Patents by Inventor Marcin A. Rabiega

Marcin A. Rabiega 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
  • 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: 20220245294
    Abstract: A method for determining a shim profile for assembling a first mating surface of a first part with a second mating surface of a second part includes: obtaining a baseline surface model of the first mating surface; scanning the first mating surface when the first part is in a deviated configuration to generate a scan-based surface model of the first mating surface; deforming the scan-based surface model of the first mating surface relative to the baseline surface model of the first mating surface to generate a first deformed surface model of the first mating surface; deforming the first deformed surface model of the first mating surface relative to a surface model of the second mating surface to generate a second deformed surface model of the first mating surface; and comparing the second deformed surface model of the first mating surface to the surface model of the second mating surface.
    Type: Application
    Filed: December 3, 2021
    Publication date: August 4, 2022
    Applicant: The Boeing Company
    Inventors: Marcin A. Rabiega, Theodore M. Boyl-Davis, Ronald J. Collins, Christopher M. Rhoads, Clifford D. Borowicz, Steve X. Cheng, Joel T. Adriance
  • Publication number: 20220234314
    Abstract: In an example, a method of shimming an uncured substructure for assembly is disclosed. The method comprises emitting a signal from an inspection system proximate a mating surface of the substructure, detecting a reflection of the signal with the inspection system, generating a data set based on detecting the reflection of the signal, the data set representing a shape of the mating surface, determining distances between a plurality of points on the mating surface and respective points on an inner surface of a support structure based on the data set, generating filler dimension data based on the distances, wherein the filler dimension data includes a varying thickness, shaping a filler structure with a computer numerical controlled shaping device using the filler dimension data, adhering a first surface of the filler structure to the mating surface of the substructure to form a shimmed substructure subassembly, and curing the shimmed substructure subassembly.
    Type: Application
    Filed: January 19, 2022
    Publication date: July 28, 2022
    Inventors: Marcin A. Rabiega, Kevin L. Braun, Jason R. Grindon, Yaniv R. Rock, John C. Osborne
  • 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: 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
  • 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