Patents by Inventor Brad J. Reeves

Brad J. Reeves 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: 10975901
    Abstract: Provided are methods of attaching parts using slot cases and assemblies comprising these slot cases. A slot case is inserted into a slot or slid on a tab of a first part prior to attaching it to a second part. The first part may have pores that are partially open at the surface of the slot or tab. These pores may receive adhesive while attaching the two parts. The adhesive volume going into these partially open pores may vary among different first parts. To ensure that enough adhesive is supplied between the slot case and first part, the adhesive is introduced in between these components before attaching the second part and while the slot case and first part are more accessible. The adhesive may be supplied through the bottom of the slot case and continue until the adhesive appears at the top edges of the slot case.
    Type: Grant
    Filed: October 1, 2019
    Date of Patent: April 13, 2021
    Assignee: The Boeing Company
    Inventors: Michael S. Lewis, Sean R. Cysewski, Brad J. Reeves, James S. Bradley
  • Publication number: 20200032827
    Abstract: Provided are methods of attaching parts using slot cases and assemblies comprising these slot cases. A slot case is inserted into a slot or slid on a tab of a first part prior to attaching it to a second part. The first part may have pores that are partially open at the surface of the slot or tab. These pores may receive adhesive while attaching the two parts. The adhesive volume going into these partially open pores may vary among different first parts. To ensure that enough adhesive is supplied between the slot case and first part, the adhesive is introduced in between these components before attaching the second part and while the slot case and first part are more accessible. The adhesive may be supplied through the bottom of the slot case and continue until the adhesive appears at the top edges of the slot case.
    Type: Application
    Filed: October 1, 2019
    Publication date: January 30, 2020
    Applicant: The Boeing Company
    Inventors: Michael S. Lewis, Sean R. Cysewski, Brad J. Reeves, James S. Bradley
  • Patent number: 10502250
    Abstract: Provided are methods of attaching parts using slot cases and assemblies comprising these slot cases. A slot case is inserted into a slot or slid on a tab of a first part prior to attaching it to a second part. The first part may have pores that are partially open at the surface of the slot or tab. These pores may receive adhesive while attaching the two parts. The adhesive volume going into these partially open pores may vary among different first parts. To ensure that enough adhesive is supplied between the slot case and first part, the adhesive is introduced in between these components before attaching the second part and while the slot case and first part are more accessible. The adhesive may be supplied through the bottom of the slot case and continue until the adhesive appears at the top edges of the slot case.
    Type: Grant
    Filed: January 19, 2016
    Date of Patent: December 10, 2019
    Assignee: The Boeing Company
    Inventors: Michael S. Lewis, Sean R. Cysewski, Brad J. Reeves, James S. Bradley
  • Patent number: 10322563
    Abstract: A panel-insert assembly including a panel having a core and a skin layer positioned over the core, wherein the skin layer defines an opening therein, and an insert positioned below the skin layer, wherein the insert is aligned with the opening.
    Type: Grant
    Filed: August 30, 2016
    Date of Patent: June 18, 2019
    Assignee: The Boeing Company
    Inventors: Michael S. Lewis, Jessica Sakurai, Brad J. Reeves
  • Patent number: 9850927
    Abstract: Systems and methods provide for the installation of fasteners in a composite panel with a fastener insert. A fastener insert for a composite panel includes a body and a at least three arms extending from the body. The body has a top face and a central hub extending rearward from the top face. The top face has an outer dimension between opposing edges. The arms extend from the central hub on a rear side of the body. In a retracted configuration, the arms are folded inward toward the central hub so that the arms do not extend beyond the outer dimension of the top face. In an extended configuration, the arms extend outward from the central hub beyond the outer dimension of the top face.
    Type: Grant
    Filed: August 4, 2015
    Date of Patent: December 26, 2017
    Assignee: The Boeing Company
    Inventors: James S. Bradley, Michael S. Lewis, Brad J. Reeves
  • Patent number: 9803668
    Abstract: A panel-insert assembly including a panel and an insert, wherein the panel includes a core and a face sheet positioned over the core, wherein the face sheet defines an opening therein, and wherein the insert is positioned below the face sheet and includes a thread member engaged with the panel, the thread member extending in a first circumferential direction about the vertical axis.
    Type: Grant
    Filed: March 10, 2016
    Date of Patent: October 31, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Brad J. Reeves, James S. Bradley, Michael S. Lewis
  • Publication number: 20170204890
    Abstract: Provided are methods of attaching parts using slot cases and assemblies comprising these slot cases. A slot case is inserted into a slot or slid on a tab of a first part prior to attaching it to a second part. The first part may have pores that are partially open at the surface of the slot or tab. These pores may receive adhesive while attaching the two parts. The adhesive volume going into these partially open pores may vary among different first parts. To ensure that enough adhesive is supplied between the slot case and first part, the adhesive is introduced in between these components before attaching the second part and while the slot case and first part are more accessible. The adhesive may be supplied through the bottom of the slot case and continue until the adhesive appears at the top edges of the slot case.
    Type: Application
    Filed: January 19, 2016
    Publication date: July 20, 2017
    Applicant: The Boeing Company
    Inventors: Michael S. Lewis, Sean R. Cysewski, Brad J. Reeves, James S. Bradley
  • Publication number: 20170037886
    Abstract: Systems and methods provide for the installation of fasteners in a composite panel with a fastener insert. A fastener insert for a composite panel includes a body and a at least three arms extending from the body. The body has a top face and a central hub extending rearward from the top face. The top face has an outer dimension between opposing edges. The arms extend from the central hub on a rear side of the body. In a retracted configuration, the arms are folded inward toward the central hub so that the arms do not extend beyond the outer dimension of the top face. In an extended configuration, the arms extend outward from the central hub beyond the outer dimension of the top face.
