公开(公告)号：US20230213196A1

公开(公告)日：2023-07-06

申请号：US18120183

申请日：2023-03-10

Applicant: Collins Engine Nozzles, Inc.

Inventor： Jason Ryon ,  Brandon P. Williams ,  Lev Alexander Prociw

IPC: F23R3/34 ,  F02C7/264

CPC classification number: F23R3/343 ,  F02C7/264 ,  F05D2240/35 ,  F05D2260/99

Abstract: An embodiment of a combustor for a gas turbine engine includes a combustor case, a combustor liner disposed within the combustor case, a fuel nozzle, and a torch igniter within the combustor case. The torch igniter includes a combustion chamber, a cap defining the upstream end of the combustion chamber and configured to receive a fuel injector and a surface igniter, a tip defining the downstream end of the combustion chamber, an annular igniter wall extending from the cap to the tip and defining a radial extent of the combustion chamber, a structural wall coaxial with and surrounding the igniter wall, and an outlet passage within the tip that fluidly connects the combustion chamber to the combustor. The torch igniter is situated such that the tip is mounted through the combustor liner, the combustion chamber is within the combustor case, and the cap extends through the combustor case.