Patents Assigned to Hughes Aircraft Company
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Patent number: 4163151Abstract: The separated ion source combines an ion source and a magnetic mass separator within a single magnetic field geometry. The preferred ion source has a low voltage Penning discharge configuration and produces a charged particle beam in the form of a ribbon with a rectangular cross section.Type: GrantFiled: December 28, 1977Date of Patent: July 31, 1979Assignee: Hughes Aircraft CompanyInventors: John R. Bayless, Robert L. Seliger, James W. Ward, James E. Wood
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Patent number: 4162525Abstract: A power system provides a duty cycle modulated high frequency carrier signal to an inductive load with positive and negative buses. During the inductive energy discharge period the energy stored in the inductive load causes a reversal in the polarity of the inductor terminal and tends to drive the new polarity towards infinity. Thus, the magnitude of one of the buses may be increased as the result of duty cycle modulation. First and second inverters are coupled in parallel across the positive and negative buses. First and second series coupled capacitors are also connected in parallel with the inverters. The power inverter senses the increased voltage on the second bus as a result of the inductive energy discharge and transfers that energy back to the first bus. Power may thus be sensed, converted in form, and transferred from one bus to another while conserving 90% of the energy which would otherwise be wasted.Type: GrantFiled: March 30, 1977Date of Patent: July 24, 1979Assignee: Hughes Aircraft CompanyInventor: Herbert N. Epp
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Patent number: 4160984Abstract: The specification describes a Schottky-gate field-effect transistor and related fabrication process wherein thin ion implanted surface stabilization regions are formed between source and gate electrodes and gate and drain electrodes of the device and to a thickness of between 100 and 1,000 angstroms. This is accomplished utilizing the source, gate and drain electrodes as an ion implantation mask against impinging inert ions which render the implanted regions semi-insulating, and this process requires no post-implantation annealing.Type: GrantFiled: November 14, 1977Date of Patent: July 10, 1979Assignee: Hughes Aircraft CompanyInventors: Glenn O. Ladd, Jr., Frederick W. Cleary
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Patent number: 4161009Abstract: A crossed-field switch device is connected in parallel to a load device which may arc. The characteristics of the crossed-field switch device are that it will not conduct when a high voltage is applied, but when the load device arcs, the crossed-field switch device conducts, taking current from the arc so that the arc quenches. The crossed-field switch device thus is a crowbar which is automatically conductive when the applied voltage decreases due to a line or load short.Type: GrantFiled: April 13, 1978Date of Patent: July 10, 1979Assignee: Hughes Aircraft CompanyInventors: Robin J. Harvey, Michael A. Lutz
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Patent number: 4160249Abstract: A system for the simultaneous storage of a plurality of components of data signals and for the retrieval and the processing thereof. The system includes a signal source coupled to a record unit that is synchronized by a record controller. A plurality of cathode ray tubes and optical imaging means are included in the record unit for storing the plurality of simultaneously occurring input signal components on a photographic film in an interleaved pattern. A single readout device scans the film in a direction transverse to the record pattern to develop read signals which are processed by a readout processor and an analyzer and then displayed on a display unit. The readout unit synchronizes the readout processor, the analyzer and the display unit.Type: GrantFiled: May 8, 1967Date of Patent: July 3, 1979Assignee: Hughes Aircraft CompanyInventor: Joseph R. Kotlarski
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Patent number: 4159873Abstract: This invention is an improved ranging system including an improved digital single shot circuit that has a resettable shift register therein so that a signal representative of the last target return occurring at any point of a predetermined range interval will be provided to the timing counter of the system. The digital single shot circuit includes a flip flop responsive to the first trigger pulse during the predetermined range interval, resetting the shift register so that, when the output pulse from the shift register representing the last target return is applied to the timing counter, it will terminate a fixed number of clock edges after the last trigger pulse determined by the number of stages of the shift register. The fixed delay in terminating the output of the shift register may represent the preset time of the readout counter.Type: GrantFiled: September 27, 1977Date of Patent: July 3, 1979Assignee: Hughes Aircraft CompanyInventor: Robert P. Farnsworth
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Patent number: 4159418Abstract: Two multimode optical fibers connected mutually at several locations along their lengths can act as an encoding or decoding structure depending on which terminals are used for the input/output of the data. Two multicoupled lines have one input which acts as the matched filter for another input, thus enabling easy correlation of data. The performance of such a structure was simulated and the results are discussed.Type: GrantFiled: June 23, 1977Date of Patent: June 26, 1979Assignee: Hughes Aircraft CompanyInventor: Emanuel Marom
