Fiber Laser Arrangement Having A High Beaming Power
    1.
    发明申请
    Fiber Laser Arrangement Having A High Beaming Power 有权
    具有高打火功率的光纤激光器排列

    公开(公告)号:US20090097508A1

    公开(公告)日:2009-04-16

    申请号:US12252107

    申请日:2008-10-15

    IPC分类号: H01S3/00

    摘要: A fiber laser arrangement having a high beaming power includes a plurality of continuously operating coherent individual fiber lasers. Pumping energy generated by a common master oscillator operated in the longitudinal mode is distributed to the fiber lasers by way of a fiber splitter, in a branched manner. An integrated electro-optical phase shifter is assigned to each individual fiber laser, and can be controlled by an electronic control system. By appropriate displacements of the optical phases in individual phases of the fiber laser arrangement atmospheric turbulence effects on the propagation path of the laser radiation to a target are compensated in order to obtain an optimal focusing of the entire laser radiation onto the remote target.

    摘要翻译: 具有高光束功率的光纤激光装置包括多个连续工作的相干单个光纤激光器。 由纵向模式工作的公共主振荡器产生的泵浦能量以分支方式通过光纤分离器分配给光纤激光器。 集成的电光移相器被分配给每个单独的光纤激光器,并且可以由电子控制系统控制。 通过在光纤激光器布置的各个相位中的光学相位的适当偏移来补偿对激光辐射到目标物的传播路径的大气湍流效应,以便获得整个激光辐射到远程目标的最佳聚焦。

    Unmanned missile and method for determining the position of an unmanned missile which may be uncoupled from an aircraft
    2.
    发明申请
    Unmanned missile and method for determining the position of an unmanned missile which may be uncoupled from an aircraft 有权
    用于确定可能与飞机脱离联系的无人导弹的位置的无人导弹和方法

    公开(公告)号:US20080035785A1

    公开(公告)日:2008-02-14

    申请号:US11705536

    申请日:2007-02-13

    申请人: Michael Grabmeier

    发明人: Michael Grabmeier

    IPC分类号: F41G9/00

    CPC分类号: F41G7/007 F41G7/346

    摘要: An unmanned missile which may be uncoupled from a preferably propelled aircraft has a navigation and control device which has a receiver for position determination signals. The receiver is electrically connected to a first antenna, and receives signals collected by the first antenna and transmits same as position determination signals to the navigation and control device. The missile has an electrical signal input by which the missile is connected to the aircraft until it is uncoupled from the aircraft, and by which the missile is supplied with signals for position determination. The missile is provided with at least one additional antenna which is also electrically connected to the receiver.

    摘要翻译: 可以从优选的推进飞机脱离的无人驾驶导弹具有导航和控制装置,其具有用于位置确定信号的接收器。 接收机电连接到第一天线,并且接收由第一天线收集的信号并将其作为位置确定信号发送到导航和控制装置。 导弹具有电信号输入,导弹连接到飞机,直到飞行器与飞机脱离,并且向导弹提供信号以进行位置确定。 该导弹设置有至少一个另外的天线,该天线也与接收器电连接。

    Valve control unit for ramjet propulsion system as well as guided missile having such a valve control unit
    3.
    发明授权
    Valve control unit for ramjet propulsion system as well as guided missile having such a valve control unit 有权
    用于冲压式推进系统的阀门控制单元以及具有这种阀门控制单元的导弹

    公开(公告)号:US08341963B2

    公开(公告)日:2013-01-01

    申请号:US12041115

    申请日:2008-03-03

    IPC分类号: F02D41/00

    CPC分类号: F02K7/10 F02C7/22

    摘要: In a valve control unit for a ram jet propulsion system having a power unit space a valve for controlling a fuel quantity required to the propulsion system, and a valve adjusting unit which is constructed to be operable by means of an electronic control unit, the valve is combined with its valve adjusting unit and its electronic control unit to form a thermally insulated valve assembly. The valve assembly is configured for the arrangement in the power unit space.

