An application of a simplified combustion model to pollutant emissions prediction in gas turbines is presented here. A critical analysis of the Rizk and Mongia semi-analytical model is conducted, and some corrections are accomplished to obtain a better agreement with experimental data. Special attention is devoted to the temperature equation, which is carefully modified, and to the schematization of several kinds of combustors. The simulation of some conventional pollutant reduction techniques, such as inert injection or exhaust gases re-circulation, is conducted with this corrected model. The results show a good agreement with experimental data both in conventional, and in innovative combustors, like Lean-Premixed or Rich-Lean concepts. The model needs a very short computation time and is likely to allow a simultaneous solution of chemical and fluid-dynamic aspect of the combustor.

A semi analytical Approach to emissions prediction in gas Turbine Combustors / B. FACCHINI; G. FERRARA; P. MAZZILLI. - STAMPA. - Paper 98-GT-216:(1998), pp. 1-8. (Intervento presentato al convegno The 43rd ASME Gas Turbine and Aeroengine Congress, Exposition and Users Symposium tenutosi a Stockholm, Sweden nel 2-5 June 1998) [10.1115/98-GT-216].

A semi analytical Approach to emissions prediction in gas Turbine Combustors

FACCHINI, BRUNO;FERRARA, GIOVANNI;
1998

Abstract

An application of a simplified combustion model to pollutant emissions prediction in gas turbines is presented here. A critical analysis of the Rizk and Mongia semi-analytical model is conducted, and some corrections are accomplished to obtain a better agreement with experimental data. Special attention is devoted to the temperature equation, which is carefully modified, and to the schematization of several kinds of combustors. The simulation of some conventional pollutant reduction techniques, such as inert injection or exhaust gases re-circulation, is conducted with this corrected model. The results show a good agreement with experimental data both in conventional, and in innovative combustors, like Lean-Premixed or Rich-Lean concepts. The model needs a very short computation time and is likely to allow a simultaneous solution of chemical and fluid-dynamic aspect of the combustor.
1998
Proc. ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1998
The 43rd ASME Gas Turbine and Aeroengine Congress, Exposition and Users Symposium
Stockholm, Sweden
2-5 June 1998
B. FACCHINI; G. FERRARA; P. MAZZILLI
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Utilizza questo identificatore per citare o creare un link a questa risorsa: https://hdl.handle.net/2158/319472
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