Patents by Inventor James Steven Payne

James Steven Payne 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: 10822071
    Abstract: Systems and methods are provided for enforcing contours onto parts of an aircraft. One embodiment is a method for enforcing a contour onto aircraft parts. The method includes removably attaching segmented ring details to aircraft skin details, attaching stringers to skin details to create skin assemblies, positioning skin assemblies at a support structure defining a contour, and fastening frames to the skin assemblies to create a panel. The method also includes removably installing a spreader section onto the panel to complete assembly of a brace prior to removal of the panel, transporting the panel while the brace enforces the contour, attaching the brace to braces for other panels to form a barrel section of a fuselage for an aircraft while the brace enforces the contour, and removing the brace from the barrel section after the barrel section has been formed.
    Type: Grant
    Filed: November 14, 2018
    Date of Patent: November 3, 2020
    Assignee: The Boeing Company
    Inventor: James Steven Payne
  • Publication number: 20190084663
    Abstract: Systems and methods are provided for enforcing contours onto parts of an aircraft. One embodiment is a method for enforcing a contour onto aircraft parts. The method includes removaby attaching segmented ring details to aircraft skin details, attaching stringers to skin details to create skin assemblies, positioning skin assemblies at a support structure defining a contour, and fastening frames to the skin assemblies to create a panel. The method also includes removably installing a spreader section onto the panel to complete assembly of a brace prior to removal of the panel, transporting the panel while the brace enforces the contour, attaching the brace to braces for other panels to form a barrel section of a fuselage for an aircraft while the brace enforces the contour, and removing the brace from the barrel section after the barrel section has been formed.
    Type: Application
    Filed: November 14, 2018
    Publication date: March 21, 2019
    Inventor: James Steven Payne
  • Patent number: 10160531
    Abstract: Systems and methods are provided for enforcing contours onto parts of an aircraft. One embodiment is a method for enforcing a contour onto aircraft parts. The method includes removably attaching segmented ring details to aircraft skin details, attaching stringers to skin details to create skin assemblies, positioning skin assemblies at a support structure defining a contour, and fastening frames to the skin assemblies to create a panel. The method also includes removably installing a spreader section onto the panel to complete assembly of a brace prior to removal of the panel, transporting the panel while the brace enforces the contour, attaching the brace to braces for other panels to form a barrel section of a fuselage for an aircraft while the brace enforces the contour, and removing the brace from the barrel section after the barrel section has been formed.
    Type: Grant
    Filed: June 22, 2016
    Date of Patent: December 25, 2018
    Assignee: The Boeing Company
    Inventor: James Steven Payne
  • Publication number: 20170369144
    Abstract: Systems and methods are provided for enforcing contours onto parts of an aircraft. One embodiment is a method for enforcing a contour onto aircraft parts. The method includes removably attaching segmented ring details to aircraft skin details, attaching stringers to skin details to create skin assemblies, positioning skin assemblies at a support structure defining a contour, and fastening frames to the skin assemblies to create a panel. The method also includes removably installing a spreader section onto the panel to complete assembly of a brace prior to removal of the panel, transporting the panel while the brace enforces the contour, attaching the brace to braces for other panels to form a barrel section of a fuselage for an aircraft while the brace enforces the contour, and removing the brace from the barrel section after the barrel section has been formed.
    Type: Application
    Filed: June 22, 2016
    Publication date: December 28, 2017
    Inventor: James Steven Payne
  • Publication number: 20110283993
    Abstract: A water heater includes: an inner tank having an internal cavity configured to hold water therein; a heating device residing in the internal cavity; an outer lining that surrounds the inner tank, a gap being present between the outer lining and the inner tank; and insulation material located in the gap. The gap is under a vacuum of between about 5 and 200 microns. In this configuration, the water heater can have an R value in excess of 500. With this level of insulative capacity, water stored in the water heater may lose only 2° F. or less over a 24 hour period, thereby substantially outperforming conventional water heaters.
    Type: Application
    Filed: September 7, 2010
    Publication date: November 24, 2011
    Inventors: Jeffrey Rex Winegar, James Steven Payne, William Robert Jones