Patents by Inventor Marc R. Matsen

Marc R. Matsen 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).

  • Publication number: 20170144337
    Abstract: Provided are induction heating cells including pressure bladders used for supporting dies and methods of using these induction heating cells. A pressure bladder may be disposed between a die and a bolster of the cell. Even when the bolster is deformed during operation of the cell, the pressure bladder continues to provide uniform support to the die thereby preserving integrity of the die and prevents its cracking or braking. As such, the cell may be operated at a higher processing pressure inside the cavity formed by the die without further strengthening the bolster. The bolster is allowed to deform without compromising the integrity of the die. The deformation of the bolster is compensated by the shape change of the pressure bladder. The number and/or position of the bladders in the cell may depend on the shape of processed parts.
    Type: Application
    Filed: November 19, 2015
    Publication date: May 25, 2017
    Applicant: The Boeing Company
    Inventors: Marc R. Matsen, David S. Nansen, Lee C. Firth, Carey E. Wilkinson, Gregory J. Hickman, William C. Dykstra
  • Patent number: 9635714
    Abstract: An induction heating system for manufacturing a part including an induction coil and a smart susceptor positioned within an oscillating electromagnetic field from the induction coil. The smart susceptor includes a ferromagnetic material cold sprayed onto a tool. The tool may be a sheet metal component formed to a desired shape by incremental sheet forming. The smart susceptor may be heated up by eddy currents generated in the ferromagnetic material by the oscillating electromagnetic field. The smart susceptor may be designed to have a desired Curie temperature based on the composition of the ferromagnetic material. The smart susceptor is formed into a desired shape by cold spraying ferromagnetic material onto a tool already formed into the desired shape. The smart susceptor may be removed from the tool by thermally shocking the smart susceptor and the tool and may be used to heat a part to be formed.
    Type: Grant
    Filed: May 6, 2013
    Date of Patent: April 25, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Marc R. Matsen, Carey E. Wilkinson
  • Patent number: 9635715
    Abstract: A radiant heater having a ferromagnetic element includes a high emissivity surface and an induction coil operatively coupled with the ferromagnetic element. The induction coil may be energized to create eddy currents heating the ferromagnetic element until the element reaches its Curie temperature. At the Curie temperature the ferromagnetic element becomes substantially nonmagnetic and the temperature of the element remains relatively constant. The high emissivity surface of the heater provides a substantially uniform radiant heat to an object in close proximity to the high emissivity surface. The object may be thermally coupled with the high emissivity surface of the radiant heater. The radiant heater having a high emissivity surface may be used to heat temperature sensitive objects such as thin films. Multiple radiant heaters having different Curie temperatures may be used to ramp up a temperature, ramp down a temperature, or provide different temperatures required during a process.
    Type: Grant
    Filed: May 8, 2013
    Date of Patent: April 25, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Robert James Miller, Marc R. Matsen, Diane C. Rawlings
  • Patent number: 9586362
    Abstract: A thermoplastic welding apparatus includes a thermoplastic welding tool, at least one tooling surface in the thermoplastic welding tool, a magnetic induction coil in the thermoplastic welding tool and generally encircling the at least one tooling surface and at least one smart susceptor in the thermoplastic welding tool at the at least one tooling surface. The magnetic induction coil is adapted to generate a magnetic flux field oriented generally parallel to a plane of the at least one smart susceptor.
    Type: Grant
    Filed: May 17, 2011
    Date of Patent: March 7, 2017
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Mark A. Negley, William Preston Geren, Robert James Miller
  • Publication number: 20170050229
    Abstract: An apparatus for forming a panel, including a first face sheet, a second face sheet and a core sheet between the first face sheet and the second face sheet, may include a molding tool defining a forming cavity shaped to correspond to the panel, a heating system positioned adjacent to the forming cavity and configured to heat the forming cavity, and a pressurization system configured to pressurize a cavity volume between the tool and the panel and pressurize a panel volume between the first face sheet and the second face sheet.
    Type: Application
    Filed: August 17, 2015
    Publication date: February 23, 2017
    Inventors: Marc R. Matsen, David S. Nansen, Lee C. Firth, Gregory A. Foltz
  • Publication number: 20170036310
    Abstract: Described herein is a method of forming tooling used to form a material. The method includes positioning a first susceptor made from a first susceptor material between first and second dies. At least one of the first and second dies includes a forming surface having a desired shape. The method further includes positioning a second susceptor made from a second susceptor material between the first and second dies such that the first susceptor is interposed between the second susceptor and the forming surface. Additionally, the method includes positioning a first bladder between the first and second dies such that the second susceptor is interposed between the first bladder and the first susceptor. Also, the method includes inflating the first bladder to concurrently deform the first susceptor and second susceptor into the desired shape.
