Patents by Inventor Ansley Michelle Pangle

Ansley Michelle Pangle 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).

  • Combustor cap assembly
    Patent number: 9003803
    Abstract: A support structure for a burner tube in a combustor cap assembly for a gas turbine combustor includes an outer annular ring; an inner annular hub; and a plurality of struts extending radially between said outer annular ring and the inner hub. The inner hub is provided with a piston ring groove and a piston ring adapted to receive and seal an inner end of the burner tube.
    Type: Grant
    Filed: August 3, 2012
    Date of Patent: April 14, 2015
    Assignee: General Electric Company
    Inventors: Ansley Michelle Pangle, Matthew Bernard Wilson, William Michael Poschel
  • COMBUSTOR CAP ASSEMBLY
    Publication number: 20140033717
    Abstract: A support structure for a burner tube in a combustor cap assembly for a gas turbine combustor includes an outer annular ring; an inner annular hub; and a plurality of struts extending radially between said outer annular ring and the inner hub. The inner hub is provided with a piston ring groove and a piston ring adapted to receive and seal an inner end of the burner tube.
    Type: Application
    Filed: August 3, 2012
    Publication date: February 6, 2014
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Ansley Michelle PANGLE, Matthew Bernard WILSON, William Michael POSCHEL
  • Combustion liner stop in a gas turbine
    Patent number: 7762075
    Abstract: A liner stop for retaining a liner within a sleeve of a combustion system, includes: a female component including a saddle, the female component adapted for coupling to one of the liner and the sleeve; a male component including a tab for insertion into the saddle, the male component adapted for coupling to an opposite one of the liner and the sleeve; and an insert adapted for being attached to the tab and ensuring dampening of vibration when the tab is disposed within the saddle. A method and a system are also disclosed.
    Type: Grant
    Filed: August 14, 2007
    Date of Patent: July 27, 2010
    Assignee: General Electric Company
    Inventors: Ansley Michelle Pangle, Jeffrey Scott Lebegue, Todd Daniel Paquin
  • COMBUSTION LINER STOP IN A GAS TURBINE
    Publication number: 20090044540
    Abstract: A liner stop for retaining a liner within a sleeve of a combustion system, includes: a female component including a saddle, the female component adapted for coupling to one of the liner and the sleeve; a male component including a tab for insertion into the saddle, the male component adapted for coupling to an opposite one of the liner and the sleeve; and an insert adapted for being attached to the tab and ensuring dampening of vibration when the tab is disposed within the saddle. A method and a system are also disclosed.
    Type: Application
    Filed: August 14, 2007
    Publication date: February 19, 2009
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Ansley Michelle Pangle, Jeffrey Scott Lebegue, Todd Daniel Paquin