General Electric Company

Narasimha Chiranthan R

Ravindra Shankar Ganiger

Pradeep Naik

Hiranya Kumar Nath

Saket Singh

Shai Birmaher

Rimple Rakeshkumar Rangrej

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.

Growing community of inventors

Bengaluru, India

Narasimha Chiranthan R