Patents by Inventor Steven Kenneth Brady
Steven Kenneth Brady 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: 11981112Abstract: A component assembly includes a core including a main body having a first surface and a second surface opposite from the first surface. One or more recessed cells are formed in each of the first surface and the second surface of the main body. The one or more recessed cells formed in the first surface extend toward the second surface. The one or more recessed cells formed in the second surface extend toward the first surface. A first layer is secured to the core at a first adhesive layer. A second layer is secured to the core at a second adhesive layer.Type: GrantFiled: October 4, 2021Date of Patent: May 14, 2024Assignee: The Boeing CompanyInventors: Steven Kenneth Brady, Marc Joel Piehl, Matthew McKinley Whitmer
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Publication number: 20230104854Abstract: A component assembly includes a core including a main body having a first surface and a second surface opposite from the first surface. One or more recessed cells are formed in each of the first surface and the second surface of the main body. The one or more recessed cells formed in the first surface extend toward the second surface. The one or more recessed cells formed in the second surface extend toward the first surface. A first layer is secured to the core at a first adhesive layer. A second layer is secured to the core at a second adhesive layer.Type: ApplicationFiled: October 4, 2021Publication date: April 6, 2023Applicant: THE BOEING COMPANYInventors: Steven Kenneth Brady, Marc Joel Piehl, Matthew McKinley Whitmer
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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: 10309893Abstract: A method of detecting inconsistencies 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 a surface of the composite structure. The wide-band ultrasonic signals are detected over a duration of time to form data. The data comprises an ultrasonic A-scan spectrum. The data is processed to identify a structure signal in a frequency domain of the ultrasonic A-scan spectrum. The structure signal of the ultrasonic A-scan spectrum is compared to a structure signal of a composite structure standard to determine whether the inconsistencies are present in the number of composite materials.Type: GrantFiled: March 15, 2016Date of Patent: June 4, 2019Assignee: The Boeing CompanyInventors: Gary Ernest Georgeson, William P. Motzer, Jill Paisley Bingham, Alan F. Stewart, Steven Kenneth Brady, James C. Kennedy
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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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Patent number: 10119939Abstract: A vehicle examination system includes an axle inspection system that is configured to inspect an axle of a vehicle. The axle inspection system includes an ultrasound scanning assembly, and an axle coupler that retains the ultrasound scanning assembly. The axle coupler is configured to moveably secure the ultrasound scanning assembly to the axle. An axle inspection control unit is in communication with the ultrasound scanning assembly. The axle inspection control unit is configured to control the ultrasound scanning assembly to ultrasonically scan the axle for anomalies as the vehicle moves.Type: GrantFiled: May 20, 2016Date of Patent: November 6, 2018Assignee: The Boeing CompanyInventors: Barry A. Fetzer, Gary E. Georgeson, Morteza Safai, Jeffrey G. Thompson, Steven Kenneth Brady, John R. Hull
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Publication number: 20170336367Abstract: A vehicle examination system includes an axle inspection system that is configured to inspect an axle of a vehicle. The axle inspection system includes an ultrasound scanning assembly, and an axle coupler that retains the ultrasound scanning assembly. The axle coupler is configured to moveably secure the ultrasound scanning assembly to the axle. An axle inspection control unit is in communication with the ultrasound scanning assembly. The axle inspection control unit is configured to control the ultrasound scanning assembly to ultrasonically scan the axle for anomalies as the vehicle moves.Type: ApplicationFiled: May 20, 2016Publication date: November 23, 2017Applicant: The Boeing CompanyInventors: Barry A. Fetzer, Gary E. Georgeson, Morteza Safai, Jeffrey G. Thompson, Steven Kenneth Brady, John R. Hull
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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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Publication number: 20170176321Abstract: A method of detecting inconsistencies 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 a surface of the composite structure. The wide-band ultrasonic signals are detected over a duration of time to form data. The data comprises an ultrasonic A-scan spectrum. The data is processed to identify a structure signal in a frequency domain of the ultrasonic A-scan spectrum. The structure signal of the ultrasonic A-scan spectrum is compared to a structure signal of a composite structure standard to determine whether the inconsistencies are present in the number of composite materials.Type: ApplicationFiled: March 15, 2016Publication date: June 22, 2017Inventors: Gary Ernest Georgeson, William P. Motzer, Jill Paisley Bingham, Alan F. Stewart, Steven Kenneth Brady, James C. Kennedy
