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    UNMANNED AERIAL VEHICLE MANAGEMENT
    11.
    发明申请
    UNMANNED AERIAL VEHICLE MANAGEMENT 审中-公开
    不定期的空中客车管理

    公开(公告)号：US20160364989A1

    公开(公告)日：2016-12-15

    申请号：US15183653

    申请日：2016-06-15

    Applicant: ImageKeeper LLC

    Inventor： Jerry Speasl ,  Mike Patterson ,  Mark Roberts

    IPC: G08G5/00 ,  B64F1/22 ,  B64C39/02

    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。

    LAUNCH DEVICE FOR REMOTELY CONTROLLED AIRCRAFT
    14.
    发明申请
    LAUNCH DEVICE FOR REMOTELY CONTROLLED AIRCRAFT 审中-公开
    远程控制飞机的启动装置

    公开(公告)号：US20160152347A1

    公开(公告)日：2016-06-02

    申请号：US14898086

    申请日：2014-06-10

    Applicant: THALES

    Inventor： Luc CARPENTIER ,  Thierry GAUTHIER

    IPC: B64F1/04 ,  B64C39/02

    CPC classification number: B64F1/04 ,  A63H27/14 ,  B64C39/024 ,  B64C2201/08

    Abstract: A device to launch a drone, comprises a rail extending along a longitudinal axis and a carriage, mobile on the rail, that can support and launch a drone by the acceleration of the carriage between a loading position and an end-of-travel position, further comprising a spring mechanism configured to exert a return force on the carriage along the longitudinal axis that is substantially constant between the two positions. The spring mechanism comprises at least one coil spring around a hub, one end of the coil spring being linked to the carriage, the return force exerted on the carriage being generated by the coiling of the spring around the hub.

    Abstract translation: 用于发射无人机的装置包括沿着纵向轴线延伸的轨道和在轨道上移动的滑架，其可以通过在装载位置和行程结束位置之间的滑架的加速度来支撑和发射无人机， 还包括弹簧机构，其构造成沿着所述两个位置之间基本上恒定的所述纵向轴线在所述托架上施加返回力。 弹簧机构包括围绕轮毂的至少一个螺旋弹簧，螺旋弹簧的一端连接到滑架，通过弹簧围绕毂盘绕而产生施加在滑架上的返回力。

    Combined submersible vessel and unmanned aerial vehicle
    15.
    发明授权
    Combined submersible vessel and unmanned aerial vehicle 有权
    组合潜艇和无人机

    公开(公告)号：US09296270B2

    公开(公告)日：2016-03-29

    申请号：US13765144

    申请日：2013-02-12

    Applicant: Aurora Flight Sciences Corporation

    Inventor： Robert Parks ,  Adam Woodworth ,  Tom Vaneck ,  Justin McClellan

    IPC: B60F5/02 ,  B64C39/02 ,  F42B15/20

    CPC classification number: B64C37/00 ,  B60F5/02 ,  B63G8/001 ,  B63G8/08 ,  B63G2008/005 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/167 ,  F42B15/20

    Abstract: A combined submersible vessel and unmanned aerial vehicle preferably includes a body structure, at least one wing structure, at least one vertical stabilizer structure, and at least one horizontal stabilizer structure. A propulsion system is coupled to the body structure and is configured to propel the flying submarine in both airborne flight and underwater operation. Preferably, the propulsion system includes a motor, a gearbox coupled to the motor and configured to receive power generated by the motor and provide variable output power, a drive shaft coupled to the gearbox and configured to transfer the variable output power provided by the gearbox, and a propeller coupled to the drive shaft and configured to accept power transferred to it from the drive shaft. The propeller is further configured to rotate and propel the flying submarine in both an airborne environment and in an underwater environment.

    Abstract translation: 组合潜艇和无人驾驶飞行器优选地包括主体结构，至少一个翼结构，至少一个垂直稳定器结构和至少一个水平稳定器结构。 推进系统联接到车身结构并且被构造成在空中飞行和水下操作中推进飞行潜艇。 优选地，推进系统包括电动机，耦合到电动机并被配置为接收由电动机产生的电力并提供可变输出功率的变速箱;耦合到齿轮箱并被配置为传递由变速箱提供的可变输出功率的驱动轴， 以及联接到所述驱动轴并被配置为接受从所述驱动轴传递到其的动力的螺旋桨。 螺旋桨进一步构造成在空中环境和水下环境中旋转和推进飞行潜艇。

    Launch Tube Restraint System For Unmanned Aerial Vehicle (UAV)
    16.
    发明申请
    Launch Tube Restraint System For Unmanned Aerial Vehicle (UAV) 有权
    无人机（UAV）发射管约束系统

    公开(公告)号：US20150267996A1

    公开(公告)日：2015-09-24

    申请号：US14281680

    申请日：2014-05-19

    Applicant: AeroVironment, Inc.

