Patents by Inventor Luis A. Perla

Luis A. Perla 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: 11911977
    Abstract: An illustrative example of the present disclosure provides a machine configured to form a composite structure. The machine includes a composite placement machine, measuring equipment, a tool path generator, and compaction equipment. The composite placement machine lays up composite plies. The measuring equipment measures surfaces of the composite plies to form measurements during layup of the composite plies. A computer includes a model of the composite plies for a structure. The tool path generator forms a modified tool path based upon a difference between the measurements and expected measurements for the composite plies in the model.
    Type: Grant
    Filed: May 6, 2021
    Date of Patent: February 27, 2024
    Assignee: The Boeing Company
    Inventors: Michael Kenneth-Que Louie, Robert Graham Albers, Jeron D. Moore, Luis A. Perla, Gagandeep Saini, Brice A. Johnson, Marcin A. Rabiega
  • Patent number: 11885770
    Abstract: A measurement probe edge guide tool includes an edge follower comprising two edge contact pins that spin around the outside of the measurement probe using a ball bearing. The edge contact pins hug the corner of a contoured edge of the workpiece or in-service part to provide a consistent distance of the center of the probe from the edge. The edge follower enables the tool to inspect the marginal portion bounded by a contoured (machined) edge of a workpiece or part. The edge follower is removable so that the tool may also be adapted for use in general acreage inspection. The tool features a spring-loaded mechanism with a positive probe protrusion relative to a roller-supported cage. The tool has either a handle which is coupled to the cage by means of a universal joint or a hand grip that is affixed to the cage.
    Type: Grant
    Filed: September 9, 2021
    Date of Patent: January 30, 2024
    Assignee: The Boeing Company
    Inventors: Nicholas J. Schnoebelen, Wallace Kwan, Brandon J. Steffensmeier, Luis A. Perla, Erika L. Berhardt, John R. Aubin
  • Publication number: 20230415429
    Abstract: A composite manufacturing system includes a lamination tool, including a lamination surface, first locating targets extending the lamination surface, and second locating targets extending the lamination surface. The system includes a computer-aided measurement system to measure the first locating targets, the second locating targets, and line profiles of the lamination surface and to generate master surface-data and master target-data. The master target-data represents target positions of the first locating targets and the second locating targets. The master surface-data represents profile positions of the line profiles. The line profiles are associated with target pairs. Each one of the target pairs includes one of the first locating targets and an opposing one of the second locating targets.
    Type: Application
    Filed: March 10, 2023
    Publication date: December 28, 2023
    Applicant: The Boeing Company
    Inventors: Marcin A. Rabiega, Michael K. Louie, Ethan G. Sherrard, Todd Rudberg, Richard E. Wood, Luis A. Perla, Brandon Poe
  • Publication number: 20220236231
    Abstract: A measurement probe edge guide tool includes an edge follower comprising two edge contact pins that spin around the outside of the measurement probe using a ball bearing. The edge contact pins hug the corner of a contoured edge of the workpiece or in-service part to provide a consistent distance of the center of the probe from the edge. The edge follower enables the tool to inspect the marginal portion bounded by a contoured (machined) edge of a workpiece or part. The edge follower is removable so that the tool may also be adapted for use in general acreage inspection. The tool features a spring-loaded mechanism with a positive probe protrusion relative to a roller-supported cage. The tool has either a handle which is coupled to the cage by means of a universal joint or a hand grip that is affixed to the cage.
    Type: Application
    Filed: September 9, 2021
    Publication date: July 28, 2022
    Applicant: The Boeing Company
    Inventors: Nicholas J. Schnoebelen, Wallace Kwan, Brandon J. Steffensmeier, Luis A. Perla, Erika L. Berhardt, John R. Aubin
  • Patent number: 11307029
    Abstract: A method for analyzing a surface quality of a laminate part including the steps of creating a planned dimensioned representation of a laminate part desired to be built which includes a first surface having a first topography; placing fibers into locations for the laminate part desired to be built; and curing a resin associated with the placed fibers fabricating an as-built laminate part which includes a second surface having a second topography which corresponds to the first surface having the first topography. The method also includes aligning the first surface, the second surface and the locations of the fibers; determining a first elevation of a first point on the first surface and a second elevation of a second point on the second surface; and observing the first surface, the second surface and the locations of the fibers in alignment and the first elevation relative to the second elevation in analyzing the surface quality of the laminate part.
