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).
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Patent number: 10179940Abstract: 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: GrantFiled: November 16, 2015Date of Patent: January 15, 2019Assignee: The Boeing CompanyInventors: Brad L. Kirkwood, Marc R. Matsen, Tony Shen, Wesley B. Crow
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Publication number: 20160068922Abstract: 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: ApplicationFiled: November 16, 2015Publication date: March 10, 2016Inventors: Brad L. Kirkwood, Marc R. Matsen, Tony Shen, Wesley B. Crow
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Patent number: 9187818Abstract: 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: GrantFiled: February 11, 2009Date of Patent: November 17, 2015Assignee: THE BOEING COMPANYInventors: Brad L. Kirkwood, Marc R. Matsen, Tony Shen, Wesley B. Crow
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Patent number: 8918978Abstract: 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: GrantFiled: December 11, 2012Date of Patent: December 30, 2014Assignee: The Boeing CompanyInventors: Brad L Kirkwood, Lee C. Firth, Richard D. Widdle, Wesley B. Crow
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Patent number: 8388292Abstract: 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: GrantFiled: December 7, 2009Date of Patent: March 5, 2013Assignee: The Boeing CompanyInventors: Brad L. Kirkwood, Lee C. Firth, Richard D. Widdle, Wesley B. Crow
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Patent number: 8343402Abstract: 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: GrantFiled: November 24, 2009Date of Patent: January 1, 2013Assignee: The Boeing CompanyInventors: Marc R. Matsen, Wesley B. Crow, Brad L. Kirkwood
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Publication number: 20110135418Abstract: 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: ApplicationFiled: December 7, 2009Publication date: June 9, 2011Inventors: Brad L. Kirkwood, Lee C. Firth, Richard D. Widdle, Wesley B. Crow
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Patent number: 7905128Abstract: 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: GrantFiled: July 24, 2008Date of Patent: March 15, 2011Assignee: The Boeing CompanyInventors: Marc R. Matsen, Wesley B. Crow, Lee C. Firth
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Publication number: 20100200123Abstract: 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: ApplicationFiled: February 11, 2009Publication date: August 12, 2010Inventors: Brad L. Kirkwood, Marc R. Matsen, Tony Shen, Wesley B. Crow
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Publication number: 20100018271Abstract: 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: ApplicationFiled: July 24, 2008Publication date: January 28, 2010Applicant: The Boeing CompanyInventors: Marc R. Matsen, Wesley B. Crow, Lee C. Firth
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Patent number: 7109451Abstract: 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: GrantFiled: April 29, 2005Date of Patent: September 19, 2006Assignee: The Boeing CompanyInventors: Ronald W. Brown, Wesley B. Crow, Marc R. Matsen, Stephen G. Moore, David S. Nansen, Charles W. Newquist, Juris Verzemnieks
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Patent number: 6906300Abstract: 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: GrantFiled: August 13, 2003Date of Patent: June 14, 2005Assignee: The Boeing CompanyInventors: Ronald W. Brown, Marc R. Matsen, Wesley B. Crow, Stephen G. Moore, David S. Nansen, Charles W. Newquist, Juris Verzemnieks
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Patent number: 5587098Abstract: 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: GrantFiled: June 7, 1995Date of Patent: December 24, 1996Assignee: The Boeing CompanyInventors: Marc R. Matsen, Richard J. Poel, Wesley B. Crow, David S. Nansen