Patents Represented by Attorney Shimokaji & Associates, P.C.
  • Patent number: 6807740
    Abstract: A laser alignment tool includes a line laser assembly including a laser and emitting a laser beam line and an electronic target assembly including a photo detector array. The laser beam line of the laser is pointed toward the center of the photo detector array with the longitudinal axis of the laser beam line being perpendicular to the centerline of the photo detector array. The line laser assembly includes a laser diode having a line-generating lens attached in front using a lens holder and being mounted onto a tilt stage. Using a line laser provides a certified accuracy of +/−0.005 inches at a distance of 10 feet. The electronic target further includes a narrow band pass filter and a discrete LED display that is controlled by a microprocessor. The microprocessor may be programmed with a variable range for each LED of the discrete LED display according to the alignment task.
    Type: Grant
    Filed: December 20, 2002
    Date of Patent: October 26, 2004
    Assignee: The Boeing Company
    Inventors: Paul W. Reed, Duncan P. Mackinnon, Ronald D. Curl, Joe R. Long
  • Patent number: 6796882
    Abstract: An appliqué film and paint removal tool includes a central rotating shaft, a spring-loaded locator pin, at least three freely rotating bearings, an arbor, and a collar. The rotating shaft may be centered with the locator pin and pushed down until the bearings touch the surface from which the appliqué or paint material is to be removed. By rotating while touching the mold line contour of the fastener the bearings will cause the appliqué film or paint treatment to separate around the mold line of the fastener. The separated material than can be peeled off and the fastener is accessible. Therefore, the appliqué film or paint treatment can be removed from fasteners without damaging the surface around the fastener. The appliqué film and paint treatment removal tool may be designed to accommodate all fastener diameters and mold line contours.
    Type: Grant
    Filed: September 3, 2003
    Date of Patent: September 28, 2004
    Assignee: The Boeing Company
    Inventors: Daniel E. Pulcher, Roy L. Tribble, Marvin C. Holwager
  • Patent number: 6796530
    Abstract: A stores ejection system for retaining stores on the underside of an aircraft and forcibly jettisoning the stores away from the aircraft is disclosed. The ejection system includes a plurality of ejector mechanisms for releasably holding and jettisoning the stores away from the aircraft, a plurality of storage devices for storing pressurized gas to actuate the ejector mechanisms, and a central control system for maintaining the pressure of the gas, and actuating the release of the gas. The central control system monitors the pressure of the storage devices and heats only those storage devices that have a pressure below the operating pressure.
    Type: Grant
    Filed: November 18, 2002
    Date of Patent: September 28, 2004
    Assignee: The Boeing Company
    Inventors: Thaddeus Jakubowski, Jr., John K. Foster, Gary T. Johnson
  • Patent number: 6797879
    Abstract: The present invention provides an avionics tray assembly that includes a seal assembly and a tray detail. The seal assembly includes a metering plate detail, a plurality of tabs disposed along the metering plate detail, a plurality of location bosses disposed along the metering plate detail, and a flange extending from the metering plate detail, while the tray detail includes a plurality of index bosses and a horizontal surface, wherein the plurality of index bosses receive the plurality of location bosses, wherein the plurality of tabs secure the seal assembly to the tray detail, and wherein the flange secures the seal assembly to the horizontal surface.
    Type: Grant
    Filed: September 17, 2002
    Date of Patent: September 28, 2004
    Assignee: The Boeing Company
    Inventors: John G. Leyda, Stephen M. Edwards
  • Patent number: 6798502
    Abstract: The nonlinear system includes a fixed visible input and tunable visible input that are directed to a location on a surface to be interrogated. The fixed visible input and the tunable visible inputs are aligned so that their surface locations of optical illumination overlap on the interrogated location. An output wavelength discriminator receives the reflected difference-frequency generated on the interrogated location. The output wavelength discriminator is substantially non-transmissive at frequencies higher than the difference-frequency, but substantially transmissive at the difference-frequency of the fixed visible input and the tunable visible input. The output of the output wavelength is a microwave output. Signal collection optics receives an output of the output wavelength discriminator and directs the propagation of the output thereof so that a collected microwave light signal is formed after propagation through the signal collection optics.
    Type: Grant
    Filed: June 20, 2002
    Date of Patent: September 28, 2004
    Assignee: The Boeing Company
    Inventor: Jeffrey H. Hunt
  • Patent number: 6788405
    Abstract: First and second laser inputs are directed to a location on a semiconductor wafer to be interrogated. A first signal analyzer receives a first light signal at a first second-harmonic wavelength generated by the first laser input and converts the signal to a first electronic signal, thus monitoring the intensity of the first second-harmonic wavelength as a function of contamination. A second surface optical signal analyzer provides a similar function at a second second-harmonic wavelength generated by the second laser input and provides a second electronic signal. A third surface optical signal analyzer receives a third light signal at a sum-frequency wavelength generated by the first laser input and the second laser input on the semiconductor wafer to be interrogated and converts the light signal to a third electronic signal. An electronic signal analyzer compares the first, second and third electronic signals for determining the level of semiconductor wafer contamination.
