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    UNMANNED AERIAL VEHICLE
    93.
    发明公开
    UNMANNED AERIAL VEHICLE 审中-公开
    无人驾驶的航空机

    公开(公告)号：EP3219612A1

    公开(公告)日：2017-09-20

    申请号：EP17163476.9

    申请日：2013-07-19

    Applicant: Astigan Limited

    Inventor： Elson, Andrew Charles

    IPC: B64D5/00 ,  B64C39/02

    CPC classification number: B64D5/00 ,  B64B1/40 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/123 ,  B64C2201/162 ,  B64C2201/187 ,  B64D2211/00

    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: 启动动力无人驾驶飞行器的方法，所述方法包括通过附接提升车辆以从基本上地面水平位置比轻的空气载体至升高的高度，其中，所述车辆是从上升过程中进入其飞行模式防止 ，使车辆从载体分离，而相对于载体的车辆的速度基本为零时，车辆在高度之后减小，因为它加速到速度，其中它能够防止任何进一步下降，并且可以开始独立持续飞行 。

    MECHANICALLY STEERED AND HORIZONTALLY POLARIZED ANTENNA FOR AERIAL VEHICLES, AND ASSOCIATED SYSTEMS AND METHODS
    94.
    发明公开
    MECHANICALLY STEERED AND HORIZONTALLY POLARIZED ANTENNA FOR AERIAL VEHICLES, AND ASSOCIATED SYSTEMS AND METHODS 审中-公开
    机械导演和水平极化天线，用于飞机和相关系统和方法

    公开(公告)号：EP3120411A1

    公开(公告)日：2017-01-25

    申请号：EP15720819.0

    申请日：2015-03-18

    Applicant: Insitu, Inc.

    Inventor： MACK, Torsten ,  KUNZ, Peter

    IPC: H01Q1/28 ,  H01Q1/12 ,  H01Q3/04 ,  H01Q3/08 ,  H01Q19/30

    CPC classification number: H01Q3/02 ,  B64C2201/122 ,  H01Q1/1257 ,  H01Q1/28 ,  H01Q1/282 ,  H01Q1/40 ,  H01Q3/005 ,  H01Q3/04 ,  H01Q3/08 ,  H01Q19/30 ,  H04B7/18508

    Abstract: A mechanically steered, horizontally polarized, directional antennae for aerial vehicles, such as UAVs. The antenna system can include a planar substrate with a horizontally polarized antenna embedded therein. A rotation member, on one end, can be attached to the planar substrate, and can extend from an external surface of the aerial vehicle. An actuator can be coupled to the rotation member to rotate the rotation member. A communication controller of the aerial vehicle can control the actuator to beam horizontally polarized radiofrequency (RF) waves to a target receiver or receive a wave front from a target transmitter.

    Abstract translation: 机械控制，水平极化，定向天线用于飞行器：如无人机。 该天线系统可以包括具有嵌入其中一个水平极化天线的平面基片。 在一个端部的旋转构件，可附接至所述平面基底，并且可以从在飞行器的外部表面延伸。 的致动器可以联接到所述旋转构件，以旋转所述旋转构件。 飞行器的通信控制器能够控制所述致动器光束水平极化的射频（RF）波至目标接收器或从目标发射器接收的波前。

    MODULAR DRONE AND METHODS FOR USE
    96.
    发明公开
    MODULAR DRONE AND METHODS FOR USE 审中-公开
    模块无声和使用方法

    公开(公告)号：EP2972628A1

    公开(公告)日：2016-01-20

    申请号：EP14807197.0

    申请日：2014-03-13

    Applicant: Azure Sky Group LLC

    Inventor： JONES, Adam ,  VALIN, Jason Van ,  KOMLA, Paul K. ,  LUTHER, Andrew

    IPC: G05D1/02

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/122 ,  B64C2201/141 ,  G05D1/0088 ,  G05D1/102 ,  G06Q30/0261 ,  G06Q30/0267 ,  H04B7/18504

