Patents Assigned to Hughes Aircraft
  • Patent number: 5669251
    Abstract: A liquid carbon dioxide dry cleaning system that employs a rotating basket inside a dry cleaning vessel that is powered by hydraulic flow. The present invention is particularly useful as a dry cleaning system that uses liquid carbon dioxide as the cleaning agent. The dry cleaning system has a pressurized vessel containing a liquid carbon dioxide bath. The basket is disposed in the vessel and has a plurality of openings around its periphery. A plurality of roller bearings are disposed between the basket and the vessel that allow it to rotate within the vessel. A plurality of manifolds are disposed between the vessel and the basket that have nozzles that produce jets of liquid carbon dioxide that agitate the garments. The nozzles are aligned with the plurality of openings in the basket. A pump is coupled between the manifolds and the vessel for circulating the liquid carbon dioxide to produce the jets that clean the garments and rotate the basket.
    Type: Grant
    Filed: July 30, 1996
    Date of Patent: September 23, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Carl W. Townsend, Edna M. Purer
  • Patent number: 5671243
    Abstract: A surface-emitting laser system includes a laser that emits a vertically divergent beam generally parallel to the substrate on which it is formed, and a turning mirror in the path of the beam that extends up from the substrate to a level well above the laser height. The extended mirror area reflects a greater portion of the beam than prior planar designs, increasing the output efficiency and providing a smoother beam pattern. One fabrication method employs a masking and ion beam milling technique that uses an accumulation of redeposited material to form the additional mirror area, with a thick mask layer that is later removed guiding the redeposition. An alternate fabrication method involves epitaxial growth of an additional layer of material above the conventional laser epilayers, with the additional layer subsequently removed from the laser region but retained in the mirror region.
    Type: Grant
    Filed: September 19, 1996
    Date of Patent: September 23, 1997
    Assignee: Hughes Aircraft Company
    Inventor: Daniel Yap
  • Patent number: 5667171
    Abstract: Methods and systems for stabilizing satellite spin about an intermediate inertia axis (Z) are disclosed. A set of gyros (22) sense the X component and the Y component of the angular velocity of the satellite body. A single degree of freedom momentum wheel (26) has a fixed transverse orientation with respect to the intermediate axis in order to store momentum. In one embodiment, the momentum wheel (26) is oriented to store momentum parallel to the Y axis. A tachometer (30) senses the rotation rate of the momentum wheel (26). A processor (24) forms a control signal representative of a control torque to be applied to the momentum wheel (26). The control torque is based upon the X component and the Y component of angular velocity of the satellite, and the angular velocity of the momentum wheel (26).
    Type: Grant
    Filed: April 28, 1995
    Date of Patent: September 16, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Richard A. Fowell, John F. Yocum
  • Patent number: 5668842
    Abstract: A plurality of biphase modulators (42) each modulate a sinusoidal radio frequency signal based upon a corresponding one of a plurality of bits contained in a time-dependent data word. The biphase modulators (42) form a plurality of biphase modulated signals which are communicated to a summing network (40). The summing network (40) contains a plurality of attenuators (44) which attenuate the modulated signals to form a plurality of attenuated signals. The summing network (40) combines the attenuated signals to form a radio frequency signal.
    Type: Grant
    Filed: February 28, 1995
    Date of Patent: September 16, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Ronald E. Sorace, Victor S. Reinhardt, Steven A. Vaughn
  • Patent number: 5667621
    Abstract: Bonding of expanded polymeric parts together to produce lost foam molds suitable for casting metallic details is accomplished by applying a non-aqueous, adhesive-free coating comprising a polar, highly dielectric component contained in a liquid vehicle to the interfacing surface of at least one of the parts to be joined. The interfacing surfaces of the parts to be joined are held in contact while the assembly is irradiated with high frequency electromagnetic energy. This energy enables the coating to dielectrically heat the mated expanded polymeric parts until a bond is effected by melting the polymeric parts and inducing expansion of the parts into one another.
