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    High Altitude Aircraft, Aircraft Unit and Method for Operating an Aircraft Unit
    182.
    发明申请
    High Altitude Aircraft, Aircraft Unit and Method for Operating an Aircraft Unit 审中-公开
    高空飞机，飞机单元和操作飞机单元的方法

    公开(公告)号：US20140252156A1

    公开(公告)日：2014-09-11

    申请号：US14354030

    申请日：2012-10-20

    Applicant: EADS Deutschland GmbH

    Inventor： Manfred Hiebl ,  Hans Wolfgang Pongratz

    IPC: B64C39/02 ,  B64D39/00 ,  B64C27/41 ,  B64C9/00

    CPC classification number: B64C39/02 ,  B64C3/30 ,  B64C9/00 ,  B64C27/41 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/105 ,  B64C2201/122 ,  B64C2201/165 ,  B64D39/00 ,  B64D2041/005 ,  B64D2211/00 ,  Y02T50/55 ,  Y02T90/36

    Abstract: A high-altitude unmanned stratosphere aerial vehicle includes a fuselage, wings, control surfaces, and a propulsion system including an engine and a propeller. Each wing has a plurality of hoses and wing spars extending in a direction perpendicularly to the longitudinal fuselage axis and are surrounded by a skin forming a wing covering that determines the cross-sectional contour of the wing, the cross-sectional contour forming a laminar flow airfoil that generates high lift when there is low flow resistance. At the free end facing away from the fuselage, each wing has a winglet extending transversely to the longitudinal wing axis. The winglet has a movable control surface, which allows an aerodynamic side force to be generated so as to bring the aerial vehicle to a banked position.

    Abstract translation: 高空无人空中平流层飞行器包括机身，机翼，控制面，以及包括发动机和推进器的推进系统。 每个翼具有沿垂直于纵向机身轴线的方向延伸的多个软管和翼梁，并且被形成机翼覆盖物的皮肤包围，所述机翼覆盖物确定机翼的横截面轮廓，横截面轮廓形成层流 当流动阻力低时产生高升力的翼型。 在远离机身的自由端处，每个翼具有横向于纵向翼轴线延伸的小翼。 小翼具有可移动的控制表面，其允许产生空气动力学侧力，以使空中飞行器处于堆积位置。

    COMBINED SUBMERSIBLE VESSEL AND UNMANNED AERIAL VEHICLE
    186.
    发明申请
    COMBINED SUBMERSIBLE VESSEL AND UNMANNED AERIAL VEHICLE 有权
    组合的不合格船只和无人驾驶的航空器

    公开(公告)号：US20140026802A1

    公开(公告)日：2014-01-30

    申请号：US13765144

    申请日：2013-02-12

    Applicant: Aurora Flight Scienes

    Inventor： ROBERT PARKS ,  ADAM WOODWORTH ,  TOM VANECK ,  JUSTIN MCCLELLAN

    IPC: B60F5/02

    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。

    Airborne, tethered, remotely stabilized surveillance platform
    187.
    发明授权
    Airborne, tethered, remotely stabilized surveillance platform 有权
    机载，系绳，远程稳定的监控平台

    公开(公告)号：US08602349B2

    公开(公告)日：2013-12-10

    申请号：US12803254

    申请日：2010-06-23

    Applicant: Dimitri Petrov

    Inventor： Dimitri Petrov

    IPC: B64C27/10

    CPC classification number: B64C39/022 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/148 ,  B64C2201/208

    Abstract: An airborne surveillance platform supporting optoelectronic and electronic sensors, including level sensors, is automatically stabilized in a horizontal plane by varying the length of two tethers out of three. Error signals from the level sensors are transmitted over a wireless link to control components on a rotating platform on the host vehicle, which automatically vary the length of tethers. Applications include images of the surrounding terrain generated by a video camera and a thermal imager in military, police and civil emergency operations.

