Patents Assigned to Hughes Aircraft Company
  • Patent number: 5763118
    Abstract: A battery system includes a battery cell having a battery cell housing, and a housing support external to the battery cell housing. The housing support is formed of at least two split shell segments. Each split shell segment includes a heat conductor inner layer having a plurality of heat-conducting fibers with heat sink ends, and a structural support outer layer overlying the heat conductor inner layer. The structural support layer is made of a fiber-reinforced composite material. A layer of a structural adhesive bonds the respective heat conductor inner layer of each split shell segment to the battery cell housing. A thermal sink is in thermal contact with the sink ends of the plurality of heat-conducting fibers of each of the split shell segments, and the structural support outer layer of each split shell segment is joined to a structural base.
    Type: Grant
    Filed: May 9, 1996
    Date of Patent: June 9, 1998
    Assignee: Hughes Aircraft Company
    Inventors: John P. Stafford, Walter Rex Oswald, Susan K. Ferer, Matt H. Russell, Patrick B. Cooke, Michael Langmack, Robert K. Taenaka
  • Patent number: 5764414
    Abstract: A biocular display system (19) for generating a virtual image (30) of a visible display (20). A diffractive binary optical element (22) is used to create the virtual image (30). The binary optical element (22) contains magnifying power to increase the size of the virtual image (30). Also, the binary optical element (22) contains prismatic power to displace the virtual image (30) away from the display (20). Multiple displays (40), (42) may be viewed by employing a binary optical element (34) having multiple diffractive orders.
    Type: Grant
    Filed: August 23, 1993
    Date of Patent: June 9, 1998
    Assignee: Hughes Aircraft Company
    Inventors: William B. King, Chungte W. Chen
  • Patent number: 5756895
    Abstract: Various structures for cantilever beam tunneling rate gyro devices formed on a single substrate are disclosed. A cantilever electrode having a plurality of portions extending from the substrate with one end of the cantilever is suspended above the substrate at a distance from a tunneling electrode so that a tunneling current flows through the cantilever and tunneling electrode in response to an applied bias voltage. The cantilever and tunneling electrodes form a circuit that produces an output signal. A force applied to the sensor urges the cantilever electrode to deflect relative to the tunneling electrode to modulate the output signal. The output signal is a control voltage that is applied between the cantilever electrode and a control electrode to maintain a constant tunneling current. In the preferred embodiment, two cantilever portions extend from the wafer surface forming a Y-shape. In a further embodiment, a strap is fabricated on the cantilever electrode.
    Type: Grant
    Filed: September 1, 1995
    Date of Patent: May 26, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Randall L. Kubena, Gary M. Atkinson, Dorian Challoner, Wallace Sunada
  • Patent number: 5754042
    Abstract: An apparatus for detecting precise angular positions of a rotating object. Two magnetoresistors (MRs) are positioned adjacent a target wheel attached to the rotating object, the target wheel having at least one element of finite length. Each MR is responsive to the passage of at least one of the elements as the target wheel is rotated, generating an analog signal with signal transitions between two voltage levels at the passage of the element's leading and trailing edges. The MRs are positioned relative to the elements such that their signals are phase shifted with respect to one another, resulting in time overlapping signals which intersect at a precise angular positions of the target wheel.
    Type: Grant
    Filed: June 20, 1994
    Date of Patent: May 19, 1998
    Assignees: General Motors Corporation, Hughes Aircraft Company
    Inventors: Thaddeus Schroeder, Bruno Patrice Bernard Lequesne, Hiro Yamasaki
  • Patent number: 5752874
    Abstract: A grazing incidence optic is fabricated by grinding, polishing, or both, using a tapered, barrel-shaped tool. The optic surface to be ground or polished is placed in contact with a selected portion of the grinding or polishing surface of the tool, and the tool is rotated about its longitudinal axis. The optic is subjected to a reciprocating grinding movement along the length of the barrel tool. A helical groove in the tool allows slurry to pass between the optic surface being worked and the tool surface. Air is forced between the optic surface and the tool surface to release the optic from the tool.
