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    Sonotube compatible unmanned aerial vehicle and system
    51.
    发明授权
    Sonotube compatible unmanned aerial vehicle and system 失效
    Sonotube兼容无人机和系统

    公开(公告)号：US6056237A

    公开(公告)日：2000-05-02

    申请号：US882368

    申请日：1997-06-25

    Applicant: Richard L. K. Woodland

    Inventor： Richard L. K. Woodland

    IPC: B64C3/40 ,  B64C3/56 ,  B64C5/12 ,  B64C39/02 ,  B64D1/02 ,  B64D7/08 ,  B64D33/02 ,  F41G3/02 ,  F42B12/36 ,  F42B15/10 ,  F41G7/00 ,  B64C1/00

    CPC classification number: B64C3/40 ,  B64C3/56 ,  B64C39/024 ,  B64C5/12 ,  B64D1/02 ,  B64D33/02 ,  B64D7/08 ,  F41G3/02 ,  F42B12/365 ,  F42B15/105 ,  F42B15/22 ,  B64C2201/046 ,  B64C2201/048 ,  B64C2201/082 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/121 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/167 ,  B64C2201/185 ,  B64C2201/203 ,  Y02T50/145

    Abstract: The present invention is generally comprised of a sonotube-compatible unmanned aerial vehicle apparatus, hereinafter referred to as a UAV, and systems for launch and control of the UAV. The UAV is generally comprised of modular sections including a nose section, a payload section, a wing and fuel tank section, and a powerplant section. The modular sections are attached to adjacent sections by uniform lock sealing rings and related components. The present invention comprises an apparatus enabling very small, man portable, ballistically launched, autonomously or semi-autonomously controlled vehicle to be deployed with preprogrammed, communicated, or telemetry mission programming. A wide range of payload packages, including emergency supplies, sensors, and antenna assemblies, may be carried, used or deployed in flight. Man-portable operation is accomplished by the use of a launch canister apparatus. The launch canister comprises retractable launch stabilizing legs, turbine engine exhaust orifices, and various antennas. The launch canister apparatus alternatively comprises a modified type "A", "B", or "C" sonotube launch canister. The system of the invention also comprises a portable Command, Control, Communications, Computer, and Intelligence (C4I) control and sensing analysis console. The console is preferably ruggedized, waterproof, shockproof, and comprises necessary control and analysis computers, input/output devices, antennas, and related hardware and software for vehicle and mission control. A C4I console and/or launch canisters may be transported by means of a backpack adapted for man portability.

    Abstract translation: 本发明通常由声纳管相容的无人驾驶飞行器装置（以下称为无人机）和用于发射和控制无人机的系统组成。 无人机通常包括模块化部分，包括鼻部，有效载荷部分，机翼和燃料箱部分以及动力装置部分。 模块化部分通过均匀的锁定密封环和相关部件连接到相邻部分。 本发明包括一种能够进行预编程，通信或遥测任务编程的非常小的，便携式的，弹道发射的，自主的或半自主控制的车辆的装置。 可以在飞行中携带，使用或部署各种有效载荷包，包括应急用品，传感器和天线组件。 便携式操作通过使用发射罐装置来实现。 发射罐包括可伸缩发射稳定腿，涡轮发动机排气孔和各种天线。 发射罐装置可选地包括修改型“A”，“B”或“C”型超声波发射罐。 本发明的系统还包括便携式命令，控制，通信，计算机和智能（C4I）控制和感测分析控制台。 控制台最好是坚固耐用，防水，防震，并且包括必要的控制和分析计算机，输入/输出设备，天线以及用于车辆和任务控制的相关硬件和软件。 C4I控制台和/或发射罐可以通过适于人的便携性的背包来运输。

    FOLDABLE WINGS FOR AN UNMANNED AERIAL VEHICLE
    53.
    发明申请
    FOLDABLE WINGS FOR AN UNMANNED AERIAL VEHICLE 审中-公开

    公开(公告)号：US20190023374A1

    公开(公告)日：2019-01-24

    申请号：US15755669

    申请日：2016-08-25

    Applicant: UVISION AIR LTD

    Inventor： MOSHE KAHLON ,  AMIT MORAG

    IPC: B64C3/56 ,  B64C39/02

    CPC classification number: B64C3/56 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/201 ,  B64C2201/203 ,  F42B10/14

