Patents Represented by Attorney David W. Collins
  • Patent number: 5911583
    Abstract: A three-dimensional stacked electrical circuit assembly that uses spherical or cylindrical metallic contacts that are surface mounted to input and output pads of circuit substrates that contact recessed wire button contacts disposed in cavities formed in a nonmetallic spacer disposed between the substrates. Each metallic contact fits into a through hole in the spacer and makes contact with a separate wire button contact in the through hole of the spacer. The metallic contacts are recessed within the spacer and are protected from contamination and handling damage. Back-to-back spacers may be employed that use plungers to make contact between wire button contacts disposed therein. The wire button contacts are recessed in the through holes, which provides for an interconnect system having low contact resistance, high current capacity, low contact force, and the ability to customize the shape of the spacer.
    Type: Grant
    Filed: November 24, 1997
    Date of Patent: June 15, 1999
    Assignee: Raytheon Company
    Inventors: Ty J. Roybal, Stephen R. Stegura, Peter J. Drake
  • Patent number: 5909190
    Abstract: A processor and method for discriminating against interference during target acquisition and reacquisition processing of densely cluttered images. The processor and method that adaptively estimates the feature probability density function of the interference from the image data. The estimated interference probability density function, along with target feature estimates are input to a Bayesian classifier that discriminates the interference from the target.
    Type: Grant
    Filed: October 30, 1997
    Date of Patent: June 1, 1999
    Assignee: Raytheon Company
    Inventors: Thomas K. Lo, W. Scott Johnston
  • Patent number: 5903659
    Abstract: An adaptive method for removing fixed pattern noise from focal plane array (FPA) imagery. A set of correction terms is applied to the focused image from the FPA, and a filter is applied to the corrected, focused image. The set of correction terms is also applied to a blurred version of the FPA image, and the filter is applied to the corrected, blurred image. Fixed pattern noise errors are then calculated using the filtered imagery, and employed to update the correction terms. The updated correction terms are then used for processing the next image. In one embodiment, the filter is an anti-median filter. In another embodiment, the filter is an anti-mean filter.
    Type: Grant
    Filed: April 17, 1997
    Date of Patent: May 11, 1999
    Assignee: Raytheon Company
    Inventor: Patrick M. Kilgore
  • Patent number: 5884864
    Abstract: A missile has a body with a substantially circular nose opening therein, and a ceramic radome sized to cover the nose opening. A compliant metallic circular transition element is disposed structurally between the radome and the body. The transition element includes an elongated compliant arm region and a crossbar region positioned adjacent to the radome such that a lower margin surface of the radome rests against an upper side of the crossbar region. A brazed butt joint is formed between the lower margin surface of the radome and the upper side of the crossbar region of the transition element. A second brazed lap joint is formed between the vehicle body and the elongated compliant arm of the transition element.
    Type: Grant
    Filed: September 10, 1996
    Date of Patent: March 23, 1999
    Assignee: Raytheon Company
    Inventors: Wayne Sunne, Oscar Ohanian, Edward Liguori, Michael Kevershan, James Samonte, James Dolan
  • Patent number: 5867307
    Abstract: A blur film is made of a polymeric film material transmissive to infrared energy of a selected waveband, which is affixed to a surface of a substrate transmissive to energy of the same selected infrared waveband. The blur film has a texture or a plurality of lenslets thereon, where the surface of each lenslet is a surface of revolution. In a spatial-filter wheel application, the blur film and substrate are affixed to a support, which in turn is rotatably mounted on a drive. The support is structured such that a portion of its circumference is covered by the blur film and a portion of its circumference is not covered by the blur film. The spatial-filter wheel is rotated in front of a detector to produce alternating blurred and direct images on the detector.
