Patents by Inventor Theodore Joseph Eilert

Theodore Joseph Eilert 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: 12599953
    Abstract: A method of manufacturing a complex-shaped metal part, including the steps of applying a metallic sheath around a sheet metal workpiece and applying an electric current through the workpiece in the metallic sheath to heat the workpiece. The method also includes shaping the workpiece in the metallic sheath into a complex-shaped metal part while it is being heated. The shaping can be performed between two ceramic dies or using other techniques for forming complex shapes and curvatures into the workpiece. The method then may include cooling the complex-shaped metal part and removing the metallic sheath from the complex-shaped metal part. This method can allow reactive and refractory material to be safely heated without oxidation when heating/forming in air when the workpiece is sealed within a sacrificial stainless steel or nickel alloy envelope to protect the enclosed workpiece.
    Type: Grant
    Filed: February 28, 2022
    Date of Patent: April 14, 2026
    Assignee: Spirit AeroSystems, Inc.
    Inventors: James Michael Wagner, Jr., Theodore Joseph Eilert, Rahbar Nasserrafi, Craig Matthew Clasper, Gerald Eugene Hicks, Jr.
  • Patent number: 12017297
    Abstract: A method of manufacturing metal matrix composite (MMC) parts, including the steps of applying a metallic sheath around a bundle of MMC laminates, heating the bundle of MMC laminates in the metallic sheath at a curing or fusing temperature to consolidate the bundle of MMC laminates into a single cured or fused part, and then cooling the cured or fused part. The bundle of MMC laminates may be formed by removing surface contamination from the dry reinforcement fibers, creating a plurality of individual MMC laminates by plating dry reinforcement fibers with electroless nickel, and/or electrodeposited nickel or cobalt, and stacking each of the plurality of individual MMC laminates into a bundle. Autocatalytic and/or electroplating may be used as the primary means to incorporate fiber reinforcement into the metal matrix composite by covering and bonding fiber reinforcement into MMC laminates/plies and/or 3-D woven parts.
    Type: Grant
    Filed: December 22, 2021
    Date of Patent: June 25, 2024
    Assignee: Spirit AeroSystems, Inc.
    Inventors: Rahbar Nasserrafi, Kerrick Robert Dando, Gerald Eugene Hicks, Jr., Theodore Joseph Eilert, Shawn Douglas Vierthaler
  • Publication number: 20230271242
    Abstract: A method of manufacturing a complex-shaped metal part, including the steps of applying a metallic sheath around a sheet metal workpiece and applying an electric current through the workpiece in the metallic sheath to heat the workpiece. The method also includes shaping the workpiece in the metallic sheath into a complex-shaped metal part while it is being heated. The shaping can be performed between two ceramic dies or using other techniques for forming complex shapes and curvatures into the workpiece. The method then may include cooling the complex-shaped metal part and removing the metallic sheath from the complex-shaped metal part. This method can allow reactive and refractory material to be safely heated without oxidation when heating/forming in air when the workpiece is sealed within a sacrificial stainless steel or nickel alloy envelope to protect the enclosed workpiece.
    Type: Application
    Filed: February 28, 2022
    Publication date: August 31, 2023
    Applicant: Spirit AeroSystems, Inc.
    Inventors: James Michael Wagner, Jr., Theodore Joseph Eilert, Rahbar Nasserrafi, Craig Matthew Clasper, Gerald Eugene Hicks, Jr.
  • Publication number: 20230191528
    Abstract: A method of manufacturing metal matrix composite (MMC) parts, including the steps of applying a metallic sheath around a bundle of MMC laminates, heating the bundle of MMC laminates in the metallic sheath at a curing or fusing temperature to consolidate the bundle of MMC laminates into a single cured or fused part, and then cooling the cured or fused part. The bundle of MMC laminates may be formed by removing surface contamination from the dry reinforcement fibers, creating a plurality of individual MMC laminates by plating dry reinforcement fibers with electroless nickel, and/or electrodeposited nickel or cobalt, and stacking each of the plurality of individual MMC laminates into a bundle. Autocatalytic and/or electroplating may be used as the primary means to incorporate fiber reinforcement into the metal matrix composite by covering and bonding fiber reinforcement into MMC laminates/plies and/or 3-D woven parts.
    Type: Application
    Filed: December 22, 2021
    Publication date: June 22, 2023
    Applicant: Spirit AeroSystems, Inc.
    Inventors: Rahbar Nasserrafi, Kerrick Robert Dando, Gerald Eugene Hicks, JR., Theodore Joseph Eilert, Shawn Douglas Vierthaler