公开(公告)号：EP3057857A1

公开(公告)日：2016-08-24

申请号：EP14854105.5

申请日：2014-10-15

Applicant: ELWHA, LLC

Inventor： HYDE, Roderick A. ,  WOOD, Lowell L., Jr. ,  DUNCAN, William David ,  KARE, Jordin T. ,  MALASKA, Stephen L. ,  MYHRVOLD, Nathan P. ,  PETROSKI, Robert C. ,  WEAVER, Thomas Allan

IPC: B62D63/02 ,  B62D63/04 ,  B64F3/02 ,  B64D39/00

CPC classification number: B64C39/024 ,  B64C39/022 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/046 ,  B64C2201/063 ,  B64C2201/066 ,  B64C2201/12 ,  B64C2201/127 ,  B64C2201/145 ,  B64C2201/146 ,  B64C2201/208 ,  B64F1/00 ,  G05D1/0094

Abstract: A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such that the vehicle can provide at least one of fuel and electrical energy to the aircraft while the aircraft is supported on the aircraft landing portion.

Abstract translation: 机动车辆系统包括包括飞行器着陆部分的机动车辆和被配置为被支撑在飞行器着陆部分上的主动推进无人飞行器。 车辆和飞行器构造成使得当飞机被支撑在飞行器着陆部分上时，车辆可以向飞机提供燃料和电能中的至少一种。

公开(公告)号：EP2976687A1

公开(公告)日：2016-01-27

申请号：EP14885848.3

申请日：2014-05-30

Applicant: SZ DJI Technology Co., Ltd.

Inventor： WANG, Ming yu

IPC: G05B19/418

CPC classification number: B64F1/222 ,  B60L11/1846 ,  B60R9/00 ,  B64C39/024 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/18 ,  B64C2201/208 ,  B64F1/00 ,  B64F1/007 ,  B64F1/22 ,  G05D1/0684

Abstract: An unmanned aerial vehicle (UAV) housing apparatus comprising a mounting component configured to attach to a vehicle; a landing connection component configured to form a connection with the UAV that prevents detachment of the UAV and the UAV housing apparatus; and a cover 730 configured to at least partially enclose the UAV when the UAV is connected to the landing connection component.

Abstract translation: 提供系统和方法用于将无人驾驶飞行器（UAV）与车辆对接。 无人机可能能够区分同伴车辆与该地区的其他车辆，反之亦然。 无人机可以起飞和/或着陆在车辆上。 无人机可以用于捕获图像并将图像流直接传输到车辆内的显示器。 车辆可以控制无人机。 无人机在飞行中可能与伴侣车辆通信。

公开(公告)号：EP2963519A1

公开(公告)日：2016-01-06

申请号：EP14382252.6

申请日：2014-07-01

Applicant: The Boeing Company

Inventor： Esteban Campillo, David ,  Casado Magaña, Enrique Juan ,  Scarlatti, David ,  Maza Alcañiz, Ivan ,  Caballero Benitez, Fernando ,  Ragel de la Torre, Ricardo

IPC: G05D1/10

CPC classification number: B64F1/007 ,  B64C39/024 ,  B64C2201/208 ,  B64F1/10 ,  G05D1/0011 ,  G05D1/104

Abstract: A mobile unmanned aerial vehicle (UAV) infrastructure and management system, and related methods to facilitate operation of one or more unmanned aerial vehicles (UAVs) in one or more areas is disclosed.

Abstract translation: 移动无人驾驶飞行器（UAV）的基础设施和管理系统，以及相关的方法，在一个或多个区域促进一个或多个无人驾驶飞行器（UAV）的手术游离缺失盘。

公开(公告)号：EP2665651A1

公开(公告)日：2013-11-27

申请号：EP11856460.8

申请日：2011-12-30

Applicant: Information Systems Laboratories, Inc.

Inventor： VAN STAAGEN, Peter, K. ,  MCDANIEL, William, Douglas ,  BOSCHMA, James, H., Jr.

IPC: B64F3/00

CPC classification number: B64B1/50 ,  B64B1/58 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/123 ,  B64C2201/201 ,  B64C2201/208 ,  B64F1/14

Abstract: A system and method for deploying a payload with an aerostat uses a mobile transporter for moving the system to a deployment site. Structurally, the system includes a base unit with a rotation head mounted thereon. An envelope container for holding a deflated aerostat is mounted on the rotation head and a rotation of the container on the rotation head positions the aerostat for optimal compliance with the existing wind condition. Also included in the system is an inflator that is mounted on the base unit to inflate the aerostat with a Helium gas. And, the system includes a tether control unit for maintaining a connection with the aerostat during its deployment, in-flight use, and recovery. Preferably, a deployment computer is used for a coordinated control of the rotation head, inflator and tether.

公开(公告)号：WO2017079587A1

公开(公告)日：2017-05-11

申请号：PCT/US2016/060569

申请日：2016-11-04

Applicant: WAL-MART STORES, INC.

