Patents by Inventor Jordan O. Birkland

Jordan O. Birkland 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: 11498288
    Abstract: Forming systems and methods for drape forming a composite charge are disclosed herein. The forming systems include a forming die having a forming surface configured to receive the composite charge and a collapsible support having a support surface. The forming surface has a forming surface edge that extends along a length of the forming surface, and the support surface has a die-proximate support surface edge that extends along the length of the support surface. The forming surface edge and the die-proximate support surface edge define a gap therebetween. A shape of the die-proximate support surface edge corresponds to a shape of the forming surface edge such that a gap width of the gap is at least substantially constant along a length of the gap. The collapsible support is configured to transition from an extended conformation to a collapsed conformation. The methods include methods of utilizing the systems.
    Type: Grant
    Filed: February 11, 2020
    Date of Patent: November 15, 2022
    Assignee: The Boeing Company
    Inventors: Richard V. Phillips, Jordan O. Birkland
  • Publication number: 20210245453
    Abstract: Forming systems and methods for drape forming a composite charge are disclosed herein. The forming systems include a forming die having a forming surface configured to receive the composite charge and a collapsible support having a support surface. The forming surface has a forming surface edge that extends along a length of the forming surface, and the support surface has a die-proximate support surface edge that extends along the length of the support surface. The forming surface edge and the die-proximate support surface edge define a gap therebetween. A shape of the die-proximate support surface edge corresponds to a shape of the forming surface edge such that a gap width of the gap is at least substantially constant along a length of the gap. The collapsible support is configured to transition from an extended conformation to a collapsed conformation. The methods include methods of utilizing the systems.
    Type: Application
    Filed: February 11, 2020
    Publication date: August 12, 2021
    Inventors: Richard V. Phillips, Jordan O. Birkland
  • Patent number: 10138627
    Abstract: A composite wall assembly edge joint, includes a first composite buildup pad secured to a first composite face sheet with the first composite buildup pad having a first tapered section with a first inclined surface which extends in a first direction and having a second section which extends from the first tapered section with a second surface which extends in a second direction, different from the first direction, toward a first end of the first composite face sheet. The assembly further includes a composite flute core member, having a tapered first portion secured to the first tapered section; a second portion secured to the first composite face sheet; and a third portion which extends in the second direction, away from the tapered first portion, toward the first end of the first composite face sheet secured to the second section.
    Type: Grant
    Filed: June 5, 2017
    Date of Patent: November 27, 2018
    Assignee: THE BOEING COMPANY
    Inventors: Douglas McCarville, Juan Carlos Guzman, Michael Leslie Hand, Jordan O. Birkland, Alexandra K. Dillon
  • Publication number: 20180230693
    Abstract: A composite wall assembly edge joint, includes a first composite buildup pad secured to a first composite face sheet with the first composite buildup pad having a first tapered section with a first inclined surface which extends in a first direction and having a second section which extends from the first tapered section with a second surface which extends in a second direction, different from the first direction, toward a first end of the first composite face sheet. The assembly further includes a composite flute core member, having a tapered first portion secured to the first tapered section; a second portion secured to the first composite face sheet; and a third portion which extends in the second direction, away from the tapered first portion, toward the first end of the first composite face sheet secured to the second section.
    Type: Application
    Filed: June 5, 2017
    Publication date: August 16, 2018
    Inventors: Douglas McCarville, Juan Carlos Guzman, Michael Leslie Hand, Jordan O. Birkland, Alexandra K. Dillon
  • Patent number: 9463864
    Abstract: A radius filler for a composite assembly may include a pair of vertical ply stacks positioned in back-to-back relation. Each one of the vertical ply stacks may be formed of one or more thick plies of composite material formed in an L-shaped cross-section having a vertical leg and a lateral leg interconnected by a stack radius and defining a crescent region. At least one of the crescent regions may include one or more thin plies of composite material positioned adjacent to a stack radius inner surface. Each one of the thin plies may have a ply thickness that is less than the ply thickness of the thick plies.
    Type: Grant
    Filed: July 28, 2015
    Date of Patent: October 11, 2016
    Assignee: The Boeing Company
    Inventors: Douglas A. McCarville, Jordan O. Birkland, Ryan S. Tidwell, Juan C. Guzman