Loading…
Carburisation layer evolution of Fe-Cr-Ni alloy in furnace after long term service: experimental study and numerical prediction
Owing to high temperature comprehensive properties, Fe-Cr-Ni alloys are designed to operate in corrosive gaseous environments of ethylene pyrolysis furnace. However, most premature failed tubes were caused by carburisation. In the present study, based on the Fick's second law and equilibrium co...
Saved in:
Published in: | Materials at high temperatures 2014-05, Vol.31 (2), p.148-154 |
---|---|
Main Authors: | , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | cdi_FETCH-LOGICAL-c374t-c64de6ff2a141cb7bcfc065fb018d7f89a7b34a4f32015818e24facc5e1b74e73 |
---|---|
cites | cdi_FETCH-LOGICAL-c374t-c64de6ff2a141cb7bcfc065fb018d7f89a7b34a4f32015818e24facc5e1b74e73 |
container_end_page | 154 |
container_issue | 2 |
container_start_page | 148 |
container_title | Materials at high temperatures |
container_volume | 31 |
creator | Shen, L. M. Gong, J. M. Liu, H. S. |
description | Owing to high temperature comprehensive properties, Fe-Cr-Ni alloys are designed to operate in corrosive gaseous environments of ethylene pyrolysis furnace. However, most premature failed tubes were caused by carburisation. In the present study, based on the Fick's second law and equilibrium constant method, study on the carburised layer evolution of HP40Nb and KHR45A alloys by pack carburising experimental investigation and numerical simulation by MATLAB software were carried out. The results show that the experimental and simulated data agree with each other acceptably. The carburising layer rate of KHR45A alloy is much smaller than that of HP40Nb alloy due to higher contents of Cr and Ni element in the former. With increasing operating temperature ranging from 1000 to 1100°C, the maximum service lives of the two alloys sharply decrease. |
doi_str_mv | 10.1179/1878641313Y.0000000002 |
format | article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_1762119997</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>3830366621</sourcerecordid><originalsourceid>FETCH-LOGICAL-c374t-c64de6ff2a141cb7bcfc065fb018d7f89a7b34a4f32015818e24facc5e1b74e73</originalsourceid><addsrcrecordid>eNqFkU1v1DAQhi1EJValfwFZ4sIlxZN445hbtaIFqYJLe-BkTZwxMnLsxU4KOfHXm7AgEBfmMl_PzGj0MvYCxCWA0q-hU10roYHm06X4bfUTttsa1dZ5ynZCt6JqpNDP2EUpvhe11gBSdjv244C5n7MvOPkUecCFMqeHFOafeXL8mqpDrj54jiGkhfvI3ZwjWuLophUOKX7mazDyQvnBW3rD6fuRsh8pThh4meZh4RgHHudxLdu1dsw0eLtdeM7OHIZCF7_8Obu_fnt3eFfdfrx5f7i6rWyj5FTZVg7UOlcjSLC96q2zot27XkA3KNdpVH0jUbqmFrDvoKNaOrR2T9ArSao5Z69Oe485fZ2pTGb0xVIIGCnNxYBqawCt9Ya-_Af9kraPw0bVQrRK7DeqPVE2p1IyOXNcX8a8GBBmk8b8JY35I806eHUa9NGlPOK3lMNgJlxCyi5jtL6Y5j87HgGAdJdb</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1720067057</pqid></control><display><type>article</type><title>Carburisation layer evolution of Fe-Cr-Ni alloy in furnace after long term service: experimental study and numerical prediction</title><source>Taylor and Francis Science and Technology Collection</source><creator>Shen, L. M. ; Gong, J. M. ; Liu, H. S.</creator><creatorcontrib>Shen, L. M. ; Gong, J. M. ; Liu, H. S.</creatorcontrib><description>Owing to high temperature comprehensive properties, Fe-Cr-Ni alloys are designed to operate in corrosive gaseous environments of ethylene pyrolysis furnace. However, most premature failed tubes were caused by carburisation. In the present study, based on the Fick's second law and equilibrium constant method, study on the carburised layer evolution of HP40Nb and KHR45A alloys by pack carburising experimental investigation and numerical simulation by MATLAB software were carried out. The results show that the experimental and simulated data agree with each other acceptably. The carburising layer rate of KHR45A alloy is much smaller than that of HP40Nb alloy due to higher contents of Cr and Ni element in the former. With increasing operating temperature ranging from 1000 to 1100°C, the maximum service lives of the two alloys sharply decrease.