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    Distributed unmanned aerial vehicle architecture
    82.
    发明授权
    Distributed unmanned aerial vehicle architecture 有权
    分布式无人机架构

    公开(公告)号：US09273981B1

    公开(公告)日：2016-03-01

    申请号：US14709263

    申请日：2015-05-11

    Applicant: Unmanned Innovation, Inc.

    Inventor： Jonathan Downey ,  Bernard J. Michini ,  Brian Richman

    IPC: G01C23/00

    CPC classification number: H04L47/25 ,  B64C39/024 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/145 ,  B64D41/00 ,  B64D47/00 ,  B64D47/08 ,  G01C23/00 ,  G05D1/0022

    Abstract: Methods, systems, and apparatus, including computer programs encoded on computer storage media, for a distributed system architecture for unmanned air vehicles. One of the methods includes obtaining information identifying flight information of a UAV, with the flight information including flight phase information or a contingency condition associated with a flight critical module included in the UAV. The obtained information is analyzed, and one or more first payload modules are determined to enter a modified power state. Requests to enter the modified power state are caused to be transmitted to each determined payload module in the one or more first payload modules.

    Abstract translation: 方法，系统和装置，包括在计算机存储介质上编码的计算机程序，用于无人驾驶飞行器的分布式系统架构。 其中一种方法包括获得识别无人机的飞行信息的信息，其中飞行信息包括飞行相位信息或与包括在UAV中的飞行关键模块相关联的应急条件。 分析所获得的信息，并且确定一个或多个第一有效载荷模块进入修改的功率状态。 使得进入修改的功率状态的请求被发送到一个或多个第一有效载荷模块中的每个确定的有效载荷模块。

    UNMANNED AERIAL DEVICE AND METHOD FOR PERFORMING A LIGHTNING PROTECTION MEASUREMENT AT A WIND TURBINE
    83.
    发明申请
    UNMANNED AERIAL DEVICE AND METHOD FOR PERFORMING A LIGHTNING PROTECTION MEASUREMENT AT A WIND TURBINE 有权
    在风力涡轮机上执行防雷措施的无人驾驶装置和方法

    公开(公告)号：US20160047850A1

    公开(公告)日：2016-02-18

    申请号：US14824958

    申请日：2015-08-12

    Applicant: Availon GmbH

    Inventor： Marcel BRUINS ,  Jochen HOLLING

    IPC: G01R27/08 ,  G01R1/067

    CPC classification number: G01R27/08 ,  B64C2201/027 ,  B64C2201/126 ,  B64C2201/127 ,  F03D17/00 ,  F03D80/00 ,  F03D80/30 ,  F03D80/50 ,  F05B2260/80 ,  F05B2260/83 ,  F05B2270/8041 ,  G01R1/067 ,  G01R1/06705 ,  G01R31/282 ,  G01R31/2827 ,  Y02E10/721

    Abstract: The invention relates to an unmanned aerial device for performing a resistance, current and/or voltage measurement at an object, in particular a lightning protection measurement at a wind turbine, comprising a contact element with an electrically conductive contact area, which can be brought into contact with a surface of the object, in particular with a lightning protection receptor of a rotor blade, of a nacelle or of a tower of a wind turbine, and comprising an electrically conductive measurement cable, which, with a first end, is connected in an electrically conductive manner to the contact area, and, with a second end, can be connected to a resistance, current and/or voltage measuring device and/or a grounding contact of the object.

    Abstract translation: 本发明涉及一种用于在物体上执行电阻，电流和/或电压测量的无人驾驶空中装置，特别是涉及风力涡轮机的雷电保护测量，包括具有导电接触区域的接触元件，其可被带入 特别是与转子叶片的防雷接收器，机舱或风力涡轮机的塔架接触，并且包括导电测量电缆，其中第一端连接到 对接触区域的导电方式，并且具有第二端，可以连接到电阻，电流和/或电压测量装置和/或物体的接地触点。

    Multi-role aircraft with interchangeable mission modules
    84.
    发明授权
    Multi-role aircraft with interchangeable mission modules 有权
    具有可互换任务模块的多角色飞机

