Patents by Inventor Jeffrey Reyner Kollgaard

Jeffrey Reyner Kollgaard 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: 10571390
    Abstract: A method of detecting local material changes in a composite structure is presented. A pulsed laser beam is directed towards the composite structure comprised of a number of composite materials. Wide-band ultrasonic signals are formed in the composite structure when radiation of the pulsed laser beam is absorbed by the composite structure. The wide-band ultrasonic signals are detected to form data. The data is processed to identify a local frequency value for the composite structure. The local frequency value is used to determine if local material changes are present in the number of composite materials.
    Type: Grant
    Filed: March 15, 2016
    Date of Patent: February 25, 2020
    Assignee: The Boeing Company
    Inventors: William P. Motzer, Gary Ernest Georgeson, Jill Paisley Bingham, Steven Kenneth Brady, Alan F. Stewart, James C. Kennedy, Ivan Pelivanov, Matthew O'Donnell, Jeffrey Reyner Kollgaard
  • Patent number: 10345267
    Abstract: A method of detecting material changes in a composite structure is presented. A pulsed laser beam is directed towards the composite structure comprised of a number of composite materials. Wide-band ultrasonic signals are formed in the composite structure when radiation of the pulsed laser beam is absorbed by the composite structure. The wide-band ultrasonic signals are detected to form data. The data comprises a number of ultrasonic A-scans. The data is processed to identify a plurality of frequency measurements for each of the number of ultrasonic A-scans. A frequency image is displayed using the plurality of frequency measurements. The material changes are represented in the frequency image.
    Type: Grant
    Filed: March 15, 2016
    Date of Patent: July 9, 2019
    Assignee: The Boeing Company
    Inventors: Matthew O'Donnell, Ivan Pelivanov, Steven Kenneth Brady, Gary Ernest Georgeson, Jeffrey Reyner Kollgaard, William P. Motzer, Clarence Lavere Gordon, III, Jill Paisley Bingham, Alan F. Stewart, James C. Kennedy
  • Patent number: 10222353
    Abstract: A method and assembly are provided in order to inspect a partially cured repair patch prior to installation. For example, an assembly for inspecting a repair patch is provided that includes a partially cured repair patch comprised of a composite material. The assembly also includes an acoustic facilitation layer disposed proximate of the surface of the repair patch through which ultrasonic signals will be introduced. The assembly further includes a vacuum bag surrounding the repair patch and the acoustic facilitation layer. The acoustic facilitation layer has an acoustic impedance that is closer to the respective acoustic impedances of the repair patch and the vacuum bag than the acoustic impedance of air is to the respective acoustic impedances of the repair patch and the vacuum bag.
    Type: Grant
    Filed: March 18, 2015
    Date of Patent: March 5, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Jeffrey Reyner Kollgaard, John F. Spalding
  • Patent number: 10126273
    Abstract: A method of detecting inconsistencies in a structure is presented. A pulsed laser beam is directed towards the structure. A plurality of types of ultrasonic signals is formed in the structure when radiation of the pulsed laser beam is absorbed by the structure. The plurality of types of ultrasonic signals is detected to form data.
    Type: Grant
    Filed: February 29, 2016
    Date of Patent: November 13, 2018
    Assignee: The Boeing Company
    Inventors: Ivan Pelivanov, William P. Motzer, Matthew O'Donnell, Steven Kenneth Brady, Gary Ernest Georgeson, Jeffrey Reyner Kollgaard, Clarence Lavere Gordon, III, Jill Paisley Bingham, Alan F. Stewart, James C. Kennedy
  • Publication number: 20170248551
    Abstract: A method of detecting inconsistencies in a structure is presented. A pulsed laser beam is directed towards the structure. A plurality of types of ultrasonic signals is formed in the structure when radiation of the pulsed laser beam is absorbed by the structure. The plurality of types of ultrasonic signals is detected to form data.
    Type: Application
    Filed: February 29, 2016
    Publication date: August 31, 2017
    Inventors: Ivan Pelivanov, William P. Motzer, Matthew O'Donnell, Steven Kenneth Brady, Gary Ernest Georgeson, Jeffrey Reyner Kollgaard, Clarence Lavere Gordon, III, Jill Paisley Bingham, Alan F. Stewart, James C. Kennedy
  • Publication number: 20170176322
    Abstract: A method of detecting local material changes in a composite structure is presented. A pulsed laser beam is directed towards the composite structure comprised of a number of composite materials. Wide-band ultrasonic signals are formed in the composite structure when radiation of the pulsed laser beam is absorbed by the composite structure. The wide-band ultrasonic signals are detected to form data. The data is processed to identify a local frequency value for the composite structure. The local frequency value is used to determine if local material changes are present in the number of composite materials.
