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    • 1. 发明授权
    • Airborne fiber optic decoy architecture
    • 机载光纤诱骗架构
    • US5136295A
    • 1992-08-04
    • US699748
    • 1991-05-14
    • James G. BullMichael de la ChapelleBernard J. Lamberty
    • James G. BullMichael de la ChapelleBernard J. Lamberty
    • G01S7/38H01Q1/30H01Q3/26
    • H01Q3/2676F41J2/00G01S7/38H01Q1/30
    • One or more decoys (22) are towed by an aircraft (18) to confuse hostile radar. The tow lines (20) to the decoys (22) include fiber optic components which optically transmit to the decoys (22) both radio frequency signals for retransmission to hostile radar (24), and direct current power. The fiber optic components absorb strain forces imposed by towing the decoys (22). Multiple decoys (22) are deployed at varying distances from the aircraft (18) to increase the overall range of frequencies covered by the system, simulate a plurality of false targets, or accomplish angle gate deception. The deception may be accomplished by transmitting signals from the decoys in sequence and can be enhanced by dynamically varying the power levels of the decoy transmitting antennas. The fiber optic components may be separate optical fibers deployed separately or joined together for simultaneous deployment. The preferred configuration is a single optical fiber with coaxial inner and outer cores. The decoy preferably has a transmitting antenna in the form of a simulated biconical dipole. In one embodiment, both halves of the dipole are simulated by a set of fins. In another embodiment, the forward half is simulated by a truncated cone.
    • 一个或多个诱饵(22)被飞机(18)拖曳以混淆敌对雷达。 到诱饵(22)的牵引线(20)包括光传输到诱饵(22)的光纤部件,两个射频信号用于重发到敌对雷达(24)和直流电力。 光纤元件吸收由诱饵(22)施加的应变力。 多个诱饵(22)部署在与飞机(18)不同的距离处,以增加系统覆盖的频率的总体范围,模拟多个假目标,或完成角门欺骗。 可以通过依次从诱饵传送信号来实现欺骗,并且可以通过动态地改变诱饵发射天线的功率电平来增强欺骗。 光纤组件可以是单独部署的或连接在一起以用于同时部署的单独光纤。 优选的配置是具有同心的内核和外核的单个光纤。 诱饵优选具有模拟双锥偶极子形式的发射天线。 在一个实施例中,偶极子的两半由一组翅片模拟。 在另一个实施例中,前半部分由截头锥体模拟。
    • 2. 发明授权
    • Airborne fiber optic decoy architecture
    • 机载光纤诱骗架构
    • US5260820A
    • 1993-11-09
    • US808439
    • 1991-12-16
    • James G. BullMichael de La ChapelleBernard J. Lamberty
    • James G. BullMichael de La ChapelleBernard J. Lamberty
    • F41J9/10G01S7/38H01Q1/30H01Q3/26H04B10/00H01Q15/00
    • H01Q3/2676F41J9/10G01S7/38H01Q1/30
    • One or more decoys (22) are towed by an aircraft (18) to confuse hostile radar. The tow lines (20) to the decoys (22) include fiber optic components which optically transmit to the decoys (22) both radio frequency signals for retransmission to hostile radar (24), and direct current power. The fiber optic components absorb strain forces imposed by towing the decoys (22). Multiple decoys (22) are deployed at varying distances from the aircraft (18) to increase the overall range of frequencies covered by the system, simulate a plurality of false targets, or accomplish angle gate deception. The deception may be accomplished by transmitting signals from the decoys in sequence and can be enhanced by dynamically varying the power levels of the decoy transmitting antennas. The fiber optic components may be separate optical fibers deployed separately or joined together for simultaneous deployment. The preferred configuration is a single optical fiber with coaxial inner and outer cores. The decoy preferably has a transmitting antenna in the form of a simulated biconical dipole. In one embodiment, both halves of the dipole are simulated by a set of fins. In another embodiment, the forward half is simulated by a truncated cone.
