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    SYSTEM AND A METHOD FOR FACILITATING TESTING OF PLURALITY OF DEVICES USING A DRONE
    84.
    发明申请
    SYSTEM AND A METHOD FOR FACILITATING TESTING OF PLURALITY OF DEVICES USING A DRONE 有权
    系统和方法，用于利用刮刀来提高设备的多样性测试

    公开(公告)号：US20160350593A1

    公开(公告)日：2016-12-01

    申请号：US14830987

    申请日：2015-08-20

    Applicant: HCL Technologies Ltd.

    Inventor： Siva Sakthivel SADASIVAM ,  Murali Krishnaan G ,  Vishal CHAUDHARY

    IPC: G06K9/00 ,  B64C39/02

    CPC classification number: G06K9/00536 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/066 ,  B64C2201/123 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/148 ,  G06K9/627 ,  G06K2209/19

    Abstract: Disclosed is a system and method for facilitating testing of a plurality of devices using a drone. At first, a locating module locates position of the drone relative to the plurality of devices. Further, a receiving module receives an image, of a device of the plurality of devices, from image capturing unit of the drone. Then, a comparing module compares the image with a reference image corresponding to the device. Based on the comparison, a determining module determines an action to be performed for testing the device. Further, a facilitating module facilitates the testing by enabling a snout associated with the drone to perform the action on the device.

    Abstract translation: 公开了一种用于促进使用无人机测试多个设备的系统和方法。 首先，定位模块相对于多个装置定位无人机的位置。 此外，接收模块从无人机的图像捕获单元接收多个设备中的设备的图像。 然后，比较模块将图像与对应于该装置的参考图像进行比较。 基于比较，确定模块确定要对设备进行测试的动作。 此外，便利模块通过启用与无人机相关联的管口来执行在该设备上的动作来促进测试。

    TETHERED UNMANNED AERIAL VEHICLE-BASED SYSTEMS AND METHODS ASSOCIATED WITH CELL SITES AND CELL TOWERS
    85.
    发明申请
    TETHERED UNMANNED AERIAL VEHICLE-BASED SYSTEMS AND METHODS ASSOCIATED WITH CELL SITES AND CELL TOWERS 有权
    与基于网络和细胞功能相关的基于无人机的基于车辆的系统和方法

    公开(公告)号：US20160309341A1

    公开(公告)日：2016-10-20

    申请号：US14736925

    申请日：2015-06-11

    Applicant: Lee PRIEST ,  Charlie TERRY ,  Ross ERICKSON

    Inventor： Lee PRIEST ,  Charlie TERRY ,  Ross ERICKSON

    IPC: H04W24/02 ,  B64D47/08 ,  G05D1/00 ,  G05D1/10 ,  B64C39/02 ,  B64C27/06

    CPC classification number: B64D47/08 ,  B64C27/06 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/148 ,  B64C2201/201 ,  G05D1/0094 ,  G05D1/0866

    Abstract: A method with a tethered Unmanned Aerial Vehicle (UAV) associated with a cell site includes causing the UAV to fly at or near the cell site while the UAV is tethered at or near the cell site via a connection, wherein flight of the UAV at or near the cell site is constrained based on the connection; and performing one or more functions via the UAV at the cell site while the UAV is flying tethered at or near the cell site. The one or more functions can include functions related to a cell site audit. Alternatively, the one or more functions include functions related to providing wireless service via the UAV at the cell site, wherein data and/or power is transferred between the UAV and the cell site to perform the wireless service.

