Patents by Inventor Roger W. Engelbart

Roger W. Engelbart 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: 9595096
    Abstract: Provided are methods, systems, and computer program products for inspecting composite items. Specifically, a method involves analyzing an image of or, more generally, data characterizing condition of a top layer, which is disposed over a bottom layer. The method also involves performing a structural integrity check based on any anomalies detected in the top layer during this analysis as well as based on any anomalies previously detected in the bottom layer. As such, this structural integrity check accounts for characteristics of multiple layers, in some embodiments, all layers applied up to point of this inspection. In addition to the detected anomalies, the structural integrity check may account for previously performed repairs. The structural integrity check may be performed on individual portions of a composite item while, for example, other portions continue receiving a new composite layer, which may be referred to as an inline inspection.
    Type: Grant
    Filed: March 10, 2014
    Date of Patent: March 14, 2017
    Assignee: The Boeing Company
    Inventors: Steven A. Dorris, Arun Ayyagari, Jonathan Blake Vance, David E. Corman, James W. Fonda, Roger W. Engelbart, Philip L. Freeman
  • Patent number: 9506879
    Abstract: A method and system are provided for non-destructively evaluating a workpiece hidden by an overlying structure. In the context of a method, a workpiece is interrogated with radiation, such as x-ray radiation, that also propagates through the overlying structure. The method further includes collecting data representative of radiation backscattered from the workpiece. Based upon a thickness and material of the overlying structure, the method compares the data that has been collected from the workpiece with reference data representative of radiation backscattered from a standard that includes different respective material loss indicators hidden by an overlying structure of the same thickness and material. Each material loss indicator is a physical representation of a different amount of material loss. As a result of the comparison, the method estimates the material loss of the workpiece.
    Type: Grant
    Filed: October 2, 2014
    Date of Patent: November 29, 2016
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, Taisia Tsukruk Lou
  • Patent number: 9360459
    Abstract: A method and apparatus for inspecting a composite structure. A thickness profile of a portion of a region of a composite structure is identified. The region has a cross-section with non-parallel surfaces. An estimated thickness for a location within the region and outside of the portion is identified using the thickness profile. An indication of whether the location has undesirable porosity is generated based on information about attenuation of response sound signals and the estimated thickness for the location.
    Type: Grant
    Filed: May 17, 2013
    Date of Patent: June 7, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Roger W. Engelbart, Christopher Mark Vaccaro, Nancy L. Wood
  • Publication number: 20160097728
    Abstract: A method, system and computer-readable storage medium are provided to facilitate inspection of a composite part during manufacture. In the context of a system, a system for inspecting a composite part during manufacture is provided that includes an inspection system configured to detect an in-process anomaly with respect to a ply of the composite part during placement of the ply. The system also includes a computing system configured to determine part location coordinates of the in-process anomaly detected by the inspection system with respect to the ply of the composite part. The computing system is also configured to map the in-process anomaly to a digital part model based upon the part location coordinates. The system additionally includes a display, responsive to the computing system, configured to present a representation of the digital part model including an indication of the in-process anomaly relative thereto.
    Type: Application
    Filed: October 6, 2014
    Publication date: April 7, 2016
    Inventors: Roger W. Engelbart, James W. Fonda, Allen Halbritter
  • Patent number: 9214018
    Abstract: A method for reworking an inconsistency on a part. A location of the inconsistency is identified for the part in a model of the part. An image is generated for a rework for the part. The image is projected for the rework on the part based on the location identified for the inconsistency. The rework is performed for the inconsistency on the part using the image projected on the part.
    Type: Grant
    Filed: April 23, 2013
    Date of Patent: December 15, 2015
    Assignee: THE BOEING COMPANY
    Inventor: Roger W. Engelbart
  • Publication number: 20150273760
    Abstract: A method and apparatus for reworking an inconsistency on a part. Information about the inconsistency on the part may be identified using data generated by a nondestructive evaluation system. A portion of a section of the part in which the inconsistency is located may be removed based on the information about the inconsistency. A profile for the section of the part may be identified. Rework image data may be generated using the profile in which the rework image data comprises a number of patch images. The number of patch images may be projected onto a rework material as a number of patch projections for use in forming a patch to be applied over the section of the part.
