Patents by Inventor Michael P. Matlack

Michael P. Matlack 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: 20240416413
    Abstract: A method for manufacturing a tool having one or more internal channels includes forming one or more channel cores by additive manufacturing, coating a metal onto the one or more channel cores to form a metal tube on each of the one or more channel cores, positioning the one or more metal tubes into a casting mold having a shape of a tool, and casting a molten metal into the casting mold to form the tool having the one or more internal channels corresponding to the one or more channel cores.
    Type: Application
    Filed: August 28, 2024
    Publication date: December 19, 2024
    Applicant: The Boeing Company
    Inventors: Michael A. Johnson, Michael P. Matlack, Daniel J. Smolinsky
  • Publication number: 20240375361
    Abstract: A tooling set for stamp forming a workpiece includes a first stamping tool, a second stamping tool and an elastomeric layer between the first and second stamping tools. The first stamping tool defines a first forming face. The second stamping tool defines a second forming face. The elastomeric layer defines first and second compliant stamping surfaces. A method for stamp forming a workpiece includes positioning a workpiece between the first stamping tool and the elastomeric layer and compressing the workpiece between the first forming face and the first compliant stamping surface in response to the first and second stamping tools being approximated. A system for stamp forming a workpiece includes the tooling set.
    Type: Application
    Filed: May 10, 2023
    Publication date: November 14, 2024
    Applicant: The Boeing Company
    Inventors: Michael P. Matlack, Gregory J. Hickman, Evan Lloyd, Emma L. Morrissey, Andrew Gutknecht
  • Publication number: 20240342974
    Abstract: A compliant stamping tool for stamp forming a workpiece includes a support structure, a fluid and a deformable membrane. The support structure includes a support wall spaced from a stamping axis. The support wall defines a chamber with an opening. The fluid is disposed within the chamber. The deformable membrane is secured to the support wall, covers the opening and seals the fluid within the chamber. The deformable membrane defines a compliant stamping surface configured to oppose different non-compliant stamping surfaces of opposing stamping tools. A system for stamp forming a workpiece includes a first stamping tool and the compliant stamping tool. The first stamping tool defines a first non-compliant stamping surface extending from the stamping axis. A method for stamp forming a workpiece is also provided.
    Type: Application
    Filed: April 12, 2023
    Publication date: October 17, 2024
    Applicant: The Boeing Company
    Inventors: Gregory J. Hickman, Michael P. Matlack, Emma L. Morrissey, Evan Lloyd, Andrew Gutknecht
  • Publication number: 20240253276
    Abstract: Tooling for stamp forming a workpiece includes a first tool, a second tool, and an elastic boundary. The second tool includes an elastomeric member. The first tool has a thickness along a stamping axis and defines a first stamping surface extending from the stamping axis. The elastomeric member having a thickness along the stamping axis and defining a second stamping surface axially opposing the first stamping surface. The elastomeric member defines a periphery spaced from the stamping axis. The elastic boundary disposed proximate to at least a portion of the periphery of the elastomeric member.
    Type: Application
    Filed: February 1, 2023
    Publication date: August 1, 2024
    Applicant: The Boeing Company
    Inventors: Michael P. Matlack, Gregory J. Hickman, Evan Lloyd, Andrew Gutknecht, Emma L. Morrissey
  • Publication number: 20240091849
    Abstract: A method for manufacturing a tool having one or more internal channels includes forming one or more channel cores by additive manufacturing, coating a metal onto the one or more channel cores to form a metal tube on each of the one or more channel cores, positioning the one or more metal tubes into a casting mold having a shape of a tool, and casting a molten metal into the casting mold to form the tool having the one or more internal channels corresponding to the one or more channel cores.
    Type: Application
    Filed: September 21, 2022
    Publication date: March 21, 2024
    Applicant: The Boeing Company
    Inventors: Michael A. Johnson, Michael P. Matlack, Daniel J. Smolinsky
  • Patent number: 11840025
    Abstract: A thermoplastic welding assembly and method for joining a plurality of thermoplastic support components to a thermoplastic component is provided. The thermoplastic welding assembly includes a frame, a plurality of heat sinks, and a plurality of individually actuatable pressurizers. The frame includes a plurality of welding slots. Each heat sink of the plurality of heat sinks is positioned within one of the welding slots. Each pressurizer of the plurality of individually actuatable pressurizers includes an alignment actuator configured to move one thermoplastic support component into alignment with one welding slot, and a clamping actuator configured to move the one thermoplastic support component into contact with the thermoplastic component. In some implementations, the thermoplastic welding assembly further includes a plurality of actuators configured to move the alignment actuator and the clamping actuator.
    Type: Grant
    Filed: September 30, 2021
    Date of Patent: December 12, 2023
    Assignee: The Boeing Company
    Inventors: Francis J. Samalot, Michael P. Matlack
  • Publication number: 20230095229
    Abstract: A thermoplastic welding assembly and method for joining a plurality of thermoplastic support components to a thermoplastic component is provided. The thermoplastic welding assembly includes a frame, a plurality of heat sinks, and a plurality of individually actuatable pressurizers. The frame includes a plurality of welding slots. Each heat sink of the plurality of heat sinks is positioned within one of the welding slots. Each pressurizer of the plurality of individually actuatable pressurizers includes an alignment actuator configured to move one thermoplastic support component into alignment with one welding slot, and a clamping actuator configured to move the one thermoplastic support component into contact with the thermoplastic component. In some implementations, the thermoplastic welding assembly further includes a plurality of actuators configured to move the alignment actuator and the clamping actuator.