    • 一个或多个诱饵(22)被飞机(18)拖曳以混淆敌对雷达。 到诱饵(22)的牵引线(20)包括光传输到诱饵(22)的光纤部件,两个射频信号用于重发到敌对雷达(24)和直流电力。 光纤元件吸收由诱饵(22)施加的应变力。 多个诱饵(22)部署在与飞机(18)不同的距离处,以增加系统覆盖的频率的总体范围,模拟多个假目标,或完成角门欺骗。 可以通过依次从诱饵传送信号来实现欺骗,并且可以通过动态地改变诱饵发射天线的功率电平来增强欺骗。 光纤组件可以是单独部署的或连接在一起以用于同时部署的单独光纤。 优选的配置是具有同心的内核和外核的单个光纤。 诱饵优选具有模拟双锥偶极子形式的发射天线。 在一个实施例中,偶极子的两半由一组翅片模拟。 在另一个实施例中,前半部分由截头锥体模拟。
    • 4. 发明授权
    • Spiral antenna with selectable impedance
    • 螺旋天线可选阻抗
    • US4630064A
    • 1986-12-16
    • US537485
    • 1983-09-30
    • George S. AndrewsThomas L. BlakneyDouglas D. ConnellBernard J. LambertyJames R. Lee
    • George S. AndrewsThomas L. BlakneyDouglas D. ConnellBernard J. LambertyJames R. Lee
    • H01Q9/27H01Q25/02H01Q1/36
    • H01Q9/27H01Q25/02
    • A monopulse spiral antenna system of the type having a minimum of three, interwound spiral arms for multimode, direction of arrival sensing, is disclosed in which the antenna arms are shaped and arranged in an overlapping configuration that allows the interarm impedance of the antenna to be adjusted, substantially independently of other electrical properties of the antenna, for matching of the antenna impedance of a mode forming network while preserving the broadband, directional capabilities of the antenna. Several different embodiments of the impedance adaptive antenna are disclosed including a preferred, eight-arm exponential spiral in which the arms are conductive strips transversely inclined relative to a plane formed by the spiral so that opposed and parallel surfaces of adjacent arm strips create a dominant interarm capacitance that in turn determines the overall input impedance of the antenna. Furthermore, the opposed, proximate surfaces of the strip-shaped arms are dimensioned, spaced and inclined at an angle that adapts the input impedance of the antenna to a value matching that of the mode forming network.
    • 公开了一种具有至少三个用于多模式的相互缠绕的螺旋臂,到达方向感测的单脉冲螺旋天线系统,其中天线臂成形并布置成重叠配置,其允许天线的间隔阻抗为 基本上独立于天线的其它电气特性进行调节,以便匹配模式形成网络的天线阻抗,同时保持天线的宽带方向性能。 公开了阻抗自适应天线的几个不同实施例,其包括优选的八臂指数螺旋,其中臂是相对于由螺旋形成的平面横向倾斜的导电条,使得相邻臂条的相对且平行的表面形成主要的间隙 电容又决定了天线的整体输入阻抗。 此外,条形臂的相对的近邻表面的尺寸,间隔和倾斜,其角度使天线的输入阻抗适应于与模式形成网络的输入阻抗匹配的值。
    • 5. 发明授权
    • Variable wide angle conical scanning antenna
    • 可变广角锥形扫描天线
    • US4862185A
    • 1989-08-29
    • US177966
    • 1988-04-05
    • George S. AndrewsBernard J. LambertyDaniel J. Tracy
    • George S. AndrewsBernard J. LambertyDaniel J. Tracy
    • H01Q3/20
    • H01Q3/20
    • Disclosed is a variable angle conical scanning antenna that employs an offset paraboloidal reflector which is rotated about an axis that extends through the focus of the paraboloid of revolution that defines the reflector. Electromagnetic energy is supplied to the reflector by an antenna feed that is mounted at the focus of the paraboloid of revolution and directed along the axis of rotation. In this arrangement the electromagnetic energy that is reflected from the offset paraboloidal reflector forms an angle between the axis of rotation and the beam of reflected electromagnetic energy that is equal to the angle between the axis of rotation and the focal axis of the paraboloid of revolution that defines the reflector. Thus, conical scanning at a cone angle that is equal to twice the angle between the axis of rotation and the reflected beam of electromagnetic energy is achieved as the offset paraboloidal reflector is rotated. Variable angle scanning (i.e., conical scanning over a range of cone angles) is achieved by tilting the offset paraboloidal reflector about the focus of the paraboloid of revolution that defines the reflector with the axis of antenna rotation and the focal axis of the paraboloid of revolution that defines the reflector remaining in substantial coplanar relationship.