    Type: Grant
    Filed: January 19, 1995
    Date of Patent: May 19, 1998
    Assignee: Hughes Aircraft Company
    Inventors: George W. Meyer, Jr., Steven S. Chuang
  • Patent number: 5749402
    Abstract: A method of loading propellant into a spacecraft that comprises storing and transferring propellant in a portable propellant loading tank, temperature conditioning and helium saturating the propellant in the propellant loading tank, transferring the loading tank to a launch site, coupling the loading tank to the propellant storage tank, and pressurizing the portable propellant loading tank to transfer the propellant to the propellant storage tank in the spacecraft. The method may further comprise weighing the propellant loading tank during propellant transfer, venting the propellant storage tank in the spacecraft to a receiver tank, and weighing the receiver tank during propellant transfer. The amount of propellant transferred to the propellant storage tank is equal to the difference between the measured weights of the respective loading and storage tanks.
    Type: Grant
    Filed: June 7, 1995
    Date of Patent: May 12, 1998
    Assignee: Hughes Aircraft Company
    Inventors: L. Scott Stotelmyer, Don K. Fulkerson
  • Patent number: 5751460
    Abstract: An articulated optical system has a pair of actuators (42, 44) each of which pivot a head mirror (34) about respective parallel axes (E.sub.1, E.sub.2) to direct the line-of-sight of an optical beam through a window (36) of a vehicle (30) to an optical sensor (38). Of the actuators, a coarse actuator (42) pivots the mirror (34) through substantially the entire desired field of regard of the optical system, and a fine actuator (44) pivots the mirror (34) for fine adjustment, e.g., less than five degrees. The coarse actuator (42) is positioned so that the axis thereof (E.sub.1) is located as close as possible to an edge of the mirror (34), so that the radial distance therebetween is small; therefore, the size of the window (36) is minimized with respect to the diameter (d.sub.b) of the optical beam. The fine actuator (44) is attached to approximately the geometric center of the mirror (34), so that the mirror (34) is statically balanced about the elevation axis (E.sub.
    Type: Grant
    Filed: October 11, 1995
    Date of Patent: May 12, 1998
    Assignee: Hughes Aircraft Company
    Inventors: John P. Harrell, Bryce A. Wheeler
  • Patent number: 5750901
    Abstract: A measurement optical fiber is placed into contact with a geological structure, and a reference optical fiber of about the same length is not contacted to the geological structure. An input beam of light is transmitted down the lengths of the measurement and reference optical fibers, and the interference fringes formed between the reflected beams in the two optical fibers are counted to determine the geological displacement, and thence the geologic strain, experienced by the measurement optical fiber. Preferably, multiple pairs of the measurement and reference optical fibers are used, the optical fibers of the various pairs being of different lengths. The difference in displacement measured by any two pairs is a measure of the geological strain in the region between the ends of the two pairs. The multiple pairs are conveniently provided in two optical fiber cables, a measurement cable which contacts the geological structure and a reference cable which extends parallel and adjacent to the measurement cable.
    Type: Grant
    Filed: June 7, 1995
    Date of Patent: May 12, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Victor Vali, I-Fu Shih, Kenn S. Bates
  • Patent number: 5750896
    Abstract: Detection and gauging of a joint (18) in a rotating and axially moving drilling tool (16) subject to transverse axial displacement is achieved by positioning an ultrasonic sensor assembly (12) coaxially encircling the tool in a plane perpendicular to the tool. The sensor assembly (12) generates more than one reflected pulse to represent changes in tool (16) diameter by transmitting a beam from at least one ultrasonic sensor (32) toward the tool (16) as the tool axially advances or recedes, perpendicularly piercing the plane of the sensor assembly (12). Each reflected pulse is converted to an electrical output signal, all of which signals are summed to minimize measurement distortion due to noise and transverse axial displacement of the rotating tool and compared to a threshold detection voltage in a signal processor (14) to generate a detection output pulse.
    Type: Grant
    Filed: July 22, 1994
    Date of Patent: May 12, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Felix E. Morgan, Randall S. Page, Sam D. Monaco
  • Patent number: 5751867
    Abstract: An intensity modulator having a Mach-Zehnder structure with first and second waveguide arms formed of an electro-optic polymer. The active molecules of the waveguide arms are poled in first and second different and substantially orthogonal directions. Electrodes are arranged to receive a modulating voltage and generate first and second electric fields which are respectively aligned with the first and second directions. As a consequence, the modulation depth of an optical signal which is transmitted through the modulator is substantially insensitive to the polarization of the signal. Other embodiments combine mode splitters and combiners with first and second Mach-Zehnder modulators which have electro-optic polymer waveguides. The active molecules of the arms of the two Mach-Zehnder modulators are poled in orthogonal directions.
