PERSONAL COMMUNICATION DRONE
    71.
    发明申请
    PERSONAL COMMUNICATION DRONE 有权
    个人通信服务

    公开(公告)号:US20160204978A1

    公开(公告)日:2016-07-14

    申请号:US14592494

    申请日:2015-01-08

    Abstract: A system of using a drone for network connectivity, the system may comprise: a connectivity module to: detect an error associated with network traffic on a network connection utilized by a user device; query a connection datastore to retrieve at least one access point location that at least one device of the user has utilized within a predetermined period; a drone coordination module to: transmit configuration settings to a drone, the configuration settings including the at least one access point location and a mode of operation for the drone; and route at least a portion of the network traffic of the user device to the drone for transmission according to the configuration settings.

    Abstract translation: 一种使用无人机进行网络连接的系统,所述系统可以包括:连接模块,用于:检测由用户设备利用的网络连接上与网络流量相关联的错误; 查询连接数据存储以检索在预定时间段内至少一个用户设备已经利用的至少一个接入点位置; 无人机协调模块,用于:将配置设置传输到无人机,所述配置设置包括所述至少一个接入点位置和所述无人机的操作模式; 并且根据配置设置将用户设备的网络流量的至少一部分路由到无人机以进行传输。

    Drag disk, small
    74.
    发明授权
    Drag disk, small 有权
    拖盘,小

    公开(公告)号:US09174738B1

    公开(公告)日:2015-11-03

    申请号:US13862434

    申请日:2013-04-14

    Applicant: Google Inc.

    Abstract: A payload drag structure having a drag disk comprised of a lightweight, flexible material, a tubular section positioned around a periphery of the drag disk, a flexible member positioned within the tubular section, a cross member having a plurality of aims attached about the periphery of the drag disk, wherein one or more arms of the cross member are adapted for attachment to a payload harness, wherein the payload harness is adapted for attachment to arms of the cross member, and wherein a payload may be secured within the payload harness.

    Abstract translation: 一种有效负载拖曳结构,其具有由轻质的柔性材料构成的拖盘,围绕所述拖盘的周边定位的管状部分,位于所述管状部分内的柔性构件,横向构件, 牵引盘,其中所述横向构件的一个或多个臂适于附接到有效载荷带,其中所述有效载荷束带适于附接到所述横梁的臂,并且其中有效载荷可固定在所述有效载荷束带内。

    Integrated wafer scale, high data rate, wireless repeater placed on fixed or mobile elevated platforms
    76.
    发明授权
    Integrated wafer scale, high data rate, wireless repeater placed on fixed or mobile elevated platforms 有权
    集成晶圆规模,高数据速率,无线中继器放置在固定或移动高架平台上

    公开(公告)号:US09119061B2

    公开(公告)日:2015-08-25

    申请号:US13722868

    申请日:2012-12-20

    Inventor: Farrokh Mohamadi

    Abstract: Methods and systems are provided for relocatable repeaters for wireless communication links to locations that may present accessibility problems using, for example, small unmanned aerial systems (sUAS). An sUAS implemented as an easy-to-operate, small vertical take-off and landing (VTOL) aircraft with hovering capability for holding station position may provide an extended range, highly secure, high data rate, repeater system for extending the range of point-to-point wireless communication links (also referred to as “crosslinks”) in which repeater locations are easily relocatable with very fast set-up and relocating times. A repeater system using beam forming and power combining techniques enables a very high gain antenna array with very narrow beam width and superb pointing accuracy. The aircraft includes a control system enabling three-dimensional pointing and sustaining directivity of the beam independently of flight path of the aircraft.

    Abstract translation: 为可重定位中继器提供方法和系统,用于到可能使用例如小型无人空中系统(sUAS)呈现可及性问题的位置的无线通信链路。 作为一种易于操作的小型垂直起降飞机(VTOL)飞机实现的sUAS可以提供​​扩展范围,高度安全,高数据速率的中继器系统,用于扩展点的范围 点对点无线通信链路(也称为“交叉”),其中中继器位置可以以非常快的建立和重定位时间容易地重新定位。 使用波束形成和功率组合技术的中继器系统能够实现非常高的增益天线阵列,其具有非常窄的波束宽度和极好的指向精度。 该飞机包括一个控制系统,能够独立于飞行器飞行路径的三维指向和维持梁的方向性。

    MOBILITY AND POWER MANAGEMENT FOR HIGH ALTITUDE PLATFORM (HAP) COMMUNICATION SYSTEMS
    77.
    发明申请
    MOBILITY AND POWER MANAGEMENT FOR HIGH ALTITUDE PLATFORM (HAP) COMMUNICATION SYSTEMS 审中-公开
    高性能平台(HAP)通信系统的移动性和功率管理

    公开(公告)号:US20150236781A1

    公开(公告)日:2015-08-20

    申请号:US14624320

    申请日:2015-02-17

    Applicant: Ahmad Jalali

    Inventor: Ahmad Jalali

    Abstract: A communication system is described. The system includes: at least one gateway able to provide broadband connectivity, a set of ground terminals, and a set of high altitude platforms (HAPs), where at least one aerial platform is able to communicate with at least one gateway using radio frequencies, each HAP is able to communicate with ground terminals using radio frequencies, and each HAP is able to communicate with each other HAP using radio frequencies. Ways to handoff a ground terminal/gateway from one HAP beam to another HAP beam are described. Ways to handoff a ground terminal/gateway from one HAP to another HAP are described. Ways that keep the communications payload radios active when there is data traffic and put the radios in sleep mode otherwise, thereby adjusting the communications payload power consumption to the data traffic requirements as a function of time and coverage area, are described.

