-
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.
-
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.
-
公开(公告)号：US20160016663A1
公开(公告)日：2016-01-21
申请号：US14333462
申请日：2014-07-16
Applicant: Ford Global Technologies, LLC
Inventor： Joe F. Stanek , Tony A. Lockwood
CPC classification number: G05D1/0276 , B60R16/02 , B60W30/00 , B64C29/0008 , B64C29/0091 , B64C29/02 , B64C39/00 , B64C39/02 , B64C39/022 , B64C39/024 , B64C2201/00 , B64C2201/02 , B64C2201/08 , B64C2201/086 , B64C2201/088 , B64C2201/12 , B64C2201/126 , B64C2201/127 , B64C2201/14 , B64C2201/141 , B64C2201/18 , B64C2201/182 , B64C2201/185 , B64C2201/187 , B64C2201/20 , B64C2201/208 , B64C2230/00 , G05D1/0022 , G05D1/0088 , G05D1/0094 , G05D1/0202 , G05D1/0212 , G05D1/0231 , G05D1/0242 , G05D1/0255 , G05D1/0257 , G05D1/028 , G05D2201/0213 , G08C17/00 , G08G1/012 , G08G1/091
Abstract: This disclosure generally relates to an automotive drone deployment system that includes at least a vehicle and a deployable drone that is configured to attach and detach from the vehicle. More specifically, the disclosure describes the vehicle and drone remaining in communication with each other to exchange information while the vehicle is being operated in an autonomous driving mode so that the vehicle's performance under the autonomous driving mode is enhanced.
Abstract translation: 本公开总体上涉及一种汽车无人机部署系统，该系统至少包括车辆和可部署的无人机，其配置为从车辆附接和分离。 更具体地，本公开描述了当车辆以自主驾驶模式操作时彼此保持通信的车辆和无人机交换信息，使得车辆在自主驾驶模式下的性能得到增强。
-
公开(公告)号：US09233754B1
公开(公告)日：2016-01-12
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
IPC: B64C29/00 , B64C27/08 , B64C27/00 , B64D43/00 , G05D1/00 , B64C25/06 , B64C39/02 , B64C25/32 , A63H27/00
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：US20150379874A1
公开(公告)日：2015-12-31
申请号：US14282345
申请日：2014-05-20
Applicant: Verizon Patent and Licensing Inc.
Inventor： Gurpreet UBHI , Ashok N. SRIVASTAVA , Douglas M. PASKO , Hani BATLA , Igor KANTOR
CPC classification number: G08G5/0069 , B60L8/003 , B60L11/1805 , B60L11/1861 , B60L2200/10 , B60L2200/40 , B60L2240/12 , B60L2240/26 , B60L2240/622 , B60L2240/66 , B60L2240/662 , B60L2240/70 , B60L2250/12 , B60L2250/16 , B60L2260/32 , B60L2260/42 , B64C39/024 , B64C2201/042 , B64C2201/122 , B64C2201/128 , B64C2201/14 , G01C21/20 , G01S5/0027 , G01S2205/005 , G05D1/101 , G06Q10/06 , G06Q50/30 , G08G5/0013 , G08G5/0034 , G08G5/0039 , G08G5/0043 , G08G5/0056 , G08G5/006 , G08G5/0086 , G08G5/0091 , H04B7/18506 , Y02T10/7005 , Y02T10/7044 , Y02T10/705 , Y02T10/7083 , Y02T10/7291 , Y02T90/16 , Y02T90/162
Abstract: A device receives a request for a flight path from a first location to a second location in a region, and calculates the flight path based on the request and based on one or more of weather information, air traffic information, obstacle information, regulatory information, or historical information associated with the region. The device determines required capabilities for the flight path based on the request, and selects, from multiple UAVs, a particular UAV based on the required capabilities for the flight path and based on a ranking of the multiple UAVs. The device generates flight path instructions for the flight path, and provides the flight path instructions to the particular UAV to permit the particular UAV to travel from the first location to the second location via the flight path.