    Type: Application
    Filed: September 30, 2021
    Publication date: March 30, 2023
    Inventors: Francis J. Samalot, Michael P. Matlack
  • Patent number: 11529771
    Abstract: A method of heating a tool assembly includes the step of joining a first piece of the tool assembly with a second piece of the tool assembly via a first joint portion and a second joint portion. The method further includes the step of inserting a fastener through the first joint portion and the second joint portion of the tool assembly. The method further includes the step of applying heat to the tool assembly, wherein upon heating, interlock surfaces of the first joint portion and the second joint portion tighten against each other.
    Type: Grant
    Filed: December 28, 2020
    Date of Patent: December 20, 2022
    Assignee: THE BOEING COMPANY
    Inventors: Michael P. Matlack, Dylan E. Polus
  • Publication number: 20220363013
    Abstract: A thermoplastic welding assembly includes a structural cage that supports a press and one or more hydraulic and pneumatic actuators. The press includes first and second plates that movable toward and away from each other to load and remove thermoplastic components to be held together for thermoplastic welding. Specifically, the first plate of the press includes non-conductive tooling inserts that are positioned to form a slot for a welding prove, and the second plates includes non-conductive tooling inserts that form cavities for plungers to move through. Plungers that are movable using the actuators are positioned in the cavities of the second plate, and compressible pressurizers are attached to the ends of the plungers. An operator uses electrical controls to move the plungers in the plunger cavities toward the thermoplastic components in the press to drive the pressurizers into the thermoplastic components and provide stabilizing pressure on the components during welding.
    Type: Application
    Filed: May 10, 2022
    Publication date: November 17, 2022
    Inventors: Michael P. Matlack, Mark A. Monzyk, Katharine Anne Bartlett, Francis J. Samalot
  • Publication number: 20210114317
    Abstract: A method of heating a tool assembly includes the step of joining a first piece of the tool assembly with a second piece of the tool assembly via a first joint portion and a second joint portion. The method further includes the step of inserting a fastener through the first joint portion and the second joint portion of the tool assembly. The method further includes the step of applying heat to the tool assembly, wherein upon heating, interlock surfaces of the first joint portion and the second joint portion tighten against each other.
    Type: Application
    Filed: December 28, 2020
    Publication date: April 22, 2021
    Inventors: Michael P. Matlack, Dylan E. Polus
  • Patent number: 10906253
    Abstract: A tool assembly includes a first piece, a second piece, and a fastener. The first piece has a first joint portion including a top surface and at least a first interlock surface. The second piece has a second joint portion configured to interlock with the first joint portion. The second joint portion includes a top surface and at least a second interlock surface that is complementary to the first interlock surface. The fastener extends through the first and second joint portions. The first interlock surface and the top surface of the first joint portion form an obtuse angle corner and the second interlock surface and the top surface of the second joint portion form an acute angle corner. The first interlock surface is configured to contact the second interlock surface to inhibit relative movement between the first piece and the second piece along a longitudinal axis of the tool assembly.
    Type: Grant
    Filed: June 14, 2018
    Date of Patent: February 2, 2021
    Assignee: THE BOEING COMPANY
    Inventors: Michael P. Matlack, Dylan E. Polus
  • Publication number: 20190381751
    Abstract: A tool assembly includes a first piece, a second piece, and a fastener. The first piece has a first joint portion including a top surface and at least a first interlock surface. The second piece has a second joint portion configured to interlock with the first joint portion. The second joint portion includes a top surface and at least a second interlock surface that is complementary to the first interlock surface. The fastener extends through the first and second joint portions. The first interlock surface and the top surface of the first joint portion form an obtuse angle corner and the second interlock surface and the top surface of the second joint portion form an acute angle corner. The first interlock surface is configured to contact the second interlock surface to inhibit relative movement between the first piece and the second piece along a longitudinal axis of the tool assembly.
    Type: Application
    Filed: June 14, 2018
    Publication date: December 19, 2019
    Inventors: Michael P. Matlack, Dylan E. Polus
  • Patent number: 9289849
    Abstract: One aspect of the disclosure relates to a friction stir welding apparatus. The friction stir welding apparatus includes a spindle housing and a pin tool concentric with an axis and rotatable relative to the spindle housing about the axis. The friction stir welding apparatus also includes a first shoulder not substantially rotatable relative to the spindle housing about the axis and a second shoulder not substantially rotatable relative to the spindle housing about the axis. The pin tool is rotatable relative to the first shoulder and the second shoulder.
