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    • 1. 发明授权
    • Fiber optic guidance system for laser guided missiles
    • 激光导弹光纤引导系统
    • US5784156A
    • 1998-07-21
    • US752326
    • 1996-11-19
    • James E. Nicholson
    • James E. Nicholson
    • F41G7/22G01S3/783G01B11/26F41G7/00
    • F41G7/226F41G7/2293G01S3/783
    • The invention provides a system and a method for determining the direction to a radiating source, for use by a vehicle guidance system, in which optical fibers are used to both collect and transmit optical signals in which the vehicle is preferably intended to home in on its target. The optical fibers disclosed herein require no separate collection optics, but instead directly collect incident radiation arriving at one end of the optical fiber for transmission to a photodiode detector coupled to the distal end. Preferably the radiation is laser radiation radiating from a target in relation to which the vehicle is guided, and preferably the vehicle is a guided missile. Elimination of collection optics reduces the complexity and cost of the apparatus and provides an unexpected increase in and selectability of the accuracy of directional determination by the system. The system includes an array of apertures disposed in selected, non-uniform locations on the vehicle. Each aperture contains a set of fibers, including start and stop fibers. The fibers receive incoming radiation, transmit the radiation as optical signals to start and stop detectors. The detectors measure a signal strength and a property related to the length of the start and stop fibers through which the optical signals have been transmitted, and provide output indicative of the signal strength and the property to a microprocessor. The microprocessor is programmed to calculate the direction to the radiation source relative to the vehicle, and to provide this information to a vehicle guidance and control system.
    • 本发明提供了一种用于确定辐射源的方向以供车辆引导系统使用的系统和方法,其中光纤用于收集和发送光信号,其中车辆优选地将其置于家中 目标。 本文公开的光纤不需要单独的收集光学器件,而是直接收集到达光纤一端的入射辐射,以传输到耦合到远端的光电二极管检测器。 优选地,辐射是从相对于车辆被引导的目标辐射的激光辐射,并且优选地,车辆是导弹。 消除采集光学器件降低了设备的复杂性和成本,并且提供了系统的方向确定精度的意外增加和可选择性。 该系统包括设置在车辆上的选定的非均匀位置的孔阵列。 每个孔包含一组纤维,包括起始和停止纤维。 纤维接收进入的辐射,将辐射作为光信号传输到启动和停止检测器。 检测器测量信号强度和与发送光信号的起始和停止光纤的长度相关的特性,并向微处理器提供指示信号强度和特性的输出。 微处理器被编程为计算相对于车辆的辐射源的方向,并将该信息提供给车辆引导和控制系统。
    • 4. 发明授权
    • Multiple squib assembly
    • 多重爆管装配
    • US5631439A
    • 1997-05-20
    • US478224
    • 1995-06-07
    • Bradley T. SalleeBeryl W. Cotton, III
    • Bradley T. SalleeBeryl W. Cotton, III
    • F42B5/08F42C19/00F42C11/00
    • F42B5/08F42C19/00
    • A multiple squib assembly is provided for use in a chaff deployment system. A method of manufacture is also provided. The assembly of this invention represents an improvement over prior art squib assemblies, such as the BBU48. In preferred embodiments, the assembly comprises a brass base plate, a pair of squibs, a center contact connected to the squibs, and a zener diode connected between one of the squibs and the baseplate. All of those components are retained within a molded rubber or plastic body, which is shaped to hold the components in the desired relative position and to form sealing elements around each of the squibs. A reliable, integral assembly is thus provided using a minimal number of parts and electrical connections. In alternative embodiments, a larger number of squibs may be incorporated into the assembly, and alternative discrimination elements may be employed.
    • 提供了一种用于谷壳部署系统中的多重爆管组件。 还提供了一种制造方法。 本发明的组件代表了现有技术的点火组件(例如BBU48)的改进。 在优选实施例中,组件包括黄铜底板,一对点火器,连接到爆管的中心触点,以及连接在其中一个点火器和底板之间的齐纳二极管。 所有这些部件都保持在模制的橡胶或塑料体内,其被成形为将部件保持在期望的相对位置并且形成围绕每个爆管的密封元件。 因此,使用最少数量的部件和电气连接提供了可靠的整体组件。 在替代实施例中,可以将大量的爆管引入到组件中,并且可以采用替代的识别元件。
    • 6. 发明授权
    • Constant width, adjustable grip, staple apparatus and method
    • 恒定宽度,可调握柄,装订装置和方法
    • US5695524A
    • 1997-12-09
    • US538001
    • 1995-10-02
    • Mark KelleyPhil McDuffie
    • Mark KelleyPhil McDuffie
    • A61B17/064A61B17/068A61B17/10A61B17/04
    • A61B17/10A61B17/0644A61B17/0686Y10S227/902Y10S411/92
    • A staple and stapler for injecting the staple in a manner so that the staple maintains a near constant width upon penetration of material to be joined and during staple closure/forming such that material perturbation and staple to staple spacing may be minimized. The staple has a rectilinear bridge part from which depend oppositely positioned side parts and from the side parts a pair of straight legs. In a preferred embodiment, the oppositely positioned side parts consist of a proximal arcuate section attached to the bridge part and an oppositely directed distal arcuate section attached to the legs. The legs may have sharpened points. Also disclosed is a stapler adapted to force the oppositely directed distal arcuate sections outward, in one embodiment, thereby forcing a reaction of the legs of the staple to face each other in linear alignment and form a closed staple. The unpreloaded fully-formed staple may be deformed in situ by means of a preload part on a cam slide so as to create a U-shaped central portion for the compression of captured material. Alternatively, a preformed staple with the U-shaped central portion may also be used.