    公开(公告)号：US09221532B2

    公开(公告)日：2015-12-29

    申请号：US14205156

    申请日：2014-03-11

    Applicant: Abe Karem

    Inventor： Abe Karem

    IPC: B64C1/00 ,  B64C3/56 ,  B64C1/06 ,  B64C39/10 ,  B64C39/02 ,  B64D37/00 ,  B64C1/26

    CPC classification number: B64C39/10 ,  B64C1/00 ,  B64C1/0009 ,  B64C1/061 ,  B64C1/065 ,  B64C1/26 ,  B64C3/56 ,  B64C25/10 ,  B64C39/024 ,  B64C2001/0072 ,  B64C2039/105 ,  B64C2201/028 ,  B64C2201/126 ,  B64C2211/00 ,  B64D37/00 ,  Y02T50/12 ,  Y02T50/14 ,  Y02T50/43

    Abstract: A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections can be removably coupled and/or replaced during the operating life span of the aircraft. In preferred embodiments the aircraft core houses the propulsive engines, avionics, at least 80% of the fuel, and all of the landing gear. The aircraft core is preferably constructed with curved forward and aft composite spars, that transfer loads across the center section, while accommodating a mid-wing configuration. The aircraft core preferably has a large central cavity dimensioned to interchangeably carry an ordnance launcher, a surveillance payload, electronic countermeasures, and other types of cargo. Contemplated aircraft can be quite large, for example having a wing span of at least 80 ft.

    Abstract translation: 飞行可操作的，真正模块化的飞机具有飞行器核心，一个或多个外翼构件，机身，驾驶舱，前后联轴器，尾翼和尾翼部分可在其运行寿命期间可拆卸地联接和/或更换 的飞机。 在优选实施例中，飞机核心容纳推进发动机，航空电子设备，至少80％的燃料和所有起落架。 飞机核心优选地构造有弯曲的前向和后部复合翼梁，其在中心部分处传递载荷，同时容纳中翼构造。 飞机核心优选地具有大的中心空间，其大小可互换地携带军械发射器，监视有效载荷，电子对抗措施和其他类型的货物。 考虑的飞机可能相当大，例如具有至少80英尺的翼展。

    OCEAN - AIR VEHICLE
    85.
    发明申请
    OCEAN - AIR VEHICLE 审中-公开
    海洋 - 空中航空

    公开(公告)号：US20150367938A1

    公开(公告)日：2015-12-24

    申请号：US14263944

    申请日：2014-04-28

    Applicant: AeroVironment Inc.

    Inventor： Thomas Zambrano ,  Tyler MacCready

    IPC: B64C35/00 ,  B64C39/02 ,  B63G8/00 ,  B63H5/125

    CPC classification number: B64C35/005 ,  B63G8/001 ,  B63G2008/004 ,  B63G2008/005 ,  B63H5/125 ,  B64C35/00 ,  B64C35/003 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/126 ,  B64C2201/14 ,  B64C2201/165

    Abstract: A vehicle having a wing, a forward propeller configured for forward flight, and an aft propeller configured for submerged travel in a rearward direction. The vehicle center of mass is aft of its floating center of buoyancy, and center of mass and the floating center of buoyancy lie between the first and second propellers. The vehicle has a natural floating orientation in which the vehicle, while floating, has its first propeller located in the air and positioned for initiating airborne flight in a forward direction, and in which the vehicle has its second propeller located in the liquid and positioned for initiating submerged travel in a rearward direction.

    Abstract translation: 一种具有机翼，配置成向前飞行的前进螺旋桨的车辆和构造成沿向后方向淹没行进的后推螺旋桨。 车辆中心处于其浮动浮力中心，质心和浮力浮动中心位于第一和第二螺旋桨之间。 车辆具有自然浮动方向，其中车辆在浮动时具有其第一螺旋桨位于空气中并且被定位成用于沿向前方向起飞空中飞行，并且其中车辆具有位于液体中的第二螺旋桨并且定位成 启动向后方向的潜水行进。