    Abstract translation: 具有与细胞位点相关联的系留无人机（UAV）的方法包括使无人机在小区站点附近飞行，而无人机通过连接系泊在小区站点附近，其中UAV在 基站连接附近受限; 并且在无人机在小区站点处或附近飞行的情况下通过无人机在小区站点执行一个或多个功能。 一个或多个功能可以包括与小区站点审核相关的功能。 或者，一个或多个功能包括与通过小区站点处的UAV提供无线服务相关的功能，其中在UAV和小区站点之间传送数据和/或功率以执行无线服务。

    Apparatus and methods for tethered aerial platform and system
    86.
    发明授权
    Apparatus and methods for tethered aerial platform and system 有权
    拴系空中平台和系统的装置和方法

    公开(公告)号：US09446858B2

    公开(公告)日：2016-09-20

    申请号：US14858467

    申请日：2015-09-18

    Applicant: Kevin Hess

    Inventor： Kevin Hess

    IPC: B64F3/02 ,  B64C39/02 ,  G08G5/00

    CPC classification number: B64F3/02 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/127 ,  B64C2201/148 ,  G08G5/0013

    Abstract: A drone system includes a drone that includes a propulsion system, a flight stabilizer system, and an air payload interface unit, and a camera system, wherein the camera system includes a camera stabilizing unit, and a ground support system to which the drone is detachably coupled through a tether unit, and for providing electrical power to the propulsion system. The drone system further includes a ground payload interface unit for receiving and transmitting command and telemetry information to the air payload interface unit through the tether unit, and a controlling device for controlling the propulsion system and the camera system through the tether unit.

    Abstract translation: 无人机系统包括无人机，其包括推进系统，飞行稳定器系统和空气有效载荷接口单元，以及照相机系统，其中所述照相机系统包括照相机稳定单元以及无人机可拆卸的地面支撑系统 通过系绳单元联接，并用于向推进系统提供电力。 无人机系统还包括接地有效载荷接口单元，用于通过系绳单元接收和发送命令和遥测信息给空载有效载荷接口单元，以及控制装置，用于通过系绳单元控制推进系统和照相机系统。

    Systems and apparatus for tether termination mount for tethered aerial vehicles
    87.
    发明授权
    Systems and apparatus for tether termination mount for tethered aerial vehicles 有权
    用于拴系航空器的系绳终端安装系统和装置

    公开(公告)号：US09216824B2

    公开(公告)日：2015-12-22

    申请号：US14620194

    申请日：2015-02-12

    Applicant: Google Inc.

    Inventor： Brian Hachtmann ,  Corwin Hardham ,  Damon Vander Lind ,  Rob Nelson

    IPC: A63H27/08 ,  B64C39/02 ,  B64F3/02 ,  H01R39/64 ,  B64F3/00 ,  F03D11/04 ,  F03D5/00

    CPC classification number: B64C39/022 ,  B64C2201/021 ,  B64C2201/148 ,  B64F3/00 ,  B64F3/02 ,  F03D5/00 ,  F05B2240/917 ,  F05B2240/921 ,  F05B2240/923 ,  H01R39/64 ,  Y02E10/70 ,  Y02E10/728

    Abstract: Wind energy systems, such as an Airborne Wind Turbine (“AWT”), may be used to facilitate conversion of kinetic energy to electrical energy. An AWT may include an aerial vehicle that flies in a path to convert kinetic wind energy to electrical energy. The aerial vehicle may be tethered to a ground station with a tether that terminates at a tether termination mount. In one aspect, the tether may be a conductive tether that can transmit electricity and/or electrical signals back and forth between the aerial vehicle and the ground station. The tether termination mount may include one or more gimbals that allow for the tether termination mount to rotate about one or more axis. In a further aspect, the tether termination mount may include a slip ring that allows for rotation of the tether without twisting the tether.

    Abstract translation: 诸如空降风力发电机（“AWT”）等风能系统可用于促进将动能转换为电能。 AWT可以包括在将动能风能转换成电能的路径中飞行的空中飞行器。 航空器可以用连接臂终止于系绳终端安装座的拴系到地面站。 在一个方面，系绳可以是可以在飞行器和地面站之间来回传递电和/或电信号的导电系绳。 系绳终端安装件可以包括一个或多个允许系绳终端安装件围绕一个或多个轴线旋转的万向节。 在另一方面，系绳终端安装件可以包括滑环，其允许系绳的旋转而不扭转系绳。

    Methods and systems for transitioning an aerial vehicle between crosswind flight and hover flight
    89.
    发明授权
    Methods and systems for transitioning an aerial vehicle between crosswind flight and hover flight 有权
    在侧风飞行和悬停飞行之间过渡飞行器的方法和系统

    公开(公告)号：US09126675B2

    公开(公告)日：2015-09-08

    申请号：US14144545

    申请日：2013-12-30

    Applicant: Google Inc.

