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    SYSTEM FOR PROVIDING A RAPIDLY ELEVATED AEROSTAT PLATFORM
    211.
    发明申请
    SYSTEM FOR PROVIDING A RAPIDLY ELEVATED AEROSTAT PLATFORM 审中-公开
    提供快速高空作战平台的系统

    公开(公告)号：US20120181380A1

    公开(公告)日：2012-07-19

    申请号：US13009207

    申请日：2011-01-19

    Applicant: Peter K. Van Staagen ,  William Douglas McDaniel ,  James H. Boschma, JR.

    Inventor： Peter K. Van Staagen ,  William Douglas McDaniel ,  James H. Boschma, JR.

    IPC: B64B1/50 ,  B64B1/40

    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.

    Abstract translation: 用空气净化器部署有效载荷的系统和方法使用移动运输装置将系统移动到部署现场。 在结构上，该系统包括其上安装有旋转头的基座单元。 用于保持放气式放气器的信封容器安装在旋转头上，并且旋转头上的容器的旋转定位了空气调节器，以最佳地符合现有的风况。 还包括在系统中的是充气机，其安装在基座单元上以用氦气对空气净化器进行充气。 而且，该系统包括一个系绳控制单元，用于在其部署，飞行中使用和恢复期间维持与浮空器的连接。 优选地，部署计算机用于旋转头，充气机和系绳的协调控制。

    Launch and capture systems for vertical take-off and landing (VTOL) vehicles
    212.
    发明授权
    Launch and capture systems for vertical take-off and landing (VTOL) vehicles 有权
    用于垂直起飞和着陆（VTOL）车辆的启动和捕获系统

    公开(公告)号：US08162256B2

    公开(公告)日：2012-04-24

    申请号：US12051552

    申请日：2008-03-19

    Applicant: Emray R. Goossen ,  Yogendra Y. Sheoran

    Inventor： Emray R. Goossen ,  Yogendra Y. Sheoran

    IPC: B64F1/00

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/088 ,  B64C2201/182 ,  B64C2201/201 ,  B64C2201/205 ,  B64C2201/208 ,  B64F1/04

    Abstract: A launch and capture system for capturing a vertical take-off and landing (VTOL) vehicle having a thruster and a duct configured to direct airflow generated by the thruster includes a capture plate and an extension. The capture plate is configured to alter the airflow and generate a force attracting the duct to the capture plate. The extension is coupled to the capture plate, and is configured to at least facilitate holding the VTOL vehicle against the capture plate.

    Abstract translation: 用于捕获具有推进器和构造成引导由推进器产生的气流的管道的垂直起飞和着陆（VTOL）车辆的发射和捕获系统包括捕获板和延伸部。 捕获板被配置为改变气流并产生吸引到捕获板的管道的力。 延伸部联接到捕获板，并且被构造成至少有利于将VTOL车辆保持抵靠捕获板。

    Communications using unmanned surface vehicles and unmanned micro-aerial vehicles
    214.
    发明授权
    Communications using unmanned surface vehicles and unmanned micro-aerial vehicles 有权
    使用无人地面车辆和无人驾驶微型飞行器的通信

    公开(公告)号：US07039367B1

    公开(公告)日：2006-05-02

    申请号：US10356931

    申请日：2003-01-31

    Applicant: Daniel Kucik

    Inventor： Daniel Kucik

    IPC: H04B1/034

    CPC classification number: G08C17/02 ,  B64C2201/122 ,  B64C2201/208 ,  G05D1/104

    Abstract: A communications system and method utilizes an unmanned surface vehicle (USV) capable of collecting data about an environment in which the USV resides. At least one micro-aerial vehicle (MAV), equipped for unmanned flight after a launch thereof, is mounted on the USV. Each MAV has onboard radio frequency (RF) communications. Each MAV launched into the air transmits the data collected by the USV using the MAV's RF communications.

    Abstract translation: 通信系统和方法利用能够收集关于USV驻留的环境的数据的无人地面车辆（USV）。 在USV上安装了至少一辆装备无人驾驶的微型飞行器（MAV）。 每个MAV具有板载射频（RF）通信。 每个MAV发射空中传输USV使用MAV的RF通信收集的数据。

    Unmanned vehicle
    215.
    发明申请
    Unmanned vehicle 有权
    无人车

    公开(公告)号：US20060074557A1

    公开(公告)日：2006-04-06

    申请号：US11011001

    申请日：2004-12-13

    Applicant: Anthony Mulligan ,  Christopher Troudt ,  Jason Michael Douglas

    Inventor： Anthony Mulligan ,  Christopher Troudt ,  Jason Michael Douglas

    IPC: G01C21/26

    CPC classification number: G05D1/0094 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/044 ,  B64C2201/104 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/205 ,  B64C2201/208

    Abstract: Methods and apparatuses provide surveillance of a convoy. At least one unmanned aerial vehicle (UAV) obtains images around the convoy's position to provide information about potential hostile activity while the UAV follows a generally curvilinear path around the convoy as instructed by one of the convoy vehicles. Path planner algorithm software is executed by the controlling convoy vehicle in which position and velocity information regarding the unmanned aerial vehicle and the convoy are processed to determine values of control variables. The determined values are sent to the unmanned aerial vehicle over a wireless communications channel. The path of the surveillance vehicle may be changed in order to provide evasive measures to avoid an attack on the surveillance vehicle by an adversary.

