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    METHOD AND APPARATUS FOR RETRIEVING A HOVERING AIRCRAFT
    281.
    发明申请
    METHOD AND APPARATUS FOR RETRIEVING A HOVERING AIRCRAFT 有权
    检测飞机的方法和装置

    公开(公告)号：US20140061378A1

    公开(公告)日：2014-03-06

    申请号：US13717147

    申请日：2012-12-17

    Applicant: Aerovel Corporation

    Inventor： Brian T. McGeer ,  Andreas H. von Flotow ,  Corydon C. Roeseler

    IPC: B64F1/02 ,  B64F1/04 ,  B64F5/00

    CPC classification number: B64F1/02 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/182 ,  B64F1/04 ,  B64F5/00

    Abstract: For retrieval of a hovering aircraft, a cable, bar, or similar fixture is suspended in an approximately horizontal orientation across the retrieval area between two well-separated supports. The aircraft slowly flies into this fixture, which then slides along the aircraft in a direction approximately parallel with the aircraft's thrust line. This leads to the aircraft becoming fastened to the fixture by an interceptor or aircraft capturer, which in alternative embodiments are respectively on the aircraft or the fixture or both. Thrust is then reduced, and the aircraft comes to rest hanging from the fixture for subsequent removal. Retrieval is thus accomplished with simple and economical apparatus, light and unobtrusive elements on the aircraft, low risk of damage, and only moderate piloting accuracy.

    Abstract translation: 为了检索悬停的飞行器，电缆，杆或类似的固定装置在两个分离好的支撑件之间的整个区域上以大致水平的方向悬挂。 飞机慢慢地飞入这个固定装置，然后沿着与飞机的推力线大致平行的方向沿飞机滑动。 这导致飞行器通过拦截器或飞行器捕获器被固定到固定装置上，在替代实施例中飞行器或飞机捕获器分别在飞行器或固定装置上或两者上。 然后减小推力，飞机从固定装置上休息，以便随后拆卸。 因此，在飞机上使用简单经济的装置，轻便和不引人注意的元件来实现检索，损坏风险低，而且只有适度的驾驶准确性。

    Radio controlled vehicle, remote controller and methods for use therewith
    282.
    发明授权
    Radio controlled vehicle, remote controller and methods for use therewith 有权
    无线电控制车辆，遥控器及其使用方法

    公开(公告)号：US08649918B2

    公开(公告)日：2014-02-11

    申请号：US13688886

    申请日：2012-11-29

    Applicant: Katherine C. Stuckman ,  Michael D. Reynolds

    Inventor： Katherine C. Stuckman ,  Michael D. Reynolds

    IPC: G05D1/00

    CPC classification number: G05D1/0022 ,  A63H27/004 ,  A63H27/02 ,  A63H27/12 ,  A63H30/04 ,  A63H31/10 ,  B64C19/00 ,  B64C27/57 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/146 ,  G05D1/0033 ,  G05D1/0202 ,  G05D1/0808

    Abstract: A radio controlled (RC) vehicle includes a receiver that is coupled to receive an RF signal from a remote control device, the RF signal containing command data in accordance with a first coordinate system, wherein the first coordinate system is from a perspective of the remote control device. A motion sensing module generates motion data based on the motion of the RC vehicle. A processing module transforms the command data into control data in accordance with a second coordinate system, wherein the second coordinate system is from a perspective of the RC vehicle. A plurality of control devices control the motion of the RC vehicle based on the control data.

    Abstract translation: 无线电控制（RC）车辆包括被耦合以从远程控制设备接收RF信号的接收机，所述RF信号包含根据第一坐标系统的命令数据，其中所述第一坐标系是从所述远程 控制装置 运动感测模块基于RC车辆的运动产生运动数据。 处理模块根据第二坐标系将命令数据转换成控制数据，其中第二坐标系是从RC车辆的角度来看的。 多个控制装置基于控制数据控制RC车辆的运动。

    ASYMMETRICAL SINGLE MAIN ROTOR UNMANNED AERIAL VEHICLE
    284.
    发明申请
    ASYMMETRICAL SINGLE MAIN ROTOR UNMANNED AERIAL VEHICLE 有权
    不对称单主转子无人驾驶车

    公开(公告)号：US20140008486A1

    公开(公告)日：2014-01-09

    申请号：US13532212

    申请日：2012-06-25

    Applicant: Mark R. Alber ,  Jessica Newman

    Inventor： Mark R. Alber ,  Jessica Newman

    IPC: B64C27/12 ,  B64C27/82 ,  B64C27/06

    CPC classification number: B64C27/12 ,  B64C27/06 ,  B64C27/82 ,  B64C39/024 ,  B64C2027/8218 ,  B64C2201/024

    Abstract: A single engine rotary wing aircraft is provided including a fuselage having a longitudinal first axis. A main rotor assembly is mounted to the fuselage for rotation about a second axis, perpendicular to the first axis. A tailboom is connected to an empennage. The tailboom is mounted to an end of the fuselage such that the tailboom is laterally offset from the first axis in a first direction. The rotary wing aircraft also includes a propulsion system. The single engine of the propulsion system is laterally offset from the first axis in a second direction opposite the first direction.