    Inventor： Erik Christopher Chubb ,  Damon Vander Lind

    IPC: B64C39/02 ,  F03D5/00 ,  B64C13/00 ,  G05D1/10

    CPC classification number: B64C39/022 ,  B64C2201/021 ,  B64C2201/12 ,  B64C2201/148 ,  F03D5/00 ,  F03D9/25 ,  F03D13/20 ,  F05B2240/921 ,  G05D1/0866 ,  Y02E10/70 ,  Y02E10/728

    Abstract: A method involves operating an aerial vehicle in a hover-flight orientation. The aerial vehicle is connected to a tether that defines a tether sphere having a radius based on a length of the tether, and the tether is connected to a ground station. The method involves positioning the aerial vehicle at a first location that is substantially on the tether sphere. The method involves transitioning the aerial vehicle from the hover-flight orientation to a forward-flight orientation, such that the aerial vehicle moves from the tether sphere. And the method involves operating the aerial vehicle in the forward-flight orientation to ascend at an angle of ascent to a second location that is substantially on the tether sphere. The first and second locations are substantially downwind of the ground station.

    Abstract translation: 一种方法涉及以悬停飞行方向操作飞行器。 航空器连接到一个系绳，该系绳限定了基于系绳长度的半径的系绳球，并且系绳连接到地面站。 该方法包括将飞行器定位在基本上在系绳球上的第一位置。 该方法包括将空中飞行器从悬停飞行方向转换到前向飞行方向，使得飞行器从系绳球移动。 并且该方法涉及以前向飞行方向操作飞行器，以升高的角度升高到基本上处于系绳球上的第二位置。 第一和第二位置基本上是地面站的顺风向。

    Methods and Systems for Transitioning an Aerial Vehicle Between Crosswind Flight and Hover Flight
    90.
    发明申请
    Methods and Systems for Transitioning an Aerial Vehicle Between Crosswind Flight and Hover Flight 有权
    在侧风飞行和悬停飞行之间转换航空器的方法和系统

    公开(公告)号：US20150183512A1

    公开(公告)日：2015-07-02

    申请号：US14144146

    申请日：2013-12-30

    Applicant: Google Inc.

    Inventor： Kenneth Jensen ,  Erik Christopher Chubb ,  Damon Vander Lind

    IPC: B64C19/00

    CPC classification number: B64C39/022 ,  B64C2201/021 ,  B64C2201/148 ,  F03D5/00 ,  F03D5/06 ,  F05B2240/921 ,  G05D1/0866 ,  G05D1/101 ,  Y02E10/70 ,  Y02E10/725

    Abstract: A method may involve operating an aerial vehicle to travel along a first closed path on a tether sphere while oriented in a crosswind-flight orientation. A tether may be connected to the aerial vehicle on a first end and may be connected to a ground station on a second end. Further, the tether sphere may have a radius corresponding to a length of the tether. The method may further involve while the aerial vehicle is in the crosswind-flight orientation, operating the aerial vehicle to travel along a second closed path on the tether sphere, such that a speed of the aerial vehicle is reduced. And the method may involve after or while the speed of the aerial vehicle is reduced, transitioning the aerial vehicle from traveling along the second closed path while in the crosswind-flight orientation to a hover-flight orientation.

    Abstract translation: 一种方法可以包括操作空中飞行器，以沿着侧风飞行方向定向，沿着系绳球体上的第一封闭路径行进。 系绳可以在第一端连接到飞行器，并且可以在第二端连接到地面站。 此外，系绳球可以具有对应于系链的长度的半径。 该方法还可以包括在空中飞行器处于侧风飞行方向的同时，操作飞行器沿着系绳球上的第二闭合路径行进，使得飞行器的速度降低。 并且该方法可能涉及在降低航空器的速度之后或同时降低航空器的速度，从而使空中飞行器沿着侧风飞行方向沿着第二闭合路径行驶到悬停飞行方位。

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