Dry low NOx single stage dual mode combustor construction for a

Power plants – Combustion products used as motive fluid – With addition of steam and/or water

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Details

60737, 60742, F23R 336, F02C 320

Patent

active

052591840

ABSTRACT:
In a gas turbine (10), a plurality of combustors (14), each having a plurality of fuel nozzles (32) arranged about a longitudinal axis of the combustor, and a single combustion zone (70), each fuel nozzle having a diffusion passage (74) and a premix passage (60), the premix passage communicating with a plurality of premix fuel distribution tubes (66) located within a dedicated premix tube (46) adapted to mix the premix fuel and combustion air prior to entry into the single combustion zone (70) located downstream of the premix tube (46).

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GE Turbine Reference Library--"Dry Low NOx Combustion for GE Heavy-Duty Gas Turbines", Dr. L. B. Davis, Jr. (no date).

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