Patents by Inventor Russell J. Heeter

Russell J. Heeter 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: 10574018
    Abstract: A conductive sleeved fastener assembly includes an electrically-conductive fastener having a fastener head and a fastener shank extending from the fastener head and an electrically-conductive fastener sleeve receiving the fastener shank of the fastener and a fastener sleeve flange provided on the fastener sleeve and disposed in direct contact with the fastener head of the fastener. A method of preparing a conductive sleeved fastener for use is also disclosed.
    Type: Grant
    Filed: March 24, 2015
    Date of Patent: February 25, 2020
    Assignee: THE BOEING COMPANY
    Inventors: Thu A. Nguyen, Michael G. Parent, Russell J. Heeter, Jeffrey A. Wilkerson
  • Patent number: 10189235
    Abstract: A repair apparatus for an electrically conductive layer of a composite structure includes a dielectric layer, having a perimeter, secured to the composite structure, a first adhesive layer, and a conductive layer, secured over the dielectric layer and to the composite structure via the first adhesive layer around an entirety of the perimeter of the dielectric layer, the first adhesive layer being scored along a perimeter region thereof to improve a conductive path between the conductive layer and the composite structure.
    Type: Grant
    Filed: September 22, 2016
    Date of Patent: January 29, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Patrice K. Ackerman, Weston K. Anderson, Russell J. Heeter
  • Patent number: 10186788
    Abstract: A conductive fastener assembly, system, and method are described. The fastener assembly includes a nut having a counterbore formed therein. The counterbore is formed to maintain a sufficient gap between the nut and the protruding end of a fastener sleeve. The nut with the counterbore improves the conductive fastener system such that the need for a solid copper grid and a cap seal is reduced or eliminated.
    Type: Grant
    Filed: May 16, 2016
    Date of Patent: January 22, 2019
    Assignee: The Boeing Company
    Inventors: Russell J. Heeter, Thu A. Nguyen, John A. Ward, John R. Porter, Jeffrey A. Wilkerson
  • Patent number: 10014593
    Abstract: A conductive fastener assembly, system, and method, wherein the fastener assembly includes a fastener, a fastener sleeve, a nut, and a lubricant coating. The lubricant coating is deposited on a distal portion of a fastener shank and is omitted from the rest of the fastener. To overcome the stresses placed on the fastener sleeve by the insertion of the fastener shank largely devoid of a lubricant coating, the fastener sleeve is reinforced by one or more of an increased thickness, a high-strength alloy, and a soft metal coating.
    Type: Grant
    Filed: April 26, 2016
    Date of Patent: July 3, 2018
    Assignee: THE BOEING COMPANY
    Inventors: Russell J. Heeter, Thu A. Nguyen, John A. Ward, John R. Porter, Jeffrey A. Wilkerson
  • Publication number: 20170008268
    Abstract: A repair apparatus for an electrically conductive layer of a composite structure includes a dielectric layer, having a perimeter, secured to the composite structure, a first adhesive layer, and a conductive layer, secured over the dielectric layer and to the composite structure via the first adhesive layer around an entirety of the perimeter of the dielectric layer, the first adhesive layer being scored along a perimeter region thereof to improve a conductive path between the conductive layer and the composite structure.
    Type: Application
    Filed: September 22, 2016
    Publication date: January 12, 2017
    Inventors: Patrice K. Ackerman, Weston K. Anderson, Russell J. Heeter
  • Patent number: 9481157
    Abstract: A repair apparatus for an electrically conductive layer of a composite structure includes a dielectric layer, having a perimeter, secured to the structure, and a conductive layer, secured over the dielectric layer and to the structure around an entirety of the perimeter of the dielectric layer, the conductive layer being treated along a perimeter region thereof to improve a conductive path between the conductive layer and the structure.
    Type: Grant
    Filed: March 6, 2014
    Date of Patent: November 1, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Patrice K Ackerman, Weston K Anderson, Russell J Heeter
  • Publication number: 20160261052
    Abstract: A conductive fastener assembly, system, and method are described. The fastener assembly includes a nut having a counterbore formed therein. The counterbore is formed to maintain a sufficient gap between the nut and the protruding end of a fastener sleeve. The nut with the counterbore improves the conductive fastener system such that the need for a solid copper grid and a cap seal is reduced or eliminated.