    Type: Grant
    Filed: May 19, 1995
    Date of Patent: September 16, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Thomas K. Dougherty, Norman H. Harris, James R. Chow
  • Patent number: 5666130
    Abstract: A method of operating a liquid crystal display, and a liquid crystal display constructed to operate in accordance with the method. The liquid crystal display has a plurality of display pixels, and the method comprises the steps of (a) operating a first switch (S1) for storing a charge on a storage capacitance (C1), the charge having a magnitude selected so as to cause a desired degree of polarization of a region (pixel) of liquid crystal material; (b) operating a second switch (S2) so as to conductively couple the stored charge to the region of liquid crystal material, thereby storing a charge on a capacitance (C2) that is associated with the region of liquid crystal material; and (c) operating a third switch (S3) so as to discharge the storage capacitance and the capacitance that is associated with the region of liquid crystal material.
    Type: Grant
    Filed: August 10, 1994
    Date of Patent: September 9, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Ronald L. Williams, Ronald M. Finnila
  • Patent number: 5665274
    Abstract: A spacecraft includes a spacecraft element, such as a deployable antenna, and a black paint on the spacecraft element. The paint has a composition of 100 parts by weight of a methyl phenyl silicone-based polymer, and from about 1.35 to about 3.5 parts by weight of an electrically conductive carbon pigment having a porous, sponge-like structure. The paint is applied by mixing these constituents with a solvent such as naphtha or xylene in an amount sufficient to permit the paint to be applied by a selected technique such as brushing or spraying.
    Type: Grant
    Filed: December 22, 1995
    Date of Patent: September 9, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Lynn E. Long, Martin R. Gallardo
  • Patent number: 5663728
    Abstract: A DAC converts a sequence of digital codewords into an approximately piecewise linear analog waveform that follows rising and falling edges between plateau levels. The DAC processes, in parallel, each bit of the codewords to produce component waveforms that are weighted according to their bits significance and summed together to produce the piecewise linear analog waveform. Waveform shaping circuits control the rise and fall times of each component waveform so that the analog waveform's rising and falling edges settle to within a desired error bound of a linear output ramp whose slope is a function of the difference between successive codewords and the rise or fall times. The rise and fall times are preferably approximately the same. Limiting switches control the plateau levels of the component waveforms so that the analog waveform's plateaus settle to within the desired error bound of the ideal values represented by the codewords.
    Type: Grant
    Filed: May 18, 1995
    Date of Patent: September 2, 1997
    Assignee: Hughes Aircraft Company
    Inventor: Kenneth A. Essenwanger
  • Patent number: 5663583
    Abstract: An epitaxial structure and method of manufacture for a field-effect transistor capable of low-noise and power applications. Preferably, the epitaxial structure includes an N-type barrier layer comprising a wide-gap semiconductor material having the formula Al.sub.1-y Ga.sub.y P.sub.0.71+z Sb.sub.0.29-z.
    Type: Grant
    Filed: June 6, 1995
    Date of Patent: September 2, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Mehran Matloubian, Takyiu Liu, Chanh Nguyen
  • Patent number: 5663095
    Abstract: A micro-dimensional coupling conductor with a shape that is customized for a particular electronic device. A fabrication method is used in which the physical dimensions of the conductor are precisely controlled with photolithographic techniques, resulting in a conductor that is more precisely tuned to the operating frequency of the device. The conductor is fabricated on an SiO.sub.2 substrate using vacuum deposition or electroplating techniques. After fabrication, the conductor is separated from the SiO.sub.2 substrate by dissolving the SiO.sub.2. Alternatively, the conductor may be fabricated on a Teflon.TM. substrate. The use of a Teflon substrate allows a user to remove the conductor from the substrate by applying a small mechanical force to the conductor.
    Type: Grant
    Filed: May 24, 1995
    Date of Patent: September 2, 1997
    Assignee: Hughes Aircraft Company
    Inventor: LeRoy H. Hackett
  • Patent number: 5658181
    Abstract: A die is disclosed for applying radial force to an eccentric workpiece. The die includes a set of faces that are each inclined from an orthogonal relationship with a different radial plane of the workpiece by an offset angle. The die also includes wedges that are positioned on the faces. They each have a jaw surface and a slide surface that are inclined from a parallel relationship with each other by a wedge angle that equals the offset angle of their respective face. The wedges can move over the faces to abut the workpiece along each of a plurality of transverse planes. In each of these planes, their movement can accommodate the workpiece's eccentricity in that plane. In addition, each jaw surface abuts the workpiece in a tangential relationship.
