Patents by Inventor Rex Allen Morgan

Rex Allen Morgan 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).

  • Publication number: 20170175650
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a scaled power output value equal to a fraction of a difference between the respective power output and a nominal power output value, and modeling an emissions value for the GT during the adjusting of the respective power output; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective modelled emissions value, a nominal emissions value at the ambient condition and a nominal emissions value at the ambient condition.
    Type: Application
    Filed: December 16, 2015
    Publication date: June 22, 2017
    Inventors: Lewis Berkley Davis, JR., Scott Arthur Day, Harold Lamar Jordan, JR., Rex Allen Morgan
  • Publication number: 20170175648
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a nominal power output value, and subsequently measuring an actual emissions value for each GT; adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition; and setting a target operating condition for each GT to match the adjusted operating condition after the adjusting of the operating condition.
    Type: Application
    Filed: December 16, 2015
    Publication date: June 22, 2017
    Inventors: Harold Lamar Jordan, JR., Lewis Berkley Davis, JR., Scott Arthur Day, David Spencer Ewens, Rex Allen Morgan
  • Publication number: 20170179790
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a scaled power output value equal to a fraction of a difference between the respective power output and a nominal power output value, and measuring an actual emissions value for each GT during the adjusting of the respective power output; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value, a nominal emissions value at the ambient condition and a nominal emissions value at the ambient condition.
    Type: Application
    Filed: December 16, 2015
    Publication date: June 22, 2017
    Inventors: Lewis Berkley Davis, JR., Scott Arthur Day, Harold Lamar Jordan, JR., Rex Allen Morgan
  • Publication number: 20170175651
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a nominal power output value, and subsequently measuring an actual emissions value for each GT; adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition; and building an independent emissions model for each GT based upon the measured actual emissions value for each GT and the adjusted operating condition of each GT.
    Type: Application
    Filed: December 16, 2015
    Publication date: June 22, 2017
    Inventors: Lewis Berkley Davis, JR., Scott Arthur Day, Timothy Andrew Healy, Harold Lamar Jordan, JR., Rex Allen Morgan
  • Publication number: 20170175644
    Abstract: A system includes: a computing device configured to tune a set of gas turbines (GTs) by: commanding each GT to a base load level; commanding each GT to adjust a respective power output to match a nominal power output value, and subsequently measuring an actual emissions value for each GT; adjusting an operating condition of each GT based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition; updating a pre-existing emissions model for each GT based upon the adjusted operating condition; running a set of operating conditions on each GT and measuring an updated emissions value; and refining the updated pre-existing emissions model based upon a difference between the updated emissions value and the updated pre-existing emissions model.
    Type: Application
    Filed: December 16, 2015
    Publication date: June 22, 2017
    Inventors: Lewis Berkley Davis, JR., Scott Arthur Day, Timothy Andrew Healy, Harold Lamar Jordan, JR., Rex Allen Morgan
  • Publication number: 20170175649
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: modelling each GT in the set of GTs at a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a scaled power output value equal to a fraction of a difference between the respective power output and a nominal power output value, and measuring an actual emissions value for each GT during the adjusting of the respective power output; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value, a nominal emissions value at the ambient condition and a nominal emissions value at the ambient condition.
    Type: Application
    Filed: December 16, 2015
    Publication date: June 22, 2017
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, JR., Scott Arthur Day, Harold Lamar Jordan, JR.
  • Publication number: 20170159575
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a scaled power output value equal to a fraction of a difference between the respective power output and a nominal power output value, and subsequently measuring an actual emissions value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value, a nominal emissions value at the ambient condition and a nominal emissions value at the ambient condition.
