Turbine combustor having more uniform mixing of fuel and air...

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

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F02C 3/00 (2006.01) F23R 3/04 (2006.01) F23R 3/34 (2006.01) F23R 3/40 (2006.01)

Patent

CA 1209813

ABSTRACT OF THE DISCLOSURE A combustor for a land based turbine comprising a generally tubular sidewall having a downstream mixing zone where a mixture of fuel and air is developed for downstream combustion, said sidewall further having an upstream primary zone into which air is admitted through sidewall openings to develop an axial airflow for mixing with downstream injection fuel, means for spraying fuel in small rapidly evaporable droplets generally radially inwardly through said sidewall at a location between said primary zone and said mixing zone for mixing with the primary air flow, a catalyst is coupled to the combustor sidewall at the outlet of said mixing zone, a plurality of circumferentially disposed air scoops located in upstream proximity to said fuel spraying means and angled down- stream to produce said booster air streams.

434626

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