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    UNMANNED AERIAL VEHICLE MANAGEMENT
    12.
    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。

    Airborne Drone Launch and Recovery Apparatus
    13.
    发明申请
    Airborne Drone Launch and Recovery Apparatus 审中-公开
    空中无人机发射和恢复装置

    公开(公告)号：US20160355261A1

    公开(公告)日：2016-12-08

    申请号：US15176250

    申请日：2016-06-08

    Applicant: Howard Martin Chin ,  Kimberly A. Carraha

    Inventor： Howard Martin Chin ,  Kimberly A. Carraha

    IPC: B64D5/00 ,  B64C39/02

    CPC classification number: B64D5/00 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/084 ,  B64C2201/206

    Abstract: An airborne drone launch and recovery apparatus for selectively launching drones located on the underside of a carrier aircraft or recovering drones following flight of the drones, the airborne launch and recovery apparatus has an extensible stinger slidable along the length of a stinger sheath between a retracted position proximal the rear portion of the carrier aircraft and an extended position in front of the carrier aircraft, and a catcher shuttle carried on the forward part of the stinger for extending into the non-turbulent air in front of the carrier aircraft when the stinger is in the extended position. The carrier shuttle includes a launch/recovery assembly for selectively either having a locked condition for the recovery guide of a drone prior to the positioning of the catcher shuttle in a selected for the launch of the drone, and having an open condition for receiving the recovery guide of a drone at the termination of the flight of the drone to terminate the flight.

    Abstract translation: 一种空中无人机发射和恢复装置，用于选择性地发射位于载体飞行器的下侧上的无人机或在无人机的飞行之后恢复无人机，机载发射和恢复装置具有可伸长的刺针，沿着刺血刺鞘的长度在缩回位置 靠近载体飞行器的后部，并且在载体飞行器的前面延伸的位置，以及在托管架前部延伸到载体飞行器前方的非湍流空气中的捕手穿梭器，当托管架处于 延长的位置。 运输班车包括发射/恢复组件，用于选择性地具有用于无人机的恢复引导件的锁定状态，在捕集器穿梭机定位在被选择用于发射无人机之前，并且具有用于接收恢复的打开状态 在无人驾驶飞机终止时终止飞行的无人机指导。

    UNMANNED AIR VEHICLE RECOVERY SYSTEM
    14.
    发明申请
    UNMANNED AIR VEHICLE RECOVERY SYSTEM 审中-公开
    无人空中车辆恢复系统

    公开(公告)号：US20160251088A1

    公开(公告)日：2016-09-01

    申请号：US15048123

    申请日：2016-02-19

    Applicant: Engineered Arresting Systems Corporation

    Inventor： Robert C. Melish ,  Kenneth J. Neeld ,  Richard L. Orner, Jr.

    IPC: B64F1/02 ,  B64D3/00

    CPC classification number: B64F1/02 ,  B64B1/40 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/182 ,  B64D1/02 ,  B64F1/025

    Abstract: Embodiments of the present disclosure relate generally to safe arrestment and recovery of an airborne unmanned air vehicle (UAV). Specific embodiments provide a recovery net that can recover a UAV approaching a cargo plane, the UAV either traveling in the same direction as the cargo plane or in an opposite direction of the cargo plane. The systems described herein may also be used as an air-only based system.

    Abstract translation: 本公开的实施例一般涉及机载无人机（UAV）的安全停止和恢复。 具体实施例提供一种恢复网，其可以恢复接近货物的UAV，UAV沿与货物平面相同的方向或者与货物平面相反的方向行进。 本文描述的系统也可以用作仅基于空气的系统。

    Aircraft deployment and retrieval of unmanned aerial vehicles
    15.
    发明授权
    Aircraft deployment and retrieval of unmanned aerial vehicles 有权
    飞机部署和无人机的检索

    公开(公告)号：US09132916B2

    公开(公告)日：2015-09-15

    申请号：US13664323

    申请日：2012-10-30

    Applicant: The Boeing Company

    Inventor： Mark Hanna ,  David R. Poling

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/082 ,  B64C2201/126 ,  B64C2201/182 ,  B64C2201/206

    Abstract: An aircraft system incorporates a first aircraft having a grappling device including a first gripper with a first actuator and a second gripper with a second actuator. The first gripper and the second gripper are movable between an open and a closed position to engage a hooking device and pivot together to change a capture angle. A first controller receives a command and operates the actuators in response to open and close the first and second grippers of the grappling device. The controller also receives a second command and operates the first and second actuators to pivot the grippers and provide grappling at a range of capture angles. A second aircraft, which may be a UAV, incorporates the hooking device. The hooking device includes a ring rotatable from the surface and a third actuator to rotate the ring between a stowed and an extended position.

