Tertiary fuel injection system for use in a dry low nox...

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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F02C 3/14 (2006.01) F23C 6/04 (2006.01) F23R 3/34 (2006.01)

Patent

CA 2103433

An improved gas turbine combustor of the type including primary and secondary combustion chambers with a venturi including a throat portion located therebetween; a plurality of primary fuel infection nozzles secured to a combustor cap an an annular array upstream of the primary combustion chamber; and a centerbody including a secondary fuel nozzle, said centerbody extending from said combustor cap to said secondary combustion chamber; the improvement comprising a plurality of tertiary foal injection nozzles arranged in a circular array about a longitudinal axis of the combustor, at a downstream of said venturi throat portion, for injecting fuel into the secondary combustion chamber.

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