Thermal fatigue analysis on cracked plenum barrier plate of open-cycle gas turbine frame

Failure investigation is carried out following repeating findings of several obvious surface-crack spots on the weld joint zone of a plenum barrier plate of open-cycle gas turbine frame. The exhausted hot compressed air will flow through the cracks entering the load compartment which contains temper...

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Main Authors: Rashid A.Z., Purbolaksono J., Ahmad A., Ahmad S.A.
Other Authors: 26326524600
Format: Article
Published: 2023
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spelling my.uniten.dspace-307072023-12-29T15:51:38Z Thermal fatigue analysis on cracked plenum barrier plate of open-cycle gas turbine frame Rashid A.Z. Purbolaksono J. Ahmad A. Ahmad S.A. 26326524600 8621252500 57214160450 57213511577 Cracking Failure analysis Finite element Gas turbine Thermal fatigue Cold storage Compressed air Cracks Failure analysis Gas turbines Microscopic examination Mining Quality assurance Safety factor Thermal fatigue Turbomachinery Visual communication Welds Compressed air Crack initiation Cracks Failure analysis Gas turbines Surface defects Thermal fatigue Welds Failure investigation Finite Element Flowthrough Life expectancies Modified model Original model Plate design Shaft bearing Temperature sensitive Visual inspection Weld joints Failure investigation Fatigue analysis Life expectancies Modified model Open cycle gas turbines Surface cracks Temperature sensitive Visual inspection Finite element method Finite element method Failure investigation is carried out following repeating findings of several obvious surface-crack spots on the weld joint zone of a plenum barrier plate of open-cycle gas turbine frame. The exhausted hot compressed air will flow through the cracks entering the load compartment which contains temperature sensitive instrumentations and shaft bearings. The modified model of the barrier plate is presented for redesign consideration. Visual inspection, microscopic examination on the cracked barrier plate and thermal fatigue analyses based on strain-life approach are carried out. The life expectancies of the original and modified models for the barrier plate design are evaluated. The finding indicates that the modified model could withstand against the thermal fatigue longer than that of the original model. � 2009 Elsevier Ltd. All rights reserved. Final 2023-12-29T07:51:38Z 2023-12-29T07:51:38Z 2010 Article 10.1016/j.engfailanal.2009.10.013 2-s2.0-72949109742 https://www.scopus.com/inward/record.uri?eid=2-s2.0-72949109742&doi=10.1016%2fj.engfailanal.2009.10.013&partnerID=40&md5=13348806e053ed2a611782929bb606c6 https://irepository.uniten.edu.my/handle/123456789/30707 17 2 579 586 Scopus
institution Universiti Tenaga Nasional
building UNITEN Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tenaga Nasional
content_source UNITEN Institutional Repository
url_provider http://dspace.uniten.edu.my/
topic Cracking
Failure analysis
Finite element
Gas turbine
Thermal fatigue
Cold storage
Compressed air
Cracks
Failure analysis
Gas turbines
Microscopic examination
Mining
Quality assurance
Safety factor
Thermal fatigue
Turbomachinery
Visual communication
Welds
Compressed air
Crack initiation
Cracks
Failure analysis
Gas turbines
Surface defects
Thermal fatigue
Welds
Failure investigation
Finite Element
Flowthrough
Life expectancies
Modified model
Original model
Plate design
Shaft bearing
Temperature sensitive
Visual inspection
Weld joints
Failure investigation
Fatigue analysis
Life expectancies
Modified model
Open cycle gas turbines
Surface cracks
Temperature sensitive
Visual inspection
Finite element method
Finite element method
spellingShingle Cracking
Failure analysis
Finite element
Gas turbine
Thermal fatigue
Cold storage
Compressed air
Cracks
Failure analysis
Gas turbines
Microscopic examination
Mining
Quality assurance
Safety factor
Thermal fatigue
Turbomachinery
Visual communication
Welds
Compressed air
Crack initiation
Cracks
Failure analysis
Gas turbines
Surface defects
Thermal fatigue
Welds
Failure investigation
Finite Element
Flowthrough
Life expectancies
Modified model
Original model
Plate design
Shaft bearing
Temperature sensitive
Visual inspection
Weld joints
Failure investigation
Fatigue analysis
Life expectancies
Modified model
Open cycle gas turbines
Surface cracks
Temperature sensitive
Visual inspection
Finite element method
Finite element method
Rashid A.Z.
Purbolaksono J.
Ahmad A.
Ahmad S.A.
Thermal fatigue analysis on cracked plenum barrier plate of open-cycle gas turbine frame
description Failure investigation is carried out following repeating findings of several obvious surface-crack spots on the weld joint zone of a plenum barrier plate of open-cycle gas turbine frame. The exhausted hot compressed air will flow through the cracks entering the load compartment which contains temperature sensitive instrumentations and shaft bearings. The modified model of the barrier plate is presented for redesign consideration. Visual inspection, microscopic examination on the cracked barrier plate and thermal fatigue analyses based on strain-life approach are carried out. The life expectancies of the original and modified models for the barrier plate design are evaluated. The finding indicates that the modified model could withstand against the thermal fatigue longer than that of the original model. � 2009 Elsevier Ltd. All rights reserved.
author2 26326524600
author_facet 26326524600
Rashid A.Z.
Purbolaksono J.
Ahmad A.
Ahmad S.A.
format Article
author Rashid A.Z.
Purbolaksono J.
Ahmad A.
Ahmad S.A.
author_sort Rashid A.Z.
title Thermal fatigue analysis on cracked plenum barrier plate of open-cycle gas turbine frame
title_short Thermal fatigue analysis on cracked plenum barrier plate of open-cycle gas turbine frame
title_full Thermal fatigue analysis on cracked plenum barrier plate of open-cycle gas turbine frame
title_fullStr Thermal fatigue analysis on cracked plenum barrier plate of open-cycle gas turbine frame
title_full_unstemmed Thermal fatigue analysis on cracked plenum barrier plate of open-cycle gas turbine frame
title_sort thermal fatigue analysis on cracked plenum barrier plate of open-cycle gas turbine frame
publishDate 2023
_version_ 1806426669709262848
score 13.222552