公开(公告)号：WO2017114501A1

公开(公告)日：2017-07-06

申请号：PCT/CN2016/113718

申请日：2016-12-30

Applicant: SHAM, Wellen

Inventor： SHAM, Wellen

IPC: H04B7/26

CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/12 ,  B64C2201/122 ,  B64C2201/123

Abstract: Embodiments are provided for facilitating an unmanned aerial vehicle (UAV) network. The UAV network in accordance with the disclosure can comprise multiple UAVs, ground processing stations, and/or any other components. A particular UAV in the network can carry payloads consisting of optical image sensors, processing devices, communication systems, and/or any other components. An individual UAV in the network can comprise photovoltaic cells capable of absorbing solar energy. Embodiments are provided for converting the solar energy to electricity for providing power to payloads aboard the UAV and as well as charging a battery aboard the UAV. In certain embodiments, the UAV can fly up to 65,000 feet and can cover as much as 500 km in range. One motivation of the present disclosure is to "outsource" some or entire information processing by an UAV to existing infrastructure, such as the ground processing station.

Abstract translation: 提供用于促进无人驾驶飞行器（UAV）网络的实施例。 根据本公开的UAV网络可以包括多个UAV，地面处理站和/或任何其他组件。 网络中的特定UAV可以携带由光学图像传感器，处理设备，通信系统和/或任何其他组件组成的有效载荷。 网络中的单个无人机可以包括能够吸收太阳能的光伏电池。 提供了用于将太阳能转换为电力的实施例，用于向无人机上的有效载荷提供电力，并且还为无人飞行器上的电池充电。 在某些实施例中，UAV可以飞行高达65,000英尺并且可以覆盖范围多达500千米。 本公开的一个动机是“外包” 一些无人机处理现有基础设施（如地面处理站）的一些或全部信息。

公开(公告)号：WO2016012055A1

公开(公告)日：2016-01-28

申请号：PCT/EP2014/066069

申请日：2014-07-25

Applicant: TELEFONAKTIEBOLAGET L M ERICSSON (PUBL)

Inventor： DJORDJEVIC, Branko ,  BRAHMI, Nadia ,  DUDDA, Torsten ,  ZHANG, Hanzhi

IPC: H04W84/00

CPC classification number: H04W24/08 ,  B64C39/024 ,  B64C2201/122 ,  H04B7/18504 ,  H04W24/10 ,  H04W36/20 ,  H04W84/005 ,  H04W84/06 ,  H04W88/08

Abstract: A technique for operating a movable radio base station, M-RBS, (200) is described. The M-RBS is configured to provide to a plurality of user equipments (120) wireless access to a telecommunications network (100). As to a method aspect of the technique, the M-RBS (200) is changed from a first mode to a second mode that is different from the first mode. Each of the first mode and the second mode specifies a set of parameter values for operating parameters of the M-RBS (200).

Abstract translation: 描述了用于操作可移动无线电基站M-RBS（200）的技术。 M-RBS被配置为向多个用户设备（120）提供对电信网络（100）的无线接入。 关于该技术的方法方面，M-RBS（200）从第一模式改变为与第一模式不同的第二模式。 第一模式和第二模式中的每一个指定用于M-RBS（200）的操作参数的一组参数值。

公开(公告)号：WO2015175057A3

公开(公告)日：2016-01-07

申请号：PCT/US2015016116

申请日：2015-02-17

Applicant: UBIQOMM LLC

Inventor： JALALI AHMAD

IPC: H04B7/185

CPC classification number: H04B7/18504 ,  B64C39/024 ,  B64C2201/122 ,  H04B7/1555 ,  H04B7/18506 ,  H04B7/18528 ,  H04B7/18539 ,  H04B7/18541 ,  H04B7/18543 ,  H04B7/18554 ,  H04B7/18578 ,  H04W24/02 ,  H04W36/0005 ,  H04W36/30 ,  H04W48/16 ,  H04W84/005 ,  H04W84/06 ,  H04W88/16 ,  Y02B60/50 ,  Y02D70/00 ,  Y02D70/1242 ,  Y02D70/1262 ,  Y02D70/142 ,  Y02D70/164 ,  Y02D70/446

Abstract: Systems and methods for providing broadband internet access to mobile platforms such as vehicles, aircraft, and portable devices, using a network of one or more entities such as drones/unmanned aerial vehicles (UAVs). In one embodiment, the drone communication system comprises an antenna sub-system, a radio sub-system and a data switching sub-system. The mobile platforms comprise antenna and radio sub-systems to communicate with the drones, detect changes in the mobile platforms azimuth and elevation changes, and adjust the mobile platform's antenna beam to compensate for the orientation changes to optimally point toward the drones. The exemplary mobile platform further comprises methods to detect the need for handoff to a different drone and to carry out the handoff. A mechanism to improve coverage to mobile platforms that may see obstruction on their path to the drone network is also disclosed, as are apparatus and methods for cost efficiently providing reliable internet access to portable devices.

