Patents by Inventor Oliver Roghe

Oliver Roghe 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).

  • Gas turbine engine combustor with CMC heat shield and methods therefor
    Patent number: 9964309
    Abstract: A combustor for a gas turbine engine is disclosed. The combustor is described as comprising a dome plate coupled to a liner thereof, with at least one heat shield comprised of a ceramic matrix composite coupled at the aft end of the dome plate. Also described is a method for assembling a combustor for a gas turbine engine, including releasing a metal alloy heat shield from a dome plate and providing a ceramic matrix composite heat shield as replacement.
    Type: Grant
    Filed: December 22, 2014
    Date of Patent: May 8, 2018
    Assignee: General Electric Company
    Inventors: Donald Michael Corsmeier, Mark Eugene Noe, Michael Todd Radwanski, Oliver Roghe, Jessica Licardi Subit, Ming Xie
  • GAS TURBINE ENGINE COMBUSTOR WITH CMC HEAT SHIELD AND METHODS THEREFOR
    Publication number: 20150107109
    Abstract: A combustor for a gas turbine engine is disclosed. The combustor is described as comprising a dome plate coupled to a liner thereof, with at least one heat shield comprised of a ceramic matrix composite coupled at the aft end of the dome plate. Also described is a method for assembling a combustor for a gas turbine engine, including releasing a metal alloy heat shield from a dome plate and providing a ceramic matrix composite heat shield as replacement.
    Type: Application
    Filed: December 22, 2014
    Publication date: April 23, 2015
    Inventors: Donald Michael Corsmeier, Mark Eugene Noe, Michael Todd Radwanski, Oliver Roghe, Jessica Licardi Subit, Ming Xie
  • Gas turbine engine combustor with CMC heat shield and methods therefor
    Patent number: 8943835
    Abstract: A combustor for a gas turbine engine is disclosed. The combustor is described as comprising a dome plate coupled to a liner thereof, with at least one heat shield comprised of a ceramic matrix composite coupled at the aft end of the dome plate. Also described is a method for assembling a combustor for a gas turbine engine, including releasing a metal alloy heat shield from a dome plate and providing a ceramic matrix composite heat shield as replacement.
    Type: Grant
    Filed: May 10, 2010
    Date of Patent: February 3, 2015
    Assignee: General Electric Company
    Inventors: Donald Michael Corsmeier, Mark Eugene Noe, Michael Todd Radwanski, Oliver Roghe, Jessica Licardi Subit, Ming Xie
  • GAS TURBINE ENGINE COMBUSTOR WITH CMC HEAT SHIELD AND METHODS THEREFOR
    Publication number: 20110271684
    Abstract: A combustor for a gas turbine engine is disclosed. The combustor is described as comprising a dome plate coupled to a liner thereof, with at least one heat shield comprised of a ceramic matrix composite coupled at the aft end of the dome plate. Also described is a method for assembling a combustor for a gas turbine engine, including releasing a metal alloy heat shield from a dome plate and providing a ceramic matrix composite heat shield as replacement.
    Type: Application
    Filed: May 10, 2010
    Publication date: November 10, 2011
    Inventors: Donald Michael CORSMEIER, Mark Eugene Noe, Michael Todd Radwanski, Oliver Roghe, Jessica Licardi Subit, Ming Xie