    Abstract: An unmanned air vehicle (UAV) having a fuselage, a foldable propulsion means to generate thrust leading to the UAV movement, a driving means to drive the propulsion means and a plurality of flight control surfaces actuators are further included. The UAV further includes at least one pair of foldable wings where the rear portion of the wings is pivotally attached to the fuselage. The wings having at least one roll control surface hinged to at least one of the foldable wings. At least a pair of tail stabilizers having ruddervators flight control surfaces hinged to the tail stabilizers. In a fully extended position or in ready to fly state position, each of the foldable wings are deployed perpendicular to one another and perpendicular to the fuselage to form an offset-x shaped wings, and in a stowed position, each of the wings are positioned parallel to one another and positioned parallel to the fuselage.

    Remote controlled aerial reconnaissance vehicle
    55.
    发明授权
    Remote controlled aerial reconnaissance vehicle 有权
    遥控空中侦察车

    公开(公告)号：US09527596B1

    公开(公告)日：2016-12-27

    申请号：US14716785

    申请日：2015-05-19

    Applicant: Richard D. Adams

    Inventor： Richard D. Adams

    IPC: B64D17/00 ,  B64C11/00 ,  B64C39/02 ,  B64C3/56

    CPC classification number: B64D17/00 ,  B64C3/56 ,  B64C11/001 ,  B64C39/024 ,  B64C2201/107 ,  B64C2201/127 ,  B64C2201/162 ,  B64C2201/185 ,  B64C2201/203

    Abstract: A remotely controlled UAV is disclosed. The UAV includes a parachute, with a cylindrical power and control module suspended vertically below the parachute. In one embodiment, a propulsion source is mounted on top of the power and control module with control lines connected to the module below the propulsion source, and in another embodiment the power and control module is suspended from a point above a propulsion source. The UAV may be flown under a parachute and guided by remote control, or the control module (fuselage) may be released from the parachute and extendable fixed wings deployed to enable the UAV to be flown as a fixed wing vehicle.

    Abstract translation: 公开了遥控无人机。 无人机包括一个降落伞，一个圆柱形的电源和控制模块垂直悬挂在降落伞下方。 在一个实施例中，推进源安装在功率和控制模块的顶部，其控制线连接到推进源下方的模块，并且在另一个实施例中，功率和控制模块从推进源上方的点悬挂。 无人机可以在降落伞下飞行并由遥控器引导，或者控制模块（机身）可以从降落伞释放并且可伸展的固定翼部署以使无人机作为固定翼车辆飞行。

    LAUNCHING AN UNMANNED AERIAL VEHICLE USING A HAND-HELD WEAPON
    57.
    发明申请
    LAUNCHING AN UNMANNED AERIAL VEHICLE USING A HAND-HELD WEAPON 有权
    使用手持武器推出无人驾驶的空中客车

    公开(公告)号：US20160009412A1

    公开(公告)日：2016-01-14

    申请号：US14187846

    申请日：2014-02-24

    Applicant: AAI CORPORATION

    Inventor： Alexander D. Manasseh

    IPC: B64F1/04 ,  B64C39/02

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/08 ,  B64C2201/203

    Abstract: A technique is directed to launching an unmanned aerial vehicle (UAV). The technique involves attaching a UAV launcher to a hand-held weapon, and installing a UAV onto the UAV launcher while the UAV launcher is attached to the hand-held weapon. The technique further involves activating the hand-held weapon to launch the UAV into flight from the UAV launcher. Since a user already may be carrying the hand-held weapon for firing ammunition, the user simply needs to further carry the UAV launcher and the UAV which, in some situations, can be packaged into an easy-to-carry container such as a backpack, a carrying case, and so on.