    Type: Grant
    Filed: April 2, 2018
    Date of Patent: April 19, 2022
    Assignee: THE BOEING COMPANY
    Inventors: Jeron D. Moore, Michael K. Louie, Luis A. Perla, Gagandeep Saini, Christopher W. Fay, Robert G. Meyer
  • Publication number: 20210252807
    Abstract: An illustrative example of the present disclosure provides a method. A first set of composite plies including a first outer ply of a first composite structure is laid up. A first intermediate surface of the first outer ply is measured to form a first set of measurements. A laydown surface for a tool path of a composite placement machine is modified to form a modified tool path, wherein modifying the laydown surface comprises modifying the laydown surface such that a laydown surface of the modified tool path matches the first set of measurements. A composite ply is laid down using the composite placement machine and the modified tool path.
    Type: Application
    Filed: May 6, 2021
    Publication date: August 19, 2021
    Inventors: Michael Kenneth-Que Louie, Robert Graham Albers, Jeron D. Moore, Luis A. Perla, Gagandeep Saini, Brice A. Johnson, Marcin A. Rabiega
  • Patent number: 11045836
    Abstract: Surface treatment of a tubular surface defining an axis extending from a first surface end to a second surface end includes partially surrounding the tubular surface, at a first position, with a first set of treating units, with the treating units arranged in a first arcuate array. Furthermore, each treating unit is configured to include a plurality of first applicator heads. In some examples, a position of each of the plurality of first applicator heads is determined relative to the tubular surface. The first set of treating units is moved from the first position towards a second position. In one non-limiting example, each of the plurality of first applicator heads is independently controlled to selectively apply a first treatment as the first set of treating units moves from the first position towards the second position.
    Type: Grant
    Filed: April 22, 2019
    Date of Patent: June 29, 2021
    Assignee: The Boeing Company
    Inventors: Shane E. Arthur, Bennett M. Moriarty, Luis A. Perla, Jeffrey S. Rebmann, Trevor S. McCrea, Jason S. Warner, Seana B. Kobak, Ryan M. Trumbo
  • Patent number: 11034100
    Abstract: A method and apparatus for forming a composite object. A first plurality of tows is laid up over a tool according to a first path. A second plurality of tows is laid up over the tool according to a second path. A first portion of the first plurality of tows runs non-parallel to a second portion of the second plurality of tows. First ends of the first portion of the first plurality of tows and second ends of the second portion of the second plurality of tows meet at a merge zone along the tool to form a ply of a composite laminate.
    Type: Grant
    Filed: June 20, 2018
    Date of Patent: June 15, 2021
    Assignee: The Boeing Company
    Inventors: Michael Kenneth-Que Louie, Jeron D. Moore, Gagandeep Saini, Luis A. Perla, Brice Aaron Johnson, Stewart James Ibbotson, Timothy D. Jackson, Robert G. Meyer, Robert Graham Albers
  • Patent number: 11020913
    Abstract: A process and system for improving surface quality of composite structures, including laying up a first set of composite plies including a first outer ply of a first composite structure. A first intermediate surface of the first outer ply is measured to form a first set of measurements. A laydown surface for a tool path of a composite placement machine is modified to form a modified tool path, wherein modifying the laydown surface comprises modifying the laydown surface such that a laydown surface of the modified tool path matches the first set of measurements. A composite ply is laid down using the composite placement machine and the modified tool path.
    Type: Grant
    Filed: May 11, 2018
    Date of Patent: June 1, 2021
    Assignee: The Boeing Company
    Inventors: Michael Kenneth-Que Louie, Robert Graham Albers, Jeron D. Moore, Luis A. Perla, Gagandeep Saini, Brice A. Johnson, Marcin A. Rabiega
  • Patent number: 10974465
    Abstract: A method and system for forming a composite laminate. A layup plan is generated for laying up a plurality of plies having a plurality of merge zones, each ply of the plurality of plies having a corresponding merge zone at which ends of a first plurality of tows for each ply and ends of a second plurality of tows for each ply meet. The locations of the plurality of merge zones are offset relative to each other through a thickness of the composite laminate. The plurality of plies is then laid up according to the layup plan to form a composite laminate.
