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).
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Patent number: 10571390Abstract: 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: GrantFiled: March 15, 2016Date of Patent: February 25, 2020Assignee: The Boeing CompanyInventors: 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
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Patent number: 10345267Abstract: 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: GrantFiled: March 15, 2016Date of Patent: July 9, 2019Assignee: The Boeing CompanyInventors: 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
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Patent number: 10222353Abstract: 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: GrantFiled: March 18, 2015Date of Patent: March 5, 2019Assignee: THE BOEING COMPANYInventors: Jeffrey Reyner Kollgaard, John F. Spalding
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Patent number: 10126273Abstract: 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: GrantFiled: February 29, 2016Date of Patent: November 13, 2018Assignee: The Boeing CompanyInventors: 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
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Publication number: 20170248551Abstract: 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: ApplicationFiled: February 29, 2016Publication date: August 31, 2017Inventors: 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
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Publication number: 20170176322Abstract: 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: ApplicationFiled: March 15, 2016Publication date: June 22, 2017Inventors: 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
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Publication number: 20170176393Abstract: 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: ApplicationFiled: March 15, 2016Publication date: June 22, 2017Inventors: 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
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Patent number: 9625423Abstract: 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: GrantFiled: October 30, 2012Date of Patent: April 18, 2017Assignee: THE BOEING COMPANYInventors: 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
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Patent number: 9495737Abstract: 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: GrantFiled: October 31, 2012Date of Patent: November 15, 2016Assignee: THE BOEING COMPANYInventors: Tyler M. Holmes, Jeffrey G. Thompson, Jeffrey Reyner Kollgaard
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Publication number: 20160274063Abstract: 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: ApplicationFiled: March 18, 2015Publication date: September 22, 2016Inventors: Jeffrey Reyner Kollgaard, John F. Spalding
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Patent number: 8527218Abstract: 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: GrantFiled: November 18, 2009Date of Patent: September 3, 2013Assignee: The Boeing CompanyInventors: Gary Ernest Georgeson, Richard Henry Bossi, Jeffrey Reyner Kollgaard
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Publication number: 20110118994Abstract: 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: ApplicationFiled: November 18, 2009Publication date: May 19, 2011Applicant: The Boeing CompanyInventors: Gary Ernest Georgeson, Richard Henry Bossi, Jeffrey Reyner Kollgaard