    Abstract translation: 一种技术旨在发射无人机（UAV）。 该技术涉及将UAV发射器连接到手持武器，并将无人机安装在UAV发射器上，而UAV发射器连接在手持武器上。 该技术进一步涉及激活手持武器以将无人机从无人机发射机发射飞行。 由于用户已经可以携带用于发射弹药的手持武器，所以用户只需要进一步携带UAV发射器和UAV，在某些情况下，UAV可以被包装到易于携带的容器中，例如背包 ，手提箱等。

    UAV kit
    58.
    发明授权
    UAV kit 有权
    无人机套件

    公开(公告)号：US09038938B2

    公开(公告)日：2015-05-26

    申请号：US14003406

    申请日：2012-03-26

    Applicant: Petter Muren ,  Trygve Frederik Marton ,  Geir Morten Mellem ,  Dag Henning Paulsen

    Inventor： Petter Muren ,  Trygve Frederik Marton ,  Geir Morten Mellem ,  Dag Henning Paulsen

    IPC: B64C39/02 ,  A63H27/00 ,  B64D47/08

    CPC classification number: B64C39/024 ,  A63H27/12 ,  B64C39/028 ,  B64C2201/024 ,  B64C2201/127 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2203/00 ,  B64D47/08

    Abstract: The embodiments herein disclose a personal UAV kit for storing, preparing and remote control of micro UAVs (40). The UAV kit includes a base unit (10), a control unit (30) and at least one UAV. The UAVs can typically be a winged aircraft with foldable wings or a helicopter with a two-bladed or foldable rotor. The base unit comprises UAV compartments for housing at least one UAV, bay (14) for storing the control unit, batteries and electronic components for charging, communication, control and processing and storing of data. In addition, the system includes an eye near display device for viewing system information and sensor data, typically live video, transmitted from the UAV.

    Abstract translation: 本文的实施方案公开了用于存储，准备和远程控制微型无人机（40）的个人UAV套件。 UAV套件包括基本单元（10），控制单元（30）和至少一个UAV。 无人机通常可以是具有可折叠翼的有翼飞机或具有双叶片或可折叠转子的直升机。 基座单元包括用于容纳至少一个UAV的UAV隔间，用于存储控制单元的舱（14），用于对数据进行充电，通信，控制和处理和存储的电池和电子组件。 此外，该系统包括用于观看系统信息的眼睛附近，以及从UAV发送的通常是实时视频的传感器数据。

    PORTABLE UNMANNED AIRCRAFT FOR NEAR-INSTANT AERIAL SURVEILLANCE
    60.
    发明申请
    PORTABLE UNMANNED AIRCRAFT FOR NEAR-INSTANT AERIAL SURVEILLANCE 审中-公开
    便宜的不间断的飞机，用于近期的空中监视

    公开(公告)号：US20140312164A1

    公开(公告)日：2014-10-23

    申请号：US13745322

    申请日：2013-01-18

    Applicant: JOSHUA M. GIBSON ,  SAGAR JASU PANARA

    Inventor： JOSHUA M. GIBSON ,  SAGAR JASU PANARA

    IPC: B64C39/02 ,  B64C27/00 ,  B64D47/08

    CPC classification number: B64D47/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/048 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/162 ,  B64C2201/203

    Abstract: A portable unmanned aerial vehicle or aircraft, capable of being easily carried by a single individual by means of a mounting device, which can be fastened on a belt or strap. The aerial vehicle comprises a wing attached at one end to a fan or turbine assembly. The fan or turbine assembly may be electrically driven, with power supplied by one or more batteries. In flight, the fan or turbine assembly causes the aerial vehicle to rotate around its center-of-mass (COM), with lift provided by the wing as it rotates. A camera is located on the aircraft at or near the COM.

    Abstract translation: 便携式无人驾驶飞行器或飞机，能够通过安装装置容易地由单个个体携带，该固定装置可紧固在皮带或皮带上。 该飞行器包括在一端附接到风扇或涡轮机组件的翼。 风扇或涡轮组件可以被电驱动，由一个或多个电池供电。 在飞行中，风扇或涡轮机组件使飞行器绕其质心（COM）旋转，随着机翼旋转时提供的升力。 相机位于COM上或附近的飞机上。

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