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Patent number: 4158838Abstract: A symbol smoothing system for synthetically increasing the effective resolution of an in-raster symbol generator memory by a factor of four. The system stores a special three bit code in selected memory elements representative of the existing and past two memory lines with the code actually being a video brightness distribution and positioning offset code. A code number in a single memory cell defines positional and intensity information for the display elements corresponding to that memory cell and to selected surrounding eight memory cells, all of the memory cells having time or positional correspondence to display element positions. The stored codes in the surrounding memory cells, as well as the instantaneous memory cell being decoded, provide intensity levels which are combined at selected display element positions.Type: GrantFiled: January 16, 1978Date of Patent: June 19, 1979Assignee: Hughes Aircraft CompanyInventors: Michael D. Pruznick, Bruce W. Keller, James R. Phelps, Gerald Wolfson, James L. Heard
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Patent number: 4158787Abstract: Arrangements are disclosed for substantially reducing the effect of the inherent transducer capacitance in a transducer-coupled electromechanical system which is subject to vibrational movement. Electrical circuitry is coupled across the transducer output to provide a negative capacitance having a magnitude substantially the same as that of the inherent transducer capacitance, thereby substantially nullifying the inherent transducer capacitance and enabling improved damping (including low-noise damping) to be achieved.Type: GrantFiled: May 8, 1978Date of Patent: June 19, 1979Assignee: Hughes Aircraft CompanyInventor: Robert L. Forward
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Patent number: 4158183Abstract: A single in-plane orthogonal mode launcher for generating circularly polarized waves having both right and left hand senses is disclosed. A 90.degree. hybrid provides first and second signals to respective input ports of the launcher. First and second coplanar sets of probes are orthogonally disposed in a cylindrical housing and connected to the first and second ports, respectively. The first set of probes generates a first vector signal. The second set of probes generates a second vector signal which is 90.degree. to the first vector signal. Since the input signals to the first and second sets of probes are 90.degree. out of phase, circularly polarized waves are thus generated.Type: GrantFiled: December 22, 1976Date of Patent: June 12, 1979Assignee: Hughes Aircraft CompanyInventors: Mon N. Wong, Stanley T. Ibrao
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Patent number: 4158141Abstract: The specification describes a process for minimizing ion scattering and thereby improving resolution in ion beam lithography. First, a substrate coated with a layer of ion beam resist is provided at a chosen spaced distance from an ion beam source. Next, a monocrystalline membrane with a patterned ion absorption region is positioned at a predetermined location between the substrate target and the ion beam source. The patterned ion absorption region may be either an ion absorption mask, such as gold, deposited on the surface of the monocrystalline membrane, or a pattern of ion-damaged regions within the monocrystalline membrane. Finally, a collimated wide area ion beam is passed perpendicular to the surface of the membrane and through crystal lattice channels therein which are exposed by the patterned ion absorption region and which extend perpendicular to the membrane surface.Type: GrantFiled: June 21, 1978Date of Patent: June 12, 1979Assignee: Hughes Aircraft CompanyInventors: Robert L. Seliger, Paul A. Sullivan
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Patent number: 4157154Abstract: Brazing alloy on detailed aluminum parts is formed in an exact pattern of the joints to be brazed. An aluminum sheet having brazing alloy coated on one or both sides (e.g., a brazing sheet) is plated with electroless nickel and electrolytic copper which are etched by use of a photoresist mask into a mask which outlines the pattern. The brazing alloy coating is then chemically milled to form the exact pattern of the joints. Parts are then assembled and dip brazed to form the completed brazed unit.Type: GrantFiled: November 21, 1977Date of Patent: June 5, 1979Assignee: Hughes Aircraft CompanyInventors: James K. Scott, Theodore C. Schmidt
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Patent number: 4156879Abstract: The specification describes a new and improved Schottky-gate field-effect transistor (FET) and process for fabricating same wherein selective and multiple ion implantation doping steps are used to form source, drain and channel regions in a semiconductor body. The semiconductor body is then selectively etched to expose the source and drain regions previously formed, while leaving intact a mesa-shaped, high resistivity stabilizing region of the semiconductor body overlying and electrically stabilizing the ion-implanted channel region. The semiconductor body is then partially passivated with a chosen dielectric layer having two openings therein for exposing source and drain regions, respectively, and a third opening which is aligned with the channel region. Ohmic contacts are deposited in the source and drain openings, and thereafter a V-shaped groove is etched in the mesa-shaped region overlying the channel region to expose a very small area of the channel region.Type: GrantFiled: February 7, 1977Date of Patent: May 29, 1979Assignee: Hughes Aircraft CompanyInventor: Don H. Lee