    Type: Application
    Filed: August 5, 2015
    Publication date: February 9, 2017
    Inventors: Marc R. Matsen, Gregory J.S. Hickman, William C. Dykstra
  • Publication number: 20170019956
    Abstract: The disclosed induction heating systems include an induction heating-resistant support beam, one or more legs, and an induction coil. The support beam includes a plurality of metal sheets and a plurality of electrically insulating layers interspersed among the metal sheets. Each metal sheet has a thickness that is sized to substantially cancel eddy currents induced in the metal sheet by an alternating magnetic field that may be generated by the induction coil. The support beam and leg(s) are configured to support a workpiece in an induction heating volume defined by the induction coil. The induction coil is configured to generate the alternating magnetic field within the induction heating volume sufficient to heat the workpiece. Methods of induction heating include placing a workpiece, such as a die, within an induction heating volume, supporting the workpiece within the induction heating volume with an induction-heating resistant support beam, and inductively heating the workpiece.
    Type: Application
    Filed: July 16, 2015
    Publication date: January 19, 2017
    Applicant: The Boeing Company
    Inventors: Cameron K. Chen, Marc R. Matsen
  • Patent number: 9517594
    Abstract: A composite structure may include a laminate and a stabilizing element. The laminate may have a plurality of composite plies. The composite structure may include a geometric discontinuity that may be associated with the laminate. The stabilizing element may be included with the composite plies and may be located proximate the geometric discontinuity.
    Type: Grant
    Filed: October 4, 2012
    Date of Patent: December 13, 2016
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Mark A. Negley
  • Patent number: 9510398
    Abstract: Induction heating apparatus are disclosed herein. An example induction heating apparatus disclosed herein includes a housing and a susceptor wire positioned in the housing. The susceptor wire is composed of a material having a relatively high magnetic permeability and a relatively high electrical resistivity sufficient to induce an eddy current in the susceptor wire when a magnetic field is applied to the susceptor wire via an induction source. The magnetic field generates the eddy current in the susceptor wire when a temperature of the susceptor wire is below a Curie point of the material of the susceptor wire. The susceptor wire limits heating to a temperature that is equal to or less than a Curie temperature associated with the material of the susceptor wire.
    Type: Grant
    Filed: October 29, 2012
    Date of Patent: November 29, 2016
    Assignee: The Boeing Company
    Inventors: Robert James Miller, Marc R. Matsen
  • Publication number: 20160339647
    Abstract: A fiber placement system including a fiber placement station at a first location, the fiber placement station including a tool and a fiber placement assembly configured to construct a reinforcement layup on the tool, the first fiber placement assembly including a compaction roller rotatable about an axis of rotation, the compaction roller at least partially defining a nip, a thermoplastic composite ply extending through the nip and a heating unit positioned to heat the thermoplastic composite ply proximate the nip, and a consolidation station at a consolidation location, the consolidation location being different from the first location, the consolidation station including a consolidation tool and a consolidation system configured to consolidate a reinforcement layup assembly that includes the reinforcement layup.
    Type: Application
    Filed: May 21, 2015
    Publication date: November 24, 2016
    Inventors: Marc R. Matsen, Mark A. Negley, Jeffery L. Marcoe, Stephen G. Moore, Brice A. Johnson, Alexandra K. Dillon, Megan M. Petersen
  • Publication number: 20160344152
    Abstract: Methods and systems for the uniform induction heating of forming dies, where the forming die may be heated by an induction coil in conjunction with a pair of electromagnetic (EM) field stabilizers, each EM field stabilizer configured to be adjacent one end of the forming die while the forming die is within the induction heating coil.
    Type: Application
    Filed: May 22, 2015
    Publication date: November 24, 2016
    Applicant: THE BOEING COMPANY
    Inventors: Cameron Kai-Ming Chen, Marc R. Matsen, Robert James Miller, Scott David Billings
  • Publication number: 20160316522
    Abstract: Described herein is a method of forming a heat-treated material includes positioning the heat-treated material between first and second susceptors. Each of the first and second susceptors includes a tool face shaped according to a desired shape of the heat-treated material. The method also includes applying a low-strength magnetic field to the first and second susceptors to heat the first and second susceptors. Further, the method includes compressing the heat-treated material between the first and second susceptors to form the heat-treated material into the desired shape. The method additionally includes applying a high-strength magnetic field to the heat-treated material before compressing the heat-treated material between the first and second susceptors.