    摘要翻译: 在用于具有动力单元空间的冲压喷气推进系统的阀控制单元中,用于控制推进系统所需的燃料量的阀以及构造成可通过电子控制单元操作的阀调节单元, 与其阀调节单元及其电子控制单元组合以形成隔热阀组件。 阀组件被配置用于动力单元空间中的布置。

    Method for Automatically Generating a Three-Dimensional Reference Model as Terrain Information for an Imaging Device
    4.
    发明申请
    Method for Automatically Generating a Three-Dimensional Reference Model as Terrain Information for an Imaging Device 有权
    用于自动生成三维参考模型作为成像装置的地形信息的方法

    公开(公告)号:US20110261162A1

    公开(公告)日:2011-10-27

    申请号:US13091703

    申请日:2011-04-21

    IPC分类号: H04N13/02

    摘要: A method for automatically generating a three-dimensional reference model as terrain information for a seeker head of an unmanned missile. A three-dimensional terrain model formed from model elements obtained with the aid of satellite and/or aerial reconnaissance is provided. Position data of the imaging device at least at one planned position and a direction vector from the planned position of the imaging device to a predetermined target point in the three-dimensional terrain model are provided. A three-dimensional reference model of the three dimensional terrain model is generated that incorporates only those model elements and sections of model elements from the terrain model, which in the viewing direction of the direction vector from the planned position of the imaging device, are not covered by other model elements and/or are not located outside the field of view of the imaging device.

    摘要翻译: 一种用于自动生成三维参考模型作为无人导弹的寻求者头部的地形信息的方法。 提供了由借助卫星和/或空中侦察获得的模型元素形成的三维地形模型。 提供了至少在一个预定位置处的成像装置的位置数据和从成像装置的规划位置到三维地形模型中的预定目标点的方向矢量。 生成三维地形模型的三维参考模型,其中仅包含来自地形模型的模型元素和模型元素的截面,其在来自成像装置的计划位置的方向向量的观察方向上不是 被其他模型元件覆盖和/或不位于成像装置的视场外。

    Valve Control Unit for Ramjet Propulsion System as well as Guided Missile Having Such a Valve Control Unit
    6.
    发明申请
    Valve Control Unit for Ramjet Propulsion System as well as Guided Missile Having Such a Valve Control Unit 有权
    用于拉姆喷气推进系统的阀门控制单元以及具有这种阀门控制单元的导向导弹

    公开(公告)号:US20080264385A1

    公开(公告)日:2008-10-30

    申请号:US12041115

    申请日:2008-03-03

    IPC分类号: F02D41/00

    CPC分类号: F02K7/10 F02C7/22

    摘要: In a valve control unit for a ram jet propulsion system having a power unit space a valve for controlling a fuel quantity required to the propulsion system, and a valve adjusting unit which is constructed to be operable by means of an electronic control unit, the valve is combined with its valve adjusting unit and its electronic control unit to form a thermally insulated valve assembly. The valve assembly is configured for the arrangement in the power unit space.

    摘要翻译: 在用于具有动力单元空间的冲压喷气推进系统的阀控制单元中,用于控制推进系统所需的燃料量的阀以及构造成可通过电子控制单元操作的阀调节单元, 与其阀调节单元及其电子控制单元组合以形成隔热阀组件。 阀组件被配置用于动力单元空间中的布置。

    DEVICE FOR LAUNCHING UNMANNED MISSILES FROM AN AIRCRAFT
    7.
    发明申请
    DEVICE FOR LAUNCHING UNMANNED MISSILES FROM AN AIRCRAFT 有权
    从飞机上发射无人机的装置

    公开(公告)号:US20080105112A1

    公开(公告)日:2008-05-08

    申请号:US11766343

    申请日:2007-06-21

    申请人: Michael Grabmeier

    发明人: Michael Grabmeier

    IPC分类号: B64D1/12

    CPC分类号: B64D1/12 B64C2201/206

    摘要: A device for launching unmanned missiles from an aircraft with a pallet, on which at least one container is provided to receive a missile. The container has an upper container section that has a pylori for the suspended, detachable support of the missile. The container has a lower container section that is embodied as a support area for the missile.

