NOx suppressant stationary gas turbine combustor

Power plants – Combustion products used as motive fluid

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Details

60 3955, 60759, 60760, F02C 330, F23R 354

Patent

active

042978424

ABSTRACT:
The NOx emissions of a stationary gas turbine are reduced by concentrating a NOx suppressant in the reaction zone of the gas turbine combustor by dividing the flow of air to the reaction zone and the dilution zone of the combustor by means of an air flow splitter and by taking advantage of the radially stratified compressor flow. The air flow to the two zones is preferably separated by a common flow shield.

REFERENCES:
patent: 3731484 (1973-05-01), Jackson et al.
patent: 3738106 (1973-06-01), Stein et al.
patent: 4044549 (1977-08-01), Zwick

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