Patents by Inventor Richard H. Bossi

Richard H. Bossi has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 7412025
    Abstract: A system for imaging in a structure may include an energy beam source to direct an energy beam at the structure and a detector to detect a backscatter of the energy beam from any object in the structure. The system may also include a time-resolved function to generate an image of any object in the structure using the backscatter of the energy beam.
    Type: Grant
    Filed: September 20, 2006
    Date of Patent: August 12, 2008
    Assignee: The Boeing Company
    Inventors: Richard H. Bossi, John L. Adamski, William G. Bartholet
  • Publication number: 20080109187
    Abstract: Systems and methods are disclosed for providing nondestructive inspection (NDI) services. For example in accordance with an embodiment of the invention, a system for remote inspection includes a nondestructive inspection (NDI) system configured to examine a structure and provide NDI data related to a damage condition of the structure, the NDI system being configured to communicate the NDI data to a remote location; and a remote computer disposed at the remote location, the remote computer being configured to receive the NDI data and provide the received NDI data for a review, the remote computer being configured to communicate an analytical result based on the review to the NDI system, the analytical result including a repair disposition decision corresponding to the damage condition.
    Type: Application
    Filed: November 2, 2006
    Publication date: May 8, 2008
    Inventors: Jeffrey R. Kollgaard, Gary E. Georgeson, Blake A. Bertrand, Richard H. Bossi
  • Patent number: 7315609
    Abstract: For inspecting a structure with non-destructive x-ray inspection, probes are magnetically coupled to opposing surfaces of the structure. An inspection device may be autonomous with a feedback-controlled motor and/or a positional encoder. An inspection device may include wireless operation for at least one probe. A display may be included to provide real-time visual images from an x-ray detector or an optical imager.
    Type: Grant
    Filed: January 24, 2005
    Date of Patent: January 1, 2008
    Assignee: The Boeing Company
    Inventors: Morteza Safai, Gary E. Georgeson, Michael D. Fogarty, Richard H. Bossi
  • Patent number: 7246631
    Abstract: A system for measuring a mixture ratio associated with a two-part fluid, at least one of the two parts including conductive particles. The system includes a pair of electrodes, a circuit, and an output. The electrodes are disposed on opposite sides of the two-part fluid and sense the dielectric strength of the fluid. The circuit communicates with the electrodes to sense the dielectric strength and outputs a signal representing the dielectric strength. Preferably, the circuit includes a capacitive bridge, an input for a set-point, and an output for an error signal. Also, the system can include a housing for the electrodes. A timer may also be provided to measure the time elapsed from the beginning of the mixing of the two-part fluid. Preferably, the two-part fluid is an adhesive with aluminum particles that is made from a resin and a hardener. Methods of producing two-part fluids are also provided.
    Type: Grant
    Filed: December 22, 2004
    Date of Patent: July 24, 2007
    Assignee: The Boeing Company
    Inventors: Gary E. Georgeson, Charles M. Richards, Richard H. Bossi
  • Patent number: 7231826
    Abstract: There is provided a non-destructive inspection device having an actuating portion and at least one inspecting portion. The inspecting portion(s) are magnetically coupled to the actuating portion so that the inspecting portion(s) may be moved into limited-access areas to inspect features of a structure. The inspecting portion(s) each include at least one inspection sensor that transmits and/or receives signals that, when processed, indicate defects in the features of the structure. The actuating portion may include a handle for manual movement of the inspection device, or alternatively may include a motorized drive wheel for motorized positioning of the inspection device. A positional encoder device, such as an encoder wheel or optical encoder, may also be included in the actuating portion or inspecting portion(s) to monitor the location of the inspection device for more accurate or informative inspection results.
    Type: Grant
    Filed: January 7, 2004
    Date of Patent: June 19, 2007
    Assignee: The Boeing Company
    Inventors: Richard H. Bossi, Gary E. Georgeson, James C. Kennedy
  • Patent number: 6993971
    Abstract: There is provided an ultrasonic inspection device that provides a locking mechanism for inspecting components at preset angles. The inspection device can inspect a component along an arc by inspecting the component at each preset angle, which provides complete and repeatable inspection results. The inspection device comprises a housing with a channel for the passage of an ultrasonic signal and an ultrasonic transducer to transmit and receive the ultrasonic signals. The housing also includes a rotating reflector to reflect the ultrasonic signal. Using a handle on the housing rotatably attached to the rotating reflector, a technician can rotatably position and lock the rotating reflector at a preset angle. The rotating reflector can be rotatably locked by a spring-loaded ball that is selectively received in detents defined by the rotating reflector or handle.