Abstract translation: 使用诸如无人机/无人驾驶飞行器（UAV）的一个或多个实体的网络来向诸如车辆，飞行器和便携式设备的移动平台提供宽带互联网接入的系统和方法。 在一个实施例中，无人机通信系统包括天线子系统，无线电子系统和数据交换子系统。 移动平台包括与无人机通信的天线和无线电子系统，检测移动平台方位角和高程变化的变化，并调整移动平台的天线波束以补偿朝向无人机的最佳方向变化。 该示例性移动平台还包括检测对不同无人机进行切换的需要并执行切换的方法。 还公开了一种用于提高可能看到其到无人机网络的路径上的阻​​碍的移动平台的覆盖的机制，以及用于成本有效地提供对便携式设备的可靠互联网访问的设备和方法。

公开(公告)号：WO2015196081A1

公开(公告)日：2015-12-23

申请号：PCT/US2015/036709

申请日：2015-06-19

Applicant: SCOTT TECHNOLOGIES, INC.

Inventor： PATTERSON, Jason, M. ,  PARSON, William, Eugene ,  PHIFER, Jerry, Alan ,  CANNON, Jason, Richard ,  PLUMMER, Darrill, Lee ,  WILLIAMS, Cedric

IPC: B64C39/02

CPC classification number: G08G5/0069 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/12 ,  B64C2201/122 ,  B64C2201/123 ,  B64C2201/127 ,  G05D1/101 ,  G08G5/0034 ,  G08G5/006

Abstract: A device, and method for situational awareness of an emergency scene for first responders uses an unmanned aerial vehicle- equipped with a sensor package in populated or otherwise restricted areas. The unmanned aerial vehicle is assigned to a control center for a designated incident while automatically tasking the unmanned aerial vehicle with the initiation of the incident response to autonomously proceed to the incident prior the control center taking active control of the unmanned aerial vehicle.

Abstract translation: 用于第一响应者的紧急情况的情境意识的装置和方法使用在人口稠密或其他限制区域中装备传感器包的无人驾驶飞行器。 无人驾驶飞行器被分配到指定事故的控制中心，同时在控制中心主动控制无人驾驶飞行器之前，随着事件响应的启动自动处理无人机，自主进行事故。

公开(公告)号：WO2015091954A3

公开(公告)日：2015-09-24

申请号：PCT/EP2014078751

申请日：2014-12-19

Applicant: KABBANI ZIAD

Inventor： KABBANI ZIAD

IPC: G09F19/18 ,  B64C39/02 ,  G09F13/02 ,  G09F21/12 ,  G09F27/00

CPC classification number: G09F21/12 ,  B64C39/024 ,  B64C2201/122 ,  G09F13/02 ,  G09F19/18 ,  G09F27/005

Abstract: The invention relates to a method for transporting at least one information or advertising medium (1) by means of a remote-controllable, helicopter-type small flying vehicle (2). In said method, the information or advertising medium (1) is held substantially in a predefined shape (3) substantially underneath the small flying vehicle (2). The invention further relates to an apparatus (15) for transporting at least one information or advertising medium as well as to an information or advertising medium (1).

Abstract translation: 本发明涉及一种通过远程可控，直升机类似的小飞行器（2），其中所述信息或广告面（1）基本上是以下的小飞机的装置运送的至少一个的信息或广告面（1）的方法，（2）基本上是（在规定的形状 3）举行。 本发明还涉及一种装置（15），用于传送至少一个信息或广告表面以及一个信息或广告面（1）。

公开(公告)号：WO2014105300A1

公开(公告)日：2014-07-03

申请号：PCT/US2013/071148

申请日：2013-11-21

Applicant: GOOGLE INC.