    • 公开了一种可变角锥形扫描天线,其采用偏移抛物面反射器,该偏移抛物面反射器围绕延伸穿过限定反射器的旋转抛物面的焦点的轴线旋转。 电磁能通过安装在旋转抛物面的焦点并沿着旋转轴线引导的天线馈送供应给反射器。 在这种布置中,从偏移抛物面反射镜反射的电磁能量在旋转轴线和反射的电磁能量束之间形成角度,其等于旋转轴线与旋转抛物面的焦点轴线之间的角度, 定义反射器。 因此,当偏移抛物面反射器旋转时,实现了等于旋转轴线和反射电磁能量束之间角度的两倍的锥角的锥形扫描。 通过将偏置抛物面反射器围绕定义反射器的旋转抛物面的焦点倾斜偏转抛物面反射器的轴线和旋转抛物面的焦点轴线来实现可变角度扫描(即,锥角范围内的锥形扫描) 其限定反射体保持基本上共面的关系。
    • 6. 发明授权
    • Broad-band antenna structure having frequency-independent, low-loss
ground plane
    • 宽带天线结构具有频率独立,低损耗的接地层
    • US4608572A
    • 1986-08-26
    • US448511
    • 1982-12-10
    • Thomas L. BlakneyDouglas D. ConnellBernard J. LambertyJames R. Lee
    • Thomas L. BlakneyDouglas D. ConnellBernard J. LambertyJames R. Lee
    • H01Q5/00H01Q5/28H01Q9/27H01Q9/28H01Q1/48H01Q1/36
    • H01Q11/10H01Q1/48H01Q5/28H01Q9/27H01Q9/28
    • To optimize antenna bandwidth and efficiency in broad-band antenna elements of the planar, multiarm spiral and log periodic types, a conically shaped ground plane characterized by progressively sized circumferential chokes, is arranged on a common axis with the axial center of the spiral or log periodic elements so that the electrical spacing between the excited regions of the log periodic of spiral elements and the ground plane maintains a constant one-quarter wavelength relationship. The progressively sized circumferential chokes on the ground plane cut off the flow of excessive radial currents along the ground plane surface to achieve an improved mix of excitation and reexcitation modes. In one embodiment, the circumferential chokes on the conical ground plane are partially shunted by shunting strips that electrically or capacitively bridge the choke walls to reestablish limited radial currents along the ground plane for sustaining certain desirable antenna modes. In another disclosed embodiment, the equivalent one-quarter wavelength relationship between the driven spiral or log elements and the reflecting ground plane is maintained in an antenna structure in which the driven elements are disposed on the surface of a dielectrically shaped cone and the ground plane and progressively sized circumferential chokes are arranged in a generally planar array. In still another disclosed embodiment, the circumferential, progressively sized chokes are disposed on the interior reflective surface of a center-fed antenna horn, wherein the array of chokes has the effect of broad-banding the otherwise inherently narrow band characteristics of the horn.
    • 为了优化平面,多臂螺旋和对数周期类型的宽带天线元件中的天线带宽和效率,以逐渐大小的圆周扼流圈为特征的圆锥形接地平面布置在与螺旋或对数轴的中心的公共轴上 使得螺旋元件的对数周期性的激发区域和接地平面之间的电气间隔保持恒定的四分之一波长关系。 接地平面上的逐渐大小的圆周扼流圈切断了沿地平面的过大的径向电流,以实现激发和再激励模式的改进混合。 在一个实施例中,锥形接地平面上的周向扼流圈通过分流带部分地分流,所述分流带电或电容地桥接阻塞壁以重新建立沿接地平面的有限径向电流,以维持某些期望的天线模式。 在另一个公开的实施例中,被驱动的螺旋或对数元件与反射接地面之间的等效四分之一波长关系保持在天线结构中,其中从动元件设置在介电圆锥体和接地平面的表面上, 大小的圆周扼流圈布置在大致平面的阵列中。 在另一个公开的实施例中,周向的逐渐尺寸的扼流器设置在中心馈电的天线喇叭的内部反射表面上,其中扼流圈阵列具有宽带化喇叭的另外固有窄带特性的效果。
    • 7. 发明授权
    • Packaging architecture for phased arrays
    • 相控阵列的包装架构
    • US5276455A
    • 1994-01-04
    • US705816
    • 1991-05-24
    • George W. FitzsimmonsBernard J. LambertyEdward J. VertatschitschDietrich E. RiemerDonn T. Harvey
    • George W. FitzsimmonsBernard J. LambertyEdward J. VertatschitschDietrich E. RiemerDonn T. Harvey
