Patents by Inventor Steven G. Lemery

Steven G. Lemery 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: 11548609
    Abstract: A moisture control system includes an anode coupled to an insulation blanket that is positioned between an inner wall and an outer wall of an aircraft fuselage, a cathode coupled to an interior surface of the outer wall, and a power control unit coupled to the anode and the cathode to apply voltage across the anode and the cathode. When the voltage is applied across the anode and the cathode, moisture is drawn away from the anode and toward the cathode on the interior surface of the outer wall and guided along a drainage path provided via structural members disposed between the inner wall and the outer wall toward a drainage port.
    Type: Grant
    Filed: February 14, 2019
    Date of Patent: January 10, 2023
    Assignee: The Boeing Company
    Inventor: Steven G. Lemery
  • Patent number: 11460070
    Abstract: Disclosed herein a bearing that comprises a base, made of a metallic base material. The base comprises a cylindrical outer surface, a cylindrical inner surface that is opposite the cylindrical outer surface, and a central channel defined by the cylindrical inner surface and extending through the base. The bearing also comprises a selective transfer material embedded in the base. The selective transfer material is different than the metallic base material and is configured to release from the base in response to frictionally-induced pressure acting on the base.
    Type: Grant
    Filed: January 3, 2020
    Date of Patent: October 4, 2022
    Assignee: The Boeing Company
    Inventor: Steven G. Lemery
  • Publication number: 20210207650
    Abstract: Disclosed herein a bearing that comprises a base, made of a metallic base material. The base comprises a cylindrical outer surface, a cylindrical inner surface that is opposite the cylindrical outer surface, and a central channel defined by the cylindrical inner surface and extending through the base. The bearing also comprises a selective transfer material embedded in the base. The selective transfer material is different than the metallic base material and is configured to release from the base in response to frictionally-induced pressure acting on the base.
    Type: Application
    Filed: January 3, 2020
    Publication date: July 8, 2021
    Inventor: Steven G. Lemery
  • Publication number: 20200262538
    Abstract: A moisture control system includes an anode coupled to an insulation blanket that is positioned between an inner wall and an outer wall of an aircraft fuselage, a cathode coupled to an interior surface of the outer wall, and a power control unit coupled to the anode and the cathode to apply voltage across the anode and the cathode. When the voltage is applied across the anode and the cathode, moisture is drawn away from the anode and toward the cathode on the interior surface of the outer wall and guided along a drainage path provided via structural members disposed between the inner wall and the outer wall toward a drainage port.
    Type: Application
    Filed: February 14, 2019
    Publication date: August 20, 2020
    Inventor: Steven G. Lemery
  • Patent number: 8512507
    Abstract: A composite structure includes at least one resin matrix layer having a resin material and a plurality of fiber elements and a plurality of titanium particles provided in the resin material. A method of toughening a resin matrix layer is also disclosed.
    Type: Grant
    Filed: September 28, 2011
    Date of Patent: August 20, 2013
    Assignee: The Boeing Company
    Inventors: Luther M. Gammon, Steven G. Lemery
  • Publication number: 20120029118
    Abstract: A composite structure includes at least one resin matrix layer having a resin material and a plurality of fiber elements and a plurality of titanium particles provided in the resin material. A method of toughening a resin matrix layer is also disclosed.
    Type: Application
    Filed: September 28, 2011
    Publication date: February 2, 2012
    Inventors: Luther M. Gammon, Steven G. Lemery
  • Patent number: 8057888
    Abstract: A composite structure includes at least one resin matrix layer having a resin material and a plurality of fiber elements and a plurality of titanium particles provided in the resin material. A method of toughening a resin matrix layer is also disclosed.
    Type: Grant
    Filed: March 28, 2011
    Date of Patent: November 15, 2011
    Assignee: The Boeing Company
    Inventors: Luther M. Gammon, Steven G. Lemery
  • Publication number: 20110171474
    Abstract: A composite structure includes at least one resin matrix layer having a resin material and a plurality of fiber elements and a plurality of titanium particles provided in the resin material. A method of toughening a resin matrix layer is also disclosed.
    Type: Application
    Filed: March 28, 2011
    Publication date: July 14, 2011
    Inventors: Luther M. Gammon, Steven G. Lemery
  • Patent number: 7935214
    Abstract: A composite structure includes at least one resin matrix layer having a resin material and a plurality of fiber elements and a plurality of titanium particles provided in the resin material. A method of toughening a resin matrix layer is also disclosed.
    Type: Grant
    Filed: November 6, 2007
    Date of Patent: May 3, 2011
    Assignee: The Boeing Company
    Inventors: Luther M. Gammon, Steven G. Lemery
  • Publication number: 20090155532
    Abstract: A composite structure includes at least one resin matrix layer having a resin material and a plurality of fiber elements and a plurality of titanium particles provided in the resin material. A method of toughening a resin matrix layer is also disclosed.
    Type: Application
    Filed: November 6, 2007
    Publication date: June 18, 2009
    Inventors: Luther M. Gammon, Steven G. Lemery