    • 一种钉和订书机,用于以这样的方式注射订书钉,使得订书钉在待接合的材料穿透时以及在缝合期间/成型期间保持接近恒定的宽度,使得材料扰动和订书针至订书钉的间隔可以最小化。 订书钉具有直线桥部分,从该位置的相对定位的侧部和从侧面部分是一对直的腿。 在优选实施例中,相对定位的侧面部分由附接到桥接部分的近端弧形部分和附接到腿部的相反方向的远端弧形部分组成。 腿可能有磨尖点。 还公开了一种订书机,其在一个实施例中适合于将相对方向的远端弓形部分向外强制,由此迫使订书针的腿部以线性对准的方式彼此面对并形成封闭的订书钉。 未加载的完全成型的订书钉可以通过凸轮滑块上的预加载部分原位变形,以便形成用于压缩所捕获材料的U形中心部分。 或者,还可以使用具有U形中心部分的预制钉。
    • 8. 发明授权
    • Shaped-charge device with progressive inward collapsing jet
    • 具有逐渐向内折叠射流的成形装置
    • US5614692A
    • 1997-03-25
    • US497541
    • 1995-06-30
    • Ronald E. BrownMark E. Majerus
    • Ronald E. BrownMark E. Majerus
    • F42B1/028F42B1/02
    • F42B1/028
    • In a shaped-charge device, the liner is so shaped that bulges are formed in the jet without causing the jet to deviate from the central axis. The shaped-charge device includes a case defining an axisymmetrical forwardly-opening cavity uniformly disposed about a central axis; an axisymmetrical, homogeneous-material, liner of variable thickness defining a forwardly-opening cavity having a closed apex, with the cavity being uniformly disposed within the casing about the central axis; and explosive material symmetrically disposed between the casing and the liner. The liner is so shaped that in response to the explosive material being detonated to thereby explode, the liner is progressively collapsed inward by the exploding material to be formed into a fluid jet of the homogeneous liner material that is forwardly expelled at a varying velocity from the casing along the central axis, with the forward portion of the jet being squeezed from the apex of the collapsing liner. The rate of change of liner thickness with respect to liner axial position varies such that, after the formation of the forward portion of the jet, the velocity of the jet-forming material at at least one intermediate position within the jet varies so as to cause the material to bunch up to form a symmetrical bulge at each intermediate position within the jet, but not such that the velocity of the jet-forming material increases at any such intermediate position while the material is bunching up, thereby inhibiting the material from so bunching up as to cause the jet to deviate from the central axis.