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Patent number: 4156859Abstract: A class of two-terminal active networks which simulate low-noise temperature resistors is disclosed. A single differential-input operational amplifier connected with a feedback resistor in an inverting amplifier configuration comprises the active element of the network. A dual-transformer feedback arrangement or a single transformer feedback arrangement comprises the remainder of the circuit. Either positive or negative simulated resistors can be obtained with a wide range of equivalent resistance values and effective noise temperatures.Type: GrantFiled: October 3, 1977Date of Patent: May 29, 1979Assignee: Hughes Aircraft CompanyInventors: Robert L. Forward, Gary D. Thurmond
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Patent number: 4156310Abstract: The specification describes a semiconductor solar cell and fabrication process therefor wherein a thin N-type gallium arsenide layer is deposited on a larger P-type substrate layer which is selected from the group of III-V ternary compounds consisting of aluminum phosphide antimonide, AlPSb, and aluminum indium phosphide, AlInP. P-type impurities are diffused from the substrate layer into a portion of the thin N-type gallium arsenide layer to form P-type region therein which defines a PN junction in the thin gallium arsenide layer. Thus, the quantity of gallium arsenide required to provide this PN photovoltaic junction layer in the cell is minimized, and the P-type substrate serves as a high bandgap window layer for the cell. Such high bandgap of this window material is especially well suited for efficiently transmitting the blue spectrum of sunlight to the PN junction, thus enhancing the power conversion efficiency of the solar cell.Type: GrantFiled: March 17, 1978Date of Patent: May 29, 1979Assignee: Hughes Aircraft CompanyInventor: G. Sanjiv Kamath
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Patent number: 4156857Abstract: A method of eliminating a substantial portion of the nonlinear effects that occur in passive microwave devices operating under relatively high power conditions by use of small lightweight permanent magnets about the device structure while monitoring the level of such undesired signals.Type: GrantFiled: May 2, 1977Date of Patent: May 29, 1979Assignee: Hughes Aircraft CompanyInventors: Neal C. Silence, Juri G. Leetmaa, Charles F. Montgomery
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Patent number: 4153529Abstract: Electrode surfaces are coated with a passivating material (silicon dioxide, aluminum oxide or titanium dioxide) or with a reflecting material (chromium or chromium and gold) or with a special alignment material (carbon) using standard vacuum sputtering, vacuum evaporation, electrodeposition, or chemical vapor deposition techniques. After sufficient thickness of material has been deposited, the substrate is exposed to a broad or narrow beam of neutralized argon ions of a few kilo-electron-volts energy. The beam of argon ions is incident at a grazing angle to the surface, typically 20.degree.. Exposure of the overcoating results in a microscopic condition believed to comprise a "corrugated" surface with "ridges" and "valleys" parallel to the direction of the incident beam.Type: GrantFiled: April 21, 1975Date of Patent: May 8, 1979Assignee: Hughes Aircraft CompanyInventors: Michael J. Little, Hugh L. Garvin, Yat-Shir Lee
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Patent number: 4152588Abstract: A scanning mirror position sensor operable from the back side of a scanning mirror which utilizes the front side of the mirror for scanning a scene to be interrogated or displayed. A rectangular uniformly distributed light source is reflected from the back surface of the scanning mirror across a grating consisting of alternate transparent and opaque regions placed in the focal plane in front of a single large area photodetector. As the light from the light source sweeps across the grating, the detector is alternately energized and deenergized to form a serial pulse train which is coupled to a pulse counter which accumulates the pulse count to thereby provide a continual and accurate measure of the mirror position.Type: GrantFiled: October 28, 1977Date of Patent: May 1, 1979Assignee: Hughes Aircraft CompanyInventors: Robert W. Klatt, A. Stevens Halsted
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Patent number: 4151523Abstract: A receiving antenna connected to a surveillance sensor feeding a target detector. The target detector provides multiple inputs of target reports, azimuth, range and scan count data into a clutter mapper circuit which in turn feeds a track-while-scan circuit feeding a CRT display. The clutter mapper circuit provides improved clutter detection in the presence of scintillating clutter conditions.Type: GrantFiled: August 25, 1976Date of Patent: April 24, 1979Assignee: Hughes Aircraft CompanyInventors: Vernon H. Platt, Richard D. Wilmot
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Patent number: 4150304Abstract: A charge transfer device is provided having a first group of electrodes embedded in a semiconductor material and a second group of electrodes embedded in a contiguous overlying layer electrically insulating material. An improvement in this device includes means for injecting charge into such device having a number of additional components consisting of a first additional electrode which is embedded in-part in the semiconductor material, and a second additional electrode which is embedded in the insulating material. The first additional electrode is energized by a bias voltage and the second additional electrode is energized by a clock signal.Type: GrantFiled: March 14, 1978Date of Patent: April 17, 1979Assignee: Hughes Aircraft CompanyInventor: William E. Jensen