Patents by Inventor Scott Richard Zearbaugh

Scott Richard Zearbaugh 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: 8191933
    Abstract: A seal assembly for a fluid coupling includes: (a) a generally planar, substantially rigid seal retainer with opposed first and second faces, having an annular first groove formed in the first face; (b) a first resilient seal disposed in the first groove; and (c) an annular first backup ring positioned radially outboard of the first resilient seal and secured to the first resilient seal, wherein the first backup ring is substantially harder than the first resilient seal.
    Type: Grant
    Filed: July 16, 2008
    Date of Patent: June 5, 2012
    Assignee: General Electric Company
    Inventors: Justin Sanjay Rao, Scott Richard Zearbaugh
  • Patent number: 7784528
    Abstract: A heat exchanger system includes a duct having a duct wall with a duct wall outer surface and a duct wall inner surface; and a heat exchanger partial shell hermetically joined to the duct wall inner surface. The heat exchanger partial shell and a shell portion of the duct wall inner surface constitute a heat exchanger. A heat exchanger inlet manifold is defined by a nonplanar inlet sheet of material hermetically joined to the duct wall outer surface. A heat exchanger outlet manifold is defined by a nonplanar outlet sheet of material hermetically joined to the duct wall outer surface. A heat exchanger inlet opening extends through the duct wall between the inlet manifold and the heat exchanger, and a heat exchanger outlet opening extends through the duct wall between the outlet manifold and the heat exchanger.
    Type: Grant
    Filed: December 27, 2006
    Date of Patent: August 31, 2010
    Assignee: General Electric Company
    Inventors: Nathan Wesley Ottow, Scott Richard Zearbaugh, Phillip Michael Lariviere
  • Publication number: 20100013220
    Abstract: A seal assembly for a fluid coupling includes: (a) a generally planar, substantially rigid seal retainer with opposed first and second faces, having an annular first groove formed in the first face; (b) a first resilient seal disposed in the first groove; and (c) an annular first backup ring positioned radially outboard of the first resilient seal and secured to the first resilient seal, wherein the first backup ring is substantially harder than the first resilient seal.
    Type: Application
    Filed: July 16, 2008
    Publication date: January 21, 2010
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Justin Sanjay Rao, Scott Richard Zearbaugh
  • Publication number: 20080156473
    Abstract: A heat exchanger system includes a duct having a duct wall with a duct wall outer surface and a duct wall inner surface; and a heat exchanger partial shell hermetically joined to the duct wall inner surface. The heat exchanger partial shell and a shell portion of the duct wall inner surface constitute a heat exchanger. A heat exchanger inlet manifold is defined by a nonplanar inlet sheet of material hermetically joined to the duct wall outer surface. A heat exchanger outlet manifold is defined by a nonplanar outlet sheet of material hermetically joined to the duct wall outer surface. A heat exchanger inlet opening extends through the duct wall between the inlet manifold and the heat exchanger, and a heat exchanger outlet opening extends through the duct wall between the outlet manifold and the heat exchanger.
    Type: Application
    Filed: December 27, 2006
    Publication date: July 3, 2008
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Nathan Wesley Ottow, Scott Richard Zearbaugh, Phillip Michael Lariviere
  • Publication number: 20020136631
    Abstract: A gas turbine engine including an active clearance control system that facilitates extending a useful life of a rotor assembly in a cost effective and reliable manner is described. The engine includes at least one rotor assembly and an engine casing that extends circumferentially around the rotor assembly, such that a tip clearance is defined between the rotor assembly and the engine casing. The clearance control system includes a plurality of panels that couple to extend circumferentially around the engine. Each clearance control system panel includes a circumferential feed duct that is formed integrally with the panel.
    Type: Application
    Filed: March 23, 2001
    Publication date: September 26, 2002
    Inventors: Scott Richard Zearbaugh, Steven Louis Brickner, James Warren Hackler, Lonnie Ray Chadwell
  • Patent number: 6454529
    Abstract: A gas turbine engine including an active clearance control system that facilitates extending a useful life of a rotor assembly in a cost effective and reliable manner is described. The engine includes at least one rotor assembly and an engine casing that extends circumferentially around the rotor assembly, such that a tip clearance is defined between the rotor assembly and the engine casing. The clearance control system includes a plurality of panels that couple to extend circumferentially around the engine. Each clearance control system panel includes a circumferential feed duct that is formed integrally with the panel.
    Type: Grant
    Filed: March 23, 2001
    Date of Patent: September 24, 2002
    Assignee: General Electric Company
    Inventors: Scott Richard Zearbaugh, Steven Louis Brickner, James Warren Hackler, Lonnie Ray Chadwell
  • Patent number: 6145578
    Abstract: A spring unit for a core pin assembly for use in molding and die casting apparatus which can be installed in and removed from a mold section as a single unit.
    Type: Grant
    Filed: August 17, 1998
    Date of Patent: November 14, 2000
    Assignee: Wayne C. Zearbaugh
    Inventors: Francis E. Zearbaugh, deceased, by Lucinda Pauline Webb, Heir, by Scott Richard Zearbaugh, Heir, by Darlene K. Zearbaugh, Heir, by Wayne Clayton Zearbaugh, legal representative