</description><identifier>ISSN: 0960-3409</identifier><identifier>EISSN: 1878-6413</identifier><identifier>DOI: 10.1179/1878641313Y.0000000002</identifier><language>eng</language><publisher>Leeds: Taylor & Francis</publisher><subject>Alloying elements ; Austenitic alloy ; Carburisation ; Carburizing ; Computer simulation ; Equilibrium constant method ; Evolution ; Furnaces ; HP40Nb ; KHR45A ; Mathematical models ; MATLAB ; Operating temperature</subject><ispartof>Materials at high temperatures, 2014-05, Vol.31 (2), p.148-154</ispartof><rights>W. S. Maney & Son Ltd. 2014 2014</rights><rights>(©) W. S. Maney & Son Ltd. 2014</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c374t-c64de6ff2a141cb7bcfc065fb018d7f89a7b34a4f32015818e24facc5e1b74e73</citedby><cites>FETCH-LOGICAL-c374t-c64de6ff2a141cb7bcfc065fb018d7f89a7b34a4f32015818e24facc5e1b74e73</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27898,27899</link.rule.ids></links><search><creatorcontrib>Shen, L. M.</creatorcontrib><creatorcontrib>Gong, J. M.</creatorcontrib><creatorcontrib>Liu, H. S.</creatorcontrib><title>Carburisation layer evolution of Fe-Cr-Ni alloy in furnace after long term service: experimental study and numerical prediction</title><title>Materials at high temperatures</title><description>Owing to high temperature comprehensive properties, Fe-Cr-Ni alloys are designed to operate in corrosive gaseous environments of ethylene pyrolysis furnace. However, most premature failed tubes were caused by carburisation. In the present study, based on the Fick's second law and equilibrium constant method, study on the carburised layer evolution of HP40Nb and KHR45A alloys by pack carburising experimental investigation and numerical simulation by MATLAB software were carried out. The results show that the experimental and simulated data agree with each other acceptably. The carburising layer rate of KHR45A alloy is much smaller than that of HP40Nb alloy due to higher contents of Cr and Ni element in the former. With increasing operating temperature ranging from 1000 to 1100°C, the maximum service lives of the two alloys sharply decrease.</description><subject>Alloying elements</subject><subject>Austenitic alloy</subject><subject>Carburisation</subject><subject>Carburizing</subject><subject>Computer simulation</subject><subject>Equilibrium constant method</subject><subject>Evolution</subject><subject>Furnaces</subject><subject>HP40Nb</subject><subject>KHR45A</subject><subject>Mathematical models</subject><subject>MATLAB</subject><subject>Operating temperature</subject><issn>0960-3409</issn><issn>1878-6413</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2014</creationdate><recordtype>article</recordtype><recordid>eNqFkU1v1DAQhi1EJValfwFZ4sIlxZN445hbtaIFqYJLe-BkTZwxMnLsxU4KOfHXm7AgEBfmMl_PzGj0MvYCxCWA0q-hU10roYHm06X4bfUTttsa1dZ5ynZCt6JqpNDP2EUpvhe11gBSdjv244C5n7MvOPkUecCFMqeHFOafeXL8mqpDrj54jiGkhfvI3ZwjWuLophUOKX7mazDyQvnBW3rD6fuRsh8pThh4meZh4RgHHudxLdu1dsw0eLtdeM7OHIZCF7_8Obu_fnt3eFfdfrx5f7i6rWyj5FTZVg7UOlcjSLC96q2zot27XkA3KNdpVH0jUbqmFrDvoKNaOrR2T9ArSao5Z69Oe485fZ2pTGb0xVIIGCnNxYBqawCt9Ya-_Af9kraPw0bVQrRK7DeqPVE2p1IyOXNcX8a8GBBmk8b8JY35I806eHUa9NGlPOK3lMNgJlxCyi5jtL6Y5j87HgGAdJdb</recordid><startdate>20140501</startdate><enddate>20140501</enddate><creator>Shen, L. M.</creator><creator>Gong, J. M.</creator><creator>Liu, H. S.</creator><general>Taylor & Francis</general><general>Taylor & Francis Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>EHMNL</scope><scope>HCIFZ</scope><scope>KB.</scope><scope>PDBOC</scope><scope>PHGZM</scope><scope>PHGZT</scope><scope>PKEHL</scope><scope>PQEST</scope><scope>PQGLB</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>7SE</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>20140501</creationdate><title>Carburisation layer evolution of Fe-Cr-Ni alloy in furnace after long term service: experimental study and numerical prediction</title><author>Shen, L. M. ; Gong, J. M. ; Liu, H. S.