-
公开(公告)号：US20180281935A1
公开(公告)日：2018-10-04
申请号：US16005309
申请日：2018-06-11
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor： Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
IPC: B64C27/08 , B64C25/06 , B64C25/32 , B64C27/00 , B64D43/00 , G01V3/16 , B64C27/54 , B64C1/30 , B64C39/02 , G05D1/00 , G01R33/00
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.
-
公开(公告)号：US20180088143A1
公开(公告)日：2018-03-29
申请号：US15809952
申请日：2017-11-10
Applicant: SZ DJI TECHNOLOGY CO, LTD.
IPC: G01P1/00 , B64D45/00 , F16F15/00 , G01C19/16 , G01C19/56 , G01C19/5628 , G01C19/5663 , G01C19/5769 , G01C19/5783 , G01C21/16 , G01C25/00 , G01P1/02 , G01P15/08
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.
-
公开(公告)号：US20180035020A1
公开(公告)日：2018-02-01
申请号：US15713430
申请日：2017-09-22
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor： Paul Pan , Xifeng Zhao , Tao Zhao
IPC: H04N5/225 , A45F5/10 , G03B17/56 , G03B15/00 , F16M13/04 , B64C39/02 , F16M11/20 , F16M11/12 , F16M11/10 , B64D47/08 , B64D1/08 , H04N5/232 , 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：US09777887B2
公开(公告)日：2017-10-03
申请号：US15092959
申请日：2016-04-07
Applicant: SZ DJI TECHNOLOGY Co., LTD
Inventor： Paul Pan , Xifeng Zhao , Tao Zhao
IPC: G03B17/56 , H04N5/225 , F16M13/04 , F16M13/02 , G03B15/00 , A45F5/10 , B64C39/02 , B64D47/08 , F16M11/04 , F16M11/12 , F16M11/18 , F16M11/20 , F16M11/22
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：US20170089513A1
公开(公告)日：2017-03-30
申请号：US15092959
申请日：2016-04-07
Applicant: SZ DJI TECHNOLOGY Co., LTD
Inventor： Paul Pan , Xifeng Zhao , Tao Zhao
IPC: F16M13/02 , G03B17/56 , H04N5/225 , A45F5/10 , F16M11/22 , B64D47/08 , F16M11/04 , F16M11/12 , F16M11/18 , F16M11/20 , G03B15/00 , 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.
-
Patent Agency Ranking
公开(公告)号：US09592744B2
公开(公告)日：2017-03-14
申请号：US14262478
申请日：2014-04-25
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor： Tao Zhao
CPC classification number: B60L11/1822 , B60L11/1861 , B60L11/1866 , B60L2200/10 , B60L2260/32 , B64C39/024 , B64C2201/108 , B64C2201/146 , H02J7/0026 , Y02T10/7005 , Y02T10/7044 , Y02T10/7061
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.
Abstract translation: 本公开提供一种电池，其可以包括电源和电源电路，电源电路连接到电源。 电源可以通过电源电路放电。 电子开关可以控制电源的接通或断开，从而避免在通电过程中产生火花，并允许电池的正常使用和飞机的安全。 本公开还提供了具有电池的飞行器。
-
公开(公告)号：US09280038B1
公开(公告)日：2016-03-08
申请号：US14463558
申请日：2014-08-19
Applicant: SZ DJI TECHNOLOGY Co., Ltd
Inventor： Paul Pan , Xifeng Zhao , Tao Zhao
IPC: G03B17/56
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.
Abstract translation: 提供了一种用于可互换地将有效载荷安装到基座支撑件的平台。 在一个方面，平台包括：支撑组件，其被配置为经由第一联接件可释放地耦合到有效载荷并且被配置为控制有效载荷的空间布置; 以及安装组件，其构造成经由第二联接件可释放地联接到从以下至少两个中选择的多种类型的基座支架：飞行器，手持支架或安装在可移动物体上的基座适配器。
-
公开(公告)号：US09162758B2
公开(公告)日：2015-10-20
申请号：US14534127
申请日：2014-11-05
Applicant: SZ DJI Technology Co., Ltd
Inventor： Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
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.
-
公开(公告)号：US09016617B2
公开(公告)日：2015-04-28
申请号：US14092653
申请日：2013-11-27
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.
Abstract translation: 本发明提供了可靠性提高的无人驾驶飞行器（UAV）的方法和装置。 根据本发明的一个方面，降低了来自车载电气部件的车载传感器所经受的干扰。 根据本发明的另一方面，电子部件的用户配置或组装被最小化以减少用户错误。
-
公开(公告)号：US20150060606A1
公开(公告)日：2015-03-05
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.
Abstract translation: 本发明提供了可靠性提高的无人驾驶飞行器（UAV）的方法和装置。 根据本发明的一个方面，降低了来自车载电气部件的车载传感器所经受的干扰。 根据本发明的另一方面，电子部件的用户配置或组装被最小化以减少用户错误。
-
-
-
-
-
-
-
-
-
Search Results
125
records
(took 0.034 seconds)