    Type: Application
    Filed: April 27, 2015
    Publication date: October 27, 2016
    Inventors: Marc R. Matsen, Mark A. Negley
  • Patent number: 9463879
    Abstract: A system and method for operating an ice detection and deicing system are provided herein. The ice detection and deicing system may use changing magnetic properties of various components caused by temperature changes to detect conditions conducive to, or indicating, ice formation. The ice detection and deicing system may further use eddy currents induced in one or more layers of the system to increase the temperature of the one or more layers to reduce the amount of ice formation or reduce the probability of ice being formed.
    Type: Grant
    Filed: March 3, 2014
    Date of Patent: October 11, 2016
    Assignee: The Boeing Company
    Inventors: Vyacheslav Khozikov, Robert J. Miller, Rangasamy Elangovan, Marc R. Matsen, Stephen R. Amorosi, Robert G. Albers, Michael Strasik, John R. Hull
  • Patent number: 9457404
    Abstract: A method for consolidating a pre-form made of powder, comprising: (a) placing the pre-form between smart susceptors; (b) heating the smart susceptors to a leveling temperature by applying a varying low-strength magnetic field having a magnetic flux that passes through surfaces of the smart susceptors; (c) applying consolidation pressure to the pre-form at least during a time period subsequent to the temperature of the smart susceptors reaching the leveling temperature; and (d) while consolidation pressure is being applied, applying a pulsed high-strength magnetic field having a magnetic flux that passes through a surface of the pre-form. The strength and pulse rate of the high-strength magnetic field are selected so that the crystallographic phase of the pre-form will rapidly oscillate at a substantially constant temperature. The pulsed high-strength magnetic field is applied sufficiently long that superplasticity of the pre-form is attained during phase oscillation.
    Type: Grant
    Filed: February 4, 2013
    Date of Patent: October 4, 2016
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Mark Alan Negley, Robert James Miller
  • Publication number: 20160107236
    Abstract: One aspect of the disclosure relates to a method of making a part from at least one elemental metal powder. The part has a near-net shape, a part volume, and a part density. The method includes providing a sintered preform having a sintered density and separating a portion from the sintered preform. The portion has a portion volume exceeding the part volume and a portion shape different from the near-net shape of the part. The method also includes thermally cycling the portion for a thermal-cycling time period at a thermal-cycling pressure while superplastically deforming the portion to form the part having the near net shape and the part density.
    Type: Application
    Filed: February 10, 2014
    Publication date: April 21, 2016
    Applicant: The Boeing Company
    Inventors: Marc R. Matsen, Matthew Douglas Carter, Carey Eugene Wilkinson, Lee C. Firth
  • Patent number: 9314975
    Abstract: A method for fabricating a thermoplastic composite component comprises inductively heating a thermoplastic pre-form with a first induction coil by inducing current to flow in susceptor wires disposed throughout the pre-form, inductively heating smart susceptors in a molding tool to a leveling temperature with a second induction coil by applying a high-strength magnetic field having a magnetic flux that passes through surfaces of the smart susceptors, shaping the magnetic flux that passes through surfaces of the smart susceptors to flow substantially parallel to a molding surface of the smart susceptors, placing the heated pre-form between the heated smart susceptors; and applying molding pressure to the pre-form to form the composite component.
    Type: Grant
    Filed: April 25, 2013
    Date of Patent: April 19, 2016
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Mark A. Negley, William C. Dykstra, Glen L. Smith, Robert J. Miller
  • 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: 9174398
    Abstract: A heating blanket may include a conductor for receiving electrical current and generating a magnetic field in response to the electrical current. A plurality of sleeve segments may be mounted on the conductor in end-to-end relation to one another. Each one of the sleeve segments may be formed of magnetic material having a Curie temperature. The sleeve segments may be inductively heated in response to the magnetic field.
    Type: Grant
    Filed: April 29, 2011
    Date of Patent: November 3, 2015
    Assignee: The Boeing Company
    Inventors: Robert J. Miller, David F. Taylor, Marc R. Matsen
  • Publication number: 20150306859
    Abstract: A method of forming a molybdenum composite hybrid laminate is disclosed. The method includes treating a surface of each of a plurality of molybdenum foil layers. The method further includes interweaving the surface treated molybdenum foil layers with a plurality of composite material layers. The method further includes bonding with an adhesive layer each of the surface treated molybdenum foil layers to adjacent composite material layers to form a molybdenum composite hybrid laminate having improved yield strength.
    Type: Application
    Filed: July 9, 2015
    Publication date: October 29, 2015
    Inventors: Marc R. Matsen, Mark A. Negley, Marc J. Piehl, Kay Y. Blohowiak, Alan E. Landmann, Richard H. Bossi, Robert L. Carlsen, Gregory Alan Foltz, Geoffrey A. Butler, Liam S. Cavanaugh Pingree, Stephen G. Moore, John Mark Gardner, Robert A. Anderson