    Type: Application
    Filed: May 16, 2016
    Publication date: September 8, 2016
    Inventors: Russell J. Heeter, Thu A. Nguyen, John A. Ward, John R. Porter, Jeffrey A. Wilkerson
  • Publication number: 20160240939
    Abstract: A conductive fastener assembly, system, and method, wherein the fastener assembly includes a fastener, a fastener sleeve, a nut, and a lubricant coating. The lubricant coating is deposited on a distal portion of a fastener shank and is omitted from the rest of the fastener. To overcome the stresses placed on the fastener sleeve by the insertion of the fastener shank largely devoid of a lubricant coating, the fastener sleeve is reinforced by one or more of an increased thickness, a high-strength alloy, and a soft metal coating.
    Type: Application
    Filed: April 26, 2016
    Publication date: August 18, 2016
    Inventors: Russell J. HEETER, Thu A. NGUYEN, John A. WARD, John R. PORTER, Jeffrey A. Wilkerson
  • Patent number: 9343824
    Abstract: The present disclosure describes a conductive fastener assembly, system, and method, wherein the fastener assembly comprises a nut having a counterbore formed therein. The counterbore is formed to maintain a sufficient gap between the nut and the protruding end of a fastener sleeve. The nut with the counterbore improves the conductive fastener system such that the need for a solid copper grid and a cap seal is reduced or eliminated.
    Type: Grant
    Filed: February 4, 2013
    Date of Patent: May 17, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Russell J Heeter, Thu A Nguyen, John A Ward, John R Porter, Jeffrey A Wilkerson
  • Patent number: 9331402
    Abstract: The present disclosure describes a conductive fastener assembly, system, and method, wherein the fastener assembly comprises a fastener, a fastener sleeve, a nut, and a lubricant coating. The lubricant coating is deposited on a distal portion of a fastener shank and is omitted from the rest of the fastener. To overcome the stresses placed on the fastener sleeve by the insertion of the fastener shank largely devoid of a lubricant coating, the fastener sleeve is reinforced by one or more of an increased thickness, a high-strength alloy, and a soft metal coating.
    Type: Grant
    Filed: February 4, 2013
    Date of Patent: May 3, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Russell J Heeter, Thu A Nguyen, John A Ward, John R Porter, Jeffrey A Wilkerson
  • Publication number: 20150251401
    Abstract: A repair apparatus for an electrically conductive layer of a composite structure includes a dielectric layer, having a perimeter, secured to the structure, and a conductive layer, secured over the dielectric layer and to the structure around an entirety of the perimeter of the dielectric layer, the conductive layer being treated along a perimeter region thereof to improve a conductive path between the conductive layer and the structure.
    Type: Application
    Filed: March 6, 2014
    Publication date: September 10, 2015
    Applicant: The Boeing Company
    Inventors: Patrice K. Ackerman, Weston K. Anderson, Russell J. Heeter
  • Publication number: 20150200517
    Abstract: A conductive sleeved fastener assembly includes an electrically-conductive fastener having a fastener head and a fastener shank extending from the fastener head and an electrically-conductive fastener sleeve receiving the fastener shank of the fastener and a fastener sleeve flange provided on the fastener sleeve and disposed in direct contact with the fastener head of the fastener. A method of preparing a conductive sleeved fastener for use is also disclosed.
    Type: Application
    Filed: March 24, 2015
    Publication date: July 16, 2015
    Inventors: Thu A. Nguyen, Michael G. Parent, Russell J. Heeter, Jeffrey A. Wilkerson
  • Patent number: 7969706
    Abstract: A lightning-protected conductive composite fuel tank includes a conductive material arrayed on an outer surface to at least partially cover a fastener centerline. Through holes extend along the fastener centerline through the conductive material and the underlying fuel tank shell. These through holes are countersunk into the fuel tank shell to a depth such that a fastener in a through hole will avoid electrical continuity or communication with the conductive material on the fuel tank outer surface. The gap in the countersunk through holes, between the fastener heads and the coextensive outer surface of the fuel tank, is filled with a dielectric or nonconductive material.
    Type: Grant
    Filed: October 5, 2009
    Date of Patent: June 28, 2011
    Assignee: The Boeing Company
    Inventors: Russell J. Heeter, Jeffrey D. Morgan, Kevin D. Pate, John R. Porter, Darrin M. Hansen, Steven C. Steckmyer, Thu A. Nguyen, Dale B. Winter, Daniel Smith, Harry E. Townsend
  • Patent number: 7898785
    Abstract: An apparatus comprises a wall, an internal structure, and a fastener. The wall has a conductive surface and a countersunk hole. The countersunk hole passes through the internal structure. The fastener has an interference fit within the countersunk hole.