    Type: Grant
    Filed: September 11, 1995
    Date of Patent: August 19, 1997
    Assignee: Hughes Aircraft Company
    Inventor: Richard A. Brown, II
  • Patent number: 5655210
    Abstract: A corona source suitable for use in vehicle ignition systems uses a conductive coil that receives an RF input at one end and has a corona discharge site at the other end, with a reference electrode capacitively coupled to the coil. The pitch and the length of the coil are selected to produce a corona discharge in response to an RF input signal at a predetermined frequency and voltage, through quarter wavelength resonation. Either the new resonant coil or other corona discharge devices can be used to remediate fluid-borne wastes by initiating and sustaining RF corona discharges within the fluid. The pulses used to initiate the corona discharge preferably have alternating positive and negative components, with high initial voltages on the positive components to initiate the discharge, followed by lower positive voltage levels to sustain the discharge. Unipolar pulses, preferably with progressively decreasing voltage levels, can also be used.
    Type: Grant
    Filed: May 31, 1995
    Date of Patent: August 5, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Daniel J. Gregoire, Robin J. Harvey, Franklin A. Dolezal, Weldon S. Williamson
  • Patent number: 5651495
    Abstract: An improved method for soldering a thermoelectric cooler between an electronic device and a heatsink. Thermoelectric coolers are assembled by soldering parts together using a first solder. The bottom surface of the thermoelectric cooler is first soldered to the heatsink using a second solder and then the top surface is soldered to the electronic device using a third solder preferably having the same melting point as the second solder, or having approximately the same melting point as the second solder. Reverse powering of the thermoelectric cooler assists the soldering of the top surface to the electronic device by heating the top surface to a temperature sufficient to melt the third solder while cooling the bottom surface of the thermoelectric cooler to a temperature lower than the melting point of the second solder.
    Type: Grant
    Filed: December 14, 1993
    Date of Patent: July 29, 1997
    Assignee: Hughes Aircraft Company
    Inventors: John L. Tocher, Jacques F. Linder
  • Patent number: 5652448
    Abstract: The gate structure for a nonvolatile memory device comprising an EEPROM and a latch transistor is fabricated on a substrate by patterning the EEPROM's floating gate in a first polysilicon layer, patterning the EEPROM's control gate over the floating gate in a second polysilicon layer, and then collectively patterning the second and first layers to form the latch transistor's stacked gate. The stacked gate includes a thin gate that is electrically connected to the EEPROM floating gate and a protective layer over and electrically isolated from the thin gate. The stacked gate design eliminates unwanted polysilicon spacers between the latch transistor's channel and its drain and source regions, which improves the control of the memory device. The protective layer prevents ion penetration during the implantation of the latch transistor's drain and source regions.
    Type: Grant
    Filed: August 2, 1996
    Date of Patent: July 29, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Chen-Chi Peter Chang, Mei F. Li, Truc Q. Vu
  • Patent number: 5651180
    Abstract: The present invention provides a method and apparatus for metallizing vias in co-fired ceramic green tape. A vacuum operated pick and place anvil comprising a porous block is used to pick up conductor balls from a bed. Air pressure is used to create a vacuum which pulls the conductor balls to the porous block. A stencil having openings is placed on a contact surface of the anvil, thereby permitting only one conductor ball to attach to each opening in the stencil. With the conductor balls attached to the anvil, the anvil is lowered onto the green tape. Next the anvil pushes the conductor balls into the tape until the conductor balls break through the opposite side of the tape. The anvil is retracted leaving the conductor balls lodged in the tape. It is possible to provide a green tape with pre-formed vias so that forcing the conductor balls into the tape is a simpler task.
