Patents by Inventor Chris G. McInelly

Chris G. McInelly 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: 10599132
    Abstract: An automated fastener insert installation system for composite panels is provided. A first module receives and secures a composite panel with respect to an origin of a first coordinate system, wherein the composite panel has opposed major surfaces and defines an insert-receiving orifice extending through one of the major surfaces, and is secured such that one of the major surfaces is externally accessible. A second module engages each of a plurality of fastener inserts with an installation aide. Third module determines a configuration of the orifice defined by the composite panel, selects a corresponding one of the fastener inserts engaged with the installation aide, inserts the selected fastener insert into the orifice, and dispenses an adhesive material through the installation aide and into the orifice about selected fastener insert such that the adhesive material secures the selected fastener insert within the orifice. Associated systems are also provided.
    Type: Grant
    Filed: February 11, 2019
    Date of Patent: March 24, 2020
    Assignee: The Boeing Company
    Inventors: Aaron Coon, Chris G. McInelly, Bret Hoeksema, Ryan Lillibridge, Tom Allen, Steve Solack, Kevin Bowe, Gary K. Allen
  • Publication number: 20190171191
    Abstract: An automated fastener insert installation system for composite panels is provided. A first module receives and secures a composite panel with respect to an origin of a first coordinate system, wherein the composite panel has opposed major surfaces and defines an insert-receiving orifice extending through one of the major surfaces, and is secured such that one of the major surfaces is externally accessible. A second module engages each of a plurality of fastener inserts with an installation aide. Third module determines a configuration of the orifice defined by the composite panel, selects a corresponding one of the fastener inserts engaged with the installation aide, inserts the selected fastener insert into the orifice, and dispenses an adhesive material through the installation aide and into the orifice about selected fastener insert such that the adhesive material secures the selected fastener insert within the orifice. Associated systems are also provided.
    Type: Application
    Filed: February 11, 2019
    Publication date: June 6, 2019
    Inventors: Aaron Coon, Chris G. McInelly, Bret Hoeksema, Ryan Lillibridge, Tom Allen, Steve Solack, Kevin Bowe, Gary K. Allen
  • Patent number: 10228684
    Abstract: An automated fastener insert installation system for composite panels is provided. A first module receives and secures a composite panel with respect to an origin of a first coordinate system, wherein the composite panel has opposed major surfaces and defines an insert-receiving orifice extending through one of the major surfaces, and is secured such that one of the major surfaces is externally accessible. A second module engages each of a plurality of fastener inserts with an installation aide. Third module determines a configuration of the orifice defined by the composite panel, selects a corresponding one of the fastener inserts engaged with the installation aide, inserts the selected fastener insert into the orifice, and dispenses an adhesive material through the installation aide and into the orifice about selected fastener insert such that the adhesive material secures the selected fastener insert within the orifice. Associated systems are also provided.
    Type: Grant
    Filed: November 23, 2015
    Date of Patent: March 12, 2019
    Assignee: The Boeing Company
    Inventors: Aaron Coon, Chris G. McInelly, Bret Hoeksema, Ryan Lillibridge, Tom Allen, Steve Solack, Kevin Bowe, Gary K. Allen
  • Patent number: 9844929
    Abstract: An automated fastener insert installation system for composite panels is provided. A first module receives and secures a composite panel with respect to an origin of a first coordinate system, wherein the composite panel has opposed major surfaces and defines an insert-receiving orifice extending through one of the major surfaces, and is secured such that one of the major surfaces is externally accessible. A second module engages each of a plurality of fastener inserts with an installation aide. Third module determines a configuration of the orifice defined by the composite panel, selects a corresponding one of the fastener inserts engaged with the installation aide, inserts the selected fastener insert into the orifice, and dispenses an adhesive material through the installation aide and into the orifice about selected fastener insert such that the adhesive material secures the selected fastener insert within the orifice. Associated systems are also provided.
    Type: Grant
    Filed: November 23, 2015
    Date of Patent: December 19, 2017
    Assignee: The Boeing Company
    Inventors: Aaron Coon, Chris G. McInelly, Bret Hoeksema, Ryan Lillibridge, Tom Allen, Steve Solack, Kevin Bowe, Gary K. Allen
  • Patent number: 8245467
    Abstract: A joint apparatus and method of assembly is disclosed for connecting building components such as panels, door jamb assemblies, windows and other structures. The apparatus includes an engagement structure with retaining elements that couple building components without the need for mechanical fasteners. The retaining element may contain serrations on which an adhesive is applied before a panel or other building component is secured to the joint apparatus. Other building components such as hinge assemblies include coupling members with a flange. The slots along a retaining element allows coupling members to snap fit into the joint apparatus once a flange is secured into the slots in order to lock the components.
    Type: Grant
    Filed: November 16, 2009
    Date of Patent: August 21, 2012
    Assignee: The Boeing Company
    Inventors: Michael S. Lewis, Bryan A. Branscome, Dean W. Habersetzer, Chris G. McInelly
  • Publication number: 20100095624
    Abstract: A joint apparatus and method of assembly is disclosed for connecting building components such as panels, door jamb assemblies, windows and other structures. The apparatus includes an engagement structure with retaining elements that couple building components without the need for mechanical fasteners. The retaining element may contain serrations on which an adhesive is applied before a panel or other building component is secured to the joint apparatus. Other building components such as hinge assemblies include coupling members with a flange. The slots along a retaining element allows coupling members to snap fit into the joint apparatus once a flange is secured into the slots in order to lock the components.
    Type: Application
    Filed: November 16, 2009
    Publication date: April 22, 2010
    Inventors: Michael S. Lewis, Bryan A. Branscome, Dean W. Habersetze, Chris G. Mcinelly
  • 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