Patents by Inventor Kevin T. Slattery

Kevin T. Slattery 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: 20200016831
    Abstract: An additive manufacturing system and method includes a powder bed, an additive manufacturing head that is configured to emit a first energy into the powder bed to form at least one layer of a component, a part exposing mechanism that is configured to operate so that the component is in a first position at a first time within the powder bed, and a second position at a second time in which a portion of the component is exposed outside of the powder bed, and a surface smoothing head that is configured to emit a second energy onto the portion of the component in the second position to smooth the portion of the component.
    Type: Application
    Filed: July 16, 2018
    Publication date: January 16, 2020
    Applicant: THE BOEING COMPANY
    Inventor: Kevin T. Slattery
  • Publication number: 20170361396
    Abstract: A method includes disposing a hydride of a transition metal on a first metallic material, where at least one of the first metallic material or a second metallic material includes a surface oxide layer. The method includes performing a diffusion bonding operation to bond the first metallic material to the second metallic material. During the diffusion bonding operation, the hydride of the transition metal chemically reacts with the surface oxide layer.
    Type: Application
    Filed: May 19, 2017
    Publication date: December 21, 2017
    Inventors: Kathleen Chou, Kevin T. Slattery
  • Patent number: 9682445
    Abstract: A method includes disposing ZrH2 nanoparticles on a first metallic material. The method includes performing a diffusion bonding operation to bond the first metallic material to a second metallic material. At least one of the first metallic material or the second metallic material includes a surface oxide layer. During the diffusion bonding operation, the ZrH2 nanoparticles chemically react with the surface oxide layer.
    Type: Grant
    Filed: February 12, 2016
    Date of Patent: June 20, 2017
    Assignee: The Boeing Company
    Inventors: Kathleen Chou, Kevin T. Slattery
  • Patent number: 8852365
    Abstract: An aluminum alloy comprises aluminum, magnesium, scandium, and an enhancing system. The magnesium is from about 0.5 percent to about 10.0 percent by weight based on the aluminum alloy. The scandium is from about 0.05 percent to about 10.0 percent by weight based on the aluminum alloy. The enhancing system is from about 0.05 percent to about 1.5 percent by weight based on the aluminum alloy.
    Type: Grant
    Filed: January 7, 2009
    Date of Patent: October 7, 2014
    Assignee: The Boeing Company
    Inventors: Krishnan K. Sankaran, Kevin T. Slattery
  • Patent number: 8844796
    Abstract: Disclosed herein is a method of making a structure by ultrasonic welding and superplastic forming. The method comprises assembling a plurality of workpieces comprising a first workpiece including a first material having superplastic characteristics; ultrasonically welding the first workpiece to a second workpiece, to form an assembly; heating the assembly to a temperature at which the first material having superplastic characteristics is capable of superplastic deformation, and injecting a fluid between the first workpiece and the second workpiece to form a cavity between the first workpiece and the second workpiece.
    Type: Grant
    Filed: March 5, 2013
    Date of Patent: September 30, 2014
    Assignee: The Boeing Company
    Inventor: Kevin T. Slattery
  • Patent number: 8601850
    Abstract: Any of various features of a workpiece are forged by a common set of tools. The feature is incrementally forged as the tool set is moved to successive forging locations on the surface of the workpiece. One of the tools is used to plasticize and extrude a portion of the workpiece while one or more of the other tools are used to form dams that contain and shape the extruded portions.
    Type: Grant
    Filed: September 25, 2012
    Date of Patent: December 10, 2013
    Assignee: The Boeing Company
    Inventors: Kevin T. Slattery, James B. Castle, Christopher S. Huskamp
  • Patent number: 8506201
    Abstract: A preform for use in forming a structural assembly is provided. The preform can be formed by linear friction welding structural members to a base member and friction welding each structural member to at least one of the other structural members. The resulting preform can be formed with dimensions and a configuration that approximate the dimensions and configuration of the structural assembly.