    Abstract translation: 提供了包括具有纵向第一轴线的机身的单个发动机旋翼飞行器。 主转子组件安装到机身上以围绕垂直于第一轴线的第二轴线旋转。 尾巴连接到一个尾翼。 尾杆安装到机身的一端，使得尾杆在第一方向上从第一轴线横向偏移。 旋翼飞机还包括推进系统。 推进系统的单个发动机在与第一方向相反的第二方向上与第一轴线横向偏移。

    Radio controlled aircraft, remote controller and methods for use therewith
    286.
    发明授权
    Radio controlled aircraft, remote controller and methods for use therewith 有权
    无线电控制飞机，遥控器和与其一起使用的方法

    公开(公告)号：US08380368B2

    公开(公告)日：2013-02-19

    申请号：US13471642

    申请日：2012-05-15

    Applicant: Katherine C. Stuckman ,  Michael D. Reynolds

    Inventor： Katherine C. Stuckman ,  Michael D. Reynolds

    IPC: G05D1/00 ,  G06F17/10

    CPC classification number: G05D1/0022 ,  A63H27/004 ,  A63H27/02 ,  A63H27/12 ,  A63H30/04 ,  A63H31/10 ,  B64C19/00 ,  B64C27/57 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/146 ,  G05D1/0033 ,  G05D1/0202 ,  G05D1/0808

    Abstract: A radio controlled (RC) aircraft includes a receiver that is coupled to receive an RF signal from a remote control device, the RF signal containing command data in accordance with a first coordinate system, wherein the first coordinate system is from a perspective of the remote control device. A motion sensing module generates motion data based on the motion of the RC aircraft. A processing module transforms the command data into control data in accordance with a second coordinate system, wherein the second coordinate system is from a perspective of the RC aircraft. A plurality of control devices control the motion of the RC aircraft based on the control data. In an embodiment, a remote control device commands the RC helicopter to substantially a hovering state when no force is applied to each of a plurality of spring-loaded interface devices.

    Abstract translation: 无线电控制（RC）飞机包括被耦合以从远程控制设备接收RF信号的接收机，所述RF信号包含根据第一坐标系统的命令数据，其中所述第一坐标系是从所述远程 控制装置 运动感测模块根据RC飞机的运动产生运动数据。 处理模块根据第二坐标系将命令数据转换成控制数据，其中第二坐标系是从RC飞机的角度来看的。 多个控制装置基于控制数据控制RC飞机的运动。 在一个实施例中，当没有力施加到多个弹簧加载的接口装置中的每一个时，远程控制装置命令RC直升机基本上是悬停状态。

    Towable aerovehicle system with automated tow line release
    287.
    发明授权
    Towable aerovehicle system with automated tow line release 有权
    牵引式飞行器系统具有自动拖线释放

    公开(公告)号：US08366037B2

    公开(公告)日：2013-02-05

    申请号：US12785420

    申请日：2010-05-21

    Applicant: John William Morris ,  Charles Jarnot

    Inventor： John William Morris ,  Charles Jarnot

    IPC: B65D3/00 ,  B65D47/00

    CPC classification number: B64C27/02 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/128 ,  B64D3/00

    Abstract: An unmanned, towable aerovehicle is described and includes a container to hold cargo, an autogyro assembly connected to the container and to provide flight characteristics, and a controller to control operation the autogyro assembly for unmanned flight. The container includes a connection to connect to a powered aircraft to provide forward motive force to power the autogyro assembly. In an example, the autogyro assembly includes a mast extending from the container, a rotatable hub on an end of the mast, and a plurality of blades connected to the hub for rotation to provide lift to the vehicle. In an example, an electrical motor rotates the blades prior to lift off to assist in take off. The electrical motor does not have enough power to sustain flight of the vehicle.