    Abstract translation: 描述通信系统。 该系统包括:能够提供宽带连接的至少一个网关,一组接地终端和一组高空平台(HAP),其中至少一个空中平台能够使用无线电频率与至少一个网关通信, 每个HAP能够使用无线电频率与接地终端通信,并且每个HAP能够使用无线电频率彼此进行HAP通信。 描述了将接地终端/网关从一个HAP波束切换到另一HAP波束的方法。 描述了将接地终端/网关从一个HAP切换到另一个HAP的方法。 描述了当存在数据业务时保持通信有效载荷无线电活动的方式,并且将无线电设置为睡眠模式,否则将调整作为时间和覆盖区域的函数的数据业务需求的通信有效载荷功率消耗。

    UNMANNED AERIAL VEHICLE AND METHOD FOR LAUNCHING
    78.
    发明申请
    UNMANNED AERIAL VEHICLE AND METHOD FOR LAUNCHING 审中-公开
    无人驾驶的空中客车和起飞方法

    公开(公告)号:US20150183520A1

    公开(公告)日:2015-07-02

    申请号:US14416035

    申请日:2013-07-19

    Abstract: A method of launching a powered unmanned aerial vehicle, the method comprising lifting the vehicle by attachment to a lighter-than-air carrier from a substantially ground-level location to an elevated altitude, wherein the vehicle is prevented from entering its flight mode during ascent, causing the vehicle to detach from the carrier while the velocity of the vehicle relative to the carrier is substantially zero, the vehicle thereafter decreasing in altitude as it accelerates to a velocity where it is capable of preventing any further descent and can begin independent sustained flight.

    Abstract translation: 一种发射有功无人驾驶飞行器的方法,该方法包括通过从基本上地平面位置到高架高度附接到比轻空载体提升车辆,其中在上升期间车辆被阻止进入其飞行模式 ,当车辆相对于承运人的速度基本上为零时,导致车辆从载体上脱离,随后车辆随着其高度减小到能够防止任何进一步下降并能够开始独立持续飞行的速度 。

    Harvester with a sensor mounted on an aircraft
    79.
    发明授权
    Harvester with a sensor mounted on an aircraft 有权
    收割机安装在飞机上的传感器

    公开(公告)号:US08909389B2

    公开(公告)日:2014-12-09

    申请号:US13187696

    申请日:2011-07-21

    Abstract: A sensor for monitoring a plant population in front of a harvester and a transfer process of the crop from the harvester to a transport vehicle is arranged on an unmanned aircraft. The aircraft moves in the vicinity of the harvester in the harvesting mode and communicates in a wireless fashion with a control unit that controls an actuator for influencing an operating parameter of the harvester and/or the transport vehicle (in real time based on signals of the sensor in the harvesting mode.

    Abstract translation: 用于监测收割机前面的植物种群的传感器和从收割机到运输车辆的作物的转移过程被安排在无人驾驶飞机上。 飞机以收割模式在收割机附近移动,并以无线方式与控制单元进行通信,该控制单元控制用于影响收割机和/或运输车辆的操作参数的致动器(基于 传感器处于收获模式。

    High Altitude Aircraft, Aircraft Unit and Method for Operating an Aircraft Unit
    80.
    发明申请
    High Altitude Aircraft, Aircraft Unit and Method for Operating an Aircraft Unit 审中-公开
    高空飞机,飞机单元和操作飞机单元的方法

    公开(公告)号:US20140252156A1

    公开(公告)日:2014-09-11

    申请号:US14354030

    申请日:2012-10-20

    Abstract: A high-altitude unmanned stratosphere aerial vehicle includes a fuselage, wings, control surfaces, and a propulsion system including an engine and a propeller. Each wing has a plurality of hoses and wing spars extending in a direction perpendicularly to the longitudinal fuselage axis and are surrounded by a skin forming a wing covering that determines the cross-sectional contour of the wing, the cross-sectional contour forming a laminar flow airfoil that generates high lift when there is low flow resistance. At the free end facing away from the fuselage, each wing has a winglet extending transversely to the longitudinal wing axis. The winglet has a movable control surface, which allows an aerodynamic side force to be generated so as to bring the aerial vehicle to a banked position.

    Abstract translation: 高空无人空中平流层飞行器包括机身,机翼,控制面,以及包括发动机和推进器的推进系统。 每个翼具有沿垂直于纵向机身轴线的方向延伸的多个软管和翼梁,并且被形成机翼覆盖物的皮肤包围,所述机翼覆盖物确定机翼的横截面轮廓,横截面轮廓形成层流 当流动阻力低时产生高升力的翼型。 在远离机身的自由端处,每个翼具有横向于纵向翼轴线延伸的小翼。 小翼具有可移动的控制表面,其允许产生空气动力学侧力,以使空中飞行器处于堆积位置。

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