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    TRANSPORTABLE GROUND STATION FOR AN UNMANNED AERIAL VEHICLE
    381.
    发明公开
    TRANSPORTABLE GROUND STATION FOR AN UNMANNED AERIAL VEHICLE 审中-公开
    无人驾驶飞机的可移动地面站

    公开(公告)号：EP3201088A1

    公开(公告)日：2017-08-09

    申请号：EP15847916.2

    申请日：2015-09-24

    Applicant: Swift Engineering, Inc.

    Inventor： STREETT, Andrew

    IPC: B64C39/02 ,  B64D41/00

    CPC classification number: B60L11/182 ,  B64C39/024 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/201 ,  B64C2201/205 ,  B64F1/222 ,  G05D1/0011 ,  G05D1/0088 ,  H02J7/35

    Abstract: A transportable ground station for a UAV includes a container in which the UAV may be transported and housed. The container includes a wireless or contact-based recharging station that recharges the UAV's batteries or other power sources after the UAV returns from a mission. The recharging station may be directly or indirectly connected to one or more solar panels that generate energy to power the recharging station. The ground station may be deployed virtually anywhere, from any vehicle (e.g., plane, train, boat, truck, etc.), and may operate over an extended period of time without human intervention.

    Abstract translation: 用于无人飞行器的可移动地面站包括其中可以运输和容纳无人飞行器的容器。 该集装箱包括无线或基于接触的充电站，在无人机返回任务后，该无线充电站可为无人机的电池或其他电源充电。 再充电站可以直接或间接地连接到一个或多个太阳能电池板，这些太阳能电池板产生能量以给再充电站供电。 地面站几乎可以从任何车辆（例如飞机，火车，船，卡车等）的任何地方部署，并且可以在延长的时间段内运行而无需人工干预。

    UNMANNED AERIAL VEHICLE COMMUNICATION, MONITORING, AND TRAFFIC MANAGEMENT
    383.
    发明公开
    UNMANNED AERIAL VEHICLE COMMUNICATION, MONITORING, AND TRAFFIC MANAGEMENT 审中-公开
    无人机空中交通，监控和交通管理

    公开(公告)号：EP3170055A2

    公开(公告)日：2017-05-24

    申请号：EP15822865.0

    申请日：2015-07-08

    Applicant: Jarrell, John A.

    Inventor： Jarrell, John A.

    IPC: G05D1/00

    CPC classification number: G08G5/0013 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/066 ,  B64C2201/141 ,  B64C2201/146 ,  B64D47/06 ,  B64F1/362 ,  G06Q30/04 ,  G06Q50/30 ,  G08G5/003 ,  G08G5/0069 ,  G08G5/0091

    Abstract: A computer-implemented method of communicating with an unmanned aerial vehicle includes transmitting a first message via a communications transmitter of a lighting assembly for receipt by an unmanned aerial vehicle. The first message includes an identifier associated with the lighting assembly, and the lighting assembly is located within a proximity of a roadway. The method also includes receiving a second message from the unmanned aerial vehicle via a communications receiver of the lighting assembly. The second message includes an identifier associated with the unmanned aerial vehicle. The method further includes transmitting a third message via the communications transmitter of the lighting assembly for receipt by the unmanned aerial vehicle. The third message includes an indication of an altitude at which the unmanned aerial vehicle should fly.

    Abstract translation: 一种与无人驾驶飞行器通信的计算机实现的方法包括经由照明组件的通信发射器发送第一消息以供无人飞行器接收。 第一消息包括与照明组件相关联的标识符，并且照明组件位于道路附近。 该方法还包括经由照明组件的通信接收器从无人驾驶飞行器接收第二消息。 第二消息包括与无人驾驶飞行器相关联的标识符。 该方法进一步包括经由照明组件的通信发射器发送第三消息以由无人驾驶飞行器接收。 第三条消息包括无人驾驶飞行器应该飞行的高度的指示。

    UNMANNED HELICOPTER
    385.
    发明公开
    UNMANNED HELICOPTER 审中-公开
    UNBEMANNTER HUBSCHRAUBER

    公开(公告)号：EP3147210A2

    公开(公告)日：2017-03-29

    申请号：EP16190742.3

    申请日：2016-09-27

    Applicant: Ewatt Technology Co., Ltd.

    Inventor： ZHAO, Guocheng ,  LUO, Wei ,  QI, Pengcheng

    IPC: B64C27/04 ,  B64C27/82 ,  B64C39/02 ,  B64D33/02 ,  B64D33/04 ,  B64D33/08

    CPC classification number: B64D33/02 ,  B64C27/82 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/044 ,  B64C2201/141 ,  B64C2201/146 ,  B64D27/08 ,  B64D33/06 ,  B64D33/08 ,  B64D2033/0246 ,  B64D2033/028

    Abstract: The present invention discloses an unmanned helicopter, and belongs to the technical field of unmanned aerial vehicles. The unmanned helicopter includes an air inlet system, an exhaust system, a cooling system and a dynamic balance system. The air inlet system is fixed on a second side; the exhaust system is fixed on a third side; and the cooling system is fixed on a first side, and the dynamic balance system is fixed on a tail. The airflow at the outside of the unmanned helicopter flows into the air inlet system smoothly, quickly and efficiently under the action of its own flow velocity relative to the unmanned helicopter, therefore the technical problem in the prior art that the air entering the fuselage with a unit volume is burnt insufficiently, which generates adverse effects on the normal flight of the unmanned helicopter, is solved.