    Abstract translation: 描述了一种无人驾驶的可拖动的飞行器，并且包括容纳货物的容器，连接到容器并提供飞行特性的自动装配组件以及用于控制无人驾驶的自动装配组件的操作的控制器。 容器包括连接到动力飞机的连接，以提供向自动装配组件供电的向前动力。 在一个示例中，自动组件组件包括从容器延伸的桅杆，在桅杆的端部上的可旋转轮毂，以及连接到轮毂以便旋转以提供车辆升力的多个叶片。 在一个示例中，电动马达在升降之前旋转叶片以帮助起飞。 电动机没有足够的电力来维持车辆的飞行。

    ELECTRONIC DEVICE AND METHOD FOR CONTROLLING UNMANNED AERIAL VEHICLE
    289.
    发明申请
    ELECTRONIC DEVICE AND METHOD FOR CONTROLLING UNMANNED AERIAL VEHICLE 审中-公开
    用于控制无人机动车的电子装置和方法

    公开(公告)号：US20120089274A1

    公开(公告)日：2012-04-12

    申请号：US13110927

    申请日：2011-05-19

    Applicant: HOU-HSIEN LEE ,  CHANG-JUNG LEE ,  CHIH-PING LO

    Inventor： HOU-HSIEN LEE ,  CHANG-JUNG LEE ,  CHIH-PING LO

    IPC: G05D1/00 ,  B64C13/20

    CPC classification number: B64C39/024 ,  B64C2201/024 ,  B64C2201/146 ,  G05D1/0038 ,  G05D1/0044

    Abstract: An electronic device for controlling an unmanned aerial vehicle (UAV) displays a portion of a 3D virtual scene of a monitored area of the UAV on a screen, and displays a representation icon of the UAV on a preset position of the screen. The electronic device further converts an operation signal to a control signal, and sends the control signal to control movements of the UAV. After receiving flight data from the UAV, the electronic device recognizes movements of the UAV according to the flight data, and determines adjustments to the portion of the 3D virtual scene, to control displaying of the 3D virtual scene based on the recognized movements while maintaining the representation icon of the UAV on the preset position and maintaining a direction the user presumed to be viewing the 3D virtual scene the same as a flight orientation of the UAV.

    Abstract translation: 用于控制无人驾驶飞行器（UAV）的电子设备在屏幕上显示UAV的被监视区域的3D虚拟场景的一部分，并且在该屏幕的预设位置上显示UAV的表示图标。 电子设备还将操作信号转换为控制信号，并发送控制信号以控制UAV的移动。 在从UAV接收到飞行数据之后，电子设备根据飞行数据识别UAV的移动，并且确定对3D虚拟场景的部分的调整，以基于所识别的移动来控制3D虚拟场景的显示，同时保持 UAV在预置位置上的表示图标，并保持用户假定正在观看与无人机的飞行方向相同的3D虚拟场景的方向。

    Decision Aid Device for Assisting the Landing of an Aircraft on the Deck of a Ship
    290.
    发明申请
    Decision Aid Device for Assisting the Landing of an Aircraft on the Deck of a Ship 有权
    用于协助飞机在船上的着陆的决策辅助装置

    公开(公告)号：US20110118910A1

    公开(公告)日：2011-05-19

    申请号：US12945602

    申请日：2010-11-12

    Applicant: Rémi GEOFFROY ,  Patrick GARREC ,  Yannick THIRY ,  Patrick CAZAUX

    Inventor： Rémi GEOFFROY ,  Patrick GARREC ,  Yannick THIRY ,  Patrick CAZAUX

    IPC: G05D1/00

    CPC classification number: B64F1/18 ,  B64C2201/024 ,  B64C2201/146 ,  B64C2201/205 ,  G05D1/0684 ,  G08G5/0013 ,  G08G5/025

    Abstract: A device for aiding the deck-landing of an aircraft, the aircraft being controlled remotely from a mobile station, such as a ship, includes means for receiving data from the aircraft, notably attitudes of the aircraft, the aircraft hovering ready to land on deck, the deck-landing decision having to be taken under certain conditions that must all be met, the device including a computer making it possible to deliver temporal indicators indicating that all the conditions are met. The device includes a temporal gauge including a temporal graduation indicating mobile graphical zones representing the periods during which all the conditions are met for authorizing a deck-landing.

    Abstract translation: 一种用于辅助飞机的甲板着陆的装置，从诸如船舶等移动台远程控制的飞机包括用于从飞行器接收数据的手段，特别是飞机的态度，飞机翱翔准备着陆在甲板上 ，必须在必须满足的某些条件下采取甲板着陆决定，该装置包括使得能够传递指示满足所有条件的时间指示的计算机。 该装置包括时间计量器，其包括表示移动图形区域的时间分度，表示满足所有条件以批准甲板着陆的时段。

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