公开(公告)号：US20250109853A1

公开(公告)日：2025-04-03

申请号：US18476595

申请日：2023-09-28

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Pradeep Naik ,  Perumallu Vukanti ,  Ravindra Shankar Ganiger ,  Sahana Narasimhan Suresh ,  Clayton S. Cooper ,  Michael A. Benjamin ,  Steven C. Vise ,  Sripathi Mohan ,  Hiranya Kumar Nath

IPC: F23R3/00 ,  F23R3/28 ,  F23R3/60

Abstract: A turbine engine with a compressor section, a combustion section, and a turbine section in serial flow arrangement along an engine centerline. The combustion section includes a primary combustor liner including an inner liner and an outer liner. A dome wall and a primary dome inlet are located in the dome wall. The outer liner defines at least one opening downstream from the primary dome inlet. A primary combustion chamber and a set of secondary combustors are fluidly coupled to the primary combustion chamber at the at least one opening.