    Abstract translation: 包括液位传感器在内的支持光电子和电子传感器的机载监控平台通过改变三个系统中的两个系绳的长度在水平面中自动稳定。 来自液位传感器的误差信号通过无线链路传输，以控制主车辆上的旋转平台上的组件，这自动改变系绳的长度。 应用包括在军事，警察和民用应急行动中由摄像机和热像仪产生的周围地形的图像。

    Unmanned aerial vehicle
    189.
    发明授权
    Unmanned aerial vehicle 失效
    无人驾驶的航空机

    公开(公告)号：US08561937B2

    公开(公告)日：2013-10-22

    申请号：US12906096

    申请日：2010-10-17

    Applicant: Hosein Goodarzi

    Inventor： Hosein Goodarzi

    IPC: B64C27/00 ,  B64C29/00

    CPC classification number: B64C39/024 ,  B64C39/064 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/146

    Abstract: The various embodiments of the present invention provide an unmanned aerial vehicle comprising a hemispherical body, a brushless type electrical, a propeller, a plurality of wingtip devices, a plurality of servo motors and each of the plurality of the servo motors is connected to each of the plurality of the wingtip devices respectively, a plurality of carbon rods, and a casing. The brushless type electrical motor provides a lifting force for a vertical take-off and landing (VTOL) and the plurality of wing tip devices are classified into three types of wing tip devices and the three types of wing tip devices are controlled by the respective servo motors to control yaw, pitch and roll movements thereby stabilizing and controlling the movement of an aircraft.

    Abstract translation: 本发明的各种实施例提供一种无人驾驶飞行器，其包括半球体，无刷电，螺旋桨，多个翼尖装置，多个伺服马达，多个伺服马达中的每一个连接到 多个翼尖装置，多个碳棒，以及壳体。 无刷式电动机为垂直起降提供提升力（VTOL），并且多个翼尖装置分为三种类型的翼尖装置，三种类型的翼尖装置由相应的伺服机构 用于控制偏航，俯仰和滚动运动的电机，从而稳定和控制飞行器的运动。

    TETHERED AERIAL SYSTEM FOR DATA GATHERING
    190.
    发明申请
    TETHERED AERIAL SYSTEM FOR DATA GATHERING 审中-公开
    数据采集​​的专用系统

    公开(公告)号：US20130233964A1

    公开(公告)日：2013-09-12

    申请号：US13413696

    申请日：2012-03-07

    Applicant: Adam Woodworth ,  James Peverill

    Inventor： Adam Woodworth ,  James Peverill

    IPC: B64C37/02 ,  H02G11/00 ,  G05D1/00 ,  B64D25/00 ,  B64D17/80

    CPC classification number: B64C39/022 ,  B64C9/00 ,  B64C25/58 ,  B64C27/006 ,  B64C27/20 ,  B64C37/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/143 ,  B64C2201/148 ,  B64D17/80 ,  B64F3/02 ,  G05D1/0866 ,  G05D1/104 ,  H02G11/00

    Abstract: A tethered unmanned aerial vehicle (“UAV”) may be outfitted with a sensor payload for data gathering. The tethered UAV may be tethered to a ground station for constricting the flight space of the UAV while also providing the option for power delivery and/or bidirectional communications. The tethered UAV's flight path may be extended by introducing one or more secondary UAVs that cooperate to extend the horizontal flight path of a primary UAV. The ground station, which may be coupled with the tethered aerial vehicle, may comprise a listening switch configured to determine a condition of the tether such that the supply of power to the tether may be terminated when tether damage or a tether severance is detected.

    Abstract translation: 系绳无人机（“UAV”）可以装备有用于数据采集的传感器有效载荷。 系缚的UAV可以被绑在地面站上，用于收缩无人机的飞行空间，同时还提供功率传送和/或双向通信的选项。 可以通过引入一个或多个辅助UAV以扩展主UAV的水平飞行路径来扩展系留的UAV的飞行路径。 可以与系留式航空器耦合的地面站可以包括侦听开关，其被配置为确定系绳的状况，使得当检测到系绳损伤或系绳断开时，可以终止对系绳的供电。

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