    Type: Grant
    Filed: April 2, 2015
    Date of Patent: March 22, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Michael P. Matlack, Amy Marie Helvey, John A. Baumann
  • Publication number: 20150209895
    Abstract: One aspect of the disclosure relates to a friction stir welding apparatus. The friction stir welding apparatus includes a spindle housing and a pin tool concentric with an axis and rotatable relative to the spindle housing about the axis. The friction stir welding apparatus also includes a first shoulder not substantially rotatable relative to the spindle housing about the axis and a second shoulder not substantially rotatable relative to the spindle housing about the axis. The pin tool is rotatable relative to the first shoulder and the second shoulder.
    Type: Application
    Filed: April 2, 2015
    Publication date: July 30, 2015
    Inventors: Michael P. Matlack, Amy Marie Helvey, John A. Baumann
  • Patent number: 9010613
    Abstract: One aspect of the disclosure relates to a friction stir welding apparatus. The friction stir welding apparatus includes a spindle housing and a pin tool concentric with an axis and rotatable relative to the spindle housing about the axis. The friction stir welding apparatus also includes a first shoulder not substantially rotatable relative to the spindle housing about the axis and a second shoulder not substantially rotatable relative to the spindle housing about the axis. The pin tool is rotatable relative to the first shoulder and the second shoulder.
    Type: Grant
    Filed: December 16, 2013
    Date of Patent: April 21, 2015
    Assignee: The Boeing Company
    Inventors: Michael P. Matlack, Amy Marie Helvey, John A. Baumann
  • Patent number: 8141859
    Abstract: An apparatus and method for separating a pin tool from a shoulder tool, after the pin tool and shoulder tool have become welded together during a friction stir welding operation. In one exemplary embodiment a frame is used to support the shoulder tool. A fluid pressure actuating assembly is used for gradually exerting a force on the pin tool while the shoulder tool is held stationary within the frame. The gradually increasing force gradually breaks the weld and separates the pin tool from the shoulder tool without damaging the pin tool.
    Type: Grant
    Filed: November 2, 2007
    Date of Patent: March 27, 2012
    Assignee: The Boeing Company
    Inventors: Michael P. Matlack, Kurt A. Burton, John A. Baumann
  • Patent number: 8112838
    Abstract: The disclosure provides for a friction stir welding tool cleaning method and apparatus for fixed and retractable pin tools. The method and apparatus use a heating component, a temperature indicator component, a controller component, and a rotatable tool cleaner component for cleaning fixed pin tools. An additional bore cleaner component is used for cleaning retractable pin tools. Heat is applied to a friction stir welding tool having a surface with weld process residue material until the process residue material is sufficiently plasticized, and then the tool cleaner component is applied to the heated tool to remove the plasticized residue on the pin and shoulder surfaces of the tool, and for retractable pin tools, the bore cleaner component is applied to the heated tool to remove the plasticized residue in the tool bore.
    Type: Grant
    Filed: November 19, 2009
    Date of Patent: February 14, 2012
    Assignee: The Boeing Company
    Inventors: Michael P. Matlack, Kurt A. Burton
  • Patent number: 8079507
    Abstract: A friction stir welding (FSW) apparatus has an FSW tool adapted for joining work pieces supportable against a backing anvil. The FSW apparatus comprises a pair of clamping rollers maintained in substantially perpendicular relationship to the backing anvil as the FSW tool moves along the tool path. A roller pivot joint of the FSW apparatus maintains a cylindrical roller outer surface of each clamping roller in substantially parallel relationship to the top sides of the work pieces. The roller pivot joint may include a gimballing roller bearing to which the clamping roller is mounted. The roller bearing is universally movable in a variety of directions to maintain the perpendicular relationship of the clamping rollers relative to the backing anvil.
    Type: Grant
    Filed: March 4, 2010
    Date of Patent: December 20, 2011
    Assignee: The Boeing Company
    Inventors: Michael P. Matlack, Kurt A. Burton
  • Patent number: 7966713
    Abstract: Embodiments of tool mounted structural positioning devices and techniques are described. In one embodiment, a positioning device includes mountings to mount the device directly to a tool device configured to travel a path and perform a manufacturing operation on an element. Engagement mechanisms coupled to the positioning device are aligned to the predefined path and are configured to exert a clamping force upon the element such that the element is secured and positioned by the positioning device in constant relation to the predefined path as the operations are performed.
    Type: Grant
    Filed: May 17, 2006
    Date of Patent: June 28, 2011
    Assignee: The Boeing Company
    Inventors: Kurt A. Burton, Michael P. Matlack
  • Patent number: 7934892
    Abstract: A collet clamping nosepiece for a power feed drill is described which includes at least one clamping piston located along a centerline of the nosepiece, an expansion mandrel comprising a frusto-conical exterior surface, and an expandable collet. The expandable collet is configured to substantially surround the expansion mandrel and operatively connect to the at least one clamping piston. Operation of the at least one clamping piston causes the mandrel to move along the exterior surface of the expansion mandrel for engagement and disengagement of the collet with a bore configured for insertion of the collet.
    Type: Grant
    Filed: December 13, 2006
    Date of Patent: May 3, 2011
    Assignee: The Boeing Company
    Inventors: David L. Fritsche, Michael P. Matlack, Dennis R. Mathis