Investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance

Variable geometry gas turbines are susceptible to various malfunctions and performance deterioration phenomena, such as variable inlet guide vane (VIGV) drift, compressor fouling, and high inlet air temperatures. The present study investigates the combined effect of these performance deterioration p...

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Main Authors: Hashmi, M.B., Lemma, T.A., Karim, Z.A.A.
Format: Article
Published: MDPI AG 2019
Online Access:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85079144833&doi=10.3390%2fe21121186&partnerID=40&md5=6f8b1554a295fd249a991af04fbccffb
http://eprints.utp.edu.my/24839/
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spelling my.utp.eprints.248392021-08-27T08:42:29Z Investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance Hashmi, M.B. Lemma, T.A. Karim, Z.A.A. Variable geometry gas turbines are susceptible to various malfunctions and performance deterioration phenomena, such as variable inlet guide vane (VIGV) drift, compressor fouling, and high inlet air temperatures. The present study investigates the combined effect of these performance deterioration phenomena on the health and overall performance of a three-shaft gas turbine engine (GE LM1600). For this purpose, a steady-state simulation model of the turbine was developed using a commercial sof tware named GasTurb 12. In addition, the eect of an inlet air cooling (IAC) technique on the gas turbine performance was examined. The design point results were validated using literature results and data from the manufacturer's catalog. The gas turbine exhibited significant deterioration in power output and thermal efficiency by 21.09 and 7.92, respectively, due to the augmented high inlet air temperature and fouling. However, the integration of the inlet air cooling technique helped in improving the power output, thermal efficiency, and surge margin by 29.67, 7.38, 32.84, respectively. Additionally, the specific fuel consumption (SFC) was reduced by 6.88. The VIGV down-drift schedule has also resulted in improved power output, thermal efficiency, and the surge margin by 14.53, 5.55, and 32.08, respectively, while the SFC decreased by 5.23. The current model can assist in troubleshooting the root cause of performance degradation and surging in an engine faced with VIGV drift and fouling simultaneously. Moreover, the combined study also indicated the optimum schedule during VIGV drift and fouling for performance improvement via the IAC technique. © 2019 The Author(s). MDPI AG 2019 Article NonPeerReviewed https://www.scopus.com/inward/record.uri?eid=2-s2.0-85079144833&doi=10.3390%2fe21121186&partnerID=40&md5=6f8b1554a295fd249a991af04fbccffb Hashmi, M.B. and Lemma, T.A. and Karim, Z.A.A. (2019) Investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance. Entropy, 21 (12). http://eprints.utp.edu.my/24839/
institution Universiti Teknologi Petronas
building UTP Resource Centre
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Petronas
content_source UTP Institutional Repository
url_provider http://eprints.utp.edu.my/
description Variable geometry gas turbines are susceptible to various malfunctions and performance deterioration phenomena, such as variable inlet guide vane (VIGV) drift, compressor fouling, and high inlet air temperatures. The present study investigates the combined effect of these performance deterioration phenomena on the health and overall performance of a three-shaft gas turbine engine (GE LM1600). For this purpose, a steady-state simulation model of the turbine was developed using a commercial sof tware named GasTurb 12. In addition, the eect of an inlet air cooling (IAC) technique on the gas turbine performance was examined. The design point results were validated using literature results and data from the manufacturer's catalog. The gas turbine exhibited significant deterioration in power output and thermal efficiency by 21.09 and 7.92, respectively, due to the augmented high inlet air temperature and fouling. However, the integration of the inlet air cooling technique helped in improving the power output, thermal efficiency, and surge margin by 29.67, 7.38, 32.84, respectively. Additionally, the specific fuel consumption (SFC) was reduced by 6.88. The VIGV down-drift schedule has also resulted in improved power output, thermal efficiency, and the surge margin by 14.53, 5.55, and 32.08, respectively, while the SFC decreased by 5.23. The current model can assist in troubleshooting the root cause of performance degradation and surging in an engine faced with VIGV drift and fouling simultaneously. Moreover, the combined study also indicated the optimum schedule during VIGV drift and fouling for performance improvement via the IAC technique. © 2019 The Author(s).
format Article
author Hashmi, M.B.
Lemma, T.A.
Karim, Z.A.A.
spellingShingle Hashmi, M.B.
Lemma, T.A.
Karim, Z.A.A.
Investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance
author_facet Hashmi, M.B.
Lemma, T.A.
Karim, Z.A.A.
author_sort Hashmi, M.B.
title Investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance
title_short Investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance
title_full Investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance
title_fullStr Investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance
title_full_unstemmed Investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance
title_sort investigation of the combined effect of variable inlet guide vane drift, fouling, and inlet air cooling on gas turbine performance
publisher MDPI AG
publishDate 2019
url https://www.scopus.com/inward/record.uri?eid=2-s2.0-85079144833&doi=10.3390%2fe21121186&partnerID=40&md5=6f8b1554a295fd249a991af04fbccffb
http://eprints.utp.edu.my/24839/
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