    Type: Grant
    Filed: January 26, 1996
    Date of Patent: May 12, 1998
    Assignee: Hughes Aircraft Company
    Inventors: James H. Schaffner, Daniel Yap
  • Patent number: 5744284
    Abstract: A method for fabricating resilient z-axis contacts to electrically interconnect IC wafers or MCMs in 3-D integrated circuits uses photolithography to provide larger carrier sizes, higher contact densities by decreasing the spacing, smaller contact footpads, and precise control of the contact's shape and position. The contacts are fabricated by forming photoresist patterns on the carrier's top and bottom surfaces that are initially rectangular, and then reflowing the photoresist materials to provide smooth surfaces suitable for forming the metal contacts, and depositing metal layers over the respective patterns. Second photoresist patterns are formed over respective metal layers to conform with the contact's shape, the metal is etched away according to the pattern, and the photoresists are removed such that the remaining metalization forms a resilient z-axis contact that is attached to the carrier and extends therefrom with a predetermined shape.
    Type: Grant
    Filed: April 9, 1997
    Date of Patent: April 28, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Soyeon P. Laub, Michael J. Little, James A. Foschaar, Hugh L. Garvin, Michael W. Yung
  • Patent number: 5740037
    Abstract: The present invention relates to a method and device for providing a graphical user interface between an individual soldier and a computer-based warfare system worn by him. The graphical user interface is made up of icon-based visual control and information screens that the soldier views on a display and manipulates with a computer mouse-like device. The interface allows the individual soldier to: view information gathered by a variety of sources, including sensor components, radios, and satellites; process information using a variety of input devices and software utilities; and, act on that information using weapons, communications devices, and the like. The graphical user interface organizes information into three distinct "combat task" groups and provides the soldier with easily understood pictorial icons to select. By tailoring the information to a particular situation, the graphical user interface allows the soldier to view critical data without being overwhelmed by too much information.
    Type: Grant
    Filed: January 22, 1996
    Date of Patent: April 14, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Thomas E. McCann, Andrew Ausman, Douglas M. Kavner, Michael W. Brogan, Larri Rosser, John R. Tiffany
  • Patent number: 5731750
    Abstract: The present invention discloses a microwave filter (10) for controlling the degenerate resonant modes of a spherical cavity resonator (12). The spherical cavity resonator (12) has an inner spherical surface (14) which defines a spherical cavity (16). A first and a second set of tuning elements (18) extend inward from the inner spherical surface (14) of the resonator (12) into the spherical cavity (16). One of the first set of tuning elements is located near an electromagnetic field peak, either a radial electric field peak or a surface magnetic field peak, of at least one of the degenerate modes for tuning a resonance thereof. One of the second set of tuning elements is located between electromagnetic field peaks, either radial electric or surface magnetic field peaks, of degenerate modes in at least one pair of the degenerate modes for intercoupling thereof.
    Type: Grant
    Filed: January 29, 1996
    Date of Patent: March 24, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Paul J. Tatomir, Ku'ulei C. Kent, Rolf Kich
  • Patent number: 5732043
    Abstract: A method for selecting a set of four target bearings from a plurality of bearing measurements to optimize rapidity, accuracy and stability of a target track solution in a bearings-only target motion algorithm. Four bearings are selected to generate the deterministic solution by first selecting a candidate bearing set, then computing a set of "n" solutions from the candidate set and others adjacent thereto. Motion parameters are then computed, and any solution exhibiting parameters outside a user defined deviation from the mean is discarded. The mean target parameters of the remaining solutions may again be computed, and further culling out performed, until the desired distribution is achieved. An optimal solution is chosen as the solution from the remaining sample space that is closest to the mean in target range, course and speed.
    Type: Grant
    Filed: June 12, 1990
    Date of Patent: March 24, 1998
    Assignee: Hughes Aircraft Company now known as Hughes Electronics
    Inventors: Dien V. Nguyen, Fredrick A. Steiner, Richard H. Scales
  • Patent number: 5731708
    Abstract: A portable integrated circuit die testing system that offers a cost-effective solution for electrically testing bare, unpackaged, integrated circuit chips or die. The system provides for direct electrical interconnection of die of various sizes and thicknesses to an automatic tester without wire bonding or packaging of the semiconductor chip or die. The system includes an X-Y table that is adjustable in horizontal X and Y directions. A contact platform is disposed above the X-Y table that has an opening therein, and is movable in a vertical direction relative to the X-Y table. An adjustment member is coupled to the contact platform for finely adjusting the movement thereof in the vertical direction. A die holder is secured to the X-Y table for holding the die that is to be tested, and in response to movement of the X-Y table. A vacuum connection is provided for drawing a vacuum on the tested die to secure it in the die holder.