    • 在成形装置中,衬套是这样的形状,使得在射流中形成凸起而不会使射流偏离中心轴线。 成形装置包括壳体,其限定围绕中心轴线均匀设置的轴对称正向开口空腔; 限定具有闭合顶点的向前开口腔的可变厚度的轴对称均匀材料衬里,其中空腔围绕中心轴线均匀地设置在壳体内; 和对称地设置在壳体和衬套之间的爆炸性材料。 内衬的形状是这样形状的:响应于爆炸材料被引爆而引起爆炸,衬套由于爆炸材料向内逐渐塌陷,以形成均匀衬垫材料的流体射流,该流体射流以不同速度向前排出 壳体沿着中心轴线,其中喷射器的前部从挤压衬套的顶点挤压。 衬套厚度相对于衬套轴向位置的变化率变化,使得在射流的前部形成之后,喷射形成材料在射流内的至少一个中间位置的速度变化,从而导致 这种材料在射流内的每个中间位置聚集形成对称的凸起,但不能使得在材料聚集时任何这样的中间位置喷射形成材料的速度增加,从而抑制材料的聚集 使飞机偏离中心轴。
    • 9. 发明授权
    • Inflatable truss frame
    • 充气桁架
    • US5311706A
    • 1994-05-17
    • US732810
    • 1991-07-19
    • Bradley Sallee
    • Bradley Sallee
    • E04C3/00E04C3/28
    • E04C3/28E04C3/005Y10S52/08
    • An inflatable truss frame member for use in the frame of a large inflatable device such as a ship or satellite decoy. A first embodiment, developed for use in satellite decoys, comprises three main inflatable tubes separated by shear load carrying interlacing inflatable tubes. The first embodiment may be manufactured by laminating two MYLAR sheets together using a triangular pattern of adhesive print to form a series of inflatable tubes. Excess material is removed from between the tubes and the edges of the MYLAR are bonded together forming a cylinder to complete the inflatable truss frame member. A second embodiment, developed for the heavier shear loading of ship decoys, comprises three main inflatable tubes separated by a shear load carrying web. The second embodiment may be manufactured by bonding an inner and outer tube made of MYLAR along arcuately spaced strips. The bonded MYLAR forms the separating web and unbonded MYLAR forms three inflatable tubes. Alternately, the second embodiment may be manufactured by separately forming three inflatable tubes and then bonding the separating web material to the inflatable tubes. Rigid stays or battens may be added between the three inflatable tubes when the separating web will not be strong enough to support the shear loading.
    • 一种用于大型充气装置如船或卫星诱饵的框架中的可充气桁架框架构件。 开发用于卫星诱饵的第一实施例包括三个主要的可充气管,其由承载交织的可充气管的剪切载荷分开。 第一实施例可以通过使用粘合剂印刷的三角形图案将两个MYLAR片层叠在一起而形成一系列可充气管来制造。 多余的材料从管之间移除,MYLAR的边缘粘接在一起形成一个圆筒,以完成可充气的桁架框架构件。 针对船舶诱饵的较重剪切载荷开发的第二个实施例包括三个主要可充气管,其由剪切承载腹板分隔开。 第二实施例可以通过将由MYLAR制成的内管和外管沿着弓形间隔的条带接合来制造。 粘合的MYLAR形成分离网,未粘合的MYLAR形成三个可充气管。 或者,第二实施例可以通过分开形成三个可充气管然后将分离纤维网材料粘合到可充气管来制造。 当分离纤维网不够坚固以支撑剪切载荷时,可以在三个可充气管之间加入刚性撑条或条板。
    • 10. 发明授权
    • In-flight electronic countermeasure payload simulator
    • 飞行中电子对抗有效载荷模拟器
    • US5198612A
    • 1993-03-30
    • US684996
    • 1991-04-15
    • Thomas R. Myers
    • Thomas R. Myers
    • F42C21/00
    • F42C21/00
    • An electronic countermeasure (ECM) simulator which fits into the housing of any actual ECM payload device and substitutes electrical components for the chaff, flares or other countermeasures which are emitted into the environment. The ECM payload simulator electrically verifies firing ability for any ECM dispensing system using a magnetic indicator which sets when the electrical signal required to fire an actual ECM payload device operates properly. The magnetic indicator can be viewed, tested and reset by a ground crew upon return of the aircraft to ground. The magnetic indicator has a parallel resistor so that the aircraft's arsenal inventorying device will indicate an unfired ECM payload device. An optional radio frequency (RF) transmitter may be substituted for the magnetic indicator to send coded transmissions to a radar site while in flight. Additionally, an electrical circuit may be added to measure amplitude and duration of the electrical firing signal and to prevent feedback into the ECM dispensing system. The ECM payload simulator can simulate both a single payload and dual payload ECM payload device. Filler material such as flexane.TM. may be is added to the simulator housing to make the weight of the simulator equal to an actual ECM payload device.
    • 一种电子对抗(ECM)模拟器,它适用于任何实际的ECM有效载荷装置的外壳,并替代发射到环境中的谷壳,火炬或其他对策的电气部件。 ECM有效载荷模拟器使用磁指示器电气地验证任何ECM分配系统的点火能力,该指示器设定何时触发实际ECM有效载荷装置所需的电信号正常工作。 当飞机返回地面时,磁性指示器可由地勤人员查看,测试和复位。 磁指示器具有并联电阻器,使得飞行器的库存盘点装置将指示未使用的ECM有效载荷装置。 可选的射频(RF)发射机可以代替磁性指示器在飞行中将编码的传输发送到雷达站点。 另外,可以添加电路以测量电击信号的幅度和持续时间并防止反馈到ECM分配系统中。 ECM有效负载模拟器可以模拟单个有效负载和双重有效负载ECM有效载荷设备。 可以将诸如flexane TM的填充材料添加到模拟器壳体中,以使模拟器的重量等于实际的ECM有效载荷装置。