    Type: Application
    Filed: December 7, 2015
    Publication date: June 8, 2017
    Inventors: Lewis Berkley Davis, JR., Scott Arthur Day, Harold Lamar Jordan, JR., Rex Allen Morgan
  • Patent number: 9665077
    Abstract: A non-transitory computer-readable medium storing computer executable code that includes instructions to receive a signal representative of a gas turbine firing temperature. The code further includes instructions to convert the signal to an actuator signal to actuate a fuel valve supplying fuel to the gas turbine by following a first reference function. The first reference function includes a first boundary function, a second boundary function, or a combination thereof. The first boundary function maps a first value to a first temperature and the second boundary function maps a second value to a second temperature.
    Type: Grant
    Filed: December 18, 2013
    Date of Patent: May 30, 2017
    Assignee: General Electric Company
    Inventors: Harold Lamar Jordan, Jr., Rex Allen Morgan
  • Publication number: 20170107902
    Abstract: The present application provides a gas turbine engine intended to be used in part in hot ambient conditions. The gas turbine engine may include a compressor, a turbine with a wheel space adjacent to a number of rotor wheels, and a wheel space water cooling system in communication with the wheel space to provide a flow of water thereto.
    Type: Application
    Filed: October 19, 2015
    Publication date: April 20, 2017
    Inventors: Pagalenthi Nandagopal, Rex allen Morgan, Sendikumaran Soundiramourty, Debabrata Mukhopadhyay
  • Patent number: 9611791
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective fuel flow to match a nominal fuel flow value, and subsequently measuring an actual power output value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual power output value and a nominal power output value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: April 4, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9599033
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective fuel flow value to match a nominal fuel flow value, and subsequently measuring an actual exhaust energy value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual exhaust energy value and a nominal exhaust energy value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: March 21, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9599029
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective fuel flow to match a nominal fuel flow value, and subsequently measuring an actual emissions value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: March 21, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9599032
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective emissions value to match a nominal emissions value, and subsequently measuring an actual fuel flow value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual fuel flow value and a nominal fuel flow value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: March 21, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9599031
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a nominal power output value, and subsequently measuring an actual emissions value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: March 21, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9599025
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective power output to match a nominal power output value, and subsequently measuring an actual exhaust energy value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual exhaust energy value and a nominal exhaust energy value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: March 21, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9599024
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective exhaust energy to match a nominal exhaust energy value, and subsequently measuring an actual emissions value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual emissions value and a nominal emissions value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: March 21, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9599026
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective exhaust energy to match a nominal exhaust energy value, and subsequently measuring an actual power output value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual power output value and a nominal power output value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: March 21, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9599027
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective emissions value to match a nominal emissions value, and subsequently measuring an actual exhaust energy value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual exhaust energy value and a nominal exhaust energy value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: March 21, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9599030
    Abstract: Various embodiments include a system having: at least one computing device configured to tune a set of gas turbines (GTs) by performing actions including: commanding each GT in the set of GTs to a base load level, based upon a measured ambient condition for each GT; commanding each GT in the set of GTs to adjust a respective exhaust energy to match a nominal exhaust energy value, and subsequently measuring an actual fuel flow value for each GT; and adjusting an operating condition of each GT in the set of GTs based upon a difference between the respective measured actual fuel flow value and a nominal fuel flow value at the ambient condition.
    Type: Grant
    Filed: April 14, 2015
    Date of Patent: March 21, 2017
    Assignee: General Electric Company
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr.
  • Patent number: 9476361
    Abstract: A system includes a gas turbine system including a compressor, a combustor, and a turbine. The system also includes a controller communicatively coupled to the gas turbine system and configured to control operations of the gas turbine system. The system further includes a life consumption model configured to determine an operating life of the gas turbine system based on both a health status of one or more components of the gas turbine system and operating conditions of the gas turbine system. The controller is configured to utilize at least the life consumption model to derive a control action for the gas turbine system.
    Type: Grant
    Filed: July 8, 2013
    Date of Patent: October 25, 2016
    Assignee: GENERAL ELECTRIC COMPANY
    Inventors: Rex Allen Morgan, Lewis Berkley Davis, Jr., Harold Lamar Jordan, Scott Richard Baker