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).

  • Patent number: 8372327
    Abstract: A composite fabrication apparatus which may include a first tooling die and a second tooling die movable with respect to each other; a temperature control system having induction coils disposed in thermal contact with the first tooling die and the second tooling die; a first die susceptor provided on the first tooling die and a second die susceptor provided on the second tooling die and connected to the induction coils; and a cooling system disposed in thermal contact with the first tooling die and the second tooling die. A resin transfer system delivers resin from a resin source to the tooling dies to allow resin transfer molding. A composite fabrication method is also disclosed.
    Type: Grant
    Filed: September 21, 2007
    Date of Patent: February 12, 2013
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Kim E. Peterson
  • Publication number: 20130034705
    Abstract: In an embodiment of the disclosure, there is provided a molybdenum composite hybrid laminate. The laminate has a plurality of composite material layers. The laminate further has a plurality of surface treated molybdenum foil layers interweaved between the composite material layers. The laminate further has a plurality of adhesive layers disposed between and bonding adjacent layers of the composite material layers and the molybdenum foil layers.
    Type: Application
    Filed: August 3, 2011
    Publication date: February 7, 2013
    Applicant: The Boeing Company
    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
  • 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
  • Patent number: 8330086
    Abstract: A heating blanket comprises a conductor for receiving current and generating a magnetic field in response to the current. The heating blanket may include a susceptor sleeve formed of magnetic material having a Curie temperature. The susceptor sleeve may extend along the conductor and may be inductively heated in response to the magnetic field.
    Type: Grant
    Filed: December 15, 2009
    Date of Patent: December 11, 2012
    Assignee: The Boeing Company
    Inventors: Robert J. Miller, David F. Taylor, Marc R. Matsen
  • Publication number: 20120291948
    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: Application
    Filed: May 17, 2011
    Publication date: November 22, 2012
    Inventors: Marc R. MATSEN, Mark A. NEGLEY, William Preston GEREN, Robert James MILLER
  • Publication number: 20120255947
    Abstract: A composite induction consolidation apparatus includes a base mandrel and a ferromagnetic base mandrel facesheet having a specific Curie temperature carried by the base mandrel. The base mandrel facesheet is adapted to support a composite part and allow ambient air pressure to compact the composite part against the base mandrel facesheet.
    Type: Application
    Filed: April 8, 2011
    Publication date: October 11, 2012
    Inventors: MARC R. MATSEN, Mark A. Negley
  • Publication number: 20120145702
    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: Application
    Filed: April 29, 2011
    Publication date: June 14, 2012
    Applicant: The Boeing Company
    Inventors: Robert J. Miller, David F. Taylor, Marc R. Matsen
  • Patent number: 8056800
    Abstract: Systems and methods for configuration management in an article of manufacture disclosed. In one embodiment, a system for documenting a configuration of an article of manufacture includes an identifier positioned on the article of manufacture. A local positioning system is used to determine a positional location of the identifier on the article of manufacture. A multifunction apparatus configured to interactively communicate with the identifier and the local positioning system is present that is operable to communicate configuration information to the identifier.
    Type: Grant
    Filed: June 30, 2005
    Date of Patent: November 15, 2011
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Brian K. Ramberg, Gloria J. Nickson, David B. Blackwell, Mahesh G. Seetharamu, Rajesh Doda, Everett Westerman, Karl L. Johnson
  • Publication number: 20110262575
    Abstract: A composite fabrication apparatus which may include a first tooling die and a second tooling die movable with respect to each other; a thermal control system having induction coils disposed in thermal contact with the first tooling die and the second tooling die; a first die susceptor provided on the first tooling die and a second die susceptor provided on the second tooling die and connected to the induction coils; and a cooling system disposed in thermal contact with the first tooling die and the second tooling die. A composite fabrication method is also disclosed.
    Type: Application
    Filed: July 6, 2011
    Publication date: October 27, 2011
    Applicant: THE BOEING COMPANY
    Inventors: Marc R. Matsen, Kim E. Peterson, William Dykstra
  • Publication number: 20110229720
    Abstract: A composite part layup is cured using a set of tools adapted to hold the layup and which include at least one tool face contacting the layup. Means are provided for heating the tool face to cure the part layup, and for selectively cooling sections of the tool face.
    Type: Application
    Filed: March 16, 2010
    Publication date: September 22, 2011
    Inventors: Marc R. Matsen, Mark A. Negley, Kim E. Peterson
  • Patent number: 8017059
    Abstract: A composite fabrication apparatus which may include a first tooling die and a second tooling die movable with respect to each other; a thermal control system having induction coils disposed in thermal contact with the first tooling die and the second tooling die; a first die susceptor provided on the first tooling die and a second die susceptor provided on the second tooling die and connected to the induction coils; and a cooling system disposed in thermal contact with the first tooling die and the second tooling die. A composite fabrication method is also disclosed.