    Type: Grant
    Filed: November 13, 1996
    Date of Patent: February 2, 1999
    Assignee: Raytheon Company
    Inventors: James R. Myers, David R. Smith, Daniel W. Brunton, Stephen M. Jensen, Nicholas B. Saccketti, Scott W. Sparrold, Lawrence A. Westhoven
  • Patent number: 5853149
    Abstract: A missile having an improved dome mounting arrangement, and a method for mounting a sapphire dome to a titanium missile turret that provides for minimum surface deformation and environmental sealing of the dome. A sealing material such as silicone rubber compound that is capable of enduring high temperatures attained during high speed missile flight is employed. The missile has a body with a nose and the dome mounting arrangement is attached to the nose. The dome mounting arrangement comprises a turret secured to the nose, the dome, and a retainer ring attached to the turret for securing the dome to the turret. An annular gap is formed between an outer surface of the dome and an inner surface of the retainer ring. The silicone rubber compound is disposed in the annular gap and cured to seal the dome. A plurality of shims may be disposed between the dome and the turret in a radial gap formed therebetween.
    Type: Grant
    Filed: April 8, 1996
    Date of Patent: December 29, 1998
    Assignee: Raytheon Company
    Inventors: Peter H. Vo, John F. Binnie, Jr.
  • Patent number: 5837090
    Abstract: A first article having a bore therein is provided with a chamfer region at one end of the bore. A second article is assembled into the bore with a clearance region therebetween, preferably using tooling to hold the articles in precisely the desired positions. A flowable, thermosetting adhesive is placed into the chamfer region. The assembly is heated so that the adhesive flows from the chamfer region into the clearance region, and the adhesive is thereafter cured to join the articles together as defined by the tooling.
    Type: Grant
    Filed: December 8, 1994
    Date of Patent: November 17, 1998
    Assignee: Raytheon Company
    Inventors: John F. Binnie, Jr., Keith W. Everill, Roderick M. Harris
  • Patent number: 5831873
    Abstract: A target's magnetic dipole includes both a permanent component and an induced component that is caused by the interaction of the target at a given heading with the ambient magnetic field. In order to accurately classify targets, a library of characterization matrices is built for a plurality of candidate targets. The matrices characterize what the magnetic dipoles would be in a given ambient magnetic field at a particular heading. In practice, some localization algorithm is used to provide a target's magnetic dipole and heading. Magnetic dipoles for each of the candidate targets are predicted using the target's heading, the ambient magnetic field, and the characterization matrices. The target is then classified as the candidate target(s) providing the best match to the target's measured magnetic dipole.
    Type: Grant
    Filed: January 27, 1997
    Date of Patent: November 3, 1998
    Inventors: Kirk K. Kohnen, Harold C. Gilbert, Wilbur W. Eaton, Jr.
  • Patent number: 5806791
    Abstract: A jet vane control system and method for a missile in which the system is compact, rugged, lightweight and detachably connected to the aft end of a missile. The system provides for very quick pitch over and roll control during launch. The system then detaches from the missile so as not to burden the missile during its flight to target. The vanes of the system are divided into quadrants, each having its own, mounting support and gear train assembly. Each vane is also connected through a, detachable coupling to the steering control system of the missile such that actuation of the steering control system simultaneously actuates the jet vane control system.
    Type: Grant
    Filed: May 26, 1995
    Date of Patent: September 15, 1998
    Assignee: Raytheon Company
    Inventors: William M. Hatalsky, Andrew B. Facciano, Stephen D. Haight, Sean A. Johnson, Aszetta D. Jordan
  • Patent number: 5794889
    Abstract: A fire retardant delivery system for delivering fire retardant onto a fire. The system 10 includes an aircraft comprises a fire retardant storage and ejection system, and a stabilized three axis gimbal system for providing signals indicative of angle and angle rates of a gimbal with respect to an axis of the aircraft. An infrared sensor system is disposed on stabilized three axis gimbal system. A display is coupled to infrared sensor system for displaying an image produced thereby to a pilot of the aircraft. Aircraft sensors are provide signals indicative of the velocity, altitude, and dive angle of the aircraft. A computer is coupled to the infrared sensor system, to the aircraft sensors, and to the fire retardant storage and ejection system, for computing distance between the aircraft and a hot spot in the fire and for computing an optimal release point for ejecting fire retardant from the aircraft onto the fire.