Inventor： HIGH, Donald R. ,  THOMPSON, John P. ,  ATCHLEY, Michael D. ,  NATARAJAN, Chandrashekar

IPC: G06Q10/08

CPC classification number: G06Q10/0833 ,  B64B1/40 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/141 ,  B64C2201/208 ,  B64F1/007

Abstract: A control circuit dispatches towards a delivery zone a terrestrial vehicle that carries at least one airborne drone and at least one item to be delivered to a customer. When the terrestrial vehicle is in the delivery zone, the drone is dispatched to carry the item to the customer. By one approach the drone exits the terrestrial vehicle without bearing the item. The item can be automatically moved from within the terrestrial vehicle to a position such that the item is at least partially exposed external to the terrestrial vehicle. The airborne drone, subsequent to exiting the terrestrial vehicle, can engage the item in order to then deliver that item to the customer. By one approach the terrestrial vehicle includes one or more platforms that support one or more airborne drones and that can be moved from within the terrestrial vehicle to a deployed position external to the terrestrial vehicle.

Abstract translation: 控制电路向运送区域发送携带至少一个空中无人机和至少一个要递送给顾客的物品的陆地车辆。 当陆地车辆处于交付区域时，无人驾驶飞机被派往将该物品运送给客户。 通过一种方法，无人驾驶飞机离开地面车辆而不承载物品。 物品可以从地面车辆内自动移动到这样的位置，使得物品至少部分暴露在陆地车辆外部。 空中无人机在离开陆地车辆后可以接合该物品，然后将该物品交付给客户。 通过一种方法，陆地交通工具包括一个或多个支撑一个或多个空中无人驾驶飞机的平台，并且该平台可以从陆地交通工具内移动到陆地交通工具外部的展开位置。

公开(公告)号：WO2017040493A1

公开(公告)日：2017-03-09

申请号：PCT/US2016/049429

申请日：2016-08-30

Applicant: UNIVERSITY OF MARYLAND, COLLEGE PARK

Inventor： VALENTE, Evandro Gurgel do Amaral ,  WERELEY, Norman, M. ,  VALENTE, Eduardo Gurgel do, Amaral

IPC: B64C3/14 ,  B64C29/00

CPC classification number: B64C39/10 ,  B64C15/12 ,  B64C29/0033 ,  B64C37/00 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/088 ,  B64C2201/208 ,  B64C2211/00

Abstract: The universal vehicle system is designed with a lifting body which is composed of a plurality of interconnected modules which are configured to form an aerodynamically viable contour of the lifting body which including a front central module, a rear module, and thrust vectoring modules displaceably connected to the front central module and operatively coupled to respective propulsive mechanisms. The thrust vectoring modules are controlled for dynamical displacement relative to the lifting body (in tilting and/or translating fashion) to direct and actuate the propulsive mechanism(s) as needed for safe and stable operation in various modes of operation and transitioning therebetween in air, water and terrain environments.

Abstract translation: 通用车辆系统设计有提升体，其由多个相互连接的模块组成，所述多个互连模块被构造成形成提升体的空气动力学上可行的轮廓，其包括前部中央模块，后部模块和可移动地连接到 前中央模块并且可操作地耦合到相应的推进机构。 控制推力矢量模块以相对于提升体（以倾斜和/或平移方式）进行动态位移，以根据需要引导并致动推进机构，以便在空气中的各种运行模式和过渡之间进行安全和稳定的操作 ，水和地形环境。

公开(公告)号：WO2016205415A1

公开(公告)日：2016-12-22

申请号：PCT/US2016/037694

申请日：2016-06-15

Applicant: IMAGEKEEPER LLC

Inventor： SPEASL, Jerry ,  PATTERSON, Mike ,  ROBERTS, Mark

IPC: B65F9/00 ,  G01C23/00 ,  B65G67/00

CPC classification number: G08G5/0034 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/08 ,  B64C2201/082 ,  B64C2201/121 ,  B64C2201/126 ,  B64C2201/128 ,  B64C2201/145 ,  B64C2201/20 ,  B64C2201/201 ,  B64C2201/205 ,  B64C2201/206 ,  B64C2201/208 ,  B64F1/222 ,  G06Q10/08 ,  G08G5/0069 ,  G08G5/0082 ,  G08G5/0091

Abstract: A base module may be used to receive and house one or more unmanned aerial vehicles (UAVs) via one or more cavities. The base module receives commands from a manager device and identifies a flight plan that allows a UAV to execute the received commands. The base module transfers the flight plan to the UAV and frees the UAV. Once the UAV returns, the base module once again receives it. The base module then receives sensor data from the UAV from one or more sensors onboard the UAV, and optionally receives additional information describing its flight and identifying success or failure of the flight plan. The base module transmits the sensor data and optionally the additional information to a storage medium locally or remotely accessible by the manager device.

