Patents by Inventor Daniel Durstock

Daniel Durstock 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: 7665308
    Abstract: A method facilitates operating a gas turbine engine. The method comprises supplying steam to a nozzle, supplying primary fuel to the nozzle, discharging the steam into a combustor from a plurality of circumferentially-spaced steam outlets defined in a tip of the nozzle, and discharging the primary fuel into the combustor from at least one outlet that is spaced circumferentially between the steam outlets.
    Type: Grant
    Filed: November 7, 2005
    Date of Patent: February 23, 2010
    Assignee: General Electric Company
    Inventors: Mark Durbin, Allen M. Danis, Timothy J. Held, James N. Cooper, Douglas Marti Fortuna, Daniel Durstock
  • Patent number: 7520134
    Abstract: A method of operating a gas turbine engine is provided. The method includes discharging pilot fuel into a combustion chamber from a nozzle through at least one pilot fuel outlet defined in a tip of the nozzle, discharging steam from the nozzle through a plurality of steam outlets that are spaced circumferentially about the plurality of pilot fuel outlets, and discharging primary fuel from the nozzle through a plurality of primary fuel outlets that are circumferentially aligned with the plurality of steam outlets. To facilitate mixing the primary fuel with the steam, the primary fuel is discharged from the nozzle tip at an oblique angle with respect to a centerline extending through the nozzle tip.
    Type: Grant
    Filed: September 29, 2006
    Date of Patent: April 21, 2009
    Assignee: General Electric Company
    Inventors: Mark D. Durbin, Allen Michael Danis, Timothy James Held, Daniel Durstock, James N. Cooper, Douglas Marti Fortuna
  • Publication number: 20080078180
    Abstract: A method of operating a gas turbine engine is provided. The method includes discharging pilot fuel into a combustion chamber from a nozzle through at least one pilot fuel outlet defined in a tip of the nozzle, discharging steam from the nozzle through a plurality of steam outlets that are spaced circumferentially about the plurality of pilot fuel outlets, and discharging primary fuel from the nozzle through a plurality of primary fuel outlets that are circumferentially aligned with the plurality of steam outlets. To facilitate mixing the primary fuel with the steam, the primary fuel is discharged from the nozzle tip at an oblique angle with respect to a centerline extending through the nozzle tip.
    Type: Application
    Filed: September 29, 2006
    Publication date: April 3, 2008
    Inventors: Mark D. Durbin, Allen Michael Danis, Timothy James Held, Daniel Durstock, James N. Cooper, Douglas Marti Fortuna
  • Publication number: 20070101726
    Abstract: A method facilitates operating a gas turbine engine. The method comprises supplying steam to a nozzle, supplying primary fuel to the nozzle, discharging the steam into a combustor from a plurality of circumferentially-spaced steam outlets defined in a tip of the nozzle, and discharging the primary fuel into the combustor from at least one outlet that is spaced circumferentially between the steam outlets.
    Type: Application
    Filed: November 7, 2005
    Publication date: May 10, 2007
    Inventors: Mark Durbin, Allen Danis, Timothy Held, James Cooper, Douglas Fortuna, Daniel Durstock