    Inventor： Guan H. Su ,  Marcos Henry Rodriguez

    IPC: F41F3/00 ,  B64C39/02

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/08 ,  B64C2201/084 ,  B64C2201/088 ,  B64C2201/201 ,  B64F1/06 ,  F41B11/80 ,  F41F3/00 ,  F41F3/042 ,  F41F3/052 ,  F41F3/073

    Abstract: An unmanned aerial launch vehicle (UAV) launch apparatus is disclosed that includes a UAV (400) having an exterior surface, an aerial vehicle (AV) tab (510) extending from the exterior surface, a tube (440) containing the UAV (400), the tube (440) including a tab stop (515) configured to controllably hinder travel of the AV tab (510) past the tab stop (515), and a pair of opposing tab guides (700, 705) configured to position the AV tab (510) for travel over the tab stop (515).

    Abstract translation: 公开了一种无人驾驶飞行器（UAV）发射装置，其包括具有外表面的UAV（400），从外表面延伸的飞行器（AV）突片（510），包含无人机（400）的管（440） ），所述管（440）包括构造成可控制地阻碍所述AV突片（510）经过所述突片止动件（515）的移动的突片止动件（515），以及一对相对的突片引导件（700,705），其被配置为 AV选项卡（510），用于在制表位（515）上移动。

    APPARATUS AND METHOD FOR LAUNCH AND RETRIEVAL OF A HOVERING AIRCRAFT
    17.
    发明申请
    APPARATUS AND METHOD FOR LAUNCH AND RETRIEVAL OF A HOVERING AIRCRAFT 有权
    装置和方法，用于启动和检索空中飞机

    公开(公告)号：US20150239578A1

    公开(公告)日：2015-08-27

    申请号：US14315899

    申请日：2014-06-26

    Applicant: Aerovel Corporation

    Inventor： Brian T. McGeer

    IPC: B64F1/02 ,  B64C39/02 ,  B64F1/04

    CPC classification number: B64F1/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/08 ,  B64C2201/182 ,  B64F1/04 ,  Y10S901/02 ,  Y10S901/31

    Abstract: Various embodiments of the present disclosure provide an apparatus and method for launch and retrieval of a hovering aircraft. Generally, the apparatus of the present disclosure is configured to capture a hovering aircraft between two or more fingers of an aircraft capturer, guide the captured aircraft into a docking station for servicing and/or storage, and launch the aircraft from the docking station. The apparatus of the present disclosure is thus configured to bring the aircraft from an imprecise, irregular hover into a secure and well-controlled rest state. The tolerance of imprecision provided by the apparatus makes it particularly suited for use under a practical conditions such as aboard a small boat in a rough sea.

    Abstract translation: 本公开的各种实施例提供了用于启动和检索悬停飞行器的装置和方法。 通常，本公开的装置被配置为在飞行器捕获器的两个或更多个手指之间捕获悬停的飞行器，将所捕获的飞行器引导到对接站中用于维修和/或存储，并且从对接站发射飞行器。 因此，本公开的装置被配置为使飞机从不精确的不规则悬停变成安全且良好控制的休息状态。 该装置提供的不准确度的公差使得它特别适合在诸如在粗糙的海洋中的小船上的实际条件下使用。

    SURVEILLANCE SYSTEM
    18.
    发明申请
    SURVEILLANCE SYSTEM 有权
    监管制度

    公开(公告)号：US20150142210A1

    公开(公告)日：2015-05-21

    申请号：US14370178

    申请日：2012-12-05

    Applicant: BAE SYSTEMS plc

    Inventor： Clyde Warsop ,  Andrew Julian Press ,  Alan Geraint Davies

    IPC: B64C39/02 ,  B64F1/04 ,  B64C3/56 ,  B64C9/08 ,  G05D1/00 ,  B64C5/06

    CPC classification number: B64C39/028 ,  B64C3/56 ,  B64C5/06 ,  B64C9/08 ,  B64C2201/08 ,  B64C2201/123 ,  B64C2201/145 ,  B64C2201/146 ,  B64F1/04 ,  F42B12/365 ,  F42B15/08 ,  G05D1/0011 ,  G05D1/0088 ,  G05D1/0094

    Abstract: The invention relates to a launched aerial surveillance vehicle, more specifically to a grenade or under-slung grenade launcher (UGL) aerial surveillance vehicle, a surveillance system and methods of providing rapid aerial surveillance.The vehicle once deployed is capable of autonomous flight paths, with basic inputs to change the circular flight paths, so as to build up surveillance for an area of interest. The vehicle comprises at least on optical sensor, which may be IR or visible range, to survey the area of interest, and feed the images back to at least one remote user.

