Combustion turbine combustor having an improved heavy- oil...

Details Combustion turbine combustor having an improved heavy- oil... Combustion turbine combustor having an improved heavy- oil...

F - Mech Eng,Light,Heat,Weapons

02

C

60/164

F02C 3/14 (2006.01) F02C 7/22 (2006.01) F23R 3/30 (2006.01)

Patent

CA 1191703

ABSTRACT OF THE DISCLOSURE A combustor for a combustion turbine comprises an enclosure having apertures for enabling the flow of gases into the enclosure, a zone for mixing and vaporizing heavy oil fuel, fuel injecting means in the downstream end of the fuel mixing zone, and means for supporting combus- tion of the fuel mixture in a combustion zone downstream of the mixing zone. The fuel injecting means is prefer- ably a multiple-point fuel injector and where combustion is by catalyst, a catalytic element is preferably struc- tured in at least two segments.

410230

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