Patents by Inventor Harold Lamar Jordan, Jr.

Harold Lamar Jordan, Jr. 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: 9771877
    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 output to match a nominal mega-watt power output value, and subsequently measuring an actual fuel flow 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 fuel flow value and a nominal fuel flow value at the ambient condition; commanding each GT in the set of GTs to a part load level, the part load level representing a fraction of the base load level, and subsequently measuring an actual fuel flow value for each GT at the part load level; and calibrating the set of GTs based upon a difference between the measured actual fuel flow value at the part load level and the measured actual fuel flow value
    Type: Grant
    Filed: November 18, 2014
    Date of Patent: September 26, 2017
    Assignee: General Electric Company
    Inventors: Lewis Berkley Davis, Jr., Scott Arthur Day, Paul Robert Fernandez, Harold Lamar Jordan, Jr., Rex Allen Morgan
  • Patent number: 9771874
    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 output to match a nominal mega-watt power output 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: November 18, 2014
    Date of Patent: September 26, 2017
    Assignee: General Electric Company
    Inventors: Lewis Berkley Davis, Jr., Scott Arthur Day, Harold Lamar Jordan, Jr., Rex Allen Morgan
  • Patent number: 9771876
    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 output to match a nominal mega-watt 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 further adjusting an operating condition of each GT in the set of GTs based upon a determined emissions measurement error.
    Type: Grant
    Filed: November 18, 2014
    Date of Patent: September 26, 2017
    Assignee: General Electric Compnay
    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: 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: 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: 20170175647
    Abstract: Commanding GTs to base load level based upon measured ambient condition for each GT; commanding each GT to adjust a power output to match scaled power output value equal to a fraction of a difference between the respective power output and a nominal power output value, and measuring 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 an emissions scale factor, wherein the nominal emissions value at the ambient condition and the emissions scale factor are stored in a pre-existing emissions model for the GT.
    Type: Application
    Filed: December 16, 2015
    Publication date: June 22, 2017
    Inventors: Lewis Berkley Davis, JR., Scott Arthur Day, Timothy Andrew Healy, Rebecca Kathryn Jaiven, Harold Lamar Jordan, JR., Rex Allen Morgan
  • Publication number: 20170176960
    Abstract: Commanding GTs to base load level based upon measured ambient condition for each GT; commanding each GT to adjust a power output to match scaled power output value equal to a fraction of a difference between the respective power output and a nominal power output value, and measuring actual emissions value for each GT during the adjusting of the respective power output; adjusting operating condition of each GT based upon a difference between the respective measured actual emissions value, a nominal emissions value at the ambient condition and emissions scale factor; updating a pre-existing emissions model for each GT based upon the adjusted operating; running set of operating conditions on each GT and measuring updated parameters for each GT including an updated emissions value; and refining 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, Rebecca Kathryn Jaiven, 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: 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: 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: 20170167300
    Abstract: A system for controlling gas turbine output for a gas turbine power plant is disclosed herein. The power plant includes a gas turbine including a combustor downstream from a compressor, a turbine downstream from the combustor and an exhaust duct downstream from the outlet of the turbine. The exhaust duct receives exhaust gas from the turbine outlet. The system further includes an exhaust damper operably connected to a downstream end of the exhaust duct. The exhaust damper increases backpressure at the turbine outlet and restricts axial exit velocity of the exhaust gas exiting the turbine outlet when the exhaust damper is partially closed. A method for controlling gas turbine output is also provided herein.
    Type: Application
    Filed: December 15, 2015
    Publication date: June 15, 2017
    Inventors: George Vargese Mathai, Alston Ilford Scipio, Harold Lamar Jordan, JR., Sanji Ekanayake, Joseph Philip Klosinski
  • 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
  • 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: 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: 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: 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: 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: 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.