PERFORMANCE OF A REDUCED NO x DIFFUSION FLAME COMBUSTOR FOR THE MS5002 GAS TURBINE
ABSTRACT This paper describes a reduced NO R diffusion flame combustor that has been developed for the MS5002 gas turbine. Laboratory tests have shown that when firing with natural gas, without water or steam injection, NO1 emissions from the new combustor are about 40% lower than NOR emissions from...
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ftciteseerx:oai:CiteSeerX.psu:10.1.1.1079.9623 2023-05-15T18:03:39+02:00 PERFORMANCE OF A REDUCED NO x DIFFUSION FLAME COMBUSTOR FOR THE MS5002 GAS TURBINE Alan S Feitelberg Michael D Starkey Richard B Schiefer Roointon E Pavri Matt Bender John L Booth Gordon R Schmidt British Petroleum Prudhoe Bay Alaska The Pennsylvania State University CiteSeerX Archives application/pdf http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.1079.9623 http://proceedings.asmedigitalcollection.asme.org/data/conferences/asmep/81863/v002t02a010-99-gt-058.pdf en eng http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.1079.9623 http://proceedings.asmedigitalcollection.asme.org/data/conferences/asmep/81863/v002t02a010-99-gt-058.pdf Metadata may be used without restrictions as long as the oai identifier remains attached to it. http://proceedings.asmedigitalcollection.asme.org/data/conferences/asmep/81863/v002t02a010-99-gt-058.pdf text ftciteseerx 2020-05-03T00:21:19Z ABSTRACT This paper describes a reduced NO R diffusion flame combustor that has been developed for the MS5002 gas turbine. Laboratory tests have shown that when firing with natural gas, without water or steam injection, NO1 emissions from the new combustor are about 40% lower than NOR emissions from the standard MS5002 combustor. CO emissions are virtually unchanged at base load, but increase at part load conditions. The laboratory results were confirmed in 1997 by a commercial demonstration test at a British Petroleum site in Prudhoe Bay, Alaska. The standard MS5002 gas turbine is equipped with a conventional, swirl stabilized diffusion flame combustion system. The twelve standard combustors in an MS5002 turbine are cylindrical cans, approximately 27 cm (10.5 inches) in diameter and 112 cm (44 inches) long. A small, annular, vortex generator surrounds the single fuel nozzle that is centered at the inlet to each can. The walls of the cans are louvered for cooling, and contain an array of mixing and dilution holes that provide the air needed to complete combustion and dilute the burned gas to the desired turbine inlet temperature. The new, reduced NOR emissions combustor (referred to as a "lean head end", or LHE, combustor) retains all of the key features of the conventional combustor; the only significant difference is the arrangement of the mixing and dilution holes in the cylindrical combustor can. By optimizing the number, diameter, and location of these holes, NOR emissions were substantially reduced. The materials of construction, fuel nozzle, and total combustor air flow were unchanged. The differences in NOR emissions between the standard and LHE combustors, as well as the variations in NOR emissions with firing temperature, were well correlated using turbulent flame length arguments. Details of this correlation are also presented. Text Prudhoe Bay Alaska Unknown Nozzle ENVELOPE(159.100,159.100,-79.917,-79.917) |
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ftciteseerx |
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English |
description |
ABSTRACT This paper describes a reduced NO R diffusion flame combustor that has been developed for the MS5002 gas turbine. Laboratory tests have shown that when firing with natural gas, without water or steam injection, NO1 emissions from the new combustor are about 40% lower than NOR emissions from the standard MS5002 combustor. CO emissions are virtually unchanged at base load, but increase at part load conditions. The laboratory results were confirmed in 1997 by a commercial demonstration test at a British Petroleum site in Prudhoe Bay, Alaska. The standard MS5002 gas turbine is equipped with a conventional, swirl stabilized diffusion flame combustion system. The twelve standard combustors in an MS5002 turbine are cylindrical cans, approximately 27 cm (10.5 inches) in diameter and 112 cm (44 inches) long. A small, annular, vortex generator surrounds the single fuel nozzle that is centered at the inlet to each can. The walls of the cans are louvered for cooling, and contain an array of mixing and dilution holes that provide the air needed to complete combustion and dilute the burned gas to the desired turbine inlet temperature. The new, reduced NOR emissions combustor (referred to as a "lean head end", or LHE, combustor) retains all of the key features of the conventional combustor; the only significant difference is the arrangement of the mixing and dilution holes in the cylindrical combustor can. By optimizing the number, diameter, and location of these holes, NOR emissions were substantially reduced. The materials of construction, fuel nozzle, and total combustor air flow were unchanged. The differences in NOR emissions between the standard and LHE combustors, as well as the variations in NOR emissions with firing temperature, were well correlated using turbulent flame length arguments. Details of this correlation are also presented. |
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The Pennsylvania State University CiteSeerX Archives |
format |
Text |
author |
Alan S Feitelberg Michael D Starkey Richard B Schiefer Roointon E Pavri Matt Bender John L Booth Gordon R Schmidt British Petroleum Prudhoe Bay Alaska |
spellingShingle |
Alan S Feitelberg Michael D Starkey Richard B Schiefer Roointon E Pavri Matt Bender John L Booth Gordon R Schmidt British Petroleum Prudhoe Bay Alaska PERFORMANCE OF A REDUCED NO x DIFFUSION FLAME COMBUSTOR FOR THE MS5002 GAS TURBINE |
author_facet |
Alan S Feitelberg Michael D Starkey Richard B Schiefer Roointon E Pavri Matt Bender John L Booth Gordon R Schmidt British Petroleum Prudhoe Bay Alaska |
author_sort |
Alan S Feitelberg |
title |
PERFORMANCE OF A REDUCED NO x DIFFUSION FLAME COMBUSTOR FOR THE MS5002 GAS TURBINE |
title_short |
PERFORMANCE OF A REDUCED NO x DIFFUSION FLAME COMBUSTOR FOR THE MS5002 GAS TURBINE |
title_full |
PERFORMANCE OF A REDUCED NO x DIFFUSION FLAME COMBUSTOR FOR THE MS5002 GAS TURBINE |
title_fullStr |
PERFORMANCE OF A REDUCED NO x DIFFUSION FLAME COMBUSTOR FOR THE MS5002 GAS TURBINE |
title_full_unstemmed |
PERFORMANCE OF A REDUCED NO x DIFFUSION FLAME COMBUSTOR FOR THE MS5002 GAS TURBINE |
title_sort |
performance of a reduced no x diffusion flame combustor for the ms5002 gas turbine |
url |
http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.1079.9623 http://proceedings.asmedigitalcollection.asme.org/data/conferences/asmep/81863/v002t02a010-99-gt-058.pdf |
long_lat |
ENVELOPE(159.100,159.100,-79.917,-79.917) |
geographic |
Nozzle |
geographic_facet |
Nozzle |
genre |
Prudhoe Bay Alaska |
genre_facet |
Prudhoe Bay Alaska |
op_source |
http://proceedings.asmedigitalcollection.asme.org/data/conferences/asmep/81863/v002t02a010-99-gt-058.pdf |
op_relation |
http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.1079.9623 http://proceedings.asmedigitalcollection.asme.org/data/conferences/asmep/81863/v002t02a010-99-gt-058.pdf |
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Metadata may be used without restrictions as long as the oai identifier remains attached to it. |
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1766174574060240896 |