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    POWER SAFETY INSTRUMENT
    72.
    发明公开
    POWER SAFETY INSTRUMENT 有权
    电力安全仪器

    公开(公告)号：EP2985226A1

    公开(公告)日：2016-02-17

    申请号：EP15174684.9

    申请日：2010-12-22

    Applicant: Bell Helicopter Textron Inc.

    Inventor： McCollough, James M. ,  Oltheten, Erik ,  Lappos, Nicholas

    IPC: B64D43/00 ,  B64C27/04

    CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

    Abstract: A power safety system (301) is configured to provide power information in an aircraft (101). The power safety system (301) includes a power safety instrument (303) having a power required indicator (311) and a power available indicator (313), each being located on a display. A position of the power required indicator (311) and the power available indicator (313) represent the power available and power required to perform a hover flight maneuver. The power safety system (301) may be operated in a flight planning mode or in a current flight mode. The power safety system (301) uses at least one sensor (309) to measure variables having an effect on the power required and the power available.

    Abstract translation: 电力安全系统（301）被配置为在飞机（101）中提供电力信息。 电力安全系统（301）包括具有电力需求指示器（311）和电力可用指示器（313）的电力安全仪器（303），每个电力安全仪器位于显示器上。 功率需求指示符（311）和功率可用指示符（313）的位置表示执行悬停飞行操纵所需的功率和功率。 电力安全系统（301）可以以飞行计划模式或当前飞行模式运行。 电力安全系统（301）使用至少一个传感器（309）来测量对所需电力和可用电力具有影响的变量。

    APPARATUS FOR UNMANNED VEHICLES
    73.
    发明公开
    APPARATUS FOR UNMANNED VEHICLES 审中-公开
    DEVICE FOR无人驾驶汽车

    公开(公告)号：EP2655185A1

    公开(公告)日：2013-10-30

    申请号：EP11807659.5

    申请日：2011-12-14

    Applicant: BAE Systems Plc.

    Inventor： BEGGS, Kevin, William ,  AXFORD, Richard, Descond, Joseph

    IPC: B64C39/02 ,  F42B12/36 ,  F42C15/42

    CPC classification number: F42B12/365 ,  B64C2201/121 ,  B64C2201/146 ,  F42C15/42

    Abstract: Apparatus and a method performed by the apparatus, the apparatus being wholly or partially mounted on an unmanned vehicle (e.g. an unmanned air vehicle) and arranged to act upon a payload (e.g. a lethal effector), the payload being mounted on the unmanned vehicle and, under an action of the apparatus, able to be changed from being in a first state to being in a second state, the method comprising: receiving an instruction that the unmanned vehicle, with the payload mounted thereon, is to travel to a location; determining that the payload is in the first state; and responsive to the step of determining that the payload is in the first state: opposing the payload being changed to being in the second state; and providing, for an entity remote from the unmanned vehicle, an indication that the payload is in the first state.

    A flying machine
    76.
    发明公开
    A flying machine 审中-公开
    Fluggerät

    公开(公告)号：EP1502852A1

    公开(公告)日：2005-02-02

    申请号：EP04017945.9

    申请日：2004-07-29

    Applicant: C.R.F. Società Consortile per Azioni

    Inventor： Perlo, Pietro ,  Bollea, Denis ,  Pairetti, Bartolo ,  Alacqua, Stefano ,  Finizio, Roberto ,  Carvignese, Cosimo ,  Repetto, Piermario ,  Innocenti, Gianfranco

    IPC: B64C27/20 ,  A63H29/22 ,  B64C39/02

    CPC classification number: B64C39/024 ,  A63H27/12 ,  A63H29/22 ,  B64C27/20 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/146

    Abstract: The flying machine (1) comprises

    a supporting structure (2) including a central rotational support (3) having a vertical axis connected to an essentially horizontal, preferably annular, peripheral support part (4), coaxial with the central support (3),
    at least one upper rotor (6) including a central hub (7) rotatable about the axis of the central support (3) of the supporting structure (2), an outer channel-section ring (8) supported by the peripheral part (4) of the supporting structure (2) by contactless suspension means (23-27), preferably magnetic suspension means, and a plurality of blades (9) which extend from the hub (7) to the channel-section ring (8) and which are inclined with respect to the horizontal plane; and
    motor devices (40-43; 50-53) carried at least partially by the peripheral part (4) of the supporting structure (2) and operable to cause rotation of the rotor (6) with respect to this structure (2) in a predetermined direction.