    Type: Grant
    Filed: September 13, 2007
    Date of Patent: September 13, 2011
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Kim E. Peterson, William Dykstra
  • Publication number: 20110139769
    Abstract: A heating blanket comprises a conductor for receiving current and generating a magnetic field in response to the current. The heating blanket may include a susceptor sleeve formed of magnetic material having a Curie temperature. The susceptor sleeve may extend along the conductor and may be inductively heated in response to the magnetic field.
    Type: Application
    Filed: December 15, 2009
    Publication date: June 16, 2011
    Applicant: THE BOEING COMPANY
    Inventors: Robert J. Miller, David F. Taylor, Marc R. Matsen
  • 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
  • Patent number: 7705725
    Abstract: Methods and systems for structural and component health monitoring are provided. A system includes a plurality of sensor systems positioned about an object to be monitored and a processing system communicatively coupled to at least one of said plurality of sensor systems wherein the processing system includes an ontology and reasoning module configured to model the object to be monitored, reason about the received sensor data associated with the object to be monitored and reason about the relationships between the received sensor data to fuse the data into contextual information for the overall object to be monitored and a contextual analyzer configured to transmit the received sensor data to said ontology and reasoning module and to store the information into a contextual information database.
    Type: Grant
    Filed: January 8, 2007
    Date of Patent: April 27, 2010
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Gary E. Georgeson, Everett Westerman, Kenneth Porad, Arun Ayyagari, Kevin Ung, Craig Farris Battles, David Blackwell
  • Publication number: 20100065552
    Abstract: A method of fabricating a thermoplastic component using inductive heating is described. The method includes positioning a plurality of induction heating coils to define a process area for the thermoplastic component, wherein the plurality of induction heating coils comprises a first set of coils and a second set of coils. The method also includes controlling a supply of electricity provided to the plurality of inductive heating coils to intermittently activate the coils. The intermittent activation is configured to facilitate prevention of electromagnetic interference between adjacent coils.
    Type: Application
    Filed: September 15, 2008
    Publication date: March 18, 2010
    Inventors: Marc R. Matsen, Mark A. Negley
  • Publication number: 20100021578
    Abstract: There are provided an apparatus and an associated method for manufacturing superplastically formed structural assemblies from preforms. The apparatus includes first and second co-operable dies structured to define a die cavity therebetween for at least partially receiving the preform, at least one heater in thermal communication with the die cavity for heating the preform to a forming temperature, and at least one injector in fluid communication with the die cavity. The injector is structured for injecting pressurized gas into the die cavity to urge the preform against one of the dies to form the preform into the structural assembly. Further, at least one of the injectors is structured for injecting a quenchant into the die cavity to thereby heat treat the structural assembly while distortion of the structural assembly is being at least partially restrained by at least one of the dies.
    Type: Application
    Filed: October 1, 2009
    Publication date: January 28, 2010
    Applicant: The Boeing Company
    Inventors: Gary W. Coleman, John R. Fischer, Marc R. Matsen, Elizabeth M. Mull, David S. Nansen
  • 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: 7621437
    Abstract: A structural assembly and an associated system and method for manufacture are provided. The structural assembly includes an elongate member and a first connector member that is connected to an end of the elongate member by a braze joint. A second connector member can be connected to an end of the elongate member opposite the first connector by another braze joint. The elongate member is formed of a metal matrix composite material that includes a plurality of fibers of a reinforcement material disposed in a metal matrix. Each connector member is formed of a material that is dissimilar to the material of the elongate member. The braze joints can be formed by selectively heating the braze material, e.g., with an inductive coil that extends circumferentially around only a portion of the structural assembly.
    Type: Grant
    Filed: February 16, 2005
    Date of Patent: November 24, 2009
    Assignee: The Boeing Company
    Inventors: David S. Nansen, Marc R. Matsen, Terry L. Smith, William R. Herb, Ronald W. Brown, Lee C. Firth
  • Publication number: 20090074905
    Abstract: A composite fabrication apparatus which may include a first tooling die and a second tooling die movable with respect to each other; a temperature control system having induction coils disposed in thermal contact with the first tooling die and the second tooling die; a first die susceptor provided on the first tooling die and a second die susceptor provided on the second tooling die and connected to the induction coils; and a cooling system disposed in thermal contact with the first tooling die and the second tooling die. A resin transfer system delivers resin from a resin source to the tooling dies to allow resin transfer molding. A composite fabrication method is also disclosed.
    Type: Application
    Filed: September 21, 2007
    Publication date: March 19, 2009
    Inventors: Marc R. Matsen, Kim E. Peterson