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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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 |
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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 |
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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 |
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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. |
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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 |
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2023 |
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1806426669709262848 |
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13.222552 |