Patents by Inventor William P. Motzer

William P. Motzer 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: 9804577
    Abstract: A self-contained, remotely operated, mobile measurement system for stand-off inspection of large target objects located at sites distant from an operations center of a distributed inspection system. In accordance with one embodiment, the system comprises a mobile platform with on-board instrumentation capable of making dimensional measurements in the local coordinate system of the target object. The system comprises multiple hardware and software components networked to a control interface that enables the operator at the operations center to teleoperate the equipment, including driving the mobile platform to a region of interest, calibrating the on-board local positioning system, acquiring measurement and image data, and communicating with on-site personnel if needed.
    Type: Grant
    Filed: May 13, 2013
    Date of Patent: October 31, 2017
    Assignee: The Boeing Company
    Inventors: James J. Troy, Scott W. Lea, Gary E. Georgeson, William P. Motzer
  • Publication number: 20170307516
    Abstract: Described herein is an apparatus, for shielding light generated by a laser during non-destructive inspection of an object. The apparatus includes a light shield at least partially enveloping the laser and defining a first opening through which light generated by the laser passes from the laser to the object. The light shield is opaque and includes at least one first biasing mechanism. The apparatus also includes at least one first light seal coupled to the light shield about the first opening of the light shield. The at least one first biasing mechanism is configured to urge resilient deformation of the at least one first light seal against the object. When the at least one first light seal is resiliently deformed against the object, light generated by the laser is constrained within a light containment space defined between the light shield, the at least one first light seal, and the object.
    Type: Application
    Filed: April 22, 2016
    Publication date: October 26, 2017
    Inventors: Gary E. Georgeson, William P. Motzer, Jeffry J. Garvey, Scott W. Lea, James C. Kennedy, Steven K. Brady, Alan F. Stewart, Jill P. Bingham
  • 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
  • Patent number: 9687981
    Abstract: A serpentine body includes a first portion, a first wheel coupled to the first portion, a second portion, a second wheel coupled to the second portion, and at least one sensor coupled to the first portion and/or the second portion. The first wheel is rotatable in a first direction. The second wheel is rotatable in a second direction opposite the first direction when the first wheel rotates in the first direction.
    Type: Grant
    Filed: November 10, 2014
    Date of Patent: June 27, 2017
    Assignee: The Boeing Company
    Inventors: Joseph L. Hafenrichter, Gary E. Georgeson, William P. Motzer
  • 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
  • Publication number: 20170176321
    Abstract: 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: Application
    Filed: March 15, 2016
    Publication date: June 22, 2017
    Inventors: Gary Ernest Georgeson, William P. Motzer, Jill Paisley Bingham, Alan F. Stewart, Steven Kenneth Brady, 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
  • 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
  • Publication number: 20160274066
    Abstract: Method and apparatus for enabling ultrasonic inspection of a changing, insufficiently defined or unknown shape (e.g., a variable radius or a noncircular radius caused by the use of soft tooling) at a rate that meets production requirements. The apparatus comprises a linear ultrasonic array (i.e., sensor) incorporated in a toppler, which in turn is slidably supported by an oscillating sensor mechanism carried by a traveling trailer vehicle. As a result of this arrangement, the sensor can undergo a back-and-forth sweeping motion coupled with motion along the spar radius. The sensor is further able to displace radially relative to a sweep pivot axis and rotate (hereinafter “topple”) about a topple pivot axis. In this manner, the orientation of the sensor can adjust to the contour of the inspected surface as the sensor scans.
    Type: Application
    Filed: September 29, 2015
    Publication date: September 22, 2016
    Applicant: The Boeing Company
    Inventors: William P. Motzer, James C. Kennedy, Steven Ray Walton, James J. Troy
  • Patent number: 9404898
    Abstract: 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: Grant
    Filed: March 15, 2013
    Date of Patent: August 2, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Gary Ernest Georgeson, Alan Frank Stewart, William P. Motzer, Steven Kenneth Brady, Richard H. Bossi, Clarence Lavere Gordon, III
  • Patent number: 9383342
    Abstract: A method and apparatus for inspecting a test object with a non-planar feature. A pattern of light is transmitted from a first array of optical fibers associated with a sensor structure onto a surface of the test object at a location of the non-planar feature. The pattern of light is configured to cause sound waves in the test object when the pattern of light encounters the test object. A response to the sound waves is detected using a second array of optical fibers associated with the sensor structure. A determination is made as to whether an inconsistency is present in the test object at the location of the non-planar feature from the response to the sound waves detected using the second array of optical fibers.