Inventor： BONAWITZ, Keith, Allen ,  TREUILLE, Adrien

IPC: H04L12/28

CPC classification number: G08G5/0034 ,  B64B1/58 ,  B64B1/60 ,  B64C2201/022 ,  B64C2201/122 ,  G05D1/104 ,  G06Q10/047 ,  G08G1/20 ,  G08G1/202 ,  G08G5/0043 ,  G08G5/0069 ,  G08G5/0091 ,  H04B7/18504

Abstract: Methods and systems for determining trajectories for vehicles of a fleet of vehicles are provided. In one example, a method comprises receiving an initial location of one or more vehicles, and receiving a sequence of coverage requirements for a region and an associated period of time. The region may be divided into a plurality of landmarks and the period of time may be divided into a plurality of phases. The method also comprises determining for each of one or more phases and at least one respective landmark, a set of starting landmarks from which a vehicle could reach the respective landmark during the phase. The method further comprises determining which respective landmark that the vehicle should travel to during the one or more phases based on the sequence of coverage requirements and the set of starting landmarks for the one or more phases and the at least one respective landmark.

Abstract translation: 提供了用于确定车队车辆轨迹的方法和系统。 在一个示例中，一种方法包括接收一个或多个车辆的初始位置，以及接收一个区域和相关时间段的覆盖要求序列。 该区域可以被划分为多个地标，并且该时间段可以被分成多个阶段。 该方法还包括确定一个或多个相位中的每一个以及至少一个相应的标记，一组起始地标，在该阶段期间车辆可从该起始地标到达相应的地标。 所述方法还包括基于所述一个或多个相位和所述至少一个相应地标的覆盖要求序列和所述一组起始地标来确定所述车辆在所述一个或多个阶段期间应该行进到哪个相应的标记。

公开(公告)号：WO2014025622A1

公开(公告)日：2014-02-13

申请号：PCT/US2013/053302

申请日：2013-08-01

Applicant: GOOGLE INC.

Inventor： DEVAUL, Richard, Wayne ,  TELLER, Eric ,  BIFFLE, Clifford, L. ,  RHODES, Brad ,  WEAVER, Joshua

IPC: B64B1/58 ,  H04W16/26 ,  B65D88/12

CPC classification number: B64B1/40 ,  B64B1/58 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/122 ,  B64C2201/201 ,  B64C2201/208 ,  B64C2201/22 ,  B64F1/04 ,  B64F1/22 ,  H04L43/0811 ,  H04L43/0817 ,  Y04S40/168

Abstract: Disclosed embodiments relate to a combined shipping container and balloon deployment system for deploying balloons into a balloon network. Such a shipping container may allow one or more balloons to be transported to a desired launch location, and then launched directly from the shipping container.

Abstract translation: 公开的实施例涉及用于将气囊部署到气球网络中的组合运输容器和气囊展开系统。 这种运输容器可以允许一个或多个气囊被运送到期望的发射位置，然后直接从运输容器发射。

公开(公告)号：WO2012063220A3

公开(公告)日：2012-07-12

申请号：PCT/IB2011055021

申请日：2011-11-10

Applicant: SHACHOR GABRIEL ,  COHEN SHY ,  KEIDAR RONEN ,  SKY SAPIENCE

Inventor： SHACHOR GABRIEL ,  COHEN SHY ,  KEIDAR RONEN

IPC: B64C25/00

CPC classification number: B64F1/12 ,  B64C27/04 ,  B64C27/08 ,  B64C29/04 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/148 ,  B64F1/007 ,  B64F1/125

Abstract: An aerial unit includes a connecting element arranged to connect a ground unit to the aerial unit. The ground unit may include a connecting element manipulator, for altering an effective length of the connecting element and a ground unit controller for controlling the connecting element manipulator. A positioning unit is arranged to image the aerial unit and to generate metadata about a location of the aerial unit. An interfacing module is provided for coupling a payload to the aerial unit. At least one of the ground unit and the aerial unit may include a controller that is arranged to control, at least in response to the metadata, at least one of a first propeller motor and at least one steering element to affect at least one of the location of the aerial unit and the orientation of the aerial unit.

Abstract translation: 天线单元包括连接元件，该连接元件将接地单元连接到天线单元。 接地单元可以包括用于改变连接元件的有效长度的连接元件操纵器和用于控制连接元件操纵器的接地单元控制器。 定位单元布置成对天线单元进行成像并生成关于天线单元的位置的元数据。 提供了用于将有效载荷耦合到天线单元的接口模块。 地面单元和天线单元中的至少一个可以包括控制器，其被布置为至少响应于元数据来控制第一螺旋桨电动机和至少一个操纵元件中的至少一个，以影响至少一个 天线单元的位置和天线单元的方向。