Abstract translation: 设备接收从区域中的第一位置到第二位置的飞行路径的请求，并且基于该请求并且基于天气信息，空中交通信息，障碍物信息，管理信息， 或与该地区相关的历史信息。 该设备基于该请求确定飞行路径的所需能力，并且基于飞行路径的所需能力并且基于多个UAV的排名从多个UAV中选择特定UAV。 该设备生成飞行路径的飞行路径指令，并且向特定UAV提供飞行路线指令，以允许特定UAV经由飞行路径从第一位置行进到第二位置。
-
Patent Agency Ranking
公开(公告)号：US20150353196A1
公开(公告)日：2015-12-10
申请号：US14733962
申请日：2015-06-09
Applicant: Izak Jan van Cruyningen , Robert Van Wart
Inventor： Izak Jan van Cruyningen , Robert Van Wart
CPC classification number: B64C39/024 , B64C2201/107 , B64C2201/127 , B64C2201/14 , G01R29/0878 , G01R31/085 , G01R31/40 , G05D1/101 , H02G1/02
Abstract: FIG. 1 shows airframe 10 with electromagnetic field sensor 12, adjustable reference electromagnetic field strength 14, comparator 16, parachute 18, parachute trigger 19, and inspection camera 20 inspecting a transmission line corridor containing towers 40, 42, and 44, phase conductors 46, 48, and 50, and shield wires 52 and 54. Reference electromagnetic field strength 14 is adjusted before the flight to set the minimum electromagnetic field strength before parachute trigger 19 deploys parachute 18. The reference electromagnetic field strength 14 corresponds to a radius, and thus virtual tunnel 22, outside of which airframe 10 cannot fly without deploying parachute 18, regardless of the state of the autopilot, GPS signal, or radio link.
Abstract translation: 图。 图1示出了具有电磁场传感器12的机身10，可调参考电磁场强度14，比较器16，降落伞18，降落伞触发器19和检查摄像机20，检查包含塔40,42和44的传输线走廊，相导体46,48 和50，以及屏蔽线52和54.在飞行之前调整参考电磁场强度14，以在降落伞触发器19部署降落伞18之前设置最小电磁场强度。参考电磁场强度14对应于半径，因此虚拟 无论自动驾驶仪，GPS信号或无线电链路的状态如何，外部机身10不能飞行而不部署降落伞18。
-
公开(公告)号：US20150314870A1
公开(公告)日：2015-11-05
申请号：US14738467
申请日：2015-06-12
Applicant: BCB INTERNATIONAL LTD.
Inventor： Barry Davies
CPC classification number: B64C39/024 , B64C19/00 , B64C39/028 , B64C2201/00 , B64C2201/14 , B64C2201/141 , B64C2230/00 , B64C2230/02 , G01S15/06 , G01S15/88 , G01S15/89 , G01S15/8913 , G01S15/8929 , G01S15/8993 , G01S15/93 , G05D1/0088 , G05D1/0202 , G05D1/101 , G05D1/102 , Y10S367/909
Abstract: A micro unmanned aerial vehicle or drone (“UAV”) 10 is remotely controlled through an HMI, although this remote control is supplemented by and selectively suppressed by an on-board controller. The controller operates to control the generation of a sonar bubble that generally encapsulates the UAV. The sonar bubble, which may be ultrasonic in nature, is produced by a multiplicity of sonar lobes generated by specific sonar emitters associated with each axis of movement for the UAV. The emitters produce individual and beamformed sonar lobes that partially overlap to provide stereo or bioptic data in the form of individual echo responses detected by axis-specific sonar detectors. In this way, the on-board controller is able to interpret and then generate 3-D spatial imaging of the physical environment in which the UAV is currently moving or positioned. The controller is therefore able to plot relative and absolute movement of the UAV through the 3-D space by recording measurements from on-board gyroscopes, magnetometers and accelerometers. Data from the sonar bubble can therefore both proactively prevent collisions with objects by imposing a corrective instruction to rotors and other flight control system and can also assess and compensate for sensor drift.
Abstract translation: 微型无人驾驶飞行器或无人驾驶飞机（“UAV”）10通过HMI进行远程控制，尽管该遥控器由车载控制器补充并选择性地抑制。 控制器用于控制通常封装无人机的声纳气泡的产生。 本质上可能是超声波的声纳气泡由与用于UAV的每个运动轴相关联的特定声纳发射器产生的多个声纳波瓣产生。 发射器产生单个和波束形成的声纳波瓣，其部分重叠以提供以轴特定声纳探测器检测的单独回波响应形式的立体声或生物数据。 以这种方式，车载控制器能够解释然后生成UAV当前正在移动或定位的物理环境的三维空间成像。 因此，控制器能够通过记录来自车载陀螺仪，磁力计和加速度计的测量值来绘制UAV通过3-D空间的相对和绝对运动。 因此，来自声纳气泡的数据可以通过对转子和其他飞行控制系统施加纠正指令来主动防止与物体的碰撞，并且还可以评估和补偿传感器漂移。
-
公开(公告)号：US20150298788A1
公开(公告)日：2015-10-22
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.