    Type: Grant
    Filed: October 31, 1995
    Date of Patent: March 24, 1998
    Assignee: Hughes Aircraft Company
    Inventor: Mohi Sobhani
  • Patent number: 5731222
    Abstract: Recesses (46) are etched into the finished peripheral boundaries of a structure formed of a generally planar electronic circuit (40) on an upper surface (42) of a wafer (44). Bonding pads (48) are deposited in the recesses (46) and interconnected to the electronic circuit (40). External leads (52) are attached to the bonding pads (48), such that the external leads (52) lie below the plane of the electronic circuit (40).
    Type: Grant
    Filed: August 1, 1995
    Date of Patent: March 24, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Gerard T. Malloy, Joe B. Tyra
  • Patent number: 5729016
    Abstract: A low cost night vision system for use in connection with law enforcement vehicles, marine vessels, and other nonmilitary surface vehicles. The invention includes a night vision camera having an array of uncooled detectors. A mechanism is provided for adjusting the pointing angle of the night vision camera in response to scan control signals. Output signals from the uncooled detectors are further processed into a standard video format and displayed on a conventional display located, for example, within a vehicle or marine vessel.
    Type: Grant
    Filed: August 26, 1996
    Date of Patent: March 17, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Stuart H. Klapper, Howard Laitin, Alex L. Kormos, Lacy G. Cook, David M. Masarik, Paul R. Salvio
  • Patent number: 5729230
    Abstract: A continuous-time tunable Gm-C architecture for a .DELTA..SIGMA. modulator includes a tunable resonator and a low bit rate, high sample rate quantizer connected in a feedback loop. The resonator shapes the quantization noise spectrum so that the bulk of the quantization noise occurs outside the signal spectrum. A tunable Gm cell tunes the resonator's resonant frequency to maximize the modulator's SNR. The tunable Gm cell includes a fixed Gm cell having transconductance G.sub.f, a current divider and a recombination circuit that together effectively multiply G.sub.f by a factor .alpha., where -1<=.alpha.<=1, without effecting the cell's common mode current I.sub.cm. A positive current source supplies I.sub.cm, while maintaining a common mode resistance of R/2 and a theoretically infinite differential mode resistance. Thus, the resonator's resonant frequency can be varied from DC to approximately 1 Ghz while maintaining a stable common mode operating point and improving the modulator's quality factor.
    Type: Grant
    Filed: January 17, 1996
    Date of Patent: March 17, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Joseph F. Jensen, Gopal Raghavan, Albert E. Cosand
  • Patent number: 5727000
    Abstract: Test equipment and test methods employing signature analysis to achieve fault isolation of parts contained in digital modules. Fault free signatures of a digital module are stored in a lookup table that are derived from physical measurement or simulation of all parts. All of the parts in the functional digital module are shorted and opened (either physically or by simulation) and each of their resulting faulty signatures are recorded in a storage device. Each signature with its corresponding faulty part is stored in the lookup table or memory. Test input signals are then applied to a tested digital module, and outputs of all parts thereof are applied to masking circuitry which allows sequential selective masking of all parts but one, for each part on the tested digital module. Outputs of the masking circuitry are applied to a multiple input shift register signal analyzer that performs pass/fail signature analysis using the applied signals.
    Type: Grant
    Filed: December 27, 1995
    Date of Patent: March 10, 1998
    Assignee: Hughes Aircraft Company
    Inventor: Stephen V. Pizzica
  • Patent number: 5726915
    Abstract: An automated system and method for testing a sensor by evaluating the output thereof with respect to a known target. The advantageous method includes the step of acquiring an output signal from the sensor in response to a known target, said output including signature signal S, random noise N.sub.R and fixed pattern noise N.sub.FP. Next, the sensor output signal is processed to provide a first signal which includes essentially signature signal S and fixed pattern noise N.sub.FP, a second signal which includes essentially random noise N.sub.R and a third signal which includes essentially fixed pattern noise N.sub.FP. The third signal is adaptively filtered to provide a filtered signal fixed pattern noise signal N'.sub.FP. The filtered signal N'.sub.FP is subtracted from the first signal to extract a signature S. In a particular embodiment, the signature is processed to acquire a modulation transfer function and a signal peak baseline therefrom.
    Type: Grant
    Filed: October 17, 1995
    Date of Patent: March 10, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Kenneth E. Prager, Robby Mauri