    Abstract translation: 方法和设备对车队进行监视。 至少一架无人驾驶飞行器（UAV）获取围绕车队位置的图像，以提供关于潜在敌对行为的信息，而无人机按照车队车辆指示的方式沿着车队周围的大致曲线路径。 路径规划器算法软件由控制车队车辆执行，其中处理关于无人机和车队的位置和速度信息以确定控制变量的值。 所确定的值通过无线通信信道发送到无人驾驶飞行器。 监视车辆的路径可能会改变，以便提供回避措施，以避免对手对监控车辆的攻击。

    Unmanned craft
    216.
    发明授权
    Unmanned craft 失效
    无人工艺

    公开(公告)号：US4410151A

    公开(公告)日：1983-10-18

    申请号：US182021

    申请日：1980-08-28

    Applicant: Heinz-Jochen Hoppner ,  Ulrich Kramer ,  Hugo Sgarz ,  Herbert Sadowski

    Inventor： Heinz-Jochen Hoppner ,  Ulrich Kramer ,  Hugo Sgarz ,  Herbert Sadowski

    IPC: B64C39/02 ,  F42B10/14 ,  B64F1/04 ,  F41F3/00

    CPC classification number: B64C39/024 ,  F42B10/14 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/208

    Abstract: A vehicle or craft is provided for propeller propulsion with start assist by a releasable rocket engine. The craft is launched from a silo of square-shaped cross-section containing the starter motor for the propeller, whose engine is started while the craft is still in the silo. Diagonally opposed corners of the silo are provided with rails, in which run guides on rudder fins of the craft. The wings are pivoted to the fuselage for deployment whereby the wing tips do not move forward. The rocket engine is jettisoned shortly after take-off by simple disengagement. Parts of the wings and/or the rear of the fuselage may be jettisoned shortly before the craft reaches the target area.

    Abstract translation: 提供用于螺旋桨推进的车辆或工具，由可释放的火箭发动机开始辅助。 该工艺是从一个方形截面的筒仓中推出的，包含用于螺旋桨的起动电机，当发动机仍然在筒仓中时，发动机起动。 筒仓的对角线相对的角落设有导轨，其中在工艺的方向舵鳍上的行进导轨。 机翼枢转到机身进行部署，由此机翼尖端不向前移动。 火箭发动机在起飞后不久就被简单的分离。 机翼的部分和/或机身的后部可能在飞机到达目标区域之前不久就被抛弃。

    MOONROOF ACCESSORY PANEL
    218.
    发明公开
    MOONROOF ACCESSORY PANEL 审中-公开

    公开(公告)号：US20230174233A1

    公开(公告)日：2023-06-08

    申请号：US17544535

    申请日：2021-12-07

    Applicant: Ford Global Technologies, LLC

    Inventor： Nelson Alexander Brock

    IPC: B64C39/02 ,  B60J7/00

    CPC classification number: B64C39/024 ,  B60J7/0007 ,  B64C2201/18 ,  B64C2201/208

    Abstract: This disclosure describes a moonroof accessory panel. The moonroof accessory panel may be a structure that may be removably attached to a moonroof area of a vehicle. The moonroof accessory panel may be used to hold a drone associated with the vehicle such that the drone may take-off from and land on the moonroof accessory panel. The top of the moonroof accessory panel may also be accessible from the cabin of the vehicle such that a user may place the drone on top of the moonroof accessory panel while inside the cabin. The moonroof accessory panel may also be used for other purposes beyond holding drones as well.

    TETHERED UNMANNED AERIAL VEHICLE SYSTEM
    220.
    发明申请
    TETHERED UNMANNED AERIAL VEHICLE SYSTEM 审中-公开

    公开(公告)号：US20190002102A1

    公开(公告)日：2019-01-03

    申请号：US16126020

    申请日：2018-09-10

    Applicant: Tribune Broadcasting Company, LLC

    Inventor： Hank J. HUNDEMER

    IPC: B64C39/02 ,  B64F1/02 ,  B64F3/00 ,  B64F3/02

    CPC classification number: B64C39/022 ,  B64C39/024 ,  B64C2201/148 ,  B64C2201/182 ,  B64C2201/208 ,  B64D2201/00 ,  B64F1/02 ,  B64F3/00 ,  B64F3/02

    Abstract: In one aspect, an example system includes: (i) a base including a bottom surface and a first coupling-point; (ii) a vertically-oriented elongate structure comprising a lower end, an upper end, and an inner channel, wherein the inner channel comprises an upper access-point disposed proximate the upper end, wherein the base is coupled to the elongate structure proximate the lower end; (iii) a deployable cushioning-device coupled to the elongate structure; and (iv) a tether comprising a first portion, a second portion, a third portion, and a fourth portion, wherein the first portion is coupled to the first coupling-point, the second portion is coupled to a second coupling-point of the UAV, the third portion extends through the inner channel, the fourth portion extends from the upper access-point to the second coupling-point, and the fourth portion has a length that is less than a distance between the upper access-point and the bottom surface.

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