    Abstract translation: 本发明公开了一种无人直升机，属于无人驾驶飞行器技术领域。 无人直升机包括进气系统，排气系统，冷却系统和动平衡系统。 进气系统固定在第二侧; 排气系统固定在第三侧; 冷却系统固定在第一侧，动平衡系统固定在尾部。 无人直升机外部的气流在相对于无人驾驶直升机的自身流速的作用下，平稳，快速而有效地流入，因此现有技术中的技术问题是空气进入机身的空气 单位体积燃烧不足，对无人直升机的正常飞行产生不利影响，得到解决。

    MECHANISMS FOR LOWERING A PAYLOAD TO THE GROUND FROM A UAV
    387.
    发明公开
    MECHANISMS FOR LOWERING A PAYLOAD TO THE GROUND FROM A UAV 有权
    机制以降低PAYLOAD从UAV在地面上

    公开(公告)号：EP3038914A4

    公开(公告)日：2017-03-08

    申请号：EP14863900

    申请日：2014-08-25

    Applicant: X DEV LLC

    Inventor： PATRICK WILLIAM GRAHAM ,  BURGESS JAMES RYAN ,  CONRAD ANDREW

    IPC: B64C39/02 ,  B64D1/02 ,  B64D1/12 ,  B64D1/22 ,  B64D47/00

    CPC classification number: B64D1/12 ,  B64C39/024 ,  B64C2201/128 ,  B64C2201/141 ,  B64C2201/145 ,  B64D1/22

    Abstract: Embodiments described herein may help to provide medical support via a fleet of unmanned aerial vehicles (UAVs). An illustrative UAV may include a housing, a payload, a line-deployment mechanism coupled to the housing and a line, and a payload-release mechanism that couples the line to the payload, wherein the payload-release mechanism is configured to release the payload from the line. The UAV may further include a control system configured to determine that the UAV is located at or near a delivery location and responsively: operate the line-deployment mechanism according to a variable deployment-rate profile to lower the payload to or near to the ground, determine that the payload is touching or is within a threshold distance from the ground, and responsively operate the payload-release mechanism to release the payload from the line.

    METHOD AND DEVICE FOR TRACKING A MOVING TARGET FROM AN AIR VEHICLE
    389.
    发明公开
    METHOD AND DEVICE FOR TRACKING A MOVING TARGET FROM AN AIR VEHICLE 有权
    的移动目标监控装置与飞机法

    公开(公告)号：EP3128386A1

    公开(公告)日：2017-02-08

    申请号：EP15382414.9

    申请日：2015-08-04

    Applicant: The Boeing Company

    Inventor： QUEREJETA MASAVEU, Carlos ,  NAVARRO FELIX, Francisco A. ,  VALLS HERNANDEZ, Ernesto ,  HAYES, Andrew

    IPC: G05D1/00 ,  G05D1/10 ,  G05D1/12

    CPC classification number: G05D1/12 ,  B64C39/024 ,  B64C2201/127 ,  B64C2201/141 ,  G05D1/0094 ,  G05D1/101 ,  G08G5/006 ,  G08G5/0069

    Abstract: A method of tracking a moving target from an air vehicle comprising determining an estimated location and speed of a moving target and instructing an air vehicle to follow the moving target, wherein the method further comprises: a) determining a detectability zone surrounding the moving target; b) calculating at least one reference location for the air vehicle; c) generating at least one guidance reference to command the air vehicle for tracking the moving target, wherein the guidance reference comprises any combination of one or more of at least: c.1) a desired course; c.2) a desired speed; c.3) a desired flying altitude; and wherein the method further comprises: d) instructing the air vehicle to fly according to the generated guidance reference; wherein the determination of the detectability zone, the calculation of a reference location and the generation of the guidance reference are performed according to at least one behavior policy.

    Abstract translation: 在空气车辆从跟踪运动目标包括在估计的位置和运动目标的速度确定性采矿和指示对空气车辆跟随移动的目标，worin该方法还包括以下方法：1）确定的采矿周围移动目标一个探测区; b）计算用于所述飞行器的至少一个参考位置; c）产生至少一个参考指导以命令飞行器用于跟踪移动目标，worin指导参考包括一种或多种至少的任何组合：C.1）一个期望路线; C.2）的期望速度; C.3）一个希望的飞行高度; 并且该方法worin还包括：D）指示所述飞行器飞gemäß到所生成的参考指导; worin可检测区的确定，一个参考位置的计算和参考指导的生成被执行gemäß到至少一个行为的策略。

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