    Abstract translation: 飞行器（1）包括支撑结构（2），其包括中心旋转支撑件（3），该中心旋转支撑件具有连接到与中心支撑件（3）同轴的基本上水平的，优选环形的外围支撑部分（4）的垂直轴线， 至少一个上转子（6），包括可围绕所述支撑结构（2）的中心支撑件（3）的轴线旋转的中心毂（7），由所述周边部分（4）支撑的外通道部分环 ）由非接触式悬挂装置（23-27），优选磁悬浮装置和从轮毂（7）延伸到通道截面环（8）的多个叶片（9）支撑结构（2），并且 相对于水平面倾斜; 以及至少部分地由所述支撑结构（2）的周边部分（4）承载并可操作以使转子（6）相对于该结构（2）旋转的马达装置（40-43; 50-53） 预定的方向。

    Tracking device
    77.
    发明公开
    Tracking device 有权
    Zielsuchende Vorrichtung

    公开(公告)号：EP1209546A1

    公开(公告)日：2002-05-29

    申请号：EP01127755.5

    申请日：2001-11-21

    Applicant: Xerox Corporation

    Inventor： Yim, Mark H.

    IPC: G05D1/12 ,  B64C11/48 ,  A63H27/00

    CPC classification number: B64C27/10 ,  B64C13/16 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/127 ,  B64C2201/145 ,  B64C2201/146 ,  Y02T50/44

    Abstract: A tracking device includes a motor, top and bottom propellers of opposite sense attached to the stator and rotor of the motor for rotation in opposite directions. Target sensors are provided on the propellers and signals from the target sensors are supplied to a controller that controls the rotation of the motor and the propellers. The tracking device also includes a power supply for the motor and the controller.

    Abstract translation: 跟踪装置包括具有相反方向的马达，顶部和底部螺旋桨，其连接到马达的定子和转子，以沿相反的方向旋转。 目标传感器提供在螺旋桨上，并且来自目标传感器的信号被提供给控制器以控制马达和螺旋桨的旋转。 跟踪装置还包括用于电动机和控制器的电源。

    공중 정찰용 무인 비행체, 이를 이용한 무인 방어 시스템 및 방법
    79.
    发明授权
    공중 정찰용 무인 비행체, 이를 이용한 무인 방어 시스템 및 방법 有权
    空中侦察用无人机，无人防御系统及使用该装置的方法

    公开(公告)号：KR101738553B1

    公开(公告)日：2017-06-08

    申请号：KR1020160109746

    申请日：2016-08-29

    Applicant: (주)세이프어스드론

    Inventor： 강종수

    IPC: B64C39/02 ,  B64D47/08 ,  B64D43/00 ,  G06T7/00 ,  F41H11/00 ,  F41H13/00

    CPC classification number: B64C39/02 ,  B64D43/00 ,  B64D47/08 ,  F41H11/00 ,  F41H13/00 ,  G06T7/00 ,  B64C39/024 ,  B64C2201/121 ,  B64C2201/127 ,  B64C2201/146 ,  G06T7/0002

    Abstract: 영상정보를기반으로객체감지및 객체타격을수행하는공중정찰용무인비행체, 이를이용한무인방어시스템및 방법이개시된다. 본공중정찰용무인비행체는기설정된영역에대한영상정보를수집하는영상정보수집부; 및상기수집된영상정보를기반으로상기기설정된영역에존재하는객체를감지하는제어부;를포함한다. 이에의해, 무인비행체를이용하여정찰및 감시를지속적으로수행하여아군및 적군의이동현황에관한정확한정보의수집및 전달함으로써, 적군으로추정되는객체감지및 피아식별을수행하고, 적군으로추정된객체의타격을수행함으로써, 전쟁발생시 다양한작전을수행할수 있으며, 이를통해아군의피해를현저히줄일수 있다.

    Abstract translation: 无人驾驶用于执行基于该图像信息侦察机，无人防御系统和方法使用相同的对象检测和对象命中中公开。 空中侦察无人机包括图像信息收集单元，用于收集预定区域的图像信息; 以及控制单元，用于基于收集的图像信息检测存在于预定区域中的物体。 在该布置中，由收集和大约友好和敌人移动进入并通过使用无人驾驶飞行器执行侦察和监视连续正确的信息传输，执行对象被估计为敌人检测和IFF，估计敌方目标 通过进行打击，并且可以在战争的情况下执行各种操作的，它可以降低显著通过它同盟的损坏。

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