Patents by Inventor Harry E. Townsend

Harry E. Townsend 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: 8657274
    Abstract: A production system for manufacturing a workpiece comprises an index system including a plurality of index devices removably mounted on the workpiece at known longitudinally spaced locations therealong, and a longitudinally extending index member releasably engaged with at least two of the index devices such that a position and orientation of the index member are fixed relative to the workpiece by the index devices, the index member having position-indicating features distributed therealong. The production system further comprises a machine module mounted for longitudinal movement along the index member and operable to perform an operation, the machine module being operable to detect the position-indicating features on the index member and thereby determine a position of the machine module relative to the workpiece.
    Type: Grant
    Filed: July 16, 2010
    Date of Patent: February 25, 2014
    Assignee: The Boeing Company
    Inventors: Laurance N. Hazlehurst, Bobby C. Philpott, Jr., James N. Buttrick, Darrell D. Jones, Kostadinos D. Papanikolaou, David P. Banks, Terrence J. Rowe, Ronald Outous, Charles H. Glaisyer, Harry E. Townsend, Mark Boberg, Paul Elfes Nelson
  • 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
  • Publication number: 20100283195
    Abstract: A production system for manufacturing a workpiece comprises an index system including a plurality of index devices removably mounted on the workpiece at known longitudinally spaced locations therealong, and a longitudinally extending index member releasably engaged with at least two of the index devices such that a position and orientation of the index member are fixed relative to the workpiece by the index devices, the index member having position-indicating features distributed therealong. The production system further comprises a machine module mounted for longitudinal movement along the index member and operable to perform an operation, the machine module being operable to detect the position-indicating features on the index member and thereby determine a position of the machine module relative to the workpiece.
    Type: Application
    Filed: July 16, 2010
    Publication date: November 11, 2010
    Inventors: Laurance N. Hazlehurst, Bobby C. Philpott, JR., James N. Buttrick, Darrell D. Jones, Kostadinos D. Papanikolaou, David P. Banks, Terrence J. Rowe, Ronald Outous, Charles H. Glaisyer, Harry E. Townsend, Mark Boberg, Paul Elfes Nelson
  • Patent number: 7770477
    Abstract: A production system for manufacturing a workpiece comprises an index system including a plurality of index devices removably mounted on the workpiece at known longitudinally spaced locations therealong, and a longitudinally extending index member releasably engaged with at least two of the index devices such that a position and orientation of the index member are fixed relative to the workpiece by the index devices, the index member having position-indicating features distributed therealong. The production system further comprises a machine module mounted for longitudinal movement along the index member and operable to perform an operation, the machine module being operable to detect the position-indicating features on the index member and thereby determine a position of the machine module relative to the workpiece.
    Type: Grant
    Filed: February 11, 2009
    Date of Patent: August 10, 2010
    Assignee: The Boeing Company
    Inventors: Laurance N. Hazlehurst, Bobby C. Philpott, Jr., James N. Buttrick, Darrell D. Jones, Kostadinos D. Papanikolaou, David P. Banks, Terrence J. Rowe, Ronald Outous, Charles H. Glaisyer, Harry E. Townsend, Mark Boberg, Paul Elfes Nelson, John R. Porter
  • 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: 7574933
    Abstract: A production system for manufacturing a workpiece comprises an index system including a plurality of index devices removably mounted on the workpiece at known longitudinally spaced locations therealong, and a longitudinally extending index member releasably engaged with at least two of the index devices such that a position and orientation of the index member are fixed relative to the workpiece by the index devices, the index member having position-indicating features distributed therealong. The production system further comprises a machine module mounted for longitudinal movement along the index member and operable to perform an operation, the machine module being operable to detect the position-indicating features on the index member and thereby determine a position of the machine module relative to the workpiece.
    Type: Grant
    Filed: September 15, 2005
    Date of Patent: August 18, 2009
    Assignee: The Boeing Company
    Inventors: Laurance N. Hazlehurst, Bobby C. Philpott, Jr., James N. Buttrick, Darrell D. Jones, Kostadinos D. Papanikolaou, David P. Banks, Terrence J. Rowe, Ronald Outous, Charles H. Glaisyer, Harry E. Townsend, Mark Boberg, Paul Elfes Nelson, John R. Porter
  • Publication number: 20090140038
    Abstract: A production system for manufacturing a workpiece comprises an index system including a plurality of index devices removably mounted on the workpiece at known longitudinally spaced locations therealong, and a longitudinally extending index member releasably engaged with at least two of the index devices such that a position and orientation of the index member are fixed relative to the workpiece by the index devices, the index member having position-indicating features distributed therealong. The production system further comprises a machine module mounted for longitudinal movement along the index member and operable to perform an operation, the machine module being operable to detect the position-indicating features on the index member and thereby determine a position of the machine module relative to the workpiece.
    Type: Application
    Filed: February 11, 2009
    Publication date: June 4, 2009
    Applicant: The Boeing Company
    Inventors: Laurance N. Hazlehurst, Bobby C. Philpott, JR., James N. Buttrick, Darrell D. Jones, Kostadinos D. Papanikolaou, David P. Banks, Terrence J. Rowe, Ronald Outous, Charles H. Glaisyer, Harry E. Townsend, Mark Boberg, Paul Elfes Nelson, John R. Porter
  • 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
  • Patent number: 6979288
    Abstract: A production system for manufacturing a workpiece comprises an index system including a plurality of index devices removably mounted on the workpiece at known longitudinally spaced locations therealong, and a longitudinally extending index member releasably engaged with at least two of the index devices such that a position and orientation of the index member are fixed relative to the workpiece by the index devices, the index member having position-indicating features distributed therealong. The production system further comprises a machine module mounted for longitudinal movement along the index member and operable to perform an operation, the machine module being operable to detect the position-indicating features on the index member and thereby determine a position of the machine module relative to the workpiece.