    Type: Grant
    Filed: June 6, 1995
    Date of Patent: August 18, 1998
    Assignee: Raytheon Company
    Inventor: James D. Bailey
  • Patent number: 5794509
    Abstract: An actuator system having a motor that drives a pneumatic spool valve to a known position based upon the number of step commands delivered to it. Valve ports or passages uncovered by the net position difference between the spool valve and a piston create gas flow to or from a control chamber. This gas flow causes a pressure differential across the face of the piston, inducing the piston to follow the spool valve. In this two-stage system, the piston acts as a force amplifier so that large forces and/or inertias may be actuated by positioning the motor. During steady state conditions, the piston achieves the same position as the spool valve is. Proportional control and very accurate positioning of the piston are provided without active position or position rate feedback control.
    Type: Grant
    Filed: June 6, 1995
    Date of Patent: August 18, 1998
    Assignee: Raytheon Company
    Inventors: Charles M. DeLair, Russell B. Cline
  • Patent number: 5786788
    Abstract: A system (10) for reducing range sidelobes adapted for use with pulsed radar systems. The inventive system (10) includes a mismatched filter (90) for correlating a received signal (84) with a correlator signal (92) having a different length than the transmit signal (84) and for providing a predetermined number of reduced range sidelobes (97) at the output of the mismatched filter (90). The mismatched filter (90) has a first locally optimum sequence that is the correlator signal (92). The mismatched filter (90) has an input device (86) for receiving an extended locally optimum sequence (84) that is a received signal (84). The first locally optimum sequence (92) is a sub-sequence of the extended locally optimum sequence (84). In a specific embodiment the mismatched filter (90) has a Barker-based code that is the correlator signal (92). The mismatched filter (90) has an input device (86) for receiving an extended Barker-based code that is a received signal (84).
    Type: Grant
    Filed: October 8, 1996
    Date of Patent: July 28, 1998
    Assignee: Raytheon Company
    Inventors: Michael B. Schober, Carlos A. Davila
  • Patent number: 5786786
    Abstract: A photonic radar decoy (50) is provided which simulates an aircraft to a radar having an interrogating signal. A plurality of receiving antenna (52, 54, 56, 58, 60) are attached to the decoy (50) with each of the receiving antenna (52, 54, 56, 58, 60) independently capable of receiving the interrogating signal from the interrogating radar system. Each signal received by an antenna (52, 54, 56, 58, 60) is transmitted to a signal combiner and amplifier (82) by delay lines (72, 74, 76, 78, 80). The combiner and amplifier (82) coherently adds the transmitted signals, thereby producing a coherent signal which is amplified and subsequently emitted by a non-directional transmission antenna 106, simulating a dynamic and complex radar signature of an aircraft.
    Type: Grant
    Filed: March 17, 1997
    Date of Patent: July 28, 1998
    Assignee: Raytheon Company
    Inventor: James G. Small
  • Patent number: 5774331
    Abstract: A miniaturized manportable tactical workstation that has a single power supply that provides power for all of the electronic components thereof. The portable workstation includes a housing having a rotatable top cover that houses a display panel. The top cover is opened to expose a screen of the display panel. The housing encloses a hard drive receiver into which a removable hard drive is inserted. A two-slot VME processor box is disposed in the housing and receives a VME processor card that is slid into the VME processor box from one side of the workstation. An air filter and a fan are disposed in the housing and draw air through the housing to cool the electronic components of the workstation. A keyboard is provided that is exposed to a user when the top cover is opened to expose the display screen. The single power supply provides supply voltages and timing signals to the display panel, the keyboard, the VME processor card, the hard drive, and the fan.
    Type: Grant
    Filed: October 6, 1997
    Date of Patent: June 30, 1998
    Assignee: Raytheon Company
    Inventor: Gary M. Sach
  • Patent number: 5769020
    Abstract: Platforms on a vessel in motion are stabilized relative to one another and relative to the vessel. Primary sensors sense the position and orientation of the vessel's center of mass, which it uses as a common reference. Secondary sensors sense local platform motion to compensate for positional variations due to the vessel flexing or other localized motion. A computational system processes secondary position information relative to the common reference and calculates adjustments required to stabilize the localized platforms. By using secondary sensors in conjunction with the primary sensors, the platforms are stabilized in real time without accumulation of position error over time and are capable of being synchronized to each other.
