Patents by Inventor Rodney E. Bahr

Rodney E. Bahr 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: 11739781
    Abstract: A cap for a temporary fastener comprises a hollow, cup-shaped body and an inwardly tapered neck. The hollow body fits over a workpiece-engaging portion of the temporary fastener, and the neck extends from the hollow body. The tapered neck terminates in a hollow tip that is sized and configured to fit over aligned holes in the joined workpieces and to contact a minimal surface area of the outermost workpiece to reduce surface damage to the workpieces such that any damage will be removed when the holes are countersunk in the normal course of assembly.
    Type: Grant
    Filed: September 1, 2022
    Date of Patent: August 29, 2023
    Assignee: Spirit AeroSystems, Inc.
    Inventors: Jeremy Michael Bodecker, Jennifer Lyn Wilson, Rodney E. Bahr
  • Publication number: 20220412386
    Abstract: A cap for a temporary fastener comprises a hollow, cup-shaped body and an inwardly tapered neck. The hollow body fits over a workpiece-engaging portion of the temporary fastener, and the neck extends from the hollow body. The tapered neck terminates in a hollow tip that is sized and configured to fit over aligned holes in the joined workpieces and to contact a minimal surface area of the outermost workpiece to reduce surface damage to the workpieces such that any damage will be removed when the holes are countersunk in the normal course of assembly.
    Type: Application
    Filed: September 1, 2022
    Publication date: December 29, 2022
    Applicant: Spirit AeroSystems, Inc.
    Inventors: Jeremy Michael Bodecker, Jennifer Lyn Wilson, Rodney E. Bahr
  • Patent number: 5919543
    Abstract: A method of forming composite sine wave spars from composite material. In accordance with the method, the sine wave spar is formed of web plies, filler plies, separator plies and cap plies. The edges of the web plies are cut to form a plurality of teeth having different geometric configurations. The web plies are first formed to the sine wave contours of a tool having the desired final part geometry. The teeth of the web plies are then folded over the edges of the tool to form a portion of the flanges of upper and lower U-shaped channels. The portions of the flanges of the U-shaped channels not covered by the teeth are formed using filler plies that intermesh with the teeth to form a layer of the flanges of the respective upper or lower U-shaped channel. The flanges are reinforced through the use of separator plies that are placed between the filler plies. The formed upper and lower U-shaped channels are joined together so that their respective flanges are located in line with each other.
    Type: Grant
    Filed: August 15, 1997
    Date of Patent: July 6, 1999
    Assignee: The Boeing Company
    Inventors: Douglas A. McCarville, Rodney E. Bahr
  • Patent number: 5843355
    Abstract: A method of forming composite sine wave spars from composite material. In accordance with the method, the sine wave spar is formed of web plies, filler plies, separator plies and cap plies. The edges of the web plies are cut to form a plurality of teeth having different geometric configurations. The web plies are first formed to the sine wave contours of a tool having the desired final part geometry. The teeth of the web plies are then folded over the edges of the tool to form a portion of the flanges of upper and lower U-shaped channels. The portions of the flanges of the U-shaped channels not covered by the teeth are formed using filler plies that intermesh with the teeth to form a layer of the flanges of the respective upper or lower U-shaped channel. The flanges are reinforced through the use of separator plies that are placed between the filler plies. The formed upper and lower U-shaped channels are joined together so that their respective flanges are located in line with each other.
    Type: Grant
    Filed: January 24, 1996
    Date of Patent: December 1, 1998
    Assignee: The Boeing Company
    Inventors: Douglas A. McCarville, Rodney E. Bahr