    Type: Grant
    Filed: July 11, 2008
    Date of Patent: March 1, 2011
    Assignee: The Boeing Company
    Inventors: Dale B. Winter, Jeffrey D. Morgan, Steven C. Steckmyer, Kevin D. Pate, Darrin M. Hansen, John R. Porter, Jeffrey Sutton, Russell J. Heeter, James F. Huffaker
  • Publication number: 20100020461
    Abstract: A lightning-protected conductive composite fuel tank includes a conductive material arrayed on an outer surface to at least partially cover a fastener centerline. Through holes extend along the fastener centerline through the conductive material and the underlying fuel tank shell. These through holes are countersunk into the fuel tank shell to a depth such that a fastener in a through hole will avoid electrical continuity or communication with the conductive material on the fuel tank outer surface. The gap in the countersunk through holes, between the fastener heads and the coextensive outer surface of the fuel tank, is filled with a dielectric or nonconductive material.
    Type: Application
    Filed: October 5, 2009
    Publication date: January 28, 2010
    Applicant: THE BOEING COMPANY
    Inventors: Russell J. Heeter, Jeffrey D. Morgan, Kevin D. Pate, John R. Porter, Darrin M. Hansen, Steven C. Steckmyer, Thu A. Nguyen, Dale B. Winter, Daniel Smith, Harry E. Townsend
  • Patent number: 7599164
    Abstract: A lightning-protected conductive composite fuel tank includes a conductive material arrayed on an outer surface to at least partially cover a fastener centerline. Through holes extend along the fastener centerline through the conductive material and the underlying fuel tank shell. These through holes are countersunk into the fuel tank shell to a depth such that a fastener in a through hole will avoid electrical continuity or communication with the conductive material on the fuel tank outer surface. The gap in the countersunk through holes, between the fastener heads and the coextensive outer surface of the fuel tank, is filled with a dielectric or nonconductive material.
    Type: Grant
    Filed: December 7, 2006
    Date of Patent: October 6, 2009
    Assignee: The Boeing Company
    Inventors: Russell J. Heeter, Jeffrey D. Morgan, Kevin D. Pate, John R. Porter, Darrin M. Hansen, Steven C. Steckmyer, Thu A. Nguyen, Dale B. Winter, Daniel Smith, Harry E. Townsend
  • Patent number: 7576966
    Abstract: A system and method for preventing sparking or arcing within a fuel tank area is provided. The method includes installing an electrical bond between a fuel access door to a fuel tank skin; isolating the fuel access door and the fuel tank skin; and installing a fuel seal between the inner side of the fuel tank skin and the fuel access door.
    Type: Grant
    Filed: February 23, 2006
    Date of Patent: August 18, 2009
    Assignee: The Boeing Company
    Inventor: Russell J. Heeter
  • Patent number: 7561402
    Abstract: A method and system of preventing lighting from puncturing composite surfaces is provided. The method includes reconfiguring plies of a composite surface so that a composite conductive ply is located on the outer surface of the composite surface and a non-conductive composite ply is located directly underneath the conductive ply and inserting a flashover point between an outer edge of the conductive ply and a fastener attaching the composite surface to a support structure.
    Type: Grant
    Filed: February 24, 2006
    Date of Patent: July 14, 2009
    Assignee: The Boeing Company
    Inventor: Russell J. Heeter
  • Publication number: 20080297967
    Abstract: An apparatus comprises a wall, an internal structure, and a fastener. The wall has a conductive surface and a countersunk hole. The countersunk hole passes through the internal structure. The fastener has an interference fit within the countersunk hole.
    Type: Application
    Filed: July 11, 2008
    Publication date: December 4, 2008
    Inventors: Dale B. Winter, Jeffrey D. Morgan, Steven C. Steckmyer, Kevin D. Pate, Darrin M. Hansen, John R. Porter, Jeffrey Sutton, Russell J. Heeter, James F. Huffaker
  • Publication number: 20080137259
    Abstract: A lightning-protected conductive composite fuel tank includes a conductive material arrayed on an outer surface to at least partially cover a fastener centerline. Through holes extend along the fastener centerline through the conductive material and the underlying fuel tank shell. These through holes are countersunk into the fuel tank shell to a depth such that a fastener in a through hole will avoid electrical continuity or communication with the conductive material on the fuel tank outer surface. The gap in the countersunk through holes, between the fastener heads and the coextensive outer surface of the fuel tank, is filled with a dielectric or nonconductive material.
    Type: Application
    Filed: December 7, 2006
    Publication date: June 12, 2008
    Inventors: Russell J. Heeter, Jeffrey D. Morgan, Kevin D. Pate, John R. Porter, Darrin M. Hansen, Steven C. Steckmyer, Thu A. Nguyen, Dale B. Winter, Daniel Smith, Harry E. Townsend