DJI TECHNOLOGY Co., Ltd
Inventor： Tao Zhao , Xi Feng Zhao , Yong Wang , Li Zhou , Tao Wang
CPC classification number: B64D47/08 , B64C39/024 , B64C2201/127 , B64C2201/128 , F16M11/10 , F16M11/18 , F16M11/2028 , F16M11/42 , G03B15/006 , G03B17/561
Abstract: Systems, devices, and methods are provided relating to improved mounting platforms for supporting a payload on a movable object. In one aspect, an apparatus for supporting a payload comprises: a first support member coupled to the payload and configured to rotate the payload; a second support member coupled to the first support member and configured to rotate the first support member relative to the second support member; and a flexible member electrically coupling the first and second support members, wherein a length of the flexible member winds around a portion of the first support member or second support member, such that the length winds up around the portion when the first support member is rotated in a first direction and unwinds from the portion when the first support member is rotated in a second direction.
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公开(公告)号：US09663244B2
公开(公告)日：2017-05-30
申请号：US14356577
申请日：2014-03-19
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor： Tao Zhao , Xi feng Zhao , Yong Wang , Li Zhou , Tao Wang
CPC classification number: B64D47/08 , B64C39/024 , B64C2201/127 , B64C2201/128 , F16M11/10 , F16M11/18 , F16M11/2028 , F16M11/42 , G03B15/006 , G03B17/561
Abstract: Systems, devices, and methods are provided relating to improved mounting platforms for supporting a payload on a movable object. In one aspect, an apparatus for supporting a payload comprises: a first support member coupled to the payload and configured to rotate the payload; a second support member coupled to the first support member and configured to rotate the first support member relative to the second support member; and a flexible member electrically coupling the first and second support members, wherein a length of the flexible member winds around a portion of the first support member or second support member, such that the length winds up around the portion when the first support member is rotated in a first direction and unwinds from the portion when the first support member is rotated in a second direction.
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公开(公告)号：USD782484S1
公开(公告)日：2017-03-28
申请号：US29559919
申请日：2016-03-31
Applicant: SZ DJI Technology Co., Ltd.
Designer： Dengfeng Hu , Yanxin Huang , Tao Zhao
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公开(公告)号：US20160349280A1
公开(公告)日：2016-12-01
申请号：US15231674
申请日：2016-08-08
Applicant: SZ DJI TECHNOLOGY CO., LTD
IPC: G01P1/00 , G01P15/08 , G01C19/5783
CPC classification number: G01P1/003 , B64C2201/14 , B64D45/00 , F16F7/104 , F16F15/00 , G01C19/16 , G01C19/56 , G01C19/5628 , G01C19/5663 , G01C19/5769 , G01C19/5783 , G01C21/16 , G01C25/00 , G01P1/023 , G01P15/08 , G01P15/0802
Abstract: The present disclosure relates to an inertia measurement module for an unmanned aircraft, which comprises a housing assembly, a sensing assembly and a vibration damper. The vibration damper comprises a first vibration-attenuation cushion; and the sensing assembly comprises a first circuit board, a second circuit board and a flexible signal line for connecting the first circuit board and the second circuit board. An inertia sensor is fixed on the second circuit board, and the first circuit board is fixed on the housing assembly. The inertia measurement module further comprises a weight block, and the second circuit board, the weight block, the first vibration-attenuation cushion and the first circuit board are bonded together. The present disclosure greatly reduces the influence of the operational vibration frequency of the unmanned aircraft on the inertia sensor and improves the measurement stability of the inertia sensor.
Abstract translation: 本公开涉及一种用于无人驾驶飞机的惯性测量模块，其包括壳体组件，感测组件和减振器。 振动阻尼器包括第一减振垫; 并且感测组件包括用于连接第一电路板和第二电路板的第一电路板，第二电路板和柔性信号线。 惯性传感器固定在第二电路板上，第一电路板固定在壳体组件上。 惯性测量模块还包括重量块，并且第二电路板，配重块，第一减振垫和第一电路板结合在一起。 本发明大大降低了无人驾驶飞行器的操作振动频率对惯性传感器的影响，提高了惯性传感器的测量稳定性。
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公开(公告)号：US09493225B2
公开(公告)日：2016-11-15
申请号：US15012068
申请日：2016-02-01
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：US20160200418A1
公开(公告)日：2016-07-14
申请号：US15012152
申请日：2016-02-01
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：US20160075431A1
公开(公告)日：2016-03-17
申请号：US14947923
申请日：2015-11-20
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：US20160031558A1
公开(公告)日：2016-02-04
申请号：US14836344
申请日：2015-08-26
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：US20160023744A1
公开(公告)日：2016-01-28
申请号：US14639550
申请日：2015-03-05
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：US20160016654A1
公开(公告)日：2016-01-21
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.
Abstract translation: 提供了用于推进自行式移动物体的系统，方法和装置。 一方面，一种用于自推进可移动物体的转子组件包括：毂，包括第一紧固特征; 驱动轴，其包括第二紧固特征并且通过所述第一和第二紧固特征的匹配连接直接联接到所述轮毂，其中所述驱动轴构造成引起所述轮毂的旋转，使得所述第一和第二紧固特征 被旋转收紧; 以及多个转子叶片，其联接到所述毂并且被配置为随其旋转以产生推进力。
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