Combustion turbine combustor having an improved fuel- rich...

Details Combustion turbine combustor having an improved fuel- rich... Combustion turbine combustor having an improved fuel- rich...

F - Mech Eng,Light,Heat,Weapons

02

C

60/164

F02C 3/00 (2006.01) F23D 11/40 (2006.01) F23R 3/18 (2006.01) F23R 3/28 (2006.01)

Patent

CA 1190051

ABSTRACT OF THE DISCLOSURE A combustion turbine combustor is provided with an improved fuel preparation zone which utilizes the ar- rangement of a static mixing structure to accelerate the flow velocity of combustible gases into a combustion zone. The increased flow velocity reduces the potential of the combustor for flashback and enables use of a fuel-rich configuration in the combustor.

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