    Type: Grant
    Filed: June 19, 2012
    Date of Patent: July 5, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Richard H. Bossi, Gary E. Georgeson, Clarence L. Gordon, III, Jeffrey R. Kollgaard, William P. Motzer, Alan Frank Stewart
  • Publication number: 20160096637
    Abstract: Systems and methods for automated maintenance of the top and bottom surfaces or skins of an integrally stiffened hollow structure (e.g., a horizontal stabilizer) using surface crawling vehicles. Each system uses dynamically controlled magnetic coupling to couple an external drive tractor to a pair of passive trailers disposed in the interior of the hollow structure on opposite sides of a vertical structural element. The external drive tractor is also coupled to an external maintenance tool, which the tractor pushes or pulls across the surface skin to perform a maintenance function. The systems allow maintenance operations to be performed on both surface skins without turning the hollow structure over. Each system is modular and can be transported to and easily set up in a building or factory.
    Type: Application
    Filed: December 11, 2015
    Publication date: April 7, 2016
    Applicant: The Boeing Company
    Inventors: James J. Troy, William P. Motzer, Scott W. Lea, James C. Kennedy, Michael C. Hutchinson
  • Patent number: 9266625
    Abstract: Systems and methods for automated non-destructive inspection scanning of the top and bottom aerodynamic surfaces or skins of an integrally stiffened wing box (e.g., a horizontal stabilizer) using surface crawling vehicles. Each system uses dynamically controlled magnetic coupling to couple an external drive tractor to a pair of passive trailers disposed in the interior of the wing box on opposite sides of a spar. The external drive tractor is also coupled to an external NDI scanner, which the tractor pushes or pulls across the surface skin being inspected. The systems allow scanning of both surface skins without turning the wing box over. Each system is modular and can be transported to and easily set up in a building or factory.
    Type: Grant
    Filed: April 9, 2013
    Date of Patent: February 23, 2016
    Assignee: The Boeing Company
    Inventors: James J. Troy, William P. Motzer, Scott W. Lea, James C. Kennedy, Michael C. Hutchinson
  • Patent number: 9250213
    Abstract: A method and apparatus for inspecting a test object. The apparatus comprises an inspection vehicle, a sensor structure, a first array of optical fibers, and a second array of optical fibers. The inspection vehicle is configured to move on a surface of the test object. The sensor structure is associated with the inspection vehicle. The first array of optical fibers is associated with the sensor structure. The first array of optical fibers is configured to transmit a pattern of light towards the surface of the test object and the pattern of light is configured to cause sound waves in the test object when the pattern of light encounters the test object. The second array of optical fibers is associated with the sensor structure. The second array of optical fibers is configured to detect a response to the sound waves.
    Type: Grant
    Filed: August 28, 2012
    Date of Patent: February 2, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Richard H. Bossi, Gary E. Georgeson, Clarence L. Gordon, III, Jeffrey R. Kollgaard, William P. Motzer, Alan Frank Stewart
  • Patent number: 9188566
    Abstract: A method for and apparatus for inspecting a location on a test object with a number of obstructions to reaching the location. An elongate optical fiber carrier holding a number of optical fibers is moved to the location on the test object with the number of obstructions to reaching the location. A pattern of light is transmitted from the number of optical fibers onto a surface of the test object at the location. The pattern of the light is configured to cause sound waves in the test object when the pattern of the light encounters the surface of the test object. A response is detected to the sound waves using the number of optical fibers.
    Type: Grant
    Filed: June 19, 2012
    Date of Patent: November 17, 2015
    Assignee: THE BOEING COMPANY
    Inventors: Gary E. Georgeson, Richard H. Bossi, Clarence L. Gordon, III, Jeffrey R. Kollgaard, William P. Motzer, Alan Frank Stewart
  • Patent number: 9182487
    Abstract: A system for inspecting a test article incorporates a diagnostic imaging system for a test article. A command controller receives two dimensional (2D) images from the diagnostic imaging system. A three dimensional (3D) computer aided design (CAD) model visualization system and an alignment system for determining local 3D coordinates are connected to the command controller. Computer software modules incorporated in the command controller are employed, in aligning, the 2D images and 3D CAD model responsive to the local 3D coordinates. The 2D images and 3D CAD model are displayed with reciprocal registration. The alignment system is then directed to selected coordinates in the 2D images or 3D CAD model.
