Patents by Inventor Narasimha Chiranthan R

Narasimha Chiranthan R 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 FOR A GAS TURBINE ENGINE
    Publication number: 20230417415
    Abstract: A combustor for a gas turbine engine, the gas turbine engine defining a longitudinal centerline extending in a longitudinal direction, a radial direction extending orthogonally outward from the longitudinal centerline, and a circumferential direction extending concentrically around the longitudinal centerline, the combustor including: a forward liner segment; an aft liner segment disposed downstream from the forward liner segment relative to a direction of flow through the combustor, the forward and aft liner segments at least partially defining a combustion chamber; and a fence disposed between the forward and aft liner segments, wherein the fence extends in the circumferential direction, and wherein the fence extends into the combustion chamber along the radial direction.
    Type: Application
    Filed: September 11, 2023
    Publication date: December 28, 2023
    Inventors: Pradeep Naik, Rimple Rakeshkumar Rangrej, Saket Singh, Narasimha Chiranthan R., Shai Birmaher, Hiranya Kumar Nath, Ravindra Shankar Ganiger
  • Combustor for a gas turbine engine
    Patent number: 11774098
    Abstract: A combustor for a gas turbine engine, the gas turbine engine defining a longitudinal centerline extending in a longitudinal direction, a radial direction extending orthogonally outward from the longitudinal centerline, and a circumferential direction extending concentrically around the longitudinal centerline, the combustor including: a forward liner segment; an aft liner segment disposed downstream from the forward liner segment relative to a direction of flow through the combustor, the forward and aft liner segments at least partially defining a combustion chamber; and a fence disposed between the forward and aft liner segments, wherein the fence extends in the circumferential direction, and wherein the fence extends into the combustion chamber along the radial direction.
    Type: Grant
    Filed: June 7, 2021
    Date of Patent: October 3, 2023
    Assignee: GENERAL ELECTRIC COMPANY
    Inventors: Pradeep Naik, Rimple Rakeshkumar Rangrej, Saket Singh, Narasimha Chiranthan R, Shai Birmaher, Hiranya Kumar Nath, Ravindra Shankar Ganiger
  • COMBUSTOR FOR A GAS TURBINE ENGINE
    Publication number: 20220390110
    Abstract: A combustor for a gas turbine engine, the gas turbine engine defining a longitudinal centerline extending in a longitudinal direction, a radial direction extending orthogonally outward from the longitudinal centerline, and a circumferential direction extending concentrically around the longitudinal centerline, the combustor including: a forward liner segment; an aft liner segment disposed downstream from the forward liner segment relative to a direction of flow through the combustor, the forward and aft liner segments at least partially defining a combustion chamber; and a fence disposed between the forward and aft liner segments, wherein the fence extends in the circumferential direction, and wherein the fence extends into the combustion chamber along the radial direction.
    Type: Application
    Filed: June 7, 2021
    Publication date: December 8, 2022
    Inventors: Pradeep Naik, Rimple Rakeshkumar Rangrej, Saket Singh, Narasimha Chiranthan R, Shai Birmaher, Hiranya Kumar Nath, Ravindra Shankar Ganiger