Patents by Inventor Eric E. Thomas

Eric E. Thomas 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: 11426942
    Abstract: Manufacturing systems with coolant supply systems and related methods. A manufacturing system includes an additive manufacturing (AM) assembly, a milling assembly, and a coolant supply system. The AM assembly includes a support assembly that supports a build component and that is in thermal communication with the build component. The coolant supply system is configured to remove heat from the support assembly by flowing the coolant through at least a portion of the support assembly. A method of operating a manufacturing system during a manufacturing process includes detecting a manufacturing mode of the manufacturing system, forming a build component via the manufacturing process, and, at least partially concurrent with the forming the build component, selectively supplying a coolant to a support assembly and/or a milling tool. The selectively supplying the coolant is based, at least in part, on the detecting the manufacturing mode.
    Type: Grant
    Filed: April 15, 2019
    Date of Patent: August 30, 2022
    Assignee: The Boeing Company
    Inventors: Andrew P. Simpson, Eric E. Thomas
  • Publication number: 20200324484
    Abstract: Manufacturing systems with coolant supply systems and related methods. A manufacturing system includes an additive manufacturing (AM) assembly, a milling assembly, and a coolant supply system. The AM assembly includes a support assembly that supports a build component and that is in thermal communication with the build component. The coolant supply system is configured to remove heat from the support assembly by flowing the coolant through at least a portion of the support assembly. A method of operating a manufacturing system during a manufacturing process includes detecting a manufacturing mode of the manufacturing system, forming a build component via the manufacturing process, and, at least partially concurrent with the forming the build component, selectively supplying a coolant to a support assembly and/or a milling tool. The selectively supplying the coolant is based, at least in part, on the detecting the manufacturing mode.
    Type: Application
    Filed: April 15, 2019
    Publication date: October 15, 2020
    Inventors: Andrew P. Simpson, Eric E. Thomas
  • Patent number: 10479474
    Abstract: Provided are wingtip torque boxes and methods of fabricating such boxes using friction stir welding. Specifically, a wingtip torque box may be formed by friction stir welding two monolithic clamshells along their respective spars thereby forming a new monolithic structure. Use of the friction stir welding and monolithic clamshells simplifies the overall fabrication process and yields a robust wingtip torque box that can be bolted on or otherwise attached to an aircraft wing. The wingtip torque box may include internal grid stiffeners and/or external stiffeners that may be also monolithic with other components of the box. For example, the stiffeners may be machined in spars or skin portions of the clamshells during fabrication of clamshells. The wingtip torque box may have a continuous cavity extending between the ends and, in some embodiments, between spars of the box and providing access for performing various operations inside the box.
    Type: Grant
    Filed: July 14, 2016
    Date of Patent: November 19, 2019
    Assignee: The Boeing Company
    Inventors: Michael P. Shemkunas, Kenneth D. Cominsky, Steven S. Heer, David P. Heck, Benjamin D. Smith, John A. Baumann, Matthew D. Uhlman, Burke L. Reichlinger, Eric E. Thomas, James P. Dobberfuhl
  • Publication number: 20190300173
    Abstract: A bulkhead partition for a passenger cabin of an aircraft includes an upper portion and a lower portion, with the lower portion forming a compartment that provides additional storage and/or foot space for passengers seated in the row of seats directly behind the bulkhead partition. Related passenger seating arrangements and methods are also disclosed.
    Type: Application
    Filed: March 28, 2018
    Publication date: October 3, 2019
    Inventor: Eric E. Thomas
  • Publication number: 20180056436
    Abstract: Systems, methods, and devices are disclosed herein that repair and fill exit holes created by welding operations on vehicle components or parts. Methods may include inserting a plug into the exit hole in one or more vehicle parts, where the exit hole is created by the welding operation performed on the one or more vehicle parts. Methods may further include positioning a first pin on the plug such that the first pin is contacting an exposed surface of the plug, and rotating the first pin while contacting the exposed surface of the plug, where the rotating generates thermal energy based on a frictional force associated with the first pin and the plug. The methods may also include filling the exit hole by heating and plasticizing the plug via the thermal energy, and consolidating a material of the plug with the one or more vehicle parts.
    Type: Application
    Filed: August 26, 2016
    Publication date: March 1, 2018
    Applicant: The Boeing Company
    Inventors: Eric E. Thomas, Sean M. Thuston, Brian J. Martinek, John A. Baumann
  • Publication number: 20180056439
    Abstract: Systems, methods, and devices are disclosed herein that repair and fill exit holes created by welding operations on vehicle components or parts. Methods disclosed herein may include inserting a plug into an exit hole in one or more vehicle parts, where the exit hole is created by a welding operation performed on the one or more vehicle parts. Methods may also include positioning a shoulder member on the plug such that the shoulder member is contacting an exposed surface of the plug. Methods may further include rotating the shoulder member while contacting the exposed surface of the plug, the rotating generating thermal energy based on a frictional force associated with the shoulder member and the plug. Methods may also include filling the exit hole by heating and plasticizing the plug via the thermal energy, and consolidating a material of the plug with the one or more vehicle parts.
    Type: Application
    Filed: February 22, 2017
    Publication date: March 1, 2018
    Applicant: THE BOEING COMPANY
    Inventors: ERIC E. THOMAS, SEAN M. THUSTON, BRIAN J. MARTINEK, JOHN A. BAUMANN
  • Publication number: 20180015996
    Abstract: Provided are wingtip torque boxes and methods of fabricating such boxes using friction stir welding. Specifically, a wingtip torque box may be formed by friction stir welding two monolithic clamshells along their respective spars thereby forming a new monolithic structure. Use of the friction stir welding and monolithic clamshells simplifies the overall fabrication process and yields a robust wingtip torque box that can be bolted on or otherwise attached to an aircraft wing. The wingtip torque box may include internal grid stiffeners and/or external stiffeners that may be also monolithic with other components of the box. For example, the stiffeners may be machined in spars or skin portions of the clamshells during fabrication of clamshells. The wingtip torque box may have a continuous cavity extending between the ends and, in some embodiments, between spars of the box and providing access for performing various operations inside the box.
    Type: Application
    Filed: July 14, 2016
    Publication date: January 18, 2018
    Applicant: The Boeing Company
    Inventors: Michael P. Shemkunas, Kenneth D. Cominsky, Steven S. Heer, David P. Heck, Benjamin D. Smith, John A. Baumann, Matthew D. Uhlman, Burke L. Reichlinger, Eric E. Thomas, James P. Dobberfuhl