Abstract translation: 基座模块可以用于经由一个或多个空腔接收和容纳一个或多个无人机（UAV）。 基本模块从管理器设备接收命令，并识别允许UAV执行接收到的命令的飞行计划。 基地模块将飞行计划转移到无人机，并释放无人机。 一旦UAV返回，基本模块再次接收它。 然后，基本模块从UAV上的一个或多个传感器接收来自UAV的传感器数据，并且可选地接收描述其飞行并识别飞行计划的成功或失败的附加信息。 基本模块将传感器数据和可选的附加信息传输到本地或由管理器设备远程访问的存储介质。

公开(公告)号：WO2016148368A1

公开(公告)日：2016-09-22

申请号：PCT/KR2015/011438

申请日：2015-10-28

Applicant: LG ELECTRONICS INC.

Inventor： CHO, Taehoon ,  SHIN, Choonghwan

IPC: B64F1/00 ,  B64C39/02 ,  B64D47/08

CPC classification number: B64C39/024 ,  B60Q1/52 ,  B60Q7/00 ,  B60Q2400/50 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/201 ,  B64C2201/208 ,  G05D1/0094 ,  G08G1/04 ,  G08G1/0955 ,  G08G1/162 ,  G08G1/205 ,  G08G7/00

Abstract: An unmanned aerial vehicle according to the present invention includes a housing mounted on a vehicle and having an inner space, the housing provided with a launching unit, an unmanned aerial vehicle accommodated in the housing and configured to be launched from the housing when a driving state of the vehicle meets a preset condition, wing units mounted to the unmanned aerial vehicle and configured to allow the flight of the unmanned aerial vehicle in response to the launch from the housing, an output unit disposed on the unmanned aerial vehicle, and a controller configured to control the wing units to move the unmanned aerial vehicle to a position set based on information related to the driving state when the unmanned aerial vehicle is launched, and control the output unit to output warning information related to the driving state.

Abstract translation: 根据本发明的无人驾驶飞行器包括安装在车辆上并具有内部空间的壳体，壳体设置有发射单元，容纳在壳体中的被构造成在驾驶状态下从壳体发射的无人驾驶飞行器 所述车辆单元安装到所述无人驾驶飞行器并且被配置为允许所述无人驾驶飞行器响应于从所述壳体的发射而被飞行，设置在所述无人驾驶飞行器上的输出单元以及被配置为 根据与无人驾驶飞行器的驾驶状态相关的信息，控制机翼单元将无人机移动到设定位置，并且控制输出单元输出与驾驶状态有关的警告信息。

公开(公告)号：WO2015160394A3

公开(公告)日：2015-12-10

申请号：PCT/US2015011149

申请日：2015-01-13

Applicant: ADVANCED PRODUCT DEV LLC

Inventor： MCDONNELL WILLIAM RANDALL

IPC: B64C3/10 ,  B64F1/04 ,  B64F3/00

CPC classification number: B64C3/10 ,  B63H9/0685 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/082 ,  B64C2201/182 ,  B64C2201/205 ,  B64C2201/208 ,  B64F1/02 ,  B64F1/04 ,  B64F1/222 ,  Y02T50/12 ,  Y02T50/826

Abstract: An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft slide into and out of the hangar on dollies (90) like circuit boards in a computer and are launched and recovered using a large towed parafoil (6).

Abstract translation: 一架不​​对称的飞机（1）和一架可从小型船只运行的飞机（1），并在一架直升机机库（107）内以三个或更多的飞机高密度存储，无需起落架或机翼折叠。 这些飞机在计算机上像电路板一样滑入和移出机库（90）的机库，并使用大型拖缆机（6）发射和恢复。

公开(公告)号：WO2015143977A1

公开(公告)日：2015-10-01

申请号：PCT/CN2015/073711

申请日：2015-03-05

Applicant: 浙江吉利控股集团有限公司 ,  浙江吉利汽车研究院有限公司

Inventor： 李书福

IPC: G05D1/10

CPC classification number: G05D1/0684 ,  B64C39/00 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/128 ,  B64C2201/18 ,  B64C2201/208 ,  G06Q10/083 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/0069

Abstract: 一种基于无人机的货物传送系统和方法，该货物传送系统包括无人机（50）以及能够发送和接收无人机（50）的车辆（10），以便能够通过无人机（50）在车辆（10）与另一终端（60）之间传送货物；无人机（50）具有引导无人机（50）在车辆（10）与另一终端（60）之间飞行的导航系统；车辆（10）包括：设置在车辆（10）的顶表面处的无人机收纳装置（40）；设置在车辆（10）处的无人机发送控制器（20）和无人机接收控制器（30）；无人机接收控制器（30）包括身份验证单元（301）和近距引导单元（302）。该基于无人机的货物传送系统能够通过车辆（10）控制无人机（50）的发送和接收，并通过无人机收纳装置（40）收纳无人机（50）。另外，车辆（10）还能通过身份验证单元（301）和近距引导单元（302）向无人机（50）提供身份验证信息和近距引导信息，使得无人机（50）能够确定目标车辆并精确降落至目标车辆处。