Patents by Inventor Mary LeAnn Parker

Mary LeAnn Parker 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: 11806948
    Abstract: Systems and methods are provided for utilizing stringer end caps. One embodiment is a method of forming a stringer. The method includes laying up a stringer preform comprising fiber-reinforced material, placing the stringer preform onto a skin panel preform, bonding an end cap to the stringer preform and the skin panel preform, and co-curing the stringer preform and the skin panel preform while the end cap is bonded to the stringer preform and the skin panel preform, resulting in a composite part that includes the end cap.
    Type: Grant
    Filed: December 12, 2019
    Date of Patent: November 7, 2023
    Assignee: The Boeing Company
    Inventors: Mary LeAnn Parker, Khanh Mai Pham, Lisa Christina Carlson, Garrett Charles Hanson
  • Patent number: 11718047
    Abstract: Systems and methods are provided for fabricating composite parts. One embodiment is a method for fabricating a composite part. The method includes forming a skin panel preform comprising fiber reinforced material, disposing rigid end caps at the skin panel preform at end locations of stringer preforms that will be placed at the skin panel, locating the stringer preforms at the skin panel preform via the rigid end caps, and anchoring the stringer preforms to the skin panel preform.
    Type: Grant
    Filed: December 12, 2019
    Date of Patent: August 8, 2023
    Assignee: The Boeing Company
    Inventors: Mary LeAnn Parker, Khanh Mai Pham, Lisa Christina Carlson, Garrett Charles Hanson
  • Publication number: 20230219308
    Abstract: A method, apparatus, system, and computer program product for fabricating a composite part. Composite materials are laid up on a mandrel. A caul is placed over the composite materials laid up on the mandrel. An inner mold line of the caul is sized to an outer surface of the composite materials in a cured state. The composite materials laid up on the mandrel with the caul over the composite materials is cured to form the composite part. The composite materials expand to the inner mold line of the caul during curing of the composite materials to form the composite part.
    Type: Application
    Filed: January 7, 2022
    Publication date: July 13, 2023
    Inventors: Mary LeAnn Parker, Khanh Mai Pham, Jonathan Santiago
  • Patent number: 11426958
    Abstract: Systems and methods are provided for composite part fabrication. One embodiment is a method for fabricating a composite part. The method includes selecting an end caul comprising a structure of sintered material surrounding volumes of unsintered particles, creating a laminate comprising fibers within a resin matrix, placing the end caul in contact with an end of the laminate, and processing the laminate.
    Type: Grant
    Filed: May 30, 2018
    Date of Patent: August 30, 2022
    Assignee: The Boeing Company
    Inventors: Lisa Christina Carlson, Scott Allen Boner, Khanh Mai Pham, Mary Leann Parker, Alicia Salcedo Medina, John A. Minerich
  • Publication number: 20210178706
    Abstract: Systems and methods are provided for fabricating composite parts. One embodiment is a method for fabricating a composite part. The method includes forming a skin panel preform comprising fiber reinforced material, disposing rigid end caps at the skin panel preform at end locations of stringer preforms that will be placed at the skin panel, locating the stringer preforms at the skin panel preform via the rigid end caps, and anchoring the stringer preforms to the skin panel preform.
    Type: Application
    Filed: December 12, 2019
    Publication date: June 17, 2021
    Inventors: Mary LeAnn Parker, Khanh Mai Pham, Lisa Christina Carlson, Garrett Charles Hanson
  • Publication number: 20210178708
    Abstract: Systems and methods are provided for utilizing stringer end caps. One embodiment is a method of forming a stringer. The method includes laying up a stringer preform comprising fiber-reinforced material, placing the stringer preform onto a skin panel preform, bonding an end cap to the stringer preform and the skin panel preform, and co-curing the stringer preform and the skin panel preform while the end cap is bonded to the stringer preform and the skin panel preform, resulting in a composite part that includes the end cap.
    Type: Application
    Filed: December 12, 2019
    Publication date: June 17, 2021
    Inventors: Mary LeAnn Parker, Khanh Mai Pham, Lisa Christina Carlson, Garrett Charles Hanson
  • Publication number: 20190366653
    Abstract: Systems and methods are provided for composite part fabrication. One embodiment is a method for fabricating a composite part. The method includes selecting an end caul comprising a structure of sintered material surrounding volumes of unsintered particles, creating a laminate comprising fibers within a resin matrix, placing the end caul in contact with an end of the laminate, and processing the laminate.
    Type: Application
    Filed: May 30, 2018
    Publication date: December 5, 2019
    Inventors: Lisa Christina Carlson, Scott Allen Boner, Khanh Mai Pham, Mary LeAnn Parker, Alicia Salcedo Medina, John A. Minerich