Minimizing nox production in operation of gas turbine...

Details Minimizing nox production in operation of gas turbine... Minimizing nox production in operation of gas turbine...

F - Mech Eng,Light,Heat,Weapons

02

C

60/111, 60/173,

F02C 3/00 (2006.01) F23C 13/00 (2006.01) F23R 3/40 (2006.01)

Patent

CA 1070963

ABSTRACT OF THE DISCLOSURE A gas turbine combustor wherein one or more catalysts, in series, are employed to effect fuel oxidation at temperatures below flame temperature and a method of operating the same to minimize NOx formation. The turbine combustor comprises a plurality of stages. In one embodiment, the turbine comprises a two zone combustion chamber including a noncatalytic zone, in which fuel is partially combusted under fuel rich conditions, and a catalytic zone, wherein excess air is used to complete the combustion. In another embodiment, a catalyst is used in each combustion stage or zone.

271387

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