    • H01Q21/00H01Q13/00H01Q3/22
    • H01Q21/0025H01Q21/0087
    • A phased array antenna structure has a distribution network, and a composite of feed, module, and antenna honeycomb structures. The distribution network distributes or collects electromagnetic (EM) energy. The feed honeycomb structure is positioned adjacent the distribution network and connected to receive the EM energy from the distribution network or to distribute EM energy to the distribution network. The module honeycomb structure is positioned adjacent the feed honeycomb structure so as to receive EM energy from the feed honeycomb structure or to transmit EM energy to the feed honeycomb structure. The antenna honeycomb structure is positioned adjacent the module honeycomb structure on a side opposite the feed honeycomb structure so as to receive EM energy from the module honeycomb structure or to transmit EM energy to the module honeycomb structure. Each of the feed, module and antenna honeycomb structures have a plurality of aligned waveguides for transmitting EM energy therealong. The module honeycomb structure includes an electronic module for each waveguide wherein each electronic module has an electronic element for adjusting at least the phase of the EM energy and transmitting the adjusted phase EM energy to the aligned waveguide of the antenna honeycomb structure or the feed honeycomb structure.
    • 相控阵天线结构具有分布网络,以及馈电,模块和天线蜂窝结构的组合。 配电网分配或收集电磁(EM)能量。 饲料蜂窝结构位于分配网络附近并被连接以从分配网络接收EM能量或将EM能量分配到分配网络。 模块蜂窝结构位于馈电蜂窝结构附近,以便从馈电蜂窝结构接收EM能量或将EM能量传递到馈电蜂窝结构。 天线蜂窝结构在与蜂窝状蜂窝结构体相对的一侧与模块蜂窝结构相邻配置,从而从模块蜂窝结构体接收EM能量,或将EM能量传递给模块蜂窝结构体。 馈电,模块和天线蜂窝结构中的每一个具有用于在其上传输EM能量的多个对准的波导。 模块蜂窝结构包括用于每个波导的电子模块,其中每个电子模块具有用于至少调节EM能量相位的电子元件,并将调整后的相位EM能量传输到天线蜂窝结构或馈电蜂窝结构的对准波导 。
    • 8. 发明授权
    • Distribution network for phased array antennas
    • 相控阵天线配电网
    • US4939527A
    • 1990-07-03
    • US299458
    • 1989-01-23
    • Bernard J. LambertyEdward J. VertatschitschGeorge W. Fitzsimmons
    • Bernard J. LambertyEdward J. VertatschitschGeorge W. Fitzsimmons
    • H01Q21/00H01Q21/06
    • H01Q21/0018H01Q21/005H01Q21/061
    • A distribution network for a modified space-fed phased array antenna consists of a planar array of radiating slots distributed along a coplanar wall in each of an ensemble of parallel waveguides. This waveguide ensemble is fed or excited by an orthogonal waveguide or waveguides, through a row of slots in a wall common to the excitation waveguides and the parallel waveguide ensemble, one slot per waveguide. A predetermined amplitude distribution is achieved in the plane parallel to the axis of the exciting waveguide by adjusting the coupling value of each exciting slot, and in the orthogonal plane by adjusting the displacement of the radiating slots from the center line of the waveguides, and by adjusting slot width, length, and geometry. Such an array of slots is used to feed the inside face of a quasi-space-fed antenna array having identical, individual electronics modules.
    • 用于修改的空间馈电相控阵天线的分配网络包括沿平行波导的整体中的每个平面壁分布的辐射槽的平面阵列。 该波导组合通过正交波导或波导馈送或激励,通过激励波导和平行波导集合共用的一排狭槽,每个波导一个槽。 通过调整每个激励槽的耦合值,并且在正交平面中,通过调整辐射槽与波导的中心线的位移,并且通过 调整槽宽度,长度和几何尺寸。 这种槽阵列用于馈送具有相同的各个电子模块的准空间馈电的天线阵列的内表面。