    Type: Grant
    Filed: December 12, 2003
    Date of Patent: February 7, 2006
    Assignee: The Boeing Company
    Inventors: Richard H. Bossi, Martin Freet, Gary E. Georgeson, Stanley W. Richardson
  • Patent number: 6991371
    Abstract: A computed tomography (CT) image quality phantom for use in calibrating explosive detection systems (EDS) at airports. A foam core block containing up to five right cylinder rod members is positioned in a housing member which is adapted to be passed through an airport luggage scanning machine. The rod members are of different lengths in order to create different data slices for analysis. The housing has a lead-in member at least at one end in order to allow passage through an EDS more easily and provide accurate CT calibrating.
    Type: Grant
    Filed: October 14, 2003
    Date of Patent: January 31, 2006
    Assignee: The Boeing Company
    Inventors: Gary E. Georgeson, James M. Nelson, Richard H. Bossi
  • Patent number: 6848321
    Abstract: A system and method for non-destructively testing the strength of bonded joints, particularly a bonded joint between two composite components, is provided. The method generally includes activating a source of rapid surface pressure application against a bonded assembly containing the bonded joint to create a shock load. The resulting shock load first generates compression and then tension within the bonded joint, along with surface motions proximate the bonded assembly, and a surface motion detector measures the surface motions to determine the minimum strength of the bonded joint. Accordingly, the surface motions are correlated to the strength of the bonded joint. Further, the magnitude of the impact may be adjusted to vary the amount of tension within the bonded joint to correspond with various load conditions.
    Type: Grant
    Filed: October 18, 2002
    Date of Patent: February 1, 2005
    Assignee: The Boeing Company
    Inventors: Richard H. Bossi, Kevin R. Housen, William B. Shepherd, Michael E. Voss
  • Patent number: 6622568
    Abstract: A method and system for measuring a strength of a test specimen are provided. The method includes the steps of selecting a tensile load of interest for the test specimen, and bulk heating the test specimen at a localized region such that the test specimen is placed under the tensile load of interest. The method further provides for determining whether the tensile load of interest has caused a failure at the localized region. Bulk heating the test specimen provides a non-destructive evaluation technique that is unachievable through conventional approaches.
    Type: Grant
    Filed: March 19, 2001
    Date of Patent: September 23, 2003
    Assignee: The Boeing Company
    Inventors: James M. Nelson, Richard H. Bossi, John E. Shrader
  • Publication number: 20030079552
    Abstract: A system and method for non-destructively testing the strength of bonded joints, particularly a bonded joint between two composite components, is provided. The method generally comprises activating a source of rapid surface pressure application against a bonded assembly containing the bonded joint to create a shock load. The resulting shock load first generates compression and then tension within the bonded joint, along with surface motions proximate the bonded assembly, and a surface motion detector measures the surface motions to determine the minimum strength of the bonded joint. Accordingly, the surface motions are correlated to the strength of the bonded joint. Further, the magnitude of the impact may be adjusted to vary the amount of tension within the bonded joint to correspond with various load conditions.
    Type: Application
    Filed: October 18, 2002
    Publication date: May 1, 2003
    Inventors: Richard H. Bossi, Kevin R. Housen, William B. Shepherd, Michael E. Voss
  • Publication number: 20020129659
    Abstract: A method and system for measuring a strength of a test specimen are provided. The method includes the steps of selecting a tensile load of interest for the test specimen, and bulk heating the test specimen at a localized region such that the test specimen is placed under the tensile load of interest. The method further provides for determining whether the tensile load of interest has caused a failure at the localized region. Bulk heating the test specimen provides a non-destructive evaluation technique that is unachievable through conventional approaches.
    Type: Application
    Filed: March 19, 2001
    Publication date: September 19, 2002
    Inventors: James M. Nelson, Richard H. Bossi, John E. Shrader
  • Patent number: D511453
    Type: Grant
    Filed: October 14, 2003
    Date of Patent: November 15, 2005
    Assignee: The Boeing Company
    Inventors: Gary E. Georgeson, James M. Nelson, Richard H. Bossi, Dan Wright, Bob Carlsen