Patents by Inventor Wesley B. Crow

Wesley B. Crow 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: 10179940
    Abstract: A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.
    Type: Grant
    Filed: November 16, 2015
    Date of Patent: January 15, 2019
    Assignee: The Boeing Company
    Inventors: Brad L. Kirkwood, Marc R. Matsen, Tony Shen, Wesley B. Crow
  • Publication number: 20160068922
    Abstract: A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.
    Type: Application
    Filed: November 16, 2015
    Publication date: March 10, 2016
    Inventors: Brad L. Kirkwood, Marc R. Matsen, Tony Shen, Wesley B. Crow
  • Patent number: 9187818
    Abstract: A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.
    Type: Grant
    Filed: February 11, 2009
    Date of Patent: November 17, 2015
    Assignee: THE BOEING COMPANY
    Inventors: Brad L. Kirkwood, Marc R. Matsen, Tony Shen, Wesley B. Crow
  • Patent number: 8918978
    Abstract: A method to join a first structure to a second structure comprises aligning a first hole in the first structure with a second hole in the second structure and inserting a fastener into the first hole and the second hole. The fastener comprises a shape memory alloy which was formed into a first shape having a diameter slightly larger than a diameter of the first hole and the second hole when the shape memory alloy was in an austenite state and reduced to a second shape having a diameter less than the diameter of the first hole and the second hole when the shape memory alloy was in a martensite state. The method further comprises heating the fastener above an austenite start transition temperature.
    Type: Grant
    Filed: December 11, 2012
    Date of Patent: December 30, 2014
    Assignee: The Boeing Company
    Inventors: Brad L Kirkwood, Lee C. Firth, Richard D. Widdle, Wesley B. Crow
  • Patent number: 8388292
    Abstract: In one embodiment a method to join a first structure to a second structure, comprises aligning a first hole in the first structure with a second hole in the second structure and inserting a fastener into the first hole and the second hole. The fastener comprises a shape memory alloy which was formed into a first shape having a diameter slightly larger than a diameter of the first hole and the second hole when the shape memory alloy was in an austenite state and reduced to a second shape having a diameter less than the diameter of the first hole and the second hole when the shape memory alloy was in a martensite state.
    Type: Grant
    Filed: December 7, 2009
    Date of Patent: March 5, 2013
    Assignee: The Boeing Company
    Inventors: Brad L. Kirkwood, Lee C. Firth, Richard D. Widdle, Wesley B. Crow
  • Patent number: 8343402
    Abstract: In one embodiment method to form a composite part from a metallic composite powder, comprises positioning a metallic composite powder preform in a mold cavity formed by a first susceptor and a second susceptor, heating the mold cavity to a first processing temperature, applying a pressure to the mold cavity, and applying a thermal oscillation cycle to the mold cavity, wherein the thermal oscillation cycle oscillates the temperature of the mold cavity between a first temperature in which the metallic composite powder is in a first phase and a second temperature in which the metallic composite powder is in a second phase, different from the first phase.
    Type: Grant
    Filed: November 24, 2009
    Date of Patent: January 1, 2013
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Wesley B. Crow, Brad L. Kirkwood
  • Publication number: 20110135418
    Abstract: In one embodiment a method to join a first structure to a second structure, comprises aligning a first hole in the first structure with a second hole in the second structure and inserting a fastener into the first hole and the second hole. The fastener comprises a shape memory alloy which was formed into a first shape having a diameter slightly larger than a diameter of the first hole and the second hole when the shape memory alloy was in an austenite state and reduced to a second shape having a diameter less than the diameter of the first hole and the second hole when the shape memory alloy was in a martensite state.
    Type: Application
    Filed: December 7, 2009
    Publication date: June 9, 2011
    Inventors: Brad L. Kirkwood, Lee C. Firth, Richard D. Widdle, Wesley B. Crow
  • Patent number: 7905128
    Abstract: A method and apparatus for forming a workpiece having a desired configuration as well as an associated preform assembly are provided. The forming method and apparatus as well as the preform assembly include a hydrostatic pressing medium, such as a layer of glass, disposed within the die cavity proximate to at least one side of the workpiece. The hydrostatic pressing medium is configured to have a relatively low viscosity at the temperatures at which the workpiece is processed, thereby facilitating the relatively even application of pressure to the workpiece. As such, a workpiece having a complex configuration may be formed utilizing a single acting die.
    Type: Grant
    Filed: July 24, 2008
    Date of Patent: March 15, 2011
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Wesley B. Crow, Lee C. Firth
  • Publication number: 20100200123
    Abstract: A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.
    Type: Application
    Filed: February 11, 2009
    Publication date: August 12, 2010
    Inventors: Brad L. Kirkwood, Marc R. Matsen, Tony Shen, Wesley B. Crow
  • Publication number: 20100018271
    Abstract: A method and apparatus for forming a workpiece having a desired configuration as well as an associated preform assembly are provided. The forming method and apparatus as well as the preform assembly include a hydrostatic pressing medium, such as a layer of glass, disposed within the die cavity proximate to at least one side of the workpiece. The hydrostatic pressing medium is configured to have a relatively low viscosity at the temperatures at which the workpiece is processed, thereby facilitating the relatively even application of pressure to the workpiece. As such, a workpiece having a complex configuration may be formed utilizing a single acting die.
    Type: Application
    Filed: July 24, 2008
    Publication date: January 28, 2010
    Applicant: The Boeing Company
    Inventors: Marc R. Matsen, Wesley B. Crow, Lee C. Firth
  • Patent number: 7109451
    Abstract: An apparatus and method for consolidating a composite workpiece are provided. The apparatus includes an electromagnetic field generator for inducing a current and thereby heating a susceptor in thermal communication with the workpiece. The workpiece is supported by one or more support tools, each of which transmits the electromagnetic field so that the support tools are not substantially heated by the electromagnetic field. Thus, the time and energy required for heating the workpiece are reduced relative to conventional consolidation techniques.
    Type: Grant
    Filed: April 29, 2005
    Date of Patent: September 19, 2006
    Assignee: The Boeing Company
    Inventors: Ronald W. Brown, Wesley B. Crow, Marc R. Matsen, Stephen G. Moore, David S. Nansen, Charles W. Newquist, Juris Verzemnieks
  • Patent number: 6906300
    Abstract: An apparatus and method for consolidating a composite workpiece are provided. The apparatus includes an electromagnetic field generator for inducing a current and thereby heating a susceptor in thermal communication with the workpiece. The workpiece is supported by one or more support tools, each of which transmits the electromagnetic field so that the support tools are not substantially heated by the electromagnetic field. Thus, the time and energy required for heating the workpiece are reduced relative to conventional consolidation techniques.
    Type: Grant
    Filed: August 13, 2003
    Date of Patent: June 14, 2005
    Assignee: The Boeing Company
    Inventors: Ronald W. Brown, Marc R. Matsen, Wesley B. Crow, Stephen G. Moore, David S. Nansen, Charles W. Newquist, Juris Verzemnieks
  • Patent number: 5587098
    Abstract: A narrow susceptor is incorporated into the die in the vicinity of a bondline between two or more parts in an induction heating workcell. When the induction coil of the workcell is energized, the susceptor heats and preferentially heats the parts near the bondline. The preferential heating is localized at the bondline and reduces energy losses otherwise expended to heat large thermal masses in the workcell or to heat the entire parts.
    Type: Grant
    Filed: June 7, 1995
    Date of Patent: December 24, 1996
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Richard J. Poel, Wesley B. Crow, David S. Nansen