Failure of first stage gas turbine blades

Gas turbine blades must exhibit a high level of resistance to the oxidizing and corrosive environment generated by the combustion gases and be resistant to any associated mechanical failure mechanisms such as erosion. In this paper different types of hot corrosion with their microscopic characterist...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Engineering failure analysis 2004-08, Vol.11 (4), p.589-597
Hauptverfasser: Khajavi, M.R, Shariat, M.H
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 597
container_issue 4
container_start_page 589
container_title Engineering failure analysis
container_volume 11
creator Khajavi, M.R
Shariat, M.H
description Gas turbine blades must exhibit a high level of resistance to the oxidizing and corrosive environment generated by the combustion gases and be resistant to any associated mechanical failure mechanisms such as erosion. In this paper different types of hot corrosion with their microscopic characteristics are reviewed, and a case study on the first stage blades of a GE-F5 gas turbine presented.
doi_str_mv 10.1016/j.engfailanal.2003.08.010
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_28168808</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S1350630703000979</els_id><sourcerecordid>28168808</sourcerecordid><originalsourceid>FETCH-LOGICAL-c350t-4de15f1e6f9d36782e16aac516109cb8b61a843f70e989e5bc2ef1a2bc0776083</originalsourceid><addsrcrecordid>eNqNkDFPwzAQhS0EEqXwH8KCxJBwFzeOPaKKFqRKLDBbjnOuXKVJsRMk_j0uZWBkuje8907vY-wWoUBA8bArqN864zvTm64oAXgBsgCEMzZDWfMclcDzpHkFueBQX7KrGHcAUJcKZ-x-lbJToGxwmfMhjlkczZayrYnZOIXG95Q1nWkpXrMLZ7pIN793zt5XT2_L53zzun5ZPm5ym16M-aIlrByScKrlopYloTDGVigQlG1kI9DIBXc1kJKKqsaW5NCUjYW6FiD5nN2deg9h-Jgojnrvo6UuLaRhirqUKKT8MaqT0YYhxkBOH4Lfm_ClEfQRjt7pP3D0EY4GqROclF2espSWfHoKOlpPvaXWB7Kjbgf_j5ZvObNyOg</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>28168808</pqid></control><display><type>article</type><title>Failure of first stage gas turbine blades</title><source>ScienceDirect Journals (5 years ago - present)</source><creator>Khajavi, M.R ; Shariat, M.H</creator><creatorcontrib>Khajavi, M.R ; Shariat, M.H</creatorcontrib><description>Gas turbine blades must exhibit a high level of resistance to the oxidizing and corrosive environment generated by the combustion gases and be resistant to any associated mechanical failure mechanisms such as erosion. In this paper different types of hot corrosion with their microscopic characteristics are reviewed, and a case study on the first stage blades of a GE-F5 gas turbine presented.</description><identifier>ISSN: 1350-6307</identifier><identifier>EISSN: 1873-1961</identifier><identifier>DOI: 10.1016/j.engfailanal.2003.08.010</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Erosion ; Failure analysis ; Gas turbine blade ; Hot corrosion ; Metallurgical examination</subject><ispartof>Engineering failure analysis, 2004-08, Vol.11 (4), p.589-597</ispartof><rights>2003 Elsevier Ltd</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c350t-4de15f1e6f9d36782e16aac516109cb8b61a843f70e989e5bc2ef1a2bc0776083</citedby><cites>FETCH-LOGICAL-c350t-4de15f1e6f9d36782e16aac516109cb8b61a843f70e989e5bc2ef1a2bc0776083</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.engfailanal.2003.08.010$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,780,784,3550,27924,27925,45995</link.rule.ids></links><search><creatorcontrib>Khajavi, M.R</creatorcontrib><creatorcontrib>Shariat, M.H</creatorcontrib><title>Failure of first stage gas turbine blades</title><title>Engineering failure analysis</title><description>Gas turbine blades must exhibit a high level of resistance to the oxidizing and corrosive environment generated by the combustion gases and be resistant to any associated mechanical failure mechanisms such as erosion. In this paper different types of hot corrosion with their microscopic characteristics are reviewed, and a case study on the first stage blades of a GE-F5 gas turbine presented.