公开(公告)号：WO1986001592A1

公开(公告)日：1986-03-13

申请号：PCT/US1985001377

申请日：1985-07-19

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  MacPHERSON, Duncan

IPC: G01C11/02

CPC classification number: G01C11/025

Abstract: A satellite imaging system (100) provides successive coregistered images from the perspective of an idealized reference position, such as the nominal geosynchronous orbit position of the satellite. The disclosed satellite (101) is spin-stabilized, and so includes a despun platform (107) which supports a communications subsystem (109), and a spun rotor (111) which supports a sensor (103). The communications subsystem transmits sensor data along a path (115) to a ground station (105). Linear interpolation of real image data as a function of satellite position and imager attitude provides the ideal images. The disclosed invention is also applied to a pointing sensor such as one employed on a three-axis stabilized satellite. The coregistered idealized images coregistered facilitate analysis of weather feature movements and enhance weather forecasting.

Abstract translation: 卫星成像系统（100）从理想化参考位置（例如卫星的地名同步轨道位置）的角度提供连续的核心成像系统。 所公开的卫星（101）是旋转稳定的，因此包括支撑通信子系统（109）的解码平台（107）和支持传感器（103）的旋转转子（111）。 通信子系统沿着路径（115）将传感器数据传送到地面站（105）。 作为卫星位置和成像器姿态的函数的实际图像数据的线性插值提供了理想的图像。 所公开的发明也适用于诸如在三轴稳定卫星上使用的指示传感器。 核心理念的理想化图像coregistered方便分析天气特征运动和增强天气预报。

公开(公告)号：WO1986001344A1

公开(公告)日：1986-02-27

申请号：PCT/US1985001411

申请日：1985-07-24

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  KAHAN, Osher

IPC: H01S03/02

CPC classification number: H01S3/042 ,  H01S3/025 ,  H01S3/0405 ,  H01S3/093

Abstract: An improved laser rod cooling system in which a laser rod (18) is cooled by conducting the heat generated thereby to a flexible, cushioning gel (21) which surrounds and contacts the rod along its length and secures the rod within a fully enclosing support (22). The support is thermally conductive and transparent to the pumping energy from a flashlamp (12). The gel material absorbs differential thermal expansion between the rod and its support to avoid any stresses otherwise exerted on the rod, while the complete surrounding of the rod by the support minimizes thermal gradients within the rod. Thus, a light beam with minimal optical distortion is generated by the laser rod.

Abstract translation: 一种改进的激光棒冷却系统，其中激光棒（18）通过将由此产生的热量导向柔性的缓冲凝胶（21）而冷却，所述柔性缓冲凝胶沿其长度包围并接触杆，并将杆固定在完全封闭的支撑件内 22）。 支撑件是导热的并且对于来自闪光灯（12）的泵送能量是透明的。 凝胶材料吸收杆和其支撑件之间的差异热膨胀，以避免施加在杆上的任何应力，而通过支撑件的杆的完整周围使杆内的热梯度最小化。 因此，激光棒产生具有最小光学失真的光束。

公开(公告)号：WO1986000685A1

公开(公告)日：1986-01-30

申请号：PCT/US1985001254

申请日：1985-07-01

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  GAGNON, Ralph, J.

IPC: F21V07/08

CPC classification number: F21V7/08 ,  G09B9/308

Abstract: An illumination system reflector (18) which provides maximum energy to an aperture (25) with high uniformity and at high efficiencies, the reflector (18) being particularly adapted for use in liquid crystal light valve projection systems. A discharge lamp (34) is utilized in conjunction with an elliptical reflector (18), the axis of the reflector between the primary and secondary focus being tilted at an angle ( theta ) to the lamp axis. The axis of the ellipse (22) is displaced from the lamp axis a predetermined amount (DH), the combination of tilt ( theta ) and displacement (DH) being effective to increase illumination uniformity and efficiency at the aperture (25). Other system parameters, such as throw distance (CTHRO) and cone angle ( alpha ) also affect uniformity and efficiency for a typical design in which the parameters are selected to provide an optimized system being disclosed. A computer program simulation may be utilized for parameter selection. The vertical displacement (DH) parameter is shown to be related to the lamp envelope dimensions.

Abstract translation: 一种照明系统反射器（18），其以高均匀性和高效率向孔（25）提供最大能量，反射器（18）特别适用于液晶光阀投影系统。 放电灯（34）与椭圆形反射器（18）结合使用，主焦点与副焦点之间的反射镜轴线以与灯轴成一定角度（θ）倾斜。 椭圆（22）的轴线从灯轴移动预定量（DH），倾斜（θ）和位移（DH）的组合对于增加孔径（25）处的照明均匀性和效率是有效的。 诸如投射距离（CTHRO）和锥角（α）的其他系统参数也影响了典型设计的均匀性和效率，其中选择参数以提供被公开的优化系统。 可以使用计算机程序模拟来进行参数选择。 垂直位移（DH）参数显示与灯泡尺寸有关。

公开(公告)号：WO1986000476A1

公开(公告)日：1986-01-16

申请号：PCT/US1985001153

申请日：1985-06-18

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  WAGNER, Gene, A. ,  NEWBERG, Irwin, L.

