Combustors with igniters having protrusions

Details Combustors with igniters having protrusions Combustors with igniters having protrusions

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/00 (2006.01) F23R 3/42 (2006.01) F23R 3/60 (2006.01) F02C 3/14 (2006.01)

Patent

CA 2638329

A combustor for a gas turbine engine is provided, and includes an inner case; an outer case circumscribing the inner case and forming an annular pressure vessel therebetween; an inner liner positioned within the annular pressure vessel; an outer liner circumscribing the inner liner and forming a combustion chamber with the inner liner; and an igniter coupled to the outer case and extending to the outer liner such that the igniter is positioned to ignite an air and fuel mixture in the combustion chamber. The igniter includes a protrusion for coupling the igniter to the outer liner.

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