    Type: Grant
    Filed: April 26, 2007
    Date of Patent: August 13, 2013
    Assignee: The Boeing Company
    Inventor: Kevin T. Slattery
  • Publication number: 20130019649
    Abstract: Any of various features of a workpiece are forged by a common set of tools. The feature is incrementally forged as the tool set is moved to successive forging locations on the surface of the workpiece. One of the tools is used to plasticize and extrude a portion of the workpiece while one or more of the other tools are used to form dams that contain and shape the extruded portions.
    Type: Application
    Filed: September 25, 2012
    Publication date: January 24, 2013
    Inventors: Kevin T. Slattery, James B. Castle, Christopher S. Huskamp
  • Patent number: 8323427
    Abstract: Disclosed embodiments disclose processes for making shaped metal alloy parts, and deal more particularly with forming features and reducing residual stresses in such parts. Residual stresses introduced into a metal alloy part by heat treatment, which may include solution annealing and quenching, are reduced by processes that plastically deform the part while forming part features. An embodiment comprises: producing a metal alloy blank; subjecting the blank to a process that introduces residual stresses into the blank and plastically deforming the blank to reduce the residual stresses in the blank. Embodiments comprise: subjecting a part to a heat treatment that introduces residual stresses in the part; and age forming the part to shape the part and reduce the residual stresses, incrementally forging at least one feature into the part and reducing the residual stresses in the part, friction welding the part, or gauge rolling the cast part to desired dimensions.
    Type: Grant
    Filed: September 14, 2009
    Date of Patent: December 4, 2012
    Assignee: The Boeing Company
    Inventors: Kevin T. Slattery, Krishnan K. Sankaran, James B. Castle, Christopher S. Huskamp
  • Patent number: 8316687
    Abstract: A method is provided for making a composite part layup tool. A surface of a base is shaped and used as a tool to incrementally form a metal sheet. The formed metal sheet is friction plug welded to the shaped surface on the base to form a metal tool surface of the layup tool.
    Type: Grant
    Filed: August 12, 2009
    Date of Patent: November 27, 2012
    Assignee: The Boeing Company
    Inventor: Kevin T. Slattery
  • Patent number: 8302450
    Abstract: Any of various features of a workpiece are forged by a common set of tools. The feature is incrementally forged as the tool set is moved to successive forging locations on the surface of the workpiece. One of the tools is used to plasticize and extrude a portion of the workpiece while one or more of the other tools are used to form dams that contain and shape the extruded portions.
    Type: Grant
    Filed: August 13, 2009
    Date of Patent: November 6, 2012
    Assignee: The Boeing Company
    Inventors: Kevin T. Slattery, Christopher S. Huskamp, James B. Castle
  • Patent number: 8177113
    Abstract: An assembly for positioning a structural assembly for friction stir welding, and a system and method for friction stir welding the structural assembly are provided. The assembly includes a frame defining an aperture therein, and at least one structural member positioned within the aperture. The assembly also includes at least one spacer positioned within the aperture such that the spacer and structural member substantially fill the aperture to secure the structural member within the frame, as well as a substrate secured to the frame and positioned adjacent to the structural member in an overlapping configuration to define an interface between the substrate and structural member. In this configuration, the substrate and structural member are capable of being friction stir welded together.
    Type: Grant
    Filed: November 21, 2006
    Date of Patent: May 15, 2012
    Assignee: The Boeing Company
    Inventor: Kevin T. Slattery
  • Patent number: 7946469
    Abstract: An assembly for positioning a structural assembly for friction stir welding, and a system and method for friction stir welding the structural assembly are provided. The assembly includes a substrate defining a recessed pattern therein, and at least one structural member positioned within the recessed pattern to at least partially secure the structural member therein. The structural member is positioned adjacent to the substrate and within the recessed pattern such that the substrate and structural member are formed of materials capable of being friction stir welded together.
