Patents by Inventor Grzegorz Mlynski

Grzegorz Mlynski 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: 7900457
    Abstract: A method for fabricating a combustor liner for a gas turbine engine is provided. The method includes providing an annular shell including a plurality of circumferentially extending panels, wherein the plurality of circumferentially extending panels includes a first panel positioned at an upstream end of the shell and a second panel positioned downstream from, and adjacent to, the first panel. The method also includes forming a plurality of primary dilution holes in the first panel and forming a plurality of secondary dilution holes in the second panel, wherein the primary and secondary dilution holes are configured to discharge dilution air into the shell.
    Type: Grant
    Filed: October 31, 2006
    Date of Patent: March 8, 2011
    Assignee: General Electric Company
    Inventors: David Bruce Patterson, Art Johnson, John Howard Starkweather, Daniel Kirtley, Grzegorz Mlynski
  • Patent number: 7775050
    Abstract: A method for assembling a combustor for use in a turbine engine is provided. The method includes providing at least one support leg, forming at least one opening in the support leg, wherein the at least one opening has a perimeter defined only by a plurality of non-linear segments, and coupling the support leg to the combustor.
    Type: Grant
    Filed: October 31, 2006
    Date of Patent: August 17, 2010
    Assignee: General Electric Company
    Inventors: David Bruce Patterson, Kelley Parker Brown, Robert Paul Czachor, Grzegorz Mlynski
  • Publication number: 20080098739
    Abstract: A method for assembling a combustor for use in a turbine engine is provided. The method includes providing at least one support leg, forming at least one opening in the support leg, wherein the at least one opening has a perimeter defined only by a plurality of non-linear segments, and coupling the support leg to the combustor.
    Type: Application
    Filed: October 31, 2006
    Publication date: May 1, 2008
    Inventors: David Bruce Patterson, Kelley Parker Brown, Robert Paul Czachor, Grzegorz Mlynski
  • Publication number: 20080010992
    Abstract: A method for fabricating a combustor liner for a gas turbine engine is provided. The method includes providing an annular shell including a plurality of circumferentially extending panels, wherein the plurality of circumferentially extending panels includes a first panel positioned at an upstream end of the shell and a second panel positioned downstream from, and adjacent to, the first panel. The method also includes forming a plurality of primary dilution holes in the first panel and forming a plurality of secondary dilution holes in the second panel, wherein the primary and secondary dilution holes are configured to discharge dilution air into the shell.
    Type: Application
    Filed: October 31, 2006
    Publication date: January 17, 2008
    Inventors: David Bruce Patterson, Art Johnson, John Howard Starkweather, Daniel Kirtley, Grzegorz Mlynski