    Abstract translation: 本发明涉及一种发射的空中监视车辆，更具体地涉及一种手榴弹或坠落手榴弹发射器（UGL）空中监视车辆，监视系统和提供快速空中监视的方法。 一旦部署的车辆能够进行自主飞行路径，基本输入可以改变循环飞行路径，以便建立对感兴趣区域的监视。 车辆至少包括可以是IR或可见范围的光学传感器，以测量感兴趣的区域，并将图像馈送给至少一个远程用户。

    LAUNCHED AIR VEHICLE SYSTEM
    19.
    发明申请
    LAUNCHED AIR VEHICLE SYSTEM 有权
    启动空气车辆系统

    公开(公告)号：US20150008280A1

    公开(公告)日：2015-01-08

    申请号：US14294073

    申请日：2014-06-02

    Applicant: Lockheed Martin Corporation

    Inventor： Thomas William Smoker

    IPC: B64F1/04 ,  B63G8/30 ,  B63G8/00

    CPC classification number: B64F1/04 ,  B63G8/001 ,  B63G8/30 ,  B63G8/38 ,  B64C2201/08 ,  B64C2201/205 ,  F41F3/07 ,  F41F3/10

    Abstract: A launch canister for ejection from a submerged launch platform, the launch canister being adapted for ejection in a direction substantially along a first axis of the launch canister and comprising: an enclosure for carrying a UAV; a nose cap releasably located in a launch opening at a forward end of the launch canister; a launch mechanism for driving a UAV carried in the enclosure out of the launch canister through the launch opening in a direction substantially along said first axis; and a water surface sensor for detecting when the nose cap of the canister broaches the surface of the water; wherein the launch canister is configured to, on the water surface sensor detecting that the nose cap of the canister has broached the surface of the water, immediately release the nose cap and initiate the launch mechanism to drive a UAV carried in the enclosure out of the launch canister through the launch opening.

    Abstract translation: 一种用于从淹没式发射平台喷射的发射罐，所述发射罐适于沿基本上沿着所述发射罐的第一轴线的方向喷射，并且包括：用于承载无人机的外壳; 可拆卸地位于发射筒前端的发射开口中的鼻盖; 发射机构，用于沿着所述第一轴线的方向，通过所述发射开口将所述外壳中携带的无人机驱动出所述发射罐; 以及水表面传感器，用于检测罐的鼻盖何时拉开水面; 其中所述发射罐被配置成在所述水表面传感器上检测到所述罐的鼻盖已经拉开了所述水面，立即释放所述鼻盖并启动所述发射机构以将所述外壳中携带的UAV驱动出 发射罐通过发射开口。

    USING UNMANNED CONTROLLER EQUIPMENT TO LAUNCH AND RECOVER UNMANNED IMAGING EQUIPMENT
    20.
    发明公开
    USING UNMANNED CONTROLLER EQUIPMENT TO LAUNCH AND RECOVER UNMANNED IMAGING EQUIPMENT 审中-公开

    公开(公告)号：US20240111302A1

    公开(公告)日：2024-04-04

    申请号：US17956730

    申请日：2022-09-29

    Applicant: AT&T Intellectual Property I, L.P.

    Inventor： Joseph Soryal

    IPC: G05D1/10 ,  B64C39/02

    CPC classification number: G05D1/104 ,  B64C39/024 ,  B64C2201/08 ,  B64C2201/123

    Abstract: The technologies described herein are generally directed to utilizing unmanned controller equipment to launch and recover unmanned imaging equipment in a fifth generation (5G) network or other next generation networks. For example, a method described herein can include receiving an indication that unmanned aerial equipment is to be captured. The method can further include, based on the indication, capturing the unmanned aerial equipment launched over a data collection area, resulting in captured unmanned aerial equipment. Further, the method can include, interfacing with the captured unmanned aerial equipment to download information associated with the data collection area collected by the unmanned aerial equipment during airborne transit over the data collection area.

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