Patents Assigned to Hughes Aircraft
  • Patent number: 5770269
    Abstract: An article includes a substrate having a thermal control coating formed of 1 part by weight of a silicone polymeric matrix having from about 3 to about 4 parts by weight aluminum-doped zinc oxide pigment particles distributed therein. The article may be either relatively thick or flexibly thin, and the coating may be greater than 0.0015 inches thick so as to have a low solar absorptance. The coating has an absorptance of about 0.2-0.3 and an emittance of about 0.9, and is sufficiently electrically conductive to dissipate electrostatic charges.
    Type: Grant
    Filed: September 20, 1996
    Date of Patent: June 23, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Lynn E. Long, Joan L. Lum
  • Patent number: 5763882
    Abstract: A low cost infrared camera (1) for night vision. The camera (1) is disposed within a housing (2) having an infrared transmissive window (6) disposed at an input aperture (5) thereof. A compact optical arrangement (10) is disposed within the housing (2) to focus energy from the window (5) onto a focal plane array (20). A chopper disk (19) is positioned between the reflective optical arrangement (10) and the focal plane array (20) to establish a reference level for the array (20) and to facilitate a sequential readout thereof. A signal processing circuit (100) is included for processing the output of the array (20) for display on a standard video screen. Thus, the problems with uncooled detectors are overcome by use of a fast optical system in combination with an uncooled detector. The fast optical system provides a high signal level to the uncooled detector, thereby compensating for losses in collection of thermal radiation.
    Type: Grant
    Filed: November 18, 1996
    Date of Patent: June 9, 1998
    Assignee: Hughes Aircraft Company
    Inventors: Stuart H. Klapper, Lacy G. Cook
  • 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: 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: 5760667
    Abstract: A bandpass filter having 4-degrees of freedom includes a plurality of resonant cavities having respective Qs where at least one of the Qs is different. A plurality of main couplings couple successive resonant cavities to establish a main signal path that provides a first degree of freedom for controlling the shape of the filter's frequency response over its passband. A plurality of bridge couplings couple pairs of the resonant cavities so that the cavities are connected in a canonical circuit topology. The bridge couplings provide second and third degrees of freedom for controlling the sharpness of the frequency response 's transition between its passband and stopband and controlling the linearity of its phase, respectively. The cavities' non-uniform Qs provide a fourth degree of freedom for controlling the amplitude of the filter's frequency response in the passband so that the amplitude is within a predetermined tolerance of a desired passband shape.
    Type: Grant
    Filed: July 12, 1995
    Date of Patent: June 2, 1998
    Assignee: Hughes Aircraft Co.
    Inventors: Frederick A. Young, Richard L. Bennett, Keith N. Loi
  • Patent number: 5756160
    Abstract: The present invention comprises a method for protecting carbon composite materials from edge or surface damage during handling and manufacturing. The method comprises forming a protective silicon coating on selected surfaces of the carbon composite material to by forming a silicon bearing suspensoid coating on the surface of the carbon composite to be protected, and drying the suspensoid to a solid. In one embodiment, the suspensoid is formed by dissolving sodium silicate in water which is then mixed with an acid salt to form an irreversible gel. The suspensoid is either formed and then deposited on a surface area or formed in place through interactions between surface coatings of the separate compounds. The irreversible gel can be heated to remove the water and form a solid protective coating from the suspensoid.
    Type: Grant
    Filed: March 28, 1988
    Date of Patent: May 26, 1998
    Assignee: Hughes Aircraft
    Inventor: Wilson N. Pratt
  • 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: 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: 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: 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: 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: 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: 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: 5739268
    Abstract: A method is provided for preparing the surface of a cyanate ester polymer or composite for metal plating. The surface is treated with a preheated solution containing a compound selected from the group consisting of at least one quaternary ammonium hydroxide and at least one primary amine. The method of the invention operates to improve adhesion between the treated surface and a subsequently plated metal, such that the resulting cyanate ester polymer or composite may replace certain metallic components in such applications as aircraft, spacecraft, and automobiles given its highly conductive metallic coating.
    Type: Grant
    Filed: April 26, 1996
    Date of Patent: April 14, 1998
    Assignee: Hughes Aircraft
    Inventor: Camille I. Van Ast
  • 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: 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