    Abstract: Various exemplary embodiments relate to a drone. The drone may include: a navigation unit configured to determine the location of the drone and navigate the drone to designated locations; a radio frequency identification (RFID) reader configured to read RFID tag information from RFID tags; and a wireless network transceiver configured to periodically transmit the location of the drone and RFID tag information to an inventory management system. Various exemplary embodiments relate to a method performed by a drone. The method may include: receiving navigation path information; navigating the drone along the navigation path based on satellite location signals; determining current position information based on the satellite location signals; reading RFID tag information from a first RFID tag; and transmitting the RFID tag information and the current position information via a wireless client to a central computing system.

    Abstract translation: 各种示例性实施例涉及无人机。 无人机可以包括：导航单元，其被配置为确定无人机的位置并且将无人机导航到指定位置; 射频识别（RFID）读取器，被配置为从RFID标签读取RFID标签信息; 以及无线网络收发器，被配置为周期性地将无人机的位置和RFID标签信息传输到库存管理系统。 各种示例性实施例涉及由无人机执行的方法。 该方法可以包括：接收导航路径信息; 基于卫星位置信号沿着导航路径导航无人机; 基于卫星位置信号确定当前位置信息; 从第一RFID标签读取RFID标签信息; 以及经由无线客户端将RFID标签信息和当前位置信息发送到中央计算系统。

    UNMANNED AERIAL VEHICLE AND METHOD OF LAUNCHING
    97.
    发明公开
    UNMANNED AERIAL VEHICLE AND METHOD OF LAUNCHING 有权
    UNBEMANNTES LUFTFAHRZEUG UND ABSCHUSSVERFAHRENDAFÜR

    公开(公告)号：EP2874875A1

    公开(公告)日：2015-05-27

    申请号：EP13742690.4

    申请日：2013-07-19

    Applicant: Elson, Andrew Charles

    Inventor： Elson, Andrew Charles

    IPC: B64D5/00 ,  B64C39/02

    CPC classification number: B64D5/00 ,  B64B1/40 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/123 ,  B64C2201/162 ,  B64C2201/187 ,  B64D2211/00

    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: 一种在至少13000米的高度上发射供电的无人驾驶飞行器的方法，所述方法包括通过将空载承载器从基本上地平面的位置附近提升到升高的高度，使得车辆 当车辆相对于承运人的速度基本上为零时，车辆离开载体，然后车辆随着其高度减小到能够防止任何进一步下降并且可以开始独立的持续飞行的速度。

    AIRSHIP AND METHOD OF OPERATION
    99.
    发明授权
    AIRSHIP AND METHOD OF OPERATION 有权
    飞艇工作程序

    公开(公告)号：EP1519873B1

    公开(公告)日：2007-10-24

    申请号：EP03737791.8

    申请日：2003-06-25

    Applicant: 21st Century Airships Inc.

    Inventor： COLTING, Hokan

    IPC: B64B1/00

    CPC classification number: B64B1/34 ,  B64B1/02 ,  B64B1/32 ,  B64C21/02 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  Y02T50/166

    Abstract: An airship (20) has a generally spherical shape and has an internal envelope (24) for containing a lifting gas such as Helium or Hydrogen. The airship has a propulsion and control system (36, 38) that permits it to be flown to a desired loitering location, and to be maintained in that location for a period of time. In one embodiment the airship may achieve neutral buoyancy when the internal envelope is as little as 7 % full of lifting gas, and may have a service ceiling of about 60,000 ft. The airship has an equipment module (180) that can include either communications equipment, or monitoring equipment, or both. The airship can be remotely controlled from a ground station. The airship has a solar cell array and electric motors (44, 46) of the propulsion and control system are driven by power obtained from the array. The airship also has an auxiliary power unit (52) that can be used to drive the electric motors. The airship can have a pusher propeller that assists in driving the airship and also moves the point of flow separation of the spherical airship further aft. In one embodiment the airship can be refuelled at altitude to permit extended loitering.

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