    Type: Grant
    Filed: June 16, 1997
    Date of Patent: June 23, 1998
    Assignee: Raytheon Company
    Inventor: Steven E. Shields
  • Patent number: 5768453
    Abstract: Methods and apparatus are disclosed for concentrating the energy of a laser diode beam by imaging a first numerical aperture of the beam in one beam plane to a reduced numerical aperture at a focal plane, and by guiding the beam between reflective boundaries to maintain the value of a lesser second numerical aperture in another beam plane at the focal plane. The reduced numerical aperture in the first plane optimally matches the second numerical aperture in the second plane so that the energy can be received into the entrance end of an optical fiber whose numerical aperture also matches the second numerical aperture. The area of this fiber preferably matches that of the image at the focal plane. A coupler that guides the beam to its focal plane preferably utilizes an imaging element, e.g., a cylindrical lens or a cylindrical elliptical mirror, and a pair of spaced reflective walls.
    Type: Grant
    Filed: December 13, 1994
    Date of Patent: June 16, 1998
    Assignee: Raytheon Company
    Inventor: Leland V. Gardner
  • Patent number: 5758845
    Abstract: A vehicle having a ceramic radome includes a vehicle body having an opening therein, a ceramic radome sized to cover the opening of the vehicle body, and an attachment structure joining the radome to the vehicle body to cover the opening. The attachment structure has a substantially cylindrically symmetric compliant metallic transition element disposed structurally between the radome and the body. The radome is joined to a first end of the transition element by a first brazed butt-joint. A primary seal is disposed between the transition element and the vehicle body. A spanner nut overlies the transition element and has a first engagement to the transition element. A threaded engagement between the spanner nut and the vehicle body allows the radome/transition element assembly to be attached and tightened to the vehicle body and to be later removed.
    Type: Grant
    Filed: September 9, 1996
    Date of Patent: June 2, 1998
    Assignee: Raytheon Company
    Inventors: Wayne Sunne, Eric Ek
  • Patent number: 5116915
    Abstract: A method is disclosed for controlling the polymerization process of olefinic hydrocarbons in an inert solvent which provides continuous control of Mooney viscosity and molecular weight distribution of the obtained polymer. In the disclosed method, means (4, 5) are included for measuring the temperature of a polymer solution in different parts of a reactor (1) provided with agitation (2), as well as means (6) for measuring the dynamic or kinematic viscosity of the polymer solution and means (7) for measuring the polymer concentration in the solution. A valve (8) mounted on the catalyst feed line controls the catalyst flow rate. A computer (9) is used to control the entire process by calculating the Mooney viscosity from the dynamic viscosity and polymer concentration and adjusting the process parameters as necessary to achieve a pre-set Mooney viscosity.
    Type: Grant
    Filed: December 28, 1987
    Date of Patent: May 26, 1992
    Assignee: Giprokautchuk
    Inventors: Ulchar A. O. Mamedov, Anatolyi E. Tokar, George J. Elbaum
  • Patent number: 5087435
    Abstract: A fused compact of polycrystalline diamond is formed by dynamically shocking either fine diamond crystals or a mixture of fine diamond crystals and graphite.
    Type: Grant
    Filed: May 26, 1987
    Date of Patent: February 11, 1992
    Assignee: California Institute of Technology
    Inventors: David K. Potter, Thomas J. Ahrens
  • Patent number: 5057902
    Abstract: A novel process is provided for fabricating transistors (14), contacts (46s, 40g, 46d) and interconnections (46c) in a novel self-aligned configuration. The process of the invention permits higher packing densities, and allows feature distances to approach 0.5 .mu.m and lower. In a preferred embodiment, the configuration is also planarized. A unique combination of masks in conjunction with a multi-layer structure (28) formed on the surface of a semiconductor wafer (16), the multi-layer structure including a buried etch-stop layer therein (28b), defined the source (18), gate (22), and drain (20) elements and their geometry relative to each to each and to interconnects. Polysilicon plug (40, 46) contacts through slots in the multi-structure layer permit vertical contact to be made to the various elements. Silicidation (56) of the polysilicon plugs reduces series resistance in the vertical direction and permits strapping of N.sup.+ and P.sup.+ polysilicon plugs.
    Type: Grant
    Filed: May 11, 1989
    Date of Patent: October 15, 1991
    Assignee: Advanced Micro Devices, Inc.
    Inventor: Jacob D. Haskell