Patents by Inventor James B. Weathers

James B. Weathers 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: 20240066637
    Abstract: A friction weld plug includes a gasket and a stud. The stud includes a nose configured to be inserted into a first hole formed within a wall. The nose includes a cavity having female threads. The stud also includes a shoulder extending radially from the nose and including a groove configured to contain the gasket. The friction weld plug also includes a spacer including a second hole and a fastener including male threads. The fastener is configured to be inserted through the second hole, into the first hole, and into the cavity such that the male threads and the female threads form an attachment that presses the spacer against a first side of the wall and presses the gasket against a second side of the wall that is opposite the first side, thereby forming a seal between the gasket and the second side of the wall.
    Type: Application
    Filed: August 30, 2022
    Publication date: February 29, 2024
    Inventors: Jeffrey W. Weathers, James B. Weathers
  • Patent number: 11435730
    Abstract: A system and method include a simulation control unit configured to receive structural data regarding a structure to be formed. The simulation control unit performs a virtual forming simulation to determine a feasibility of forming the structure based on the structural data. In response to the simulation control unit determining that the structure can be feasibly formed based on the structural data, the simulation control unit outputs a forming plan for forming the structure based on the structural data.
    Type: Grant
    Filed: June 4, 2020
    Date of Patent: September 6, 2022
    Assignee: THE BOEING COMPANY
    Inventors: James B. Weathers, Jeffrey W. Weathers
  • Publication number: 20210382468
    Abstract: A system and method include a simulation control unit configured to receive structural data regarding a structure to be formed. The simulation control unit performs a virtual forming simulation to determine a feasibility of forming the structure based on the structural data. In response to the simulation control unit determining that the structure can be feasibly formed based on the structural data, the simulation control unit outputs a forming plan for forming the structure based on the structural data.
    Type: Application
    Filed: June 4, 2020
    Publication date: December 9, 2021
    Applicant: THE BOEING COMPANY
    Inventors: James B. Weathers, Jeffrey W. Weathers
  • Patent number: 10306984
    Abstract: Provided are toroidal support structures and assemblies comprising these structures. A toroidal support structure comprises one or more side panels forming a tubular ring and one or more floor panels forming a planar ring. These rings define the toroidal shape of the structure. The structure also comprises multiple isolating linear support components connected to a top edge of the tubular ring. During installation of the structure, the isolating linear support components are attached to a mounting base for supporting the structure relative to the base, while providing thermal isolation to the rings and preventing their mechanical distortion. As such, a toroidal support structure can be attached to various types of mounting bases, such as a cryogenic tank of a spacecraft. Both rings provide supporting and mounting surfaces for equipment, cables, and pipes, while the toroidal opening allows external components to protrude through the support structure.
    Type: Grant
    Filed: December 20, 2016
    Date of Patent: June 4, 2019
    Assignee: The Boeing Company
    Inventors: Rodney H. Jones, Zachary S. Hopkins, Murray S. Edmondson, James B. Weathers, Shawn E. Mills
  • Publication number: 20180055227
    Abstract: Provided are toroidal support structures and assemblies comprising these structures. A toroidal support structure comprises one or more side panels forming a tubular ring and one or more floor panels forming a planar ring. These rings define the toroidal shape of the structure. The structure also comprises multiple isolating linear support components connected to a top edge of the tubular ring. During installation of the structure, the isolating linear support components are attached to a mounting base for supporting the structure relative to the base, while providing thermal isolation to the rings and preventing their mechanical distortion. As such, a toroidal support structure can be attached to various types of mounting bases, such as a cryogenic tank of a spacecraft. Both rings provide supporting and mounting surfaces for equipment, cables, and pipes, while the toroidal opening allows external components to protrude through the support structure.
    Type: Application
    Filed: December 20, 2016
    Publication date: March 1, 2018
    Applicant: The Boeing Company
    Inventors: Rodney H. Jones, Zachary S. Hopkins, Murray S. Edmondson, James B. Weathers, Shawn E. Mills