</description><subject>Erosion</subject><subject>Failure analysis</subject><subject>Gas turbine blade</subject><subject>Hot corrosion</subject><subject>Metallurgical examination</subject><issn>1350-6307</issn><issn>1873-1961</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2004</creationdate><recordtype>article</recordtype><recordid>eNqNkDFPwzAQhS0EEqXwH8KCxJBwFzeOPaKKFqRKLDBbjnOuXKVJsRMk_j0uZWBkuje8907vY-wWoUBA8bArqN864zvTm64oAXgBsgCEMzZDWfMclcDzpHkFueBQX7KrGHcAUJcKZ-x-lbJToGxwmfMhjlkczZayrYnZOIXG95Q1nWkpXrMLZ7pIN793zt5XT2_L53zzun5ZPm5ym16M-aIlrByScKrlopYloTDGVigQlG1kI9DIBXc1kJKKqsaW5NCUjYW6FiD5nN2deg9h-Jgojnrvo6UuLaRhirqUKKT8MaqT0YYhxkBOH4Lfm_ClEfQRjt7pP3D0EY4GqROclF2espSWfHoKOlpPvaXWB7Kjbgf_j5ZvObNyOg</recordid><startdate>20040801</startdate><enddate>20040801</enddate><creator>Khajavi, M.R</creator><creator>Shariat, M.H</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SE</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope></search><sort><creationdate>20040801</creationdate><title>Failure of first stage gas turbine blades</title><author>Khajavi, M.R ; Shariat, M.H</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c350t-4de15f1e6f9d36782e16aac516109cb8b61a843f70e989e5bc2ef1a2bc0776083</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2004</creationdate><topic>Erosion</topic><topic>Failure analysis</topic><topic>Gas turbine blade</topic><topic>Hot corrosion</topic><topic>Metallurgical examination</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Khajavi, M.R</creatorcontrib><creatorcontrib>Shariat, M.H</creatorcontrib><collection>CrossRef</collection><collection>Corrosion Abstracts</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><jtitle>Engineering failure analysis</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Khajavi, M.R</au><au>Shariat, M.H</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Failure of first stage gas turbine blades</atitle><jtitle>Engineering failure analysis</jtitle><date>2004-08-01</date><risdate>2004</risdate><volume>11</volume><issue>4</issue><spage>589</spage><epage>597</epage><pages>589-597</pages><issn>1350-6307</issn><eissn>1873-1961</eissn><abstract>Gas turbine blades must exhibit a high level of resistance to the oxidizing and corrosive environment generated by the combustion gases and be resistant to any associated mechanical failure mechanisms such as erosion. In this paper different types of hot corrosion with their microscopic characteristics are reviewed, and a case study on the first stage blades of a GE-F5 gas turbine presented.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.engfailanal.2003.08.010</doi><tpages>9</tpages></addata></record>
fulltext fulltext
identifier ISSN: 1350-6307
ispartof Engineering failure analysis, 2004-08, Vol.11 (4), p.589-597
issn 1350-6307
1873-1961
language eng
recordid cdi_proquest_miscellaneous_28168808
source ScienceDirect Journals (5 years ago - present)
subjects Erosion
Failure analysis
Gas turbine blade
Hot corrosion
Metallurgical examination
title Failure of first stage gas turbine blades
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T01%3A04%3A03IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Failure%20of%20first%20stage%20gas%20turbine%20blades&rft.jtitle=Engineering%20failure%20analysis&rft.au=Khajavi,%20M.R&rft.date=2004-08-01&rft.volume=11&rft.issue=4&rft.spage=589&rft.epage=597&rft.pages=589-597&rft.issn=1350-6307&rft.eissn=1873-1961&rft_id=info:doi/10.1016/j.engfailanal.2003.08.010&rft_dat=%3Cproquest_cross%3E28168808%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=28168808&rft_id=info:pmid/&rft_els_id=S1350630703000979&rfr_iscdi=true