    Type: Grant
    Filed: August 24, 1995
    Date of Patent: July 29, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Richard P. Himmel, Raymond Brown
  • Patent number: 5652586
    Abstract: A Sigma Rho A/D converter (10) includes a transconductance element (R) having an input node for receiving an input voltage signal V.sub.in and an output node providing an analog current I.sub.in ; a charge integrator (12) having an input coupled to the output node, the charge integrator having feedback provided by an integrating capacitor C and an output node providing an output signal V.sub.o ; and a clocked voltage comparator (14) having an input coupled to V.sub.o for comparing V.sub.o to a reference potential. An output of the comparator updates in response to an occurrence of a first clock signal CLK1. A current sink (16) is switchably coupled to the output node of the transconductance element as a function of the logic state of the output of the comparator.
    Type: Grant
    Filed: March 17, 1995
    Date of Patent: July 29, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Thomas Y. Chuh, Arthur L. Morse
  • Patent number: 5652512
    Abstract: Digital logic comprising a high speed analog to digital converter, a high speed analog to digital converter, a digital multiplier, and an infinite impulse response filter and decimation circuit are used to digitize a magnetic signal that is subsequently processed by magnetic data processing algorithms. The high resolution digital to analog converter is directly incorporated in a feedback loop of a magnetometer sensor, and an expensive precision analog to digital converter is replaced by a less expensive, lower power digital to analog converter. The improvement provided by the present invention includes a high speed analog to digital converter coupled between the oscillator and a first input of a multiplier, and a second analog to digital converter that is coupled between the sense coil of the sensor and a second input of the multiplier. The output of the multiplier is coupled to an infinite impulse response filter and decimation circuit that produces the digital output signal from the magnetometer.
    Type: Grant
    Filed: April 23, 1996
    Date of Patent: July 29, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Paul L. Feintuch, Eric K. Slater, Kirk Kohnen
  • Patent number: 5652696
    Abstract: A high frequency microwave integrated circuit assembly (14,20) includes a fragile monolithic microwave integrated circuit (MMIC) chip (22) mounted in an MMIC subassembly (20) that is completely assembled, tested and burned in independent of the main high frequency microwave integrated circuit assembly and is mechanically attached to the main assembly by a captivation screw (100). The MMIC chip (22) is bonded to an uppermost tier (30) of a multi-tier spaced pedestal (26) and is received within an aperture (46) within a slave board (44) that itself is mounted and bonded to a lower tier (28) of the pedestal (26). The main integrated circuit assembly is formed with a rectangular opening (84) in an upper portion of its substrate to non-rotationally receive the rectangular slave board and a slightly larger internally threaded circular hole (94) in a lower portion of the main assembly substrate that threadedly receive the captivation screw (100).
    Type: Grant
    Filed: September 25, 1995
    Date of Patent: July 29, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Patrick A. Traylor, Richard A. Holloway
  • Patent number: 5652534
    Abstract: A phase shifter that employs digital circuitry to achieve arbitrarily fine phase control of reference signals at frequencies extending to the Gigahertz region. The phase shifter includes a cascade of identical phase shift units that provide progressively finer phase control resolution over a full 360 degree range. The phase precision is set by the number of stages used.
    Type: Grant
    Filed: December 21, 1995
    Date of Patent: July 29, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Stephen D. Taylor, Steve I. Hsu, Howard S. Nussbaum, William P. Posey
  • Patent number: 5651276
    Abstract: Substantial amounts of particulate soils in garments can be removed by agitation in gas-jet in a solvent-free, low-pressure environment. The ability of the present gas-jet agitation system to remove particulate soils from garments and fabrics rivals that of conventional dry-cleaning processes which agitate the garments and fabrics while immersed in solvent. Thus, a dry-cleaning operation may consist of a solvent-immersion step for removing soluble soils and a gas-jet agitation step to remove particulates. Considerable savings in equipment and operating costs may be realized in the practice of the invention, since solvent flow rates need not be boosted to provide necessary agitation for particulate soil removal. The savings achievable by employing gas-jet agitation are even more pronounced in dense phase gas dry cleaning systems, which require pressurized environments to maintain a liquified solvent.
    Type: Grant
    Filed: January 26, 1996
    Date of Patent: July 29, 1997
    Assignee: Hughes Aircraft Company
    Inventors: Edna M. Purer, Angela Y. Wilkerson, Carl W. Townsend, Sidney C. Chao