    Type: Grant
    Filed: June 22, 2011
    Date of Patent: November 10, 2015
    Assignee: The Boeing Company
    Inventors: James J. Troy, Scott W. Lea, Gary E. Georgeson, William P. Motzer, Peter J. Hellenbrand, Kevin Puterbaugh
  • Patent number: 9176099
    Abstract: Method and apparatus for enabling ultrasonic inspection of a changing, insufficiently defined or unknown shape (e.g., a variable radius or a noncircular radius caused by the use of soft tooling) at a rate that meets production requirements. The apparatus comprises a linear ultrasonic array (i.e., sensor) incorporated in a toppler, which in turn is slidably supported by an oscillating sensor mechanism carried by a traveling trailer vehicle. As a result of this arrangement, the sensor can undergo a back-and-forth sweeping motion coupled with motion along the spar radius. The sensor is further able to displace radially relative to a sweep pivot axis and rotate (hereinafter “topple”) about a topple pivot axis. In this manner, the orientation of the sensor can adjust to the contour of the inspected surface as the sensor scans.
    Type: Grant
    Filed: May 8, 2012
    Date of Patent: November 3, 2015
    Assignee: The Boeing Company
    Inventors: William P. Motzer, James C. Kennedy, Steven Ray Walton, James J. Troy
  • Patent number: 9164066
    Abstract: A method and apparatus comprises a sensor structure, a first array of optical fibers, and a second array of optical fibers. The first array of optical fibers is associated with the sensor structure. The first array of optical fibers is configured to transmit a pattern of light towards a test object and the pattern of light is configured to cause sound waves in the test object when the pattern of light encounters the test object. The second array of optical fibers is associated with the sensor structure. The second array of optical fibers is configured to detect a response to the sound waves.
    Type: Grant
    Filed: June 19, 2012
    Date of Patent: October 20, 2015
    Assignee: THE BOEING COMPANY
    Inventors: Richard H. Bossi, Gary E. Georgeson, Clarence L. Gordon, III, Jeffrey R. Kollgaard, William P. Motzer, Alan Frank Stewart
  • Patent number: 9149929
    Abstract: Methods and systems are provided for positioning a remote sensor within a target object. An articulated robotic system is coupled to the remote sensor. A positioning system determines a position of the target object to be inspected and determines a first position of the remote sensor. A control system calibrates a virtual representation of the target object with respect to the position of the target object, and tracks movement of the remote sensor relative to the target object.
    Type: Grant
    Filed: May 26, 2010
    Date of Patent: October 6, 2015
    Assignee: THE BOEING COMPANY
    Inventors: William P. Motzer, Gary E. Georgeson, Scott W. Lea, Peter J. Hellenbrand, James J. Troy
  • Patent number: 9010684
    Abstract: A system and method that allow inspection of hollow structures made of composite material, such as an integrally stiffened wing box of an aircraft. A wing box comprises top and bottom skins connected by a plurality of spaced spars. The system employs a plurality of scanners for inspecting different portions of each spar. The system uses dynamically controlled magnetic coupling to connect an external drive tractor to computer-controlled scanners that carry respective sensors, e.g., linear ultrasonic transducer arrays. A system operator can control the various components by means of a graphical user interface comprising multiple interaction regions that represent the individual scanner motion paths and are associated with respective motion script files.
    Type: Grant
    Filed: June 27, 2012
    Date of Patent: April 21, 2015
    Assignee: The Boeing Company
    Inventors: William P. Motzer, James C. Kennedy, Michael C. Hutchinson, Martin L. Freet, Ronald E. VonWahlde, Steven Ray Walton, Jeffry J. Garvey, Scott W. Lea, James J. Troy, Daniel James Wright, Hien T. Bui, Michael Joseph Duncan, Mark L. Little, William Joseph Tapia, Barry A. Fetzer, Richard C. Krotzer