    Type: Application
    Filed: June 10, 2015
    Publication date: October 1, 2015
    Inventor: Roger W. Engelbart
  • Publication number: 20150254835
    Abstract: Provided are methods, systems, and computer program products for inspecting composite items. Specifically, a method involves analyzing an image of or, more generally, data characterizing condition of a top layer, which is disposed over a bottom layer. The method also involves performing a structural integrity check based on any anomalies detected in the top layer during this analysis as well as based on any anomalies previously detected in the bottom layer. As such, this structural integrity check accounts for characteristics of multiple layers, in some embodiments, all layers applied up to point of this inspection. In addition to the detected anomalies, the structural integrity check may account for previously performed repairs. The structural integrity check may be performed on individual portions of a composite item while, for example, other portions continue receiving a new composite layer, which may be referred to as an inline inspection.
    Type: Application
    Filed: March 10, 2014
    Publication date: September 10, 2015
    Applicant: The Boeing Company
    Inventors: Steven A. Dorris, Arun Ayyagari, Jonathan Blake Vance, David E. Corman, James W. Fonda, Roger W. Engelbart, Philip L. Freeman
  • Patent number: 9082209
    Abstract: A method and apparatus for reworking an inconsistency on a part. Image data for the inconsistency on the part may be identified using data for the part generated by a nondestructive evaluation system. Information about the inconsistency may be identified using the image data. Rework image data may be generated using the information identified about the inconsistency. The rework image data may comprise a number of patch images. The number of patch images may be projected onto a rework material for use in forming a patch for the inconsistency.
    Type: Grant
    Filed: May 25, 2012
    Date of Patent: July 14, 2015
    Assignee: THE BOEING COMPANY
    Inventor: Roger W. Engelbart
  • Patent number: 9038470
    Abstract: A method and apparatus for inspecting a composite structure. A response sound signal to a sound signal sent into the composite structure at a location on the composite structure is detected. An attenuation is identified in the response sound signal detected in response to the sound signal sent into the composite structure at the location on the composite structure. An indication of whether additional evaluation of the location is needed based on a comparison of the attenuation in the response sound signal to a baseline attenuation value for porosity for the location on the composite structure is generated.
    Type: Grant
    Filed: August 7, 2012
    Date of Patent: May 26, 2015
    Assignee: THE BOEING COMPANY
    Inventors: Roger W. Engelbart, Christopher M. Vaccaro, Scott E. Black, Nancy Wood
  • Patent number: 9027621
    Abstract: A system comprises a feed assembly for applying composite tape; a unit for forming lateral stripes across a portion of the tape that has been applied; a camera for capturing images of the lateral stripes; and a processor programmed to process the images of the lateral stripes to identify any discontinuities in the tape. Those stripes intersecting any discontinuities will make those discontinuities apparent.
    Type: Grant
    Filed: January 14, 2014
    Date of Patent: May 12, 2015
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, Reed E. Hannebaum, Timothy Pollock
  • Publication number: 20150055757
    Abstract: A method and system are provided for non-destructively evaluating a workpiece hidden by an overlying structure. In the context of a method, a workpiece is interrogated with radiation, such as x-ray radiation, that also propagates through the overlying structure. The method further includes collecting data representative of radiation backscattered from the workpiece. Based upon a thickness and material of the overlying structure, the method compares the data that has been collected from the workpiece with reference data representative of radiation backscattered from a standard that includes different respective material loss indicators hidden by an overlying structure of the same thickness and material. Each material loss indicator is a physical representation of a different amount of material loss. As a result of the comparison, the method estimates the material loss of the workpiece.
    Type: Application
    Filed: October 2, 2014
    Publication date: February 26, 2015
    Inventors: Roger W. Engelbart, Taisia Tsukruk Lou
  • Patent number: 8934702
    Abstract: A system for determining cumulative tow gap width includes an in-process vision system having at least one camera adapted to record images of a composite material and a data analysis computer communicating with and adapted to receive image data from the in-process vision system. The data analysis computer may be adapted to calculate a cumulative gap width of tow gaps in the composite material. A user interface may communicate with and be adapted to receive data analysis results from the data analysis computer. A method for determining cumulative tow width gap of tow gaps in a composite structure is also disclosed.
    Type: Grant
    Filed: January 2, 2008
    Date of Patent: January 13, 2015
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, Reed Hannebaum, Eric Rector, Jeffrey Haywood
  • Publication number: 20140338453
    Abstract: A method and apparatus for inspecting a composite structure. A thickness profile of a portion of a region of a composite structure is identified. The region has a cross-section with non-parallel surfaces. An estimated thickness for a location within the region and outside of the portion is identified using the thickness profile. An indication of whether the location has undesirable porosity is generated based on information about attenuation of response sound signals and the estimated thickness for the location.