    Type: Grant
    Filed: November 1, 2010
    Date of Patent: May 24, 2011
    Assignee: The Boeing Company
    Inventors: Kevin T. Slattery, Christopher H. Swallow
  • Publication number: 20110042445
    Abstract: An assembly for positioning a structural assembly for friction stir welding, and a system and method for friction stir welding the structural assembly are provided. The assembly includes a substrate defining a recessed pattern therein, and at least one structural member positioned within the recessed pattern to at least partially secure the structural member therein. The structural member is positioned adjacent to the substrate and within the recessed pattern such that the substrate and structural member are formed of materials capable of being friction stir welded together.
    Type: Application
    Filed: November 1, 2010
    Publication date: February 24, 2011
    Inventors: Kevin T. Slattery, Christopher H. Swallow
  • Patent number: 7891535
    Abstract: A method of making a tailored blank comprising the following steps: (a) friction welding first and second structural members together at a substantially right angle with respect to each other to form an intersection comprising a first joining surface formed by adjoining bottom faces of the first and second structural members, and a second joining surface formed by an angled face of the first structural member that is disposed at a first oblique angle relative to the bottom face of the first structural member; (b) friction welding the first joining surface of the intersection to a first portion of a surface of a base member; and (c) concurrently linear friction welding first and second joining surfaces of a third structural member to the second joining surface of the intersection and to a second portion of the surface of the base member respectively.
    Type: Grant
    Filed: October 13, 2005
    Date of Patent: February 22, 2011
    Assignee: The Boeing Company
    Inventors: Kevin T. Slattery, Christopher H. Swallow, Loren J. Strahm
  • Publication number: 20110036139
    Abstract: A method is provided for making a composite part layup tool. A surface of a base is shaped and used as a tool to incrementally form a metal sheet. The formed metal sheet is friction plug welded to the shaped surface on the base to form a metal tool surface of the layup tool.
    Type: Application
    Filed: August 12, 2009
    Publication date: February 17, 2011
    Inventor: Kevin T. Slattery
  • Publication number: 20110036141
    Abstract: Any of various features of a workpiece are forged by a common set of tools. The feature is incrementally forged as the tool set is moved to successive forging locations on the surface of the workpiece. One of the tools is used to plasticize and extrude a portion of the workpiece while one or more of the other tools are used to form dams that contain and shape the extruded portions.
    Type: Application
    Filed: August 13, 2009
    Publication date: February 17, 2011
    Inventors: Kevin T. Slattery, Christopher S. Huskamp, James B. Castle
  • Patent number: 7854363
    Abstract: A preform and method for forming a structural assembly are provided. The preform can be formed by friction welding structural members to a base member and subsequently providing a connection material to join the structural members. The resulting preform can be formed with dimensions and a configuration that approximate the dimensions and configuration of the structural assembly. Thus, the structural assembly can be formed by joining multiple members that are generally smaller than the finished assembly.
    Type: Grant
    Filed: July 7, 2008
    Date of Patent: December 21, 2010
    Assignee: The Boeing Company
    Inventors: Kevin T. Slattery, Keith A. Young
  • Patent number: 7841504
    Abstract: An assembly for positioning a structural assembly for friction stir welding, and a system and method for friction stir welding the structural assembly are provided. The assembly includes a substrate defining a recessed pattern therein, and at least one structural member positioned within the recessed pattern to at least partially secure the structural member therein. The structural member is positioned adjacent to the substrate and within the recessed pattern such that the substrate and structural member are formed of materials capable of being friction stir welded together.
    Type: Grant
    Filed: September 21, 2004
    Date of Patent: November 30, 2010
    Assignee: The Boeing Company
    Inventors: Kevin T. Slattery, Christopher H. Swallow
  • Publication number: 20100170996
    Abstract: An aluminum alloy comprises aluminum, magnesium, scandium, and an enhancing system. The magnesium is from about 0.5 percent to about 10.0 percent by weight based on the aluminum alloy. The scandium is from about 0.05 percent to about 10.0 percent by weight based on the aluminum alloy. The enhancing system is from about 0.05 percent to about 1.5 percent by weight based on the aluminum alloy.
    Type: Application
    Filed: January 7, 2009
    Publication date: July 8, 2010
    Inventors: Krishnan K. Sankaran, Kevin T. Slattery