Patents by Inventor Mark Broomer

Mark Broomer 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: 8292573
    Abstract: A turbine nozzle includes outer and inner bands bounding nozzle vanes. The outer band includes an aft flange. An impingement baffle bridges the outer band and aft flange at the root thereof to provide impingement cooling.
    Type: Grant
    Filed: April 21, 2009
    Date of Patent: October 23, 2012
    Assignee: General Electric Company
    Inventors: Mark Broomer, Robert Francis Manning, Haidong Liu
  • Patent number: 8281604
    Abstract: A turbine nozzle includes a row of vanes extending radially in span between inner and outer bands. The vanes include opposite pressure and suction sidewalls and opposite leading and trailing edges. Each vane includes an inner pattern of inner cooling holes and an outer pattern of outer cooling holes distributed along the leading edge. The inner and outer holes diverge toward the corresponding inner and outer bands to preferentially discharge cooling air.
    Type: Grant
    Filed: December 17, 2007
    Date of Patent: October 9, 2012
    Assignee: General Electric Company
    Inventors: Mark Broomer, Victor Hugo Silva Correia, Robert Francis Manning, Stephen Kin-Keung Tung, Bhanu Mahasamudram Reddy
  • Patent number: 8235652
    Abstract: A turbine nozzle segment includes a band having a flowpath side and a non-flowpath side and an enclosure disposed on the non-flowpath side of the band. A plenum may be defined between the band and the enclosure and a discourager may extend from the enclosure.
    Type: Grant
    Filed: December 29, 2007
    Date of Patent: August 7, 2012
    Assignee: General Electric Company
    Inventors: Mark Broomer, Victor Hugo Silva Correia
  • Publication number: 20100266386
    Abstract: A turbine nozzle includes outer and inner bands bounding nozzle vanes. The outer band includes an aft flange. An impingement baffle bridges the outer band and aft flange at the root thereof to provide impingement cooling.
    Type: Application
    Filed: April 21, 2009
    Publication date: October 21, 2010
    Inventors: Mark Broomer, Robert Francis Manning, Haidong Liu
  • Publication number: 20090169360
    Abstract: A turbine nozzle segment includes a band having a flowpath side and a non-flowpath side and an enclosure disposed on the non-flowpath side of the band. A plenum may be defined between the band and the enclosure and a discourager may extend from the enclosure.
    Type: Application
    Filed: December 29, 2007
    Publication date: July 2, 2009
    Inventors: Mark Broomer, Victor Hugo Silva Correia
  • Publication number: 20090165301
    Abstract: A method for repairing a turbine nozzle segment includes providing a turbine nozzle segment having an enclosure with an integral discourager, removing the enclosure and/or the discourager from the turbine nozzle segment and attaching a new enclosure ad/or discourager to the turbine nozzle segment.
    Type: Application
    Filed: December 29, 2007
    Publication date: July 2, 2009
    Inventors: Mark Broomer, Victor Hugo Silva Correia
  • Publication number: 20090155050
    Abstract: A turbine nozzle includes a row of vanes extending radially in span between inner and outer bands. The vanes include opposite pressure and suction sidewalls and opposite leading and trailing edges. Each vane includes an inner pattern of inner cooling holes and an outer pattern of outer cooling holes distributed along the leading edge. The inner and outer holes diverge toward the corresponding inner and outer bands to preferentially discharge cooling air.
    Type: Application
    Filed: December 17, 2007
    Publication date: June 18, 2009
    Inventors: Mark Broomer, Victor Hugo Silva Correia, Robert Francis Manning, Stephen Kin-Keung Tung, Bhanu Mahasamudram Reddy