Patents by Inventor Steve Solack

Steve Solack 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
  • Publication number: 20170144425
    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: November 23, 2015
    Publication date: May 25, 2017
    Inventors: Aaron Coon, Chris G. Mclnelly, Bret Hoeksema, Ryan Lillibridge, Tom Allen, Steve Solack, Kevin Bowe, Gary K. Allen