IPC: H03C01/06

CPC classification number: G01S7/023 ,  G01S7/282 ,  H03C1/06

Abstract: An RF amplifier arrangement for providing output signals having a controlled frequency distribution and wherein the amplitude and phase of the input signals to an RF amplifier (18) are controlled as a function of the amplitude and phase, respectively, of the output signals from the RF amplifier (18) and also the amplitude of the input signals are adjusted so as to cause the power of the output signal to vary in accordance with a predetermined sequence, whereby such amplitude control of the input signals results in a modified frequency distribution in the energy of the output signals.

公开(公告)号：WO1986000466A1

公开(公告)日：1986-01-16

申请号：PCT/US1985001057

申请日：1985-06-04

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  HARVEY, Robin, J. ,  GALLAGHER, Hayden, E.

IPC: H01J03/02

CPC classification number: H01J3/021 ,  H01J17/44

Abstract: An Electron Beam Controlled Switch employing a radial geometry and a Wire-Ion Plasma-Electron gun (WIP E-gun) as an electron source. The switch comprises an inner cylinder (10) that serves as the WIP E-gun cathode, a cylindrical grid (15) that serves as the WIP E-gun anode, an array of fine wire anodes (20) disposed in the WIP E-gun ionization chamber, a foil support cylinder (25) to support the foil windows which also serve as the switch anode, and an outer cylinder (30) which also serves as the switch cathode. The WIP E-gun and ionization chamber (35, 40) is gas filled at low pressure, while the switch cavity (45) is filled with a high pressure gas. A voltage pulse is applied to the wire anodes (20) to ionize the gas in the ionization chamber (35). The ions are extracted through the chamber grid (15) and accelerated through a high voltage to bombard the E-gun cathode (10). The electrons emitted from the ion bombardment are accelerated outwardly through the high voltage, penetrate through the foil windows and into the pressurized gas in the switch cavity (45). The high energy electrons ionize the gas between the switch anode (15) and cathode (10), thereby turning "ON" the switch. In the absence of the electron beam, the switch gas deionizes and switch conduction is quickly extinguished.

Abstract translation: 采用放射几何形状的电子束控制开关和线离子等离子体电子枪（WIP E-gun）作为电子源。 开关包括用作WIP E枪阴极的内筒（10），用作WIP E枪阳极的圆柱形网格（15），布置在WIPE-gun阳极中的细线阳极阵列（20） 枪电离室，用​​于支撑也用作开关阳极的箔窗的箔支撑筒（25）以及也用作开关阴极的外筒（30）。 WIP电子枪和电离室（35,40）是在低压下填充的气体，而开关腔（45）填充有高压气体。 对电线阳极（20）施加电压脉冲以电离电离室（35）中的气体。 离子通过室格栅（15）提取并通过高电压加速以轰击电子枪阴极（10）。 从离子轰击发射的电子通过高电压向外加速，穿过箔窗口并进入开关腔（45）中的加压气体。 高能电子使开关阳极（15）和阴极（10）之间的气体电离，从而使开关“接通”。 在没有电子束的情况下，开关气体去离子并且开关导通快速熄灭。

公开(公告)号：WO1985005489A1

公开(公告)日：1985-12-05

申请号：PCT/US1985000682

申请日：1985-04-17

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  SCHUMACHER, Robert, W. ,  HARVEY, Robin, J.

IPC: H01J17/44

CPC classification number: H01J17/44 ,  H01J17/14

Abstract: A cold-cathode, plasma discharge modulator switch (Fig. 2). A corssed-field discharge plasma (30) supplies charge carriers for the switch. A dc magnetic field (25) is employed to provide a highly localized cusp magnetic field near the cathode (7), so that plasma ionization occurs primarily in the cathode-source grid gap. The region between the cathode (7) and anode (1) is filled with a relatively low pressure gas. A highly transparent control grid (8) with small apertures is closely spaced from the anode (1). The switch is closed through application of positive potential (relative to the plasma) to the control grid (8), and opened through application of negative potential relative to the plasma to the control grid (8). The application of negative potential to the control grid (8) creates an ion sheath around the control grid (8) which permits plasma cut-off to the anode region provided the sheath size is larger than the control grid aperture radius. Upon plasma cut-off, the switch current is interrupted as the remaining plasma in the control grid-anode gap decays. Low pressure operation insures that ionization cannot sustain the plasma in the narrow, isolated control grid-anode gap.

公开(公告)号：WO1985005225A1

公开(公告)日：1985-11-21

申请号：PCT/US1985000654

申请日：1985-04-12

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  MINAHAN, Joseph, A. ,  RALPH, Eugene, L. ,  DILL, Hans, G.