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c374t-c64de6ff2a141cb7bcfc065fb018d7f89a7b34a4f32015818e24facc5e1b74e73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2014</creationdate><topic>Alloying elements</topic><topic>Austenitic alloy</topic><topic>Carburisation</topic><topic>Carburizing</topic><topic>Computer simulation</topic><topic>Equilibrium constant method</topic><topic>Evolution</topic><topic>Furnaces</topic><topic>HP40Nb</topic><topic>KHR45A</topic><topic>Mathematical models</topic><topic>MATLAB</topic><topic>Operating temperature</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Shen, L. M.</creatorcontrib><creatorcontrib>Gong, J. M.</creatorcontrib><creatorcontrib>Liu, H. S.</creatorcontrib><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central</collection><collection>UK & Ireland Database</collection><collection>SciTech Premium Collection</collection><collection>Materials Science Database</collection><collection>Materials Science Collection</collection><collection>ProQuest Central (New)</collection><collection>ProQuest One Academic (New)</collection><collection>ProQuest One Academic Middle East (New)</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Applied & Life Sciences</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Corrosion Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Materials at high temperatures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Shen, L. M.</au><au>Gong, J. M.</au><au>Liu, H. S.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Carburisation layer evolution of Fe-Cr-Ni alloy in furnace after long term service: experimental study and numerical prediction</atitle><jtitle>Materials at high temperatures</jtitle><date>2014-05-01</date><risdate>2014</risdate><volume>31</volume><issue>2</issue><spage>148</spage><epage>154</epage><pages>148-154</pages><issn>0960-3409</issn><eissn>1878-6413</eissn><abstract>Owing to high temperature comprehensive properties, Fe-Cr-Ni alloys are designed to operate in corrosive gaseous environments of ethylene pyrolysis furnace. However, most premature failed tubes were caused by carburisation. In the present study, based on the Fick's second law and equilibrium constant method, study on the carburised layer evolution of HP40Nb and KHR45A alloys by pack carburising experimental investigation and numerical simulation by MATLAB software were carried out. The results show that the experimental and simulated data agree with each other acceptably. The carburising layer rate of KHR45A alloy is much smaller than that of HP40Nb alloy due to higher contents of Cr and Ni element in the former. With increasing operating temperature ranging from 1000 to 1100°C, the maximum service lives of the two alloys sharply decrease.</abstract><cop>Leeds</cop><pub>Taylor & Francis</pub><doi>10.1179/1878641313Y.0000000002</doi><tpages>7</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0960-3409 |
ispartof | Materials at high temperatures, 2014-05, Vol.31 (2), p.148-154 |
issn | 0960-3409 1878-6413 |
language | eng |
recordid | cdi_proquest_miscellaneous_1762119997 |
source | Taylor and Francis Science and Technology Collection |
subjects | Alloying elements Austenitic alloy Carburisation Carburizing Computer simulation Equilibrium constant method Evolution Furnaces HP40Nb KHR45A Mathematical models MATLAB Operating temperature |
title | Carburisation layer evolution of Fe-Cr-Ni alloy in furnace after long term service: experimental study and numerical prediction |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-27T00%3A35%3A20IST&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=Carburisation%20layer%20evolution%20of%20Fe-Cr-Ni%20alloy%20in%20furnace%20after%20long%20term%20service:%20experimental%20study%20and%20numerical%20prediction&rft.jtitle=Materials%20at%20high%20temperatures&rft.au=Shen,%20L.%20M.&rft.date=2014-05-01&rft.volume=31&rft.issue=2&rft.spage=148&rft.epage=154&rft.pages=148-154&rft.issn=0960-3409&rft.eissn=1878-6413&rft_id=info:doi/10.1179/1878641313Y.0000000002&rft_dat=%3Cproquest_cross%3E3830366621%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c374t-c64de6ff2a141cb7bcfc065fb018d7f89a7b34a4f32015818e24facc5e1b74e73%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=1720067057&rft_id=info:pmid/&rfr_iscdi=true |