    摘要翻译: 用于从具有托盘的飞机发射无人导弹的装置,其上提供至少一个容器以接收导弹。 容器具有上部容器部分,其具有用于导弹的悬挂的可分离支撑件的幽门。 容器具有较低的容器部分,其被实施为导弹的支撑区域。

    Antenna elements for a missile
    8.
    发明授权
    Antenna elements for a missile 失效
    天线元素为导弹

    公开(公告)号:US07030820B2

    公开(公告)日:2006-04-18

    申请号:US10475488

    申请日:2002-04-25

    申请人: Axel Stiller

    发明人: Axel Stiller

    IPC分类号: H01Q1/28

    CPC分类号: H01Q13/085 F41G7/306

    摘要: The invention relates to antenna elements for the UHF and VHF range for antennas of an airborne vehicle with empennage parts. These antenna elements are integrated into the empennage parts (L) which are made of a dielectric material and are configured in such a way that they radiate directionally broadband in flight direction. The empennage parts are made, for example, of ceramic, and the antenna elements are embedded therein or are applied to their surface.The antenna elements (A) are preferably expanding Vivaldi-type slot radiators that are halved along their axis of symmetry and use the airborne vehicle (F) as an electrical mirror.Arranging the antenna elements in the area of the rudder maximizes both the aperture and the distance between the phase centers of the individual elements, but no additional volume is required for the antennas.

    摘要翻译: 本发明涉及用于具有尾翼部件的机载车辆的天线的UHF和VHF范围的天线元件。 这些天线元件集成到由电介质材料制成的尾翼部件(L)中,并且被配置成使得它们在飞行方向上辐射定向宽带。 尾翼部件例如由陶瓷制成,并且天线元件嵌入其中或施加到其表面。 天线元件(A)优选是扩展的Vivaldi型槽式散热器,其沿其对称轴线减半,并使用机载车辆(F)作为电反射镜。 在方向舵区域内布置天线元件使孔径和各个元件的相位中心之间的距离最大化,但是天线不需要额外的体积。

    Missile for detecting and combatting enemy helicopters
    9.
    发明授权
    Missile for detecting and combatting enemy helicopters 失效
    用于侦察和对抗敌方直升机的导弹

    公开(公告)号:US06007020A

    公开(公告)日:1999-12-28

    申请号:US811290

    申请日:1997-03-04

    摘要: A missile for detecting and combatting enemy helicopters has an infrared homing head with an infrared lens and infrared sensor that will emit electrical signals, depending on incident infrared radiation, and the sensor is designed as a two-dimensional detector matrix consisting of a number of punctiform detector cells arranged essentially in the focal plane of the infrared lens. The homing head includes an arrangement for acquiring a target and determining the type of target from the target information by individually scanning each of the detector cells quickly one after another by evaluating the amplitude and frequency of the electrical signals. The determination includes determining the relative position of the target to the optical axis of the homing head and the homing head will then steer the missile to hit the target. To improve the target acquisition and recognition phase, the matrix detector can be periodically swung around the axis of the flight path of the missile and, after target pick-up, is stabilized to lock on any helicopter to initiate and carry out the target-type recognition.

    摘要翻译: 用于检测和对付敌方直升机的导弹具有红外导向头,其具有红外透镜和红外传感器,其将根据入射的红外辐射发射电信号,并且传感器被设计为由许多点状构成的二维检测器矩阵 检测器单元基本上布置在红外透镜的焦平面中。 归属头包括用于获取目标的装置,并且通过对电信号的幅度和频率进行评估,逐个地逐个扫描每个检测器单元,从目标信息确定目标的类型。 确定包括确定目标相对于归位头的光轴的相对位置,并且归位头然后引导导弹击中目标。 为了改善目标获取和识别阶段,矩阵检测器可以围绕导弹的飞行路径的轴定期摆动,并且在目标拾取之后被稳定以锁定任何直升机以启动并执行目标类型 承认。