Abstract translation: 提供了可变形飞行器的系统，装置和方法。 一方面，可变形飞行器包括：中心体和分别设置在中心体上的至少两个可变形框架组件，所述至少两个可变形框架组件中的每一个具有枢转地联接到中心体的近侧部分和远端部分 ; 驱动组件，其安装在所述中心主体上并且构造成将所述至少两个框架组件相对于所述中心体枢转到多个不同的垂直角度; 以及安装在所述至少两个可变形框架组件上并可操作以移动所述可变形飞行器的多个推进单元。
-
公开(公告)号：US09108713B2
公开(公告)日：2015-08-18
申请号：US13318459
申请日：2010-09-09
Applicant: Tony Shuo Tao , Nathan Olson , Carlos Thomas Miralles , Robert Nickerson Plumb
Inventor： Tony Shuo Tao , Nathan Olson , Carlos Thomas Miralles , Robert Nickerson Plumb
IPC: B64C1/26 , B64C3/56 , B64C9/02 , B64C3/44 , B64C3/50 , B64C5/12 , B64C13/18 , B64C13/28 , B64C39/02
CPC classification number: B64C13/28 , B64C3/44 , B64C3/50 , B64C3/56 , B64C5/12 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64C13/18 , B64C39/024 , B64C2009/005 , B64C2201/021 , B64C2201/08 , B64C2201/102 , B64C2201/121 , B64C2201/14 , B64C2201/145 , B64C2201/146
Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100, 400, 1000, 1500) configured to control pitch, roll, and/or yaw via airfoils (141, 142, 1345, 1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621, 622). Embodiments include one or more rudder elements (1045, 1046, 1145, 1146, 1245, 1345, 1346, 1445, 1446, 1545, 1546) which may be rotatably attached and actuated by an effector member (1049, 1149, 1249, 1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.
Abstract translation: 一种包括飞行器或无人驾驶飞行器（UAV）（100,400,1000,1500）的系统，其被配置成通过具有弹性安装的后缘的翼型件（141,142,1345,1346）来控制俯仰，滚动和/或偏航 与机身偏转致动器喇叭（621,622）相反。 实施例包括一个或多个舵元件（1045,1046,1145,1146,1245,1345,1346,1445,1446,1545,1546），其可以由效应构件（1049,1149，1249,1349）旋转地附接和致动， 设置在机身壳体（1001）内并且部分地可扩展以接合一个或多个舵元件。
-
公开(公告)号：US08985504B2
公开(公告)日：2015-03-24
申请号：US13524937
申请日：2012-06-15
Applicant: Tony Shuo Tao , Nathan Olson , Carlos Thomas Miralles , Robert Nickerson Plumb
Inventor： Tony Shuo Tao , Nathan Olson , Carlos Thomas Miralles , Robert Nickerson Plumb
CPC classification number: B64C13/28 , B64C3/44 , B64C3/50 , B64C3/56 , B64C5/12 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64C13/18 , B64C39/024 , B64C2009/005 , B64C2201/021 , B64C2201/08 , B64C2201/102 , B64C2201/121 , B64C2201/14 , B64C2201/145 , B64C2201/146
Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) configured to control pitch, roll, and/or yaw via airfoils having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns. Embodiments include one or more rudder elements which may be rotatably attached and actuated by an effector member disposed within the fuselage housing and extendible in part to engage the one or more rudder elements.
Abstract translation: 一种包括飞行器或无人驾驶飞行器（UAV）的系统，其构造成经由具有弹性安装的后缘的机翼来控制俯仰，滚动和/或偏航，所述后翼与机身偏转致动器角相对。 实施例包括一个或多个舵元件，其可以由设置在机身壳体内的效应器构件可旋转地附接和致动，并且部分地可部分地接合一个或多个舵元件。
-
-
-
-
-
-
-
-
-
Search Results
283
records
(took 0.024 seconds)