    Type: Grant
    Filed: June 20, 2018
    Date of Patent: April 13, 2021
    Assignee: The Boeing Company
    Inventors: Jeron D. Moore, Michael Kenneth-Que Louie, Gagandeep Saini, Luis A. Perla, Brice Aaron Johnson, Stewart James Ibbotson, Robert G. Meyer
  • Publication number: 20190389149
    Abstract: A method and system for forming a composite laminate. A layup plan is generated for laying up a plurality of plies having a plurality of merge zones, each ply of the plurality of plies having a corresponding merge zone at which ends of a first plurality of tows for each ply and ends of a second plurality of tows for each ply meet. The locations of the plurality of merge zones are offset relative to each other through a thickness of the composite laminate. The plurality of plies is then laid up according to the layup plan to form a composite laminate.
    Type: Application
    Filed: June 20, 2018
    Publication date: December 26, 2019
    Inventors: Jeron D. Moore, Michael Kenneth-Que Louie, Gagandeep Saini, Luis A. Perla, Brice Aaron Johnson, Stewart James Ibbotson, Robert G. Meyer
  • Publication number: 20190389150
    Abstract: A method and apparatus for forming a composite object. A first plurality of tows is laid up over a tool according to a first path. A second plurality of tows is laid up over the tool according to a second path. A first portion of the first plurality of tows runs non-parallel to a second portion of the second plurality of tows. First ends of the first portion of the first plurality of tows and second ends of the second portion of the second plurality of tows meet at a merge zone along the tool to form a ply of a composite laminate.
    Type: Application
    Filed: June 20, 2018
    Publication date: December 26, 2019
    Inventors: Michael Kenneth-Que Louie, Jeron D. Moore, Gagandeep Saini, Luis A. Perla, Brice Aaron Johnson, Stewart James Ibbotson, Timothy D. Jackson, Robert G. Meyer, Robert Graham Albers
  • Publication number: 20190344513
    Abstract: An illustrative example of the present disclosure provides a method. A first set of composite plies including a first outer ply of a first composite structure is laid up. A first intermediate surface of the first outer ply is measured to form a first set of measurements. A laydown surface for a tool path of a composite placement machine is modified to form a modified tool path, wherein modifying the laydown surface comprises modifying the laydown surface such that a laydown surface of the modified tool path matches the first set of measurements. A composite ply is laid down using the composite placement machine and the modified tool path.
    Type: Application
    Filed: May 11, 2018
    Publication date: November 14, 2019
    Inventors: Michael Kenneth-Que Louie, Robert Graham Albers, Jeron D. Moore, Luis A. Perla, Gagandeep Saini, Brice A. Johnson, Marcin A. Rabiega
  • Publication number: 20190301860
    Abstract: A method for analyzing a surface quality of a laminate part including the steps of creating a planned dimensioned representation of a laminate part desired to be built which includes a first surface having a first topography; placing fibers into locations for the laminate part desired to be built; and curing a resin associated with the placed fibers fabricating an as-built laminate part which includes a second surface having a second topography which corresponds to the first surface having the first topography. The method also includes aligning the first surface, the second surface and the locations of the fibers; determining a first elevation of a first point on the first surface and a second elevation of a second point on the second surface; and observing the first surface, the second surface and the locations of the fibers in alignment and the first elevation relative to the second elevation in analyzing the surface quality of the laminate part.
    Type: Application
    Filed: April 2, 2018
    Publication date: October 3, 2019
    Inventors: Jeron D. Moore, Michael K. Louie, Luis A. Perla, Gagandeep Saini, Christopher W. Fay, Robert G. Meyer
  • Publication number: 20190247884
    Abstract: Surface treatment of a tubular surface defining an axis extending from a first surface end to a second surface end includes partially surrounding the tubular surface, at a first position, with a first set of treating units, with the treating units arranged in a first arcuate array. Furthermore, each treating unit is configured to include a plurality of first applicator heads. In some examples, a position of each of the plurality of first applicator heads is determined relative to the tubular surface. The first set of treating units is moved from the first position towards a second position. In one non-limiting example, each of the plurality of first applicator heads is independently controlled to selectively apply a first treatment as the first set of treating units moves from the first position towards the second position.