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Patent number: 9404898Abstract: A method and apparatus for inspecting a structure. In one illustrative embodiment, an apparatus comprises a laser system located outside of an area that includes a region of a structure to be inspected, a mobile platform located within the area to be inspected, and a projection system associated with the mobile platform. The laser system is configured to generate a laser beam. The projection system receives the laser beam and projects the laser beam onto a surface of the region of the structure. The laser beam causes a number of ultrasonic waves to form within the structure.Type: GrantFiled: March 15, 2013Date of Patent: August 2, 2016Assignee: THE BOEING COMPANYInventors: Gary Ernest Georgeson, Alan Frank Stewart, William P. Motzer, Steven Kenneth Brady, Richard H. Bossi, Clarence Lavere Gordon, III
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Patent number: 8770031Abstract: A method and apparatus for non-destructive testing. An embodiment of the present disclosure provides a non-destructive inspection system comprising a capacitive acoustic transducer and a control unit connected to the capacitive transducer.Type: GrantFiled: August 15, 2007Date of Patent: July 8, 2014Assignee: The Boeing CompanyInventor: Steven Kenneth Brady
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Patent number: 8446154Abstract: A system for the measurement of degradation of electrical wire insulation quality is described. The system includes a clamping device for engaging the electrical wire to be tested for insulation degradation, the clamping device comprising a channel formed therein for placement of the electrical wire, a plurality of plates placed proximate the channel, the plates electrically connected to generate a capacitance and placed proximate the channel such that the wire insulation provides a portion of a dielectric for the generated capacitance, and a measurement device operatively attached to the plurality of plates such that the measurement device is configured to indicate an amount of degradation associated with the wire insulation based on at least one of the measured capacitance and dissipation factor.Type: GrantFiled: September 24, 2010Date of Patent: May 21, 2013Assignee: The Boeing CompanyInventors: Steven Kenneth Brady, Donald Duane Palmer, Jr., Selina Brownridge
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Patent number: 8319182Abstract: A system for the measurement of degradation of electrical wire insulation is described. The system includes an infrared (IR) spectrometer, a fiber optic cable having a first end and a second end, where the first end is configured to interface to the IR spectrometer, and a clamping device for engaging the electrical wire to be tested for insulation degradation. The second end of said fiber optic cable is mounted within the clamping device such that the second end is adjacent the wire insulation.Type: GrantFiled: July 27, 2010Date of Patent: November 27, 2012Assignee: The Boeing CompanyInventors: Steven Kenneth Brady, Paul H. Shelley, Paul Griffin Vahey
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Publication number: 20120074955Abstract: A system for the measurement of degradation of electrical wire insulation quality is described. The system includes a clamping device for engaging the electrical wire to be tested for insulation degradation, the clamping device comprising a channel formed therein for placement of the electrical wire, a plurality of plates placed proximate the channel, the plates electrically connected to generate a capacitance and placed proximate the channel such that the wire insulation provides a portion of a dielectric for the generated capacitance, and a measurement device operatively attached to the plurality of plates such that the measurement device is configured to indicate an amount of degradation associated with the wire insulation based on at least one of the measured capacitance and dissipation factor.Type: ApplicationFiled: September 24, 2010Publication date: March 29, 2012Inventors: Steven Kenneth Brady, Donald Duane Palmer, JR., Selina Brownridge
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Publication number: 20090044627Abstract: A method and apparatus for non-destructive testing. An embodiment of the present disclosure provides a non-destructive inspection system comprising a capacitive electromagnetic acoustic transducer and a control unit connected to the capacitive electromagnetic transducer.Type: ApplicationFiled: August 15, 2007Publication date: February 19, 2009Inventor: Steven Kenneth Brady