公开(公告)号：WO0176941A9

公开(公告)日：2002-12-27

申请号：PCT/US0110876

申请日：2001-04-03

Applicant: AEROVIRONMENT INC

Inventor： MACCREADY PAUL ,  HIBBS BART D ,  CURTIN ROBERT F JR ,  SWANSON KYLE D ,  BELIK PAUL

IPC: B64C1/26 ,  B64C3/10 ,  B64C3/14 ,  B64C3/36 ,  B64C9/24 ,  B64C39/02 ,  B64C39/10 ,  B64D27/02 ,  B64D27/24 ,  B64D37/30 ,  H01M8/00 ,  B64C9/22 ,  F17C9/02 ,  H01M8/04

CPC classification number: B64D27/24 ,  B64C1/26 ,  B64C3/10 ,  B64C3/14 ,  B64C9/24 ,  B64C39/024 ,  B64C39/10 ,  B64C2201/021 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/187 ,  B64D27/02 ,  B64D37/30 ,  B64D2041/005 ,  Y02T50/12 ,  Y02T50/32 ,  Y02T50/44 ,  Y02T50/64 ,  Y02T90/36

Abstract: Disclosed is an aircraft (101), configured to have a wide range of flight speeds, consuming low levels of power for an extended period of time, while supporting a communications platform with an unobstructed downward-looking view. The aircraft (101) includes an extendable slat (205) at the leading edge of the wing (103), and a reflexed trailing edge. The aircraft comprises a flying wing (103) extending laterally between two ends and a center point. The wing (103) is swept and has a relatively constant chord. The aircraft (101) also includes a power module configured to provide power via a fuel cell (131). The fuel cell (131) stores liquid hydrogen as fuel, but uses gaseous hydrogen in the fuel cell (131). A fuel tank heater is used to control the boil-rate of the fuel in the fuel tank. The aircraft (101) of the invention includes a support structure including a plurality of supports, where the supports form a tetrahedron that affixes to the wing (103).

Abstract translation: 公开了一种飞机（101），其被配置为具有宽范围的飞行速度，在较长的时间段内消耗较低的功率水平，同时支撑具有无遮挡的向下看的视图的通信平台。 飞机（101）包括在机翼（103）的前缘处的可伸展缝翼（205）和反折后缘。 该飞机包括在两端和中心点之间横向延伸的飞翼（103）。 翼（103）被扫过并且具有相对恒定的弦。 飞机（101）还包括配置成经由燃料电池（131）提供电力的电力模块。 燃料电池（131）储存液态氢作为燃料，但在燃料电池（131）中使用气态氢。 燃料箱加热器用于控制燃料箱中的燃料的沸腾率。 本发明的飞行器（101）包括包括多个支撑件的支撑结构，其中支撑件形成附着到机翼（103）的四面体。

公开(公告)号：WO0158758A3

公开(公告)日：2002-05-02

申请号：PCT/US0104632

申请日：2001-02-12

Applicant: AEROVIRONMENT INC

Inventor： MACCREADY PAUL ,  HIBBS BART D ,  COX EARL C ,  LISOSKI DEREK L ,  KENDALL GREG T

IPC: B64C39/00 ,  B64C3/42 ,  B64C3/52 ,  B64C15/02 ,  B64C39/02 ,  B64C39/10 ,  B64D27/24 ,  B64D31/06 ,  G05D1/00 ,  H04B7/185

CPC classification number: B64C3/42 ,  B64C3/52 ,  B64C15/02 ,  B64C39/024 ,  B64C39/10 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/102 ,  B64C2201/122 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64D27/24 ,  B64D31/06 ,  B64D2211/00 ,  G05D1/0022 ,  G05D1/0077 ,  H04B7/18504 ,  Y02T50/12 ,  Y02T50/145 ,  Y02T50/44 ,  Y02T50/62 ,  Y02T50/69

Abstract: This disclosure provides a solar rechargeable aircraft (10) that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. The aircraft can be remotely piloted through multiple, redundant communication subsystems. The availability and reliability of each separate communication subsystem is continuously monitored. The aircraft has a wide variety of applications, which include serving as a long term high altitude platform that serves to link a ground station using radio wave signals and a satellite using optical signals.

Abstract translation: 本公开提供了一种太阳能可再充电飞机（10），其生产便宜，是可操纵的，并且可以几乎无限期地保持机载。 首选飞机是一个装有跨距的飞翼，没有机身或方向舵。 飞机可以通过多个冗余通信子系统进行远程驾驶。 每个单独的通信子系统的可用性和可靠性被不断地监视。 该飞机具有广泛的应用，其中包括作为长期高空平台，用于使用无线电波信号连接地面站和使用光信号的卫星。