    REMOTELY CONTROLLED MICRO/NANOSCALE AERIAL VEHICLE COMPRISING A SYSTEM FOR TRAVELING ON THE GROUND, VERTICAL TAKEOFF, AND LANDING
    89.
    发明申请
    REMOTELY CONTROLLED MICRO/NANOSCALE AERIAL VEHICLE COMPRISING A SYSTEM FOR TRAVELING ON THE GROUND, VERTICAL TAKEOFF, AND LANDING 有权
    远程控制的微型/纳米级空中客车包含在地面，垂直起落和行驶的行驶系统

    公开(公告)号：US20140319266A1

    公开(公告)日：2014-10-30

    申请号：US14008707

    申请日：2012-03-27

    Applicant: Jean-Marc Moschetta ,  Chinnapat Thipyopas

    Inventor： Jean-Marc Moschetta ,  Chinnapat Thipyopas

    IPC: B64C39/02 ,  B64C19/00 ,  B64C25/36

    CPC classification number: B64C39/028 ,  B64C25/36 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/086 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/126 ,  B64C2201/165 ,  B64C2201/18 ,  B64D45/06

    Abstract: A microscale radio-controlled aerial micro-drone vehicle, having a fixed wing (as opposed to a rotary wing) having a propulsion device the vehicle including wheels for traveling on the ground, which are attached to the side ends of a section of the wing. The rotational axis Y1 of the wheels being located in front of the center of gravity of the micro-drone, the center of gravity of the micro-drone being located in front of the aerodynamic center of the micro-drone. The rotational axis Y1 of the wheels being aligned with the thrust axis of the propulsion device and the wheels are sized such that the radius D/2 thereof is greater than the distance between the rotational axis Y1 of the wheels and the trailing edge of the wing.

    Abstract translation: 具有具有推进装置的固定翼（相对于旋转翼）的微型无线电遥控的空中微型无人驾驶车辆，该车辆包括用于在地面上行驶的车轮，其附接到翼的一部分的侧端 。 车轮的旋转轴线Y1位于微型无人驾驶飞机重心的前方，微型无人机的重心位于微型无人机的空气动力学中心的前方。 车轮的旋转轴线Y1与推进装置的推力轴线对准，车轮的尺寸使其半径D / 2大于车轮的旋转轴线Y1和机翼的后缘之间的距离 。

    VEHICLE WITH AERIAL AND GROUND MOBILITY
    90.
    发明申请
    VEHICLE WITH AERIAL AND GROUND MOBILITY 有权
    具有航空和地面机动性的车辆

    公开(公告)号：US20140061362A1

    公开(公告)日：2014-03-06

    申请号：US13846074

    申请日：2013-03-18

    Applicant: DRAGANFLY INNOVATIONS INC.

    Inventor： Orville OLM ,  Greg WOOD ,  Zenon DRAGAN

    IPC: B60F5/00

    CPC classification number: B64C37/00 ,  B60B1/00 ,  B60F5/02 ,  B60Y2200/80 ,  B64C39/005 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/162

    Abstract: A combination rotor and wheel assembly for an unmanned vehicle with ground and aerial mobility has a rotor arm adapted to be attached at an inner end thereof to a vehicle body. A rotor is rotatably connected to an outer end of the rotor arm about a rotor axis, and a rotor drive mounted on the rotor arm rotates the rotor such that the rotor exerts an upward lift force on the rotor arm. An open spoked wheel is rotatably connected about the rotor axis independent of the rotor The diameter of the wheel is greater than that of the rotor, and a bottom edge of the wheel is below the rotor. A wheel drive rotates the wheel. Vehicles can have various numbers and orientations of the rotor and wheel assembly to provide aerial and ground mobility.

    Abstract translation: 用于具有地面和空中移动性的无人驾驶车辆的组合转子和车轮组件具有适于在其内端附接到车体的转子臂。 转子围绕转子轴线可旋转地连接到转子臂的外端，并且安装在转子臂上的转子驱动器使转子旋转，使得转子在转子臂上施加向上的升力。 开放式的轮轮围绕转子轴线可旋转地连接，与转子无关。轮的直径大于转子的直径，并且车轮的底部边缘在转子下方。 轮驱动器旋转车轮。 车辆可以具有转子和车轮组件的各种数量和方向，以提供空中和地面的移动性。

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