Patents by Inventor Cori A. Jackson

Cori A. Jackson 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).

  • Publication number: 20210229328
    Abstract: There is provided an over-molded thermoplastic composite part having an over-molded color, and including a consolidated thermoplastic composite laminate formed by a consolidation process. The consolidated thermoplastic composite laminate is made of a laminate polymer material. The over-molded thermoplastic composite part further includes an over-mold layer over-molded, via an over-molding process, over a first side of the consolidated thermoplastic composite laminate. The over-mold layer includes an over-mold mixture of an over-mold polymer material mixed with one or more additives, including at least a color additive to impart a color to the consolidated thermoplastic composite laminate during the over-molding process. The over-mold polymer material has a melting temperature that is greater than, or equal to, a melting temperature of the laminate polymer material, and that is less than a thermal degradation temperature of the laminate polymer material.
    Type: Application
    Filed: January 29, 2020
    Publication date: July 29, 2021
    Inventors: Christopher H. Childers, Cori A. Jackson Oliver, Gregg R. Bogucki
  • Patent number: 10821651
    Abstract: A method for continuously fabricating a composite sandwich structure includes the steps of: (1) preheating a laminate to a preforming temperature above a glass transition temperature of the laminate but below or equal to a crystalline melt temperature of the laminate as the laminate is substantially continuously moved through a preheating zone, wherein the laminate comprises a first face sheet, a second face sheet and a core sandwiched between the first face sheet and the second face sheet; (2) consolidating the laminate as the laminate is substantially continuously moved through a consolidation zone in line with the preheating zone to form a continuous length of the composite sandwich structure; (3) moving the composite sandwich structure, substantially continuously, through at least one of a texturing zone and a coating zone; and (4) incrementally applying at least one of a surface texture and a surface coating to at least one surface of the composite sandwich structure.
    Type: Grant
    Filed: February 17, 2017
    Date of Patent: November 3, 2020
    Assignee: The Boeing Company
    Inventors: Christopher H. Childers, Cori A. Jackson, Charles Prebil
  • Patent number: 10618213
    Abstract: A method for continuously fabricating a composite sandwich structure includes the steps of: (1) moving a laminate, substantially continuously, through a preheating zone, wherein the laminate includes a first face sheet, a second face sheet and a core sandwiched between the first face sheet and the second face sheet; (2) preheating the laminate to a preforming temperature above a glass transition temperature of the laminate and below or equal to a crystalline melt temperature of the laminate as the laminate is being moved through the preheating zone; (3) moving the laminate, substantially continuously, through a consolidation zone; and (4) consolidating the laminate as the laminate is being moved through the consolidation zone to form a continuous length of the composite sandwich structure.
    Type: Grant
    Filed: February 17, 2017
    Date of Patent: April 14, 2020
    Assignee: The Boeing Company
    Inventors: Christopher H. Childers, Cori A. Jackson
  • Publication number: 20180236732
    Abstract: A method for continuously fabricating a composite sandwich structure includes the steps of: (1) preheating a laminate to a preforming temperature above a glass transition temperature of the laminate but below or equal to a crystalline melt temperature of the laminate as the laminate is substantially continuously moved through a preheating zone, wherein the laminate comprises a first face sheet, a second face sheet and a core sandwiched between the first face sheet and the second face sheet; (2) consolidating the laminate as the laminate is substantially continuously moved through a consolidation zone in line with the preheating zone to form a continuous length of the composite sandwich structure; (3) moving the composite sandwich structure, substantially continuously, through at least one of a texturing zone and a coating zone; and (4) incrementally applying at least one of a surface texture and a surface coating to at least one surface of the composite sandwich structure.
    Type: Application
    Filed: February 17, 2017
    Publication date: August 23, 2018
    Applicant: The Boeing Company
    Inventors: Christopher H. Childers, Cori A. Jackson, Charles Prebil
  • Publication number: 20180236734
    Abstract: A method for continuously fabricating a composite sandwich structure includes the steps of: (1) moving a laminate, substantially continuously, through a preheating zone, wherein the laminate includes a first face sheet, a second face sheet and a core sandwiched between the first face sheet and the second face sheet; (2) preheating the laminate to a preforming temperature above a glass transition temperature of the laminate and below or equal to a crystalline melt temperature of the laminate as the laminate is being moved through the preheating zone; (3) moving the laminate, substantially continuously, through a consolidation zone; and (4) consolidating the laminate as the laminate is being moved through the consolidation zone to form a continuous length of the composite sandwich structure.
    Type: Application
    Filed: February 17, 2017
    Publication date: August 23, 2018
    Applicant: The Boeing Company
    Inventors: Christopher H. Childers, Cori A. Jackson