    Type: Grant
    Filed: December 30, 2004
    Date of Patent: December 27, 2005
    Assignee: The Boeing Company
    Inventors: Laurance N. Hazlehurst, Bobby C. Philpott, Jr., James N. Buttrick, Darrell D. Jones, Kostadinos D. Papanikolaou, David P. Banks, Terrence J. Rowe, Ronald Outous, Charles H. Glaisyer, Harry E. Townsend, Mark Boberg, Paul Elfes Nelson, John R. Porter
  • Patent number: 6855099
    Abstract: A production system for manufacturing a workpiece comprises an index system including a plurality of index devices removably mounted on the workpiece at known longitudinally spaced locations therealong, and a longitudinally extending index member releasably engaged with at least two of the index devices such that a position and orientation of the index member are fixed relative to the workpiece by the index devices, the index member having position-indicating features distributed therealong. The production system further comprises a machine module mounted for longitudinal movement along the index member and operable to perform an operation, the machine module being operable to detect the position-indicating features on the index member and thereby determine a position of the machine module relative to the workpiece.
    Type: Grant
    Filed: October 31, 2001
    Date of Patent: February 15, 2005
    Assignee: The Boeing Company
    Inventors: Laurance N. Hazlehurst, Bobby C. Philpott, Jr., James N. Buttrick, Darrell D. Jones, Kostadinos D. Papanikolaou, David P. Banks, Terrence J. Rowe, Ronald Outous, Charles H. Glaisyer, Harry E. Townsend, Mark Boberg, Paul Elfes Nelson, John R. Porter
  • Patent number: 6779272
    Abstract: A method for assembling wings includes supporting a pair of wing spars, which include a plurality of coordination features, upon a pair of stanchions in a generally horizontal position. A plurality of ribs and wing panels are accurately fastened to the pair of wing spars at a first workstation using the coordination features to position accurately the parts. The combination is transferred to downstream workstations via a ground transport vehicle for further processing and assembly to define a pulsed flow wing assembly system.
    Type: Grant
    Filed: August 30, 2002
    Date of Patent: August 24, 2004
    Assignee: The Boeing Company
    Inventors: Dan D. Day, Clayton L. Munk, Luis A. Perla, Harry E. Townsend
  • Publication number: 20040040154
    Abstract: A method for assembling wings includes supporting a pair of wing spars, which include a plurality of coordination features, upon a pair of stanchions in a generally horizontal position. A plurality of ribs and wing panels are accurately fastened to the pair of wing spars at a first workstation using the coordination features to position accurately the parts. The combination is transferred to downstream workstations via a ground transport vehicle for further processing and assembly to define a pulsed flow wing assembly system.
    Type: Application
    Filed: August 30, 2002
    Publication date: March 4, 2004
    Inventors: Dan D. Day, Clayton L. Munk, Luis A. Perla, Harry E. Townsend
  • Publication number: 20030207742
    Abstract: A production system for manufacturing a workpiece comprises an index system including a plurality of index devices removably mounted on the workpiece at known longitudinally spaced locations therealong, and a longitudinally extending index member releasably engaged with at least two of the index devices such that a position and orientation of the index member are fixed relative to the workpiece by the index devices, the index member having position-indicating features distributed therealong. The production system further comprises a machine module mounted for longitudinal movement along the index member and operable to perform an operation, the machine module being operable to detect the position-indicating features on the index member and thereby determine a position of the machine module relative to the workpiece.
    Type: Application
    Filed: October 31, 2001
    Publication date: November 6, 2003
    Applicant: The Boeing Company
    Inventors: Laurance N. Hazlehurst, Bobby C. Philpott, James N. Buttrick, Darrell D. Jones, Kostadinos D. Papanikolaou, David P. Banks, Terrence J. Rowe, Ronald Outous, Charles H. Glaisyer, Harry E. Townsend, Mark Boberg, Paul Elfes Nelson, John R. Porter
  • Patent number: 4951849
    Abstract: An applicator for applying a fluid substance to a drilled hole as part of an automatic fastening machine. The fastener machine drills the hole in the workpiece, such as an aircraft wing panel, and then the substance applicator applies the substance to the hole, prior to subsequent installation of the fastener within the hole. The substance applicator, which is connected to a movable pressure foot, is pneumatically operated so that a head portion of the applicator is extended laterally over the hole, and a tip assembly in the head is extended vertically downward toward the hole. This operational sequence is accomplished by means of variable rate springs which bias the tip assembly and base to retracted positions. The substance is delivered to the tip assembly from a storage reservoir by means of a peristaltic pump. Positive shutoff of the substance to the tip assembly is achieved by a pivotally mounted shutoff arm assembly.
    Type: Grant
    Filed: September 30, 1988
    Date of Patent: August 28, 1990
    Assignee: The Boeing Company
    Inventors: Harry E. Townsend, Paul J. Shemeta, Avinoam Zafir