Patents by Inventor Gordon Dale Davis

Gordon Dale Davis 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: 11370159
    Abstract: A flexible punch and die are used to form a flat composite laminate charge into a stiffener having a desired cross sectional shape. A desired contour is formed in the stiffener by bending the punch and die. Ply wrinkling is avoided during contouring by maintaining those portions of the stiffener subject to wrinkling in tension as the contouring is being performed. Bridging of the plies during the contouring process is avoided by first contouring those sections of the stiffener that are subject to wrinkling, and then contouring the remaining sections of the stiffener.
    Type: Grant
    Filed: August 5, 2019
    Date of Patent: June 28, 2022
    Assignee: The Boeing Company
    Inventors: Michael Robert Chapman, Gordon Dale Davis
  • Publication number: 20200001516
    Abstract: A flexible punch and die are used to form a flat composite laminate charge into a stiffener having a desired cross sectional shape. A desired contour is formed in the stiffener by bending the punch and die. Ply wrinkling is avoided during contouring by maintaining those portions of the stiffener subject to wrinkling in tension as the contouring is being performed. Bridging of the plies during the contouring process is avoided by first contouring those sections of the stiffener that are subject to wrinkling, and then contouring the remaining sections of the stiffener.
    Type: Application
    Filed: August 5, 2019
    Publication date: January 2, 2020
    Inventors: Michael Robert Chapman, Gordon Dale Davis
  • Patent number: 10369740
    Abstract: A flexible punch and die are used to form a flat composite laminate charge into a stiffener having a desired cross sectional shape. A desired contour is formed in the stiffener by bending the punch and die. Ply wrinkling is avoided during contouring by maintaining those portions of the stiffener subject to wrinkling in tension as the contouring is being performed. Bridging of the plies during the contouring process is avoided by first contouring those sections of the stiffener that are subject to wrinkling, and then contouring the remaining sections of the stiffener.
    Type: Grant
    Filed: July 9, 2015
    Date of Patent: August 6, 2019
    Assignee: The Boeing Company
    Inventors: Michael Robert Chapman, Gordon Dale Davis
  • Publication number: 20170008217
    Abstract: A flexible punch and die are used to form a flat composite laminate charge into a stiffener having a desired cross sectional shape. A desired contour is formed in the stiffener by bending the punch and die. Ply wrinkling is avoided during contouring by maintaining those portions of the stiffener subject to wrinkling in tension as the contouring is being performed. Bridging of the plies during the contouring process is avoided by first contouring those sections of the stiffener that are subject to wrinkling, and then contouring the remaining sections of the stiffener.
    Type: Application
    Filed: July 9, 2015
    Publication date: January 12, 2017
    Inventors: Michael Robert Chapman, Gordon Dale Davis
  • Patent number: 9272793
    Abstract: An apparatus for supporting a wing assembly at a wing assembly support height. Base sections are provided, each having a different predetermined height with respect to one another. A movable platform carries a plurality of base sections, and a plurality of wing assembly support sections rest on base sections and include wing assembly connectors, which are movable in a first plane and a second plane generally perpendicular relative to the first plane. A differential height is defined between the wing assembly support height and the combined heights of the platform and the height of wing assembly connector, relative to the bottom of the wing assembly support section. At least one of the base sections is of a predetermined height approximating the differential height and is carried on the platform. The wing assembly support section is carried on such base section.
    Type: Grant
    Filed: April 30, 2014
    Date of Patent: March 1, 2016
    Assignee: The Boeing Company
    Inventors: Kim Marie Larson, Raymond Cho Eng, Clayton Lynn Munk, Dan Dresskell Day, Gordon Dale Davis
  • Publication number: 20150344154
    Abstract: An apparatus for supporting a wing assembly at a wing assembly support height. Base sections are provided, each having a different predetermined height with respect to one another. A movable platform carries a plurality of base sections, and a plurality of wing assembly support sections rest on base sections and include wing assembly connectors, which are movable in a first plane and a second plane generally perpendicular relative to the first plane. A differential height is defined between the wing assembly support height and the combined heights of the platform and the height of wing assembly connector, relative to the bottom of the wing assembly support section. At least one of the base sections is of a predetermined height approximating the differential height and is carried on the platform. The wing assembly support section is carried on such base section.
    Type: Application
    Filed: April 30, 2014
    Publication date: December 3, 2015
    Applicant: The Boeing Company
    Inventors: Kim Marie Larson, Raymond Cho Eng, Clayton Lynn Munk, Dan Dresskell Day, Gordon Dale Davis