Patents by Inventor Edward John Sharrow

Edward John Sharrow 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: 10612420
    Abstract: Rotor support structures for industrial machines are disclosed. The support structures may include a rigid base component including a top portion, a slide plate positioned above the rigid base component, and a bearing housing for a rotor, coupled to the slide plate. The bearing housing and the slide plate may be configured to slide or move over the rigid base component. The support structure may also include a plurality of retention blocks coupled to the bearing housing. Each of the plurality of retention blocks may include a moveable retention pin positioned through each of the plurality of retention blocks. The axial movement of the bearing housing and slide plate may compensate for thermal expansion of a turbine shell and/or may reduce vibrations of the rotor and bearing housing during operation of the industrial machines.
    Type: Grant
    Filed: November 17, 2016
    Date of Patent: April 7, 2020
    Assignee: General Electric Company
    Inventors: Edward John Sharrow, Craig Daniel Ivancic, David Montgomery Ritz
  • Publication number: 20180135465
    Abstract: Rotor support structures for industrial machines are disclosed. The support structures may include a rigid base component including a top portion, a slide plate positioned above the rigid base component, and a bearing housing for a rotor, coupled to the slide plate. The bearing housing and the slide plate may be configured to slide or move over the rigid base component. The support structure may also include a plurality of retention blocks coupled to the bearing housing. Each of the plurality of retention blocks may include a moveable retention pin positioned through each of the plurality of retention blocks. The axial movement of the bearing housing and slide plate may compensate for thermal expansion of a turbine shell and/or may reduce vibrations of the rotor and bearing housing during operation of the industrial machines.
    Type: Application
    Filed: November 17, 2016
    Publication date: May 17, 2018
    Inventors: Edward John Sharrow, Craig Daniel Ivancic, David Montgomery Ritz
  • Patent number: 9376934
    Abstract: A standard for supporting a turbine rotor and a turbine shell includes a bearing block including a housing enclosing bearing surfaces engageable by the turbine rotor. Turbine shell-arm supports are located on opposite sides of the housing, the turbine shell-arm supports each having a horizontal and one or more vertical surfaces adapted to be engaged by support arms of a turbine shell enclosing at least a portion of the turbine. An internal cooling/heating circuit is arranged to simultaneously cool or heat the bearing block and the turbine shell-arm supports to thereby reduce differential thermal growth characteristics of the turbine rotor and turbine shell.
    Type: Grant
    Filed: August 24, 2012
    Date of Patent: June 28, 2016
    Assignee: General Electric Company
    Inventors: Edward Jay Cooper, Peter John Eizenzopf, Xiaoqing Zheng, William Patrick Rusch, Hemanth GS Kumar, Craig Daniel Ivancic, Edward John Sharrow
  • Publication number: 20140053394
    Abstract: A standard for supporting a turbine rotor and a turbine shell includes a bearing block including a housing enclosing bearing surfaces engageable by the turbine rotor. Turbine shell-arm supports are located on opposite sides of the housing, the turbine shell-arm supports each having a horizontal and one or more vertical surfaces adapted to be engaged by support arms of a turbine shell enclosing at least a portion of the turbine. An internal cooling/heating circuit is arranged to simultaneously cool or heat the bearing block and the turbine shell-arm supports to thereby reduce differential thermal growth characteristics of the turbine rotor and turbine shell.
    Type: Application
    Filed: August 24, 2012
    Publication date: February 27, 2014
    Applicant: General Electric Company
    Inventors: Edward Jay COOPER, Peter John EIZENZOPF, Xiaoqing ZHENG, William Patrick RUSCH, Hemanth GS. KUMAR, Craig Daniel IVANCIC, Edward John SHARROW
  • Patent number: 8398367
    Abstract: An extraction unit for a steam turbine includes an end plate mounted downstream of a selected stage of a steam turbine, the end plate sealing the selected stage from the atmosphere, and an extraction pipe passing through the end plate for extracting steam from the selected stage.
    Type: Grant
    Filed: February 10, 2009
    Date of Patent: March 19, 2013
    Assignee: General Electric Company
    Inventors: Karthik Gopal Rao Agara, Daniel Ross Predmore, Edward John Sharrow
  • Publication number: 20100202879
    Abstract: An extraction unit for a steam turbine includes an end plate mounted downstream of a selected stage of a steam turbine, the end plate sealing the selected stage from the atmosphere, and an extraction pipe passing through the end plate for extracting steam from the selected stage.
    Type: Application
    Filed: February 10, 2009
    Publication date: August 12, 2010
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Karthik Gopal Rao Agara, Daniel Ross Predmore, Edward John Sharrow
  • Patent number: 6854954
    Abstract: A method for assembling a power system is provided. The method includes coupling a first turbine and second turbine together with a coupling that extends between a first rotor of a first turbine and a second rotor of the second turbine, and such that the first turbine has fluid flow along a first flow path, and the second turbine has fluid flow along a second flow path. The method further includes fixedly coupling an outer wall to the first turbine that directs fluid flow from the first flow path towards the second flow path.
    Type: Grant
    Filed: March 3, 2003
    Date of Patent: February 15, 2005
    Assignee: General Electric Company
    Inventors: Douglas Carl Hofer, Daniel Mark Brown, Scott William Blackwell, Norman Douglas Lathrop, Edward John Sharrow
  • Publication number: 20040175267
    Abstract: A method for assembling a power system is provided. The method includes coupling a first turbine and second turbine together with a coupling that extends between a first rotor of a first turbine and a second rotor of the second turbine, and such that the first turbine has fluid flow along a first flow path, and the second turbine has fluid flow along a second flow path. The method further includes fixedly coupling an outer wall to the first turbine that directs fluid flow from the first flow path towards the second flow path.
    Type: Application
    Filed: March 3, 2003
    Publication date: September 9, 2004
    Inventors: Douglas Carl Hofer, Daniel Mark Brown, Scott William Blackwell, Norman Douglas Lathrop, Edward John Sharrow
  • Patent number: 6783321
    Abstract: The shafts of upstream and downstream turbines are interconnected by a coupling. A diffuser is provided in an intermediate cavity between the upstream and downstream turbines to recover kinetic energy, as well as minimize or eliminate windage and spinning losses resultant from exposure of the coupling to the flowpath along the turbines. A radial entry inlet provides a supplemental fluid admission into the intermediate cavity, the admission being turned axially and circumferentially for joining with the flow exiting the upstream turbine for combined flow to the downstream turbine.
    Type: Grant
    Filed: November 6, 2002
    Date of Patent: August 31, 2004
    Assignee: General Electric Company
    Inventors: Norman Douglas Lathrop, Daniel Mark Brown, Edward John Sharrow, Kristin Segreto, Douglas Carl Hofer
  • Publication number: 20040086375
    Abstract: The shafts of upstream and downstream turbines are interconnected by a coupling. A diffuser is provided in an intermediate cavity between the upstream and downstream turbines to recover kinetic energy, as well as minimize or eliminate windage and spinning losses resultant from exposure of the coupling to the flowpath along the turbines. A radial entry inlet provides a supplemental fluid admission into the intermediate cavity, the admission being turned axially and circumferentially for joining with the flow exiting the upstream turbine for combined flow to the downstream turbine.
    Type: Application
    Filed: November 6, 2002
    Publication date: May 6, 2004
    Inventors: Norman Douglas Lathrop, Daniel Mark Brown, Edward John Sharrow, Kristin Segreto, Douglas Carl Hofer