公开(公告)号：US20230417415A1

公开(公告)日：2023-12-28

申请号：US18464550

申请日：2023-09-11

Applicant: General Electric Company

Inventor： Pradeep Naik ,  Rimple Rakeshkumar Rangrej ,  Saket Singh ,  Narasimha Chiranthan R. ,  Shai Birmaher ,  Hiranya Kumar Nath ,  Ravindra Shankar Ganiger

IPC: F23R3/16 ,  F23R3/00 ,  F23R3/08 ,  F23R3/06 ,  F23R3/34

CPC classification number: F23R3/16 ,  F23R3/002 ,  F23R3/08 ,  F23R3/06 ,  F23R3/346 ,  F23M5/085

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.