    Abstract translation: 飞行器系统包括具有抓斗装置的第一飞行器，该抓斗装置包括具有第一致动器的第一夹持器和具有第二致动器的第二夹持器。 第一夹持器和第二夹持器可在打开位置和关闭位置之间移动以接合钩挂装置并枢转在一起以改变捕获角度。 响应于打开和关闭抓斗装置的第一和第二夹持器，第一控制器接收命令并操作致动器。 控制器还接收第二命令并且操作第一和第二致动器以枢转夹持器并且在捕获角度范围内提供抓斗。 可能是UAV的第二架飞机结合了挂钩装置。 挂钩装置包括从表面可旋转的环和第三致动器，以在收起和伸出位置之间旋转环。

    Air-drop device tail charger
    16.
    发明授权
    Air-drop device tail charger 有权
    放气装置尾充电器

    公开(公告)号：US09035475B1

    公开(公告)日：2015-05-19

    申请号：US13534083

    申请日：2012-06-27

    Applicant: John G. Cunningham

    Inventor： John G. Cunningham

    IPC: F02B63/04 ,  F03D9/00 ,  B64C19/00 ,  H02J7/00

    CPC classification number: F03D9/25 ,  B64C39/024 ,  B64C2201/066 ,  B64C2201/082 ,  F03D5/00 ,  F03D9/11 ,  F42B12/365 ,  F42B12/58 ,  F42B15/08 ,  F42C11/008 ,  G01W1/08 ,  H02J7/0052 ,  H02J7/14 ,  Y02E10/70 ,  Y02E10/725

    Abstract: A system and method for powering an air-drop device is presented. One configuration of the system includes an energy capture device, a generator and an electrical logic unit. The energy capture device converts the movement air passing by the air-drop tail device into kinetic energy. The generator converts that kinetic energy into electrical energy and the electrical logic unit can then be powered by the electrical energy allowing it to perform at least a portion of a mission.

    Abstract translation: 提出了一种用于为空降设备供电的系统和方法。 该系统的一个配置包括能量捕获装置，发电机和电逻辑单元。 能量捕获装置将通过空气滴尾装置的运动空气转换成动能。 发电机将该动能转换为电能，然后电逻辑单元可以通过电能来供电，从而允许它执行任务的至少一部分。

    In-line staged horizontal takeoff vehicles and related methods
    18.
    发明授权
    In-line staged horizontal takeoff vehicles and related methods 有权
    直升式水平起飞车辆及相关方法

    公开(公告)号：US08925857B2

    公开(公告)日：2015-01-06

    申请号：US14101690

    申请日：2013-12-10

    Applicant: David Luther

    Inventor： David Luther

    IPC: B64C37/02 ,  B64C39/10 ,  B64C39/02 ,  B64D5/00

    CPC classification number: B64C39/10 ,  B64C39/024 ,  B64C2201/082 ,  B64D5/00 ,  Y02T50/12

    Abstract: Aircraft systems that are optimized for multiple phases of flight are disclosed. In an aspect, an in-line staged aircraft is disclosed comprising a launch vehicle and a flight vehicle which are configured to join together along a common center line and form a single air foil in the joined configuration. The flight vehicle and the launch vehicle are separable in flight. In an aspect, the flight vehicle is an unmanned aerial vehicle configured for high-altitude, long-endurance operations.

    Abstract translation: 披露了针对多个飞行阶段进行了优化的飞机系统。 在一方面，公开了一种在线分级飞行器，其包括运载火箭和飞行器，其构造成沿着公共中心线连接在一起并且形成接合构造中的单个空气箔。 飞行器和运载火箭在飞行中是分离的。 在一方面，飞行器是配置用于高空，长时间运行的无人机。

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