Effect of air-preheating on NOx emissions from a gas turbine combustor

A 76 mm diameter can combustor equipped with a 45° curved-blade radial swirler was used to study the effect of high inlet temperature gas turbine combustion on NOx emission characteristics. High inlet temperature combustion was simulated using preheat air at 400°K, 600°K, 740°K and 900°K. Natur...

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Main Author: Mustafa, Azeman
Format: Article
Language:English
Published: Faculty of Chemical & Natural Resources Engineering 1994
Subjects:
Online Access:http://eprints.utm.my/6639/
http://eprints.utm.my/6639/1/AzemanMustafa1994_EffectOfAirPreheatingOnNOxEmissions.pdf
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author Mustafa, Azeman
author_facet Mustafa, Azeman
author_sort Mustafa, Azeman
building UTeM Institutional Repository
collection Online Access
description A 76 mm diameter can combustor equipped with a 45° curved-blade radial swirler was used to study the effect of high inlet temperature gas turbine combustion on NOx emission characteristics. High inlet temperature combustion was simulated using preheat air at 400°K, 600°K, 740°K and 900°K. Natural gas was investigated using passage injection technique. It was demonstrated that increasing the inlet air temperature significantly widened the weak extinction limit and improved the NOx emission characteristics. An optimum NOx emission of less than 4.5 ppm at 15% oxygen, compatible with 99% efficiency was demonstrated at 900K inlet temperature. It was also demonstrated that with high inlet temperature operation lean well-mixed combustion required for an adequate control of NOx emissions could be achieved. The major conclusion reached is that high inlet temperature combustion could be a promising approach for low NOx emissions with high combustion efficiency and good flame stability.
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spelling utm-66392010-06-01T15:45:18Z http://eprints.utm.my/6639/ Effect of air-preheating on NOx emissions from a gas turbine combustor Mustafa, Azeman T Technology (General) A 76 mm diameter can combustor equipped with a 45° curved-blade radial swirler was used to study the effect of high inlet temperature gas turbine combustion on NOx emission characteristics. High inlet temperature combustion was simulated using preheat air at 400°K, 600°K, 740°K and 900°K. Natural gas was investigated using passage injection technique. It was demonstrated that increasing the inlet air temperature significantly widened the weak extinction limit and improved the NOx emission characteristics. An optimum NOx emission of less than 4.5 ppm at 15% oxygen, compatible with 99% efficiency was demonstrated at 900K inlet temperature. It was also demonstrated that with high inlet temperature operation lean well-mixed combustion required for an adequate control of NOx emissions could be achieved. The major conclusion reached is that high inlet temperature combustion could be a promising approach for low NOx emissions with high combustion efficiency and good flame stability. Faculty of Chemical & Natural Resources Engineering 1994 Article PeerReviewed application/pdf en http://eprints.utm.my/6639/1/AzemanMustafa1994_EffectOfAirPreheatingOnNOxEmissions.pdf Mustafa, Azeman (1994) Effect of air-preheating on NOx emissions from a gas turbine combustor. Buletin FKKKSA, 8 (1). pp. 50-61. ISSN 0128-0740
spellingShingle T Technology (General)
Mustafa, Azeman
Effect of air-preheating on NOx emissions from a gas turbine combustor
title Effect of air-preheating on NOx emissions from a gas turbine combustor
title_full Effect of air-preheating on NOx emissions from a gas turbine combustor
title_fullStr Effect of air-preheating on NOx emissions from a gas turbine combustor
title_full_unstemmed Effect of air-preheating on NOx emissions from a gas turbine combustor
title_short Effect of air-preheating on NOx emissions from a gas turbine combustor
title_sort effect of air-preheating on nox emissions from a gas turbine combustor
topic T Technology (General)
url http://eprints.utm.my/6639/
http://eprints.utm.my/6639/1/AzemanMustafa1994_EffectOfAirPreheatingOnNOxEmissions.pdf