Patents by Inventor Kelsi Hurley

Kelsi Hurley 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: 11203176
    Abstract: A ply for fabricating composite material includes a first tow of a plurality of fibers, which are spread in a direction along a width of a cross section of the ply, wherein a first sheet of enhanced performance material overlies the first tow. A second tow of a plurality of fibers, which are spread in the direction along the width of the cross section of the ply, overlies the first sheet of the enhanced performance material. Another tow of a plurality of fibers, which are spread in the direction along the width of the cross section of the ply, are positioned against and laterally extend from the first tow, the second tow and the first sheet of enhanced performance material.
    Type: Grant
    Filed: December 9, 2019
    Date of Patent: December 21, 2021
    Assignee: THE BOEING COMPANY
    Inventors: Samuel James Meure, Kelsi Hurley, Mark Stewart Wilenski
  • Patent number: 10870221
    Abstract: A gradient tool for forming a part, the gradient tool comprising a first tool component comprising a first surface and a second surface. The first surface comprising a first material having a first coefficient of thermal expansion (CTE), and the second surface comprising a second material having a second CTE. The first CTE of the first material is different than the second CTE of the second material.
    Type: Grant
    Filed: April 16, 2015
    Date of Patent: December 22, 2020
    Assignee: The Boeing Company
    Inventors: Keith Daniel Humfeld, Kelsi Hurley
  • Patent number: 10647084
    Abstract: A ply for fabricating composite material which includes a first tow including a plurality of fibers spread in a direction along a width of a cross section of the ply. A first sheet of enhancement performance material extends within the plurality of fibers and between a top and a bottom of the cross section of the ply.
    Type: Grant
    Filed: November 25, 2014
    Date of Patent: May 12, 2020
    Assignee: THE BOEING COMPANY
    Inventors: Samuel James Meure, Kelsi Hurley, Mark Stewart Wilenski
  • Publication number: 20200114616
    Abstract: A ply for fabricating composite material includes a first tow of a plurality of fibers, which are spread in a direction along a width of a cross section of the ply, wherein a first sheet of enhanced performance material overlies the first tow. A second tow of a plurality of fibers, which are spread in the direction along the width of the cross section of the ply, overlies the first sheet of the enhanced performance material. Another tow of a plurality of fibers, which are spread in the direction along the width of the cross section of the ply, are positioned against and laterally extend from the first tow, the second tow and the first sheet of enhanced performance material.
    Type: Application
    Filed: December 9, 2019
    Publication date: April 16, 2020
    Inventors: Samuel James Meure, Kelsi Hurley, Mark Stewart Wilenski
  • Publication number: 20160354994
    Abstract: A ply for fabricating composite material which includes a first tow including a plurality of fibers spread in a direction along a width of a cross section of the ply. A first sheet of enhancement performance material extends within the plurality of fibers and between a top and a bottom of the cross section of the ply.
    Type: Application
    Filed: November 25, 2014
    Publication date: December 8, 2016
    Inventors: Samuel James Meure, Kelsi Hurley, Mark Stewart Wilenski
  • Publication number: 20160303808
    Abstract: A gradient tool for forming a part, the gradient tool comprising a first tool component comprising a first surface and a second surface. The first surface comprising a first material having a first coefficient of thermal expansion (CTE), and the second surface comprising a second material having a second CTE. The first CTE of the first material is different than the second CTE of the second material.
    Type: Application
    Filed: April 16, 2015
    Publication date: October 20, 2016
    Inventors: Keith Daniel Humfeld, Kelsi Hurley
  • Patent number: 8863809
    Abstract: In an embodiment of the disclosure, there is provided a method and system for recycling a cured composite laminate material into a delaminated recyclate that maintains a fiber volume fraction and a lamina level fiber alignment substantially the same as the cured composite laminate material. The method provides a cured composite laminate material having a fiber volume fraction and a lamina level fiber alignment. The cured composite laminate material undergoes solvent soak preconditioning, liquid solvent removal, pre-heating, and rapid heating with phase change delamination of the cured composite laminate material to obtain the delaminated recyclate that maintains a fiber volume fraction and a lamina level fiber alignment substantially the same as the cured composite laminate material.
    Type: Grant
    Filed: November 14, 2011
    Date of Patent: October 21, 2014
    Assignee: The Boeing Company
    Inventors: Panagiotis Emanuel George, Kelsi Hurley, Erika Carter
  • Publication number: 20130118691
    Abstract: In an embodiment of the disclosure, there is provided a method and system for recycling a cured composite laminate material into a delaminated recyclate that maintains a fiber volume fraction and a lamina level fiber alignment substantially the same as the cured composite laminate material. The method provides a cured composite laminate material having a fiber volume fraction and a lamina level fiber alignment. The cured composite laminate material undergoes solvent soak preconditioning, liquid solvent removal, pre-heating, and rapid heating with phase change delamination of the cured composite laminate material to obtain the delaminated recyclate that maintains a fiber volume fraction and a lamina level fiber alignment substantially the same as the cured composite laminate material.
    Type: Application
    Filed: November 14, 2011
    Publication date: May 16, 2013
    Applicant: The Boeing Company
    Inventors: Panagiotis Emanuel George, Kelsi Hurley, Erika Carter