IPC: H01L31/02

CPC classification number: H01L31/1804 ,  H01L31/022425 ,  H01L31/02245 ,  Y02E10/547 ,  Y02P70/521

Abstract: Process for fabricating wraparound solar cells wherein vertical slots are scribed in a semiconductor wafer to initially define the lateral dimensions of the cell. Thereafter, photolithographic masking, etching and diffusion steps are used to define the geometry of a p-n junction of the cell. Then, using lift-off photolithography and a multiple-element metal deposition process, the solar cell grid lines are formed on one surface of the cell and p- and n-type metal contacts are extended around to the opposite surface of the cell. In this manner, the dimensions of the cell can be made less than the diameter of the semiconductor wafer from which it is made.

Abstract translation: 制造环绕太阳能电池的方法，其中在半导体晶片中刻划垂直狭缝以最初限定电池的横向尺寸。 此后，使用光刻掩模，蚀刻和扩散步骤来定义电池的p-n结的几何形状。 然后，使用剥离光刻法和多元素金属沉积工艺，在电池的一个表面上形成太阳能电池栅格线，并且将p型和n型金属触点延伸到电池的相对表面。 以这种方式，可以使电池的尺寸小于制造电池的半导体晶片的直径。

公开(公告)号：WO1985005215A1

公开(公告)日：1985-11-21

申请号：PCT/US1984001383

申请日：1984-08-30

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  OLDHAM, Susan, L.

IPC: H01B03/40

CPC classification number: H01B3/40 ,  C08G59/28 ,  C08G59/3227 ,  C08G59/42 ,  Y10T428/31529

Abstract: A highly fluid, solventless heat curable resin is formulated from an admixture comprising a polyglycidyl aromatic amine, a polycarboxylic acid anhydride curing agent, and a curing accelerator. The heat curable formulation exhibits low viscosity and is useful as an encapsulant and insulation for electrical members exposed to high electrical stress. Magnetic coils encapsulated with the cured formulation resist corona discharge at electrical stresses in excess of 2100 volts per mil.

公开(公告)号：WO1985004887A1

公开(公告)日：1985-11-07

申请号：PCT/US1985000612

申请日：1985-04-08

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  ROSSER, Robin, W. ,  TEDESCO, James, S. ,  SEIBOLD, Robert, W. ,  MILEWSKI, John, V.

IPC: C08K07/02

CPC classification number: C08J3/21 ,  C08J5/04 ,  C08K7/02

Abstract: A composite material comprising an ultra-high molecular weight polymer and fibers having lengths of about 0.05 inch (1270 micrometers). This composite is formed by first dispersing the fibers with particles of the polymer in an inert liquid carrier. The dispersion is drawn through a filter which collects the particles and fibers as an intermediate structure in which the fibers are oriented in a quasi-isotropic array and the particles are dispersed throughout this fiber network. The intermediate structure is removed from the filter, dried, compacted, and then compressed at an elevated temperature such that the polymer melts, while the fibers remain unmelted. Upon cooling, there is formed a composite comprising a continuous polymer matrix reinforced with the randomly oriented and intertwined fibers of relatively long length. This material can be formed into articles, such as piston rings or seals, to provide a self-lubricating structure having good wear resistance and creep resistance.

Abstract translation: 包含超高分子量聚合物和长度为约0.05英寸（1270微米）的纤维的复合材料。 该复合物通过首先将纤维与聚合物颗粒分散在惰性液体载体中而形成。 分散体通过过滤器吸收，该过滤器收集颗粒和纤维作为其中纤维以准各向同性阵列取向的中间结构，并且颗粒分散在整个纤维网络中。 将中间结构从过滤器中除去，干燥，压实，然后在升高的温度下压缩，使得聚合物熔融，同时纤维保持未熔化。 在冷却时，形成复合材料，该复合材料包括用相对较长长度的随机取向和相互缠绕的纤维增强的连续聚合物基体。 该材料可以形成诸如活塞环或密封件的制品，以提供具有良好的耐磨性和抗蠕变性的自润滑结构。

公开(公告)号：WO1985004508A1

公开(公告)日：1985-10-10

申请号：PCT/US1985000248

申请日：1985-02-15

Applicant: HUGHES AIRCRAFT COMPANY

Inventor： HUGHES AIRCRAFT COMPANY ,  AUTREY, Samuel, W. ,  DRAB, Harold, G.

IPC: G10K11/34

CPC classification number: H01Q3/38 ,  G10K11/346 ,  H03H19/004

Abstract: A narrow-band phase shift beamformer system. The outputs from the elements in a transducer array are each divided into two components whose amplitudes are respectively proportional to the sine and cosine of the required phase shift, which are then processed so that the steered beam may be formed by coherent summation. The proportionalities of the respective sine and cosine components are achieved by switched capacitor circuits, which are preferably implemented by LSI circuits, permitting substantial hardware savings and yielding highly accurate component proportionalities.