    Type: Application
    Filed: August 4, 2015
    Publication date: February 9, 2017
    Inventors: James S. Bradley, Michael S. Lewis, Brad J. Reeves
  • Publication number: 20160368242
    Abstract: A panel-insert assembly including a panel having a core and a skin layer positioned over the core, wherein the skin layer defines an opening therein, and an insert positioned below the skin layer, wherein the insert is aligned with the opening.
    Type: Application
    Filed: August 30, 2016
    Publication date: December 22, 2016
    Inventors: MICHAEL S. LEWIS, JESSICA SAKURAI, BRAD J. REEVES
  • Patent number: 9457540
    Abstract: A panel-insert assembly including a panel having a core and a skin layer positioned over the core, wherein the skin layer defines an opening therein, and an insert positioned below the skin layer, wherein the insert is aligned with the opening.
    Type: Grant
    Filed: July 29, 2014
    Date of Patent: October 4, 2016
    Assignee: The Boeing Company
    Inventors: Michael S. Lewis, Jessica Sakurai, Brad J. Reeves
  • Publication number: 20160186441
    Abstract: A panel-insert assembly including a panel and an insert, wherein the panel includes a core and a face sheet positioned over the core, wherein the face sheet defines an opening therein, and wherein the insert is positioned below the face sheet and includes a thread member engaged with the panel, the thread member extending in a first circumferential direction about the vertical axis.
    Type: Application
    Filed: March 10, 2016
    Publication date: June 30, 2016
    Inventors: Brad J. Reeves, James S. Bradley, Michael S. Lewis
  • Patent number: 9284972
    Abstract: A panel-insert assembly including a panel and an insert, wherein the panel includes a core and a face sheet positioned over the core, wherein the face sheet defines an opening therein, and wherein the insert is positioned below the face sheet and includes a thread member engaged with the panel, the thread member extending in a first circumferential direction about the vertical axis.
    Type: Grant
    Filed: November 17, 2014
    Date of Patent: March 15, 2016
    Assignee: The Boeing Company
    Inventors: Brad J. Reeves, James S. Bradley, Michael S. Lewis
  • Publication number: 20160031184
    Abstract: A panel-insert assembly including a panel having a core and a skin layer positioned over the core, wherein the skin layer defines an opening therein, and an insert positioned below the skin layer, wherein the insert is aligned with the opening.
    Type: Application
    Filed: July 29, 2014
    Publication date: February 4, 2016
    Inventors: Michael S. Lewis, Jessica Sakurai, Brad J. Reeves
  • Patent number: 8961059
    Abstract: A method of fabricating a self-locking joint in a panel structure. The method provides a panel structure having at least two face sheets and a core portion sandwiched therebetween. The method further fabricates in a first portion of the panel structure at least one mortice opening having self-locking end portions. The method further fabricates on a second portion of the panel structure at least one tenon extension having flexible self-locking members. The method further interlocks the flexible self-locking members of the at least one tenon extension with the self-locking end portions of the at least one mortice opening to form a self-locking joint in the panel structure.
    Type: Grant
    Filed: September 6, 2012
    Date of Patent: February 24, 2015
    Assignee: The Boeing Company
    Inventors: Brad J. Reeves, Paul L. Gooch
  • Publication number: 20140064833
    Abstract: There is provided in an embodiment a method of fabricating a self-locking joint in a panel structure. The method provides a panel structure having at least two face sheets and a core portion sandwiched therebetween. The method further fabricates in a first portion of the panel structure at least one mortise opening having self-locking end portions. The method further fabricates on a second portion of the panel structure at least one tenon extension having flexible self-locking members. The method further interlocks the flexible self-locking members of the at least one tenon extension with the self-locking end portions of the at least one mortise opening to form a self-locking joint in the panel structure.
    Type: Application
    Filed: September 6, 2012
    Publication date: March 6, 2014
    Applicant: The Boeing Company
    Inventors: Brad J. Reeves, Paul L. Gooch
  • Patent number: 7599756
    Abstract: A production moving line system. An illustrative embodiment of the production moving line system includes at least one metallic guide strip and at least one tow vehicle which may be adapted to follow the guide strip. The tow vehicle may include control circuitry and a power source and a wireless transceiver connected to the control circuitry. An assembly fixture cart may be coupled to the tow vehicle. A wireless communication link may be provided between a central control computer and the wireless transceiver of the tow vehicle. A production moving line method is also disclosed.
    Type: Grant
    Filed: October 4, 2007
    Date of Patent: October 6, 2009
    Assignee: The Boeing Company
    Inventors: Brad J. Reeves, James S. Bradley, Richard S. Irvine, Chris G. McInelly
  • Publication number: 20090093900
    Abstract: A production moving line system. An illustrative embodiment of the production moving line system includes at least one metallic guide strip and at least one tow vehicle which may be adapted to follow the guide strip. The tow vehicle may include control circuitry and a power source and a wireless transceiver connected to the control circuitry. An assembly fixture cart may be coupled to the tow vehicle. A wireless communication link may be provided between a central control computer and the wireless transceiver of the tow vehicle. A production moving line method is also disclosed.
    Type: Application
    Filed: October 4, 2007
    Publication date: April 9, 2009
    Inventors: Brad J. Reeves, James S. Bradley, Richard S. Irvine, Chris G. McInelly