    Type: Grant
    Filed: June 12, 2002
    Date of Patent: September 7, 2004
    Assignee: The Boeing Company
    Inventor: Jeffrey H. Hunt
  • Patent number: 6780015
    Abstract: A training system and method for use of simulated night vision goggles (NVG) which provides the full dynamic range of NVG simulation including low intensity, medium intensity and high intensity irradiance images of night-time terrain. Each of three 12-bit video signals are allocated to a preselected portion or all of the total irradiance range representing scene elements corresponding to low, medium and high light intensity and a video camera scans and converts the resultant generated image to preserve its resolution and dynamic range. The image is viewable in the simulated goggles.
    Type: Grant
    Filed: November 14, 2001
    Date of Patent: August 24, 2004
    Assignee: The Boeing Company
    Inventors: Steven D. Swaine, Harold R. Streid
  • Patent number: 6781686
    Abstract: Two laser inputs having pulse durations of about 50-100 femtoseconds are directed to an area of a surface to be interrogated. The lasers are aligned so that their surface areas of optical illumination overlap on the interrogated surface. An optical delay line temporarily synchronizes the two inputs. An output wavelength discriminator receives reflections of the inputs from the interrogated surface and is substantially non-transmissive at the frequencies of the first laser input and the second laser input, but is substantially transmissive at the sum-frequency of the first input and the second input. Imaging optics direct the propagation of the output so that a real image is formed. A position sensitive detector monitors the intensity of the real image at the sum-frequency and an electronic signal equivalent to the real image is provided.
    Type: Grant
    Filed: June 19, 2002
    Date of Patent: August 24, 2004
    Assignee: The Boeing Company
    Inventor: Jeffrey H. Hunt
  • Patent number: 6768455
    Abstract: A method for detecting calibration probe displacement for a phased array antenna includes steps of: creating a gold standard set of antenna element phases of the phased array antenna; determining a set of element phase sensitivities of the phased array antenna; measuring a set of antenna element phases relative to array displacement of the phased array antenna; and forming a set of equations using the gold standard set of antenna element phases, the set of element phase sensitivities, and the set of antenna element phases relative to array displacement. The set of equations has an array displacement vector x as unknown; and solving the set of equations for the array displacement vector x provides the location and orientation of the calibration probe displacement.
    Type: Grant
    Filed: May 20, 2003
    Date of Patent: July 27, 2004
    Assignee: The Boeing Company
    Inventors: Paul C. Werntz, Sien-Chang C. Liu, Lauriston Wah
  • Patent number: 6761783
    Abstract: A method for repairing a damaged area, referred to as the repair area, of a composite structure comprises steps of: making alignment markings on the repair area; fabricating a pair of alignment templates; preparing the repair area for a hot bonded, vacuum bagged repair; assembling a repair patch; consolidating the repair patch; heating the repair patch; transferring and aligning the repair patch to the repair area; vacuum bagging, heating, and cooling the repair patch for a partial cure at the repair area; heating and cooling the repair patch in an oven; and bonding the repair patch to the repair area.
    Type: Grant
    Filed: April 9, 2002
    Date of Patent: July 13, 2004
    Assignee: The Boeing Company
    Inventors: Russell L. Keller, Wesley S. Owen
  • Patent number: 6742377
    Abstract: A passive-adaptive indentor is provided for cold working a material that includes a material surface and a depth extending in a direction that is perpendicular to a direction of the material surface. The passive-adaptive indentor has a first member that includes a first working end that is configured to create a first residual stress field that extends to a predetermined depth in the material. The passive-adaptive indentor also has a second member that includes a second working end that is configured to create a second residual stress field that extends to a generally fixed second depth of the material regardless of the depth to which the first residual stress field extends. A method of using a passive-adaptive indentor for cold working a material is also presented.
    Type: Grant
    Filed: June 13, 2002
    Date of Patent: June 1, 2004
    Assignee: The Boeing Company
    Inventors: Mark A. Woods, Jeffrey A. Wilkerson
  • Patent number: 6739552
    Abstract: An apparatus and method is disclosed for increasing available space in an aircraft cabin cross section to improve passenger comfort. Use of one side wall supported armrest on each side of the aircraft's cross section, rather then seat supported armrest as are provided conventionally elsewhere, enables use of wider seats. Side wall supported armrests may be secured by means of rails or other conventional mounting means, and the armrests may be contoured an/or cushioned to provide a better ergonomic arm support. Contoured armrests may also be recessed into the space between aircraft cabin body frames.
    Type: Grant
    Filed: November 29, 2001
    Date of Patent: May 25, 2004
    Assignee: The Boeing Company
    Inventors: Mithra M. K. V. Sankrithi, Mark A. Stadum