    Type: Application
    Filed: May 17, 2013
    Publication date: November 20, 2014
    Applicant: THE BOEING COMPANY
    Inventors: Roger W. Engelbart, Christopher Mark Vaccaro, Nancy L. Wood
  • Patent number: 8873711
    Abstract: A method and system for visualizing the effects of corrosion are provided. In the context of a method, a workpiece is interrogated with radiation, such as by interrogating the workpiece with x-ray radiation. By relying upon a radiographic technique, the workpiece may be hidden and may be interrogated without disassembly. The method generates a backscatter image of the workpiece based upon radiation backscattered from the workpiece. The method also compares one or more regions of the backscatter image of the workpiece with respect to backscatter images of different metal loss indicators. Each metal loss indicator is representative of a different amount of metal loss. As a result of the comparison, the method estimates the metal loss attributable to corrosion of the workpiece.
    Type: Grant
    Filed: June 19, 2012
    Date of Patent: October 28, 2014
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, Taisia V. Tsukruk
  • Patent number: 8753458
    Abstract: The three dimensional (3-D) locations of splices in pre-preg tows placed by an automatic fiber placement machine to form a laminated composite structure are mapped to allow visualization of alignment patterns in the splices.
    Type: Grant
    Filed: July 26, 2009
    Date of Patent: June 17, 2014
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, Reed Hannebaum, Eric Rector
  • Patent number: 8720314
    Abstract: Methods and systems for an armor system are provided. The system includes a first face sheet and a shaped preform extending from the first face sheet. The preform includes a first edge proximate the first face sheet, a sidewall extending from the first edge to a flange extending substantially perpendicularly from the sidewall. The preform circumscribes an area of the first face sheet. The system also includes a tile of armor material complementarily-shaped to fit within the area circumscribed by the preform. The tile is positioned within the preform such that at least a portion of the tile is between the first face sheet and the flange. The system includes a second face sheet covering the preform and the tile on a side opposite from the first face sheet.
    Type: Grant
    Filed: June 29, 2010
    Date of Patent: May 13, 2014
    Assignee: The Boeing Company
    Inventor: Roger W. Engelbart
  • Publication number: 20140124142
    Abstract: A system comprises a feed assembly for applying composite tape; a unit for forming lateral stripes across a portion of the tape that has been applied; a camera for capturing images of the lateral stripes; and a processor programmed to process the images of the lateral stripes to identify any discontinuities in the tape. Those stripes intersecting any discontinuities will make those discontinuities apparent.
    Type: Application
    Filed: January 14, 2014
    Publication date: May 8, 2014
    Applicant: THE BOEING COMPANY
    Inventors: Roger W. Engelbart, Reed E. Hannebaum, Timothy Pollock
  • Patent number: 8695669
    Abstract: The three dimensional (3-D) locations of splices in pre-preg tows placed by an automatic fiber placement machine to form a laminated composite structure are mapped to allow visualization of alignment patterns in the splices.
    Type: Grant
    Filed: May 9, 2012
    Date of Patent: April 15, 2014
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, Reed Hannebaum, Eric Rector
  • Patent number: 8687872
    Abstract: A method for remote rework imaging a part for an inconsistency is provided. The part is scanned with a nondestructive inspection device. An image of a part inconsistency is communicated from the nondestructive inspection device to a programmable device. The image of the part inconsistency is viewed with the programmable device. The image of the part inconsistency is edited with the programmable device using an input device in communication with the programmable device. The edited image is communicated from the programmable device to a visible light projector. The edited image is projected onto the part inconsistency using the visible light projector.
    Type: Grant
    Filed: December 22, 2011
    Date of Patent: April 1, 2014
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, Richard J. Steckel
  • Patent number: 8668793
    Abstract: Systems and methods for in-process vision inspection for automated machines are disclosed. In one embodiment, a head assembly includes a tool moveable over a workpiece and adapted to perform a manufacturing operation on the workpiece, and an inspection unit operatively positioned proximate the tool and moveable with the tool relative to the workpiece. The inspection unit is adapted to perform a vision inspection of a portion of the workpiece simultaneously with the performance of the manufacturing operation on the workpiece. In a particular embodiment, the inspection unit includes a camera adapted to monitor an area including the portion of the workpiece upon which the tool has performed the manufacturing operation, and a processor operatively coupled to the camera and adapted to receive an image from the camera and to analyze the image to determine a presence of a defect within the portion of the workpiece.
    Type: Grant
    Filed: August 11, 2005
    Date of Patent: March 11, 2014
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, Reed E. Hannebaum, Timothy Pollock