    Type: Application
    Filed: March 15, 2016
    Publication date: June 22, 2017
    Inventors: William P. Motzer, Gary Ernest Georgeson, Jill Paisley Bingham, Steven Kenneth Brady, Alan F. Stewart, James C. Kennedy, Ivan Pelivanov, Matthew O'Donnell, Jeffrey Reyner Kollgaard
  • Publication number: 20170176393
    Abstract: A method of detecting material changes in a composite structure is presented. A pulsed laser beam is directed towards the composite structure comprised of a number of composite materials. Wide-band ultrasonic signals are formed in the composite structure when radiation of the pulsed laser beam is absorbed by the composite structure. The wide-band ultrasonic signals are detected to form data. The data comprises a number of ultrasonic A-scans. The data is processed to identify a plurality of frequency measurements for each of the number of ultrasonic A-scans. A frequency image is displayed using the plurality of frequency measurements. The material changes are represented in the frequency image.
    Type: Application
    Filed: March 15, 2016
    Publication date: June 22, 2017
    Inventors: Matthew O'Donnell, Ivan Pelivanov, Steven Kenneth Brady, Gary Ernest Georgeson, Jeffrey Reyner Kollgaard, William P. Motzer, Clarence Lavere Gordon, III, Jill Paisley Bingham, Alan F. Stewart, James C. Kennedy
  • Patent number: 9625423
    Abstract: A method and apparatus for testing a composite structure. A pulsed laser beam having a number of properties is generated. Each of the number of properties is within a selected range. The pulsed laser beam generated by the generation laser system is directed towards a composite structure comprised of a number of composite materials. A number of ultrasonic waves are formed in the composite structure when the pulsed laser beam contacts the composite structure without causing any undesired inconsistencies in the composite structure outside of selected tolerances.
    Type: Grant
    Filed: October 30, 2012
    Date of Patent: April 18, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Richard H. Bossi, Gary Ernest Georgeson, Jeffrey Reyner Kollgaard, Alan Frank Stewart, William P. Motzer, Clarence Lavere Gordon, III, Matthew O'Donnell, Jinjun Xia, Ivan Pelivanov, Chen-wei Wei
  • Patent number: 9495737
    Abstract: A method and apparatus for inspecting a structure. Images of heat generated by an inconsistency in the structure are received. A final image is generated from the images using portions of the images having a greatest amount of heat.
    Type: Grant
    Filed: October 31, 2012
    Date of Patent: November 15, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Tyler M. Holmes, Jeffrey G. Thompson, Jeffrey Reyner Kollgaard
  • Publication number: 20160274063
    Abstract: A method and assembly are provided in order to inspect a partially cured repair patch prior to installation. For example, an assembly for inspecting a repair patch is provided that includes a partially cured repair patch comprised of a composite material. The assembly also includes an acoustic facilitation layer disposed proximate of the surface of the repair patch through which ultrasonic signals will be introduced. The assembly further includes a vacuum bag surrounding the repair patch and the acoustic facilitation layer. The acoustic facilitation layer has an acoustic impedance that is closer to the respective acoustic impedances of the repair patch and the vacuum bag than the acoustic impedance of air is to the respective acoustic impedances of the repair patch and the vacuum bag.
    Type: Application
    Filed: March 18, 2015
    Publication date: September 22, 2016
    Inventors: Jeffrey Reyner Kollgaard, John F. Spalding
  • Patent number: 8527218
    Abstract: The different advantageous embodiments provide a method and apparatus for inspecting a structure. In one advantageous embodiment, an electromagnetic force is generated on a portion of a bond line for a plurality of parts in the structure. The structure contains a conductive material. A determination is made as to whether an inconsistency is present in the portion of the bond line after generating the electromagnetic force on the portion of the bond line.
    Type: Grant
    Filed: November 18, 2009
    Date of Patent: September 3, 2013
    Assignee: The Boeing Company
    Inventors: Gary Ernest Georgeson, Richard Henry Bossi, Jeffrey Reyner Kollgaard
  • Publication number: 20110118994
    Abstract: The different advantageous embodiments provide a method and apparatus for inspecting a structure. In one advantageous embodiment, an electromagnetic force is generated on a portion of a bond line for a plurality of parts in the structure. The structure contains a conductive material. A determination is made as to whether an inconsistency is present in the portion of the bond line after generating the electromagnetic force on the portion of the bond line.
    Type: Application
    Filed: November 18, 2009
    Publication date: May 19, 2011
    Applicant: The Boeing Company
    Inventors: Gary Ernest Georgeson, Richard Henry Bossi, Jeffrey Reyner Kollgaard