    Type: Application
    Filed: April 22, 2019
    Publication date: August 15, 2019
    Applicant: The Boeing Company
    Inventors: Shane E. Arthur, Bennett M. Moriarty, Luis A. Perla, Jeffrey S. Rebmann, Trevor S. McCrea, Jason S. Warner, Seana B. Kobak, Ryan M. Trumbo
  • Patent number: 10307788
    Abstract: A method of treating a tubular surface which defines an axis extending from a first surface end to a second surface end includes partially surrounding the tubular surface, at a first position, with a first set of treating units, with the treating units arranged in a first arcuate array. Furthermore, each treating unit is configured to include a plurality of first applicator heads. Additionally, an embodiment of the method includes determining a position of each of the plurality of first applicator heads relative to the tubular surface and moving the first set of treating units from the first position towards a second position. In one non-limiting example, the method further includes independently controlling each of the plurality of first applicator heads to selectively apply a first treatment as the first set of treating units moves from the first position towards the second position.
    Type: Grant
    Filed: November 9, 2016
    Date of Patent: June 4, 2019
    Assignee: The Boeing Company
    Inventors: Shane E. Arthur, Bennett M. Moriarty, Luis A. Perla, Jeffrey S. Rebmann, Trevor S. McCrea, Jason S. Warner, Seana B. Kobak, Ryan M. Trumbo
  • Publication number: 20180126416
    Abstract: A method of treating a tubular surface which defines an axis extending from a first surface end to a second surface end includes partially surrounding the tubular surface, at a first position, with a first set of treating units, with the treating units arranged in a first arcuate array. Furthermore, each treating unit is configured to include a plurality of first applicator heads. Additionally, an embodiment of the method includes determining a position of each of the plurality of first applicator heads relative to the tubular surface and moving the first set of treating units from the first position towards a second position. In one non-limiting example, the method further includes independently controlling each of the plurality of first applicator heads to selectively apply a first treatment as the first set of treating units moves from the first position towards the second position.
    Type: Application
    Filed: November 9, 2016
    Publication date: May 10, 2018
    Applicant: The Boeing Company
    Inventors: Shane E. Arthur, Bennett M. Moriarty, Luis A. Perla, Jeffrey S. Rebmann, Trevor S. McCrea, Jason S. Warner, Seana B. Kobak, Ryan M. Trumbo
  • Patent number: 9669579
    Abstract: A method for forming a structural member and a structural member produced thereby includes positioning a first composite section and a second composite section within a tool. The tool has an inner surface and a wall intersection and is supported by a tool platform. The tool platform and a pressure platform are relatively movable between an open position and a closed position. The tool has a non-planar outer surface against which the member may be pressed. A composite splice member is positioned at least partially overlapping both the first composite section and the second composite section to form a joint in the composite structural member. The composite structural member is pressed against the non-planar outer surface of the tool by applying pressure to the joint from a pressure bladder. Heat is applied to the composite structural member at the joint to cure the composite splice member to the first composite section and the second composite section.
    Type: Grant
    Filed: September 17, 2014
    Date of Patent: June 6, 2017
    Assignee: THE BOEING COMPANY
    Inventors: William T. Kline, Charles J. Nelson, Thang D. Phung, Curtis M. Groth, Robert G. Meyer, Peter J. VanVoast, Charles Y. Hu, Geoffrey A. Butler, Dan D. Day, Thomas J. Kennedy, Luis A. Perla, Richard A. Ransom, Justin L. Holland, Erik Lund, Joseph F. Warren
  • Patent number: 9395041
    Abstract: A method and apparatus for performing an operation on a structure. In one illustrative embodiment, an apparatus comprises a tool system and a movement system. The tool system is configured to perform an operation at a location on a structure. The movement system is configured to move the tool system along an elongate frame on the structure to the location.
    Type: Grant
    Filed: May 14, 2013
    Date of Patent: July 19, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Luis A. Perla, Clayton Lynn Munk, Stephen Glade Holley
  • Publication number: 20140339394
    Abstract: A method and apparatus for performing an operation on a structure. In one illustrative embodiment, an apparatus comprises a tool system and a movement system. The tool system is configured to perform an operation at a location on a structure. The movement system is configured to move the tool system along an elongate frame on the structure to the location.
    Type: Application
    Filed: May 14, 2013
    Publication date: November 20, 2014
    Applicant: THE BOEING COMPANY
    Inventors: Luis A. Perla, Clayton Lynn Munk, Stephen Glade Holley