Effects of performance deterioration on gas path measurements in an industrial gas turbine

Studying gas turbine degradation causes and their consequences helps to obtain profound comprehension in how performance deterioration affects the dependent parameters and to explore relevant information about the nature of the fault signatures for fault diagnostics purpose. In this paper, the effec...

Full description

Saved in:
Bibliographic Details
Main Authors: Amare, D.F., Aklilu, T.B., Gilani, S.I.
Format: Article
Published: Asian Research Publishing Network 2016
Online Access:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85009193746&partnerID=40&md5=4f2fa9150a564c3cea3fd6166f477f3e
http://eprints.utp.edu.my/25326/
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Universiti Teknologi Petronas
id my.utp.eprints.25326
record_format eprints
spelling my.utp.eprints.253262021-08-27T12:57:41Z Effects of performance deterioration on gas path measurements in an industrial gas turbine Amare, D.F. Aklilu, T.B. Gilani, S.I. Studying gas turbine degradation causes and their consequences helps to obtain profound comprehension in how performance deterioration affects the dependent parameters and to explore relevant information about the nature of the fault signatures for fault diagnostics purpose. In this paper, the effects of compressor fouling, gas generator turbine erosion, and power turbine erosion on the engine dependent parameters were considered separately and together. In this regard, firstly, performance prediction model was developed to LM2500 engine using gas turbine simulation program. It was then used to simulate the deterioration effects by means of artificially implanted fault case patterns. Comparison of the clean and deteriorated measurement gives the deviation due to performance degradation. Accordingly, sensitivity order of the gas path parameters to the corresponding performance deterioration was assessed. This helps to select the key parameters, which are crucial in the process of fault detection and isolation. The results showed that, in most of the cases, air mass flow rate, compressor delivery pressure and temperature, gas generator rotational speed, power turbine inlet pressure, and exhaust gas temperature showed significant deviations. Particularly, the compressor delivery pressure and exhaust gas temperature were the parameters highly influenced by all the fault cases. Moreover, faults that have similar impacts are identified, in order to show the difficulty of gas turbine health assessment through direct observation to the measurement deviations. © 2006-2016 Asian Research Publishing Network (ARPN). All rights reserved. Asian Research Publishing Network 2016 Article NonPeerReviewed https://www.scopus.com/inward/record.uri?eid=2-s2.0-85009193746&partnerID=40&md5=4f2fa9150a564c3cea3fd6166f477f3e Amare, D.F. and Aklilu, T.B. and Gilani, S.I. (2016) Effects of performance deterioration on gas path measurements in an industrial gas turbine. ARPN Journal of Engineering and Applied Sciences, 11 (24). pp. 14202-14207. http://eprints.utp.edu.my/25326/
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 Studying gas turbine degradation causes and their consequences helps to obtain profound comprehension in how performance deterioration affects the dependent parameters and to explore relevant information about the nature of the fault signatures for fault diagnostics purpose. In this paper, the effects of compressor fouling, gas generator turbine erosion, and power turbine erosion on the engine dependent parameters were considered separately and together. In this regard, firstly, performance prediction model was developed to LM2500 engine using gas turbine simulation program. It was then used to simulate the deterioration effects by means of artificially implanted fault case patterns. Comparison of the clean and deteriorated measurement gives the deviation due to performance degradation. Accordingly, sensitivity order of the gas path parameters to the corresponding performance deterioration was assessed. This helps to select the key parameters, which are crucial in the process of fault detection and isolation. The results showed that, in most of the cases, air mass flow rate, compressor delivery pressure and temperature, gas generator rotational speed, power turbine inlet pressure, and exhaust gas temperature showed significant deviations. Particularly, the compressor delivery pressure and exhaust gas temperature were the parameters highly influenced by all the fault cases. Moreover, faults that have similar impacts are identified, in order to show the difficulty of gas turbine health assessment through direct observation to the measurement deviations. © 2006-2016 Asian Research Publishing Network (ARPN). All rights reserved.
format Article
author Amare, D.F.
Aklilu, T.B.
Gilani, S.I.
spellingShingle Amare, D.F.
Aklilu, T.B.
Gilani, S.I.
Effects of performance deterioration on gas path measurements in an industrial gas turbine
author_facet Amare, D.F.
Aklilu, T.B.
Gilani, S.I.
author_sort Amare, D.F.
title Effects of performance deterioration on gas path measurements in an industrial gas turbine
title_short Effects of performance deterioration on gas path measurements in an industrial gas turbine
title_full Effects of performance deterioration on gas path measurements in an industrial gas turbine
title_fullStr Effects of performance deterioration on gas path measurements in an industrial gas turbine
title_full_unstemmed Effects of performance deterioration on gas path measurements in an industrial gas turbine
title_sort effects of performance deterioration on gas path measurements in an industrial gas turbine
publisher Asian Research Publishing Network
publishDate 2016
url https://www.scopus.com/inward/record.uri?eid=2-s2.0-85009193746&partnerID=40&md5=4f2fa9150a564c3cea3fd6166f477f3e
http://eprints.utp.edu.my/25326/
_version_ 1738656714369007616