Fatigue Behavior of Al-Cu Alloy Subjected to Different Numbers of ECAP Passes
The cast alloy Al‐0.63wt.% Cu was subjected to different number of equal channel angular pressing (ECAP) passes. Fatigue properties and shear bands on the surface of the alloy after fatigue were investigated. It is found that the ECAPed Al‐Cu alloy displays obvious cyclic softening. Meanwhile, multi...
Gespeichert in:
| Veröffentlicht in: | Advanced engineering materials 2007-10, Vol.9 (10), p.860-866 |
|---|---|
| Hauptverfasser: | , , , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 866 |
|---|---|
| container_issue | 10 |
| container_start_page | 860 |
| container_title | Advanced engineering materials |
| container_volume | 9 |
| creator | Fang, D. R. Zhang, P. Duan, Q. Q. Wu, S. D. Zhang, Z. F. Li, J. J. Zhao, N. Q. |
| description | The cast alloy Al‐0.63wt.% Cu was subjected to different number of equal channel angular pressing (ECAP) passes. Fatigue properties and shear bands on the surface of the alloy after fatigue were investigated. It is found that the ECAPed Al‐Cu alloy displays obvious cyclic softening. Meanwhile, multipass ECAP treatment can decrease the shape parameter of hysteresis loops, indicative of a large Bauschinger effect. It is shown that the shear bands orient at about 45° with respect to the cyclic load axis. The current research proves that there is no one‐to‐one relationship between the shear bands induced by fatigue and the shear plane of the last ECAP extrusion, and the orientation of shear bands under fatigue should be parallel to the maximum shear stress plane of the specimen. In addition, it is noted that fatigue cracks can also occur in the area away from shear bands at low number of ECAP passes. |
| doi_str_mv | 10.1002/adem.200700110 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_30832984</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>30832984</sourcerecordid><originalsourceid>FETCH-LOGICAL-c4540-2f16e26e4af96e2a6b61afe24e8be3033533ffe924835db7c8554e18f684ac3e3</originalsourceid><addsrcrecordid>eNqFkEtPwkAUhRujiYhuXXeju-K8O11CeWgCSMTHcjItd7RYKM60Kv_eYom6c3PvWXznnOR43jlGHYwQudILWHUIQiFCGKMDr4U5CQMimDysNaMywIKLY-_EueU3gmnLmwx1mT1X4PfgRb9nhfUL43fzIK7qmxdbf14lS0hLWPhl4fczY8DCuvSn1SoB63b0IO7O_Jl2Dtypd2R07uBs_9vew3BwH18H49vRTdwdBynjDAXEYAFEANMmqoUWicDaAGEgE6CIUk5pXRQRJilfJGEqOWeApRGS6ZQCbXuXTe7GFm8VuFKtMpdCnus1FJVTFElKIslqsNOAqS2cs2DUxmYrbbcKI7VbTe1WUz-r1YaLfbJ2qc6N1es0c7-uCIdScFlzUcN9ZDls_0lV3f5g8rcjaLyZK-Hzx6vtqxIhDbl6mo5U7zGeIzGdqDv6Bfsyi0s</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>30832984</pqid></control><display><type>article</type><title>Fatigue Behavior of Al-Cu Alloy Subjected to Different Numbers of ECAP Passes</title><source>Wiley Online Library Journals Frontfile Complete</source><creator>Fang, D. R. ; Zhang, P. ; Duan, Q. Q. ; Wu, S. D. ; Zhang, Z. F. ; Li, J. J. ; Zhao, N. Q.</creator><creatorcontrib>Fang, D. R. ; Zhang, P. ; Duan, Q. Q. ; Wu, S. D. ; Zhang, Z. F. ; Li, J. J. ; Zhao, N. Q.</creatorcontrib><description>The cast alloy Al‐0.63wt.% Cu was subjected to different number of equal channel angular pressing (ECAP) passes. Fatigue properties and shear bands on the surface of the alloy after fatigue were investigated. It is found that the ECAPed Al‐Cu alloy displays obvious cyclic softening. Meanwhile, multipass ECAP treatment can decrease the shape parameter of hysteresis loops, indicative of a large Bauschinger effect. It is shown that the shear bands orient at about 45° with respect to the cyclic load axis. The current research proves that there is no one‐to‐one relationship between the shear bands induced by fatigue and the shear plane of the last ECAP extrusion, and the orientation of shear bands under fatigue should be parallel to the maximum shear stress plane of the specimen. In addition, it is noted that fatigue cracks can also occur in the area away from shear bands at low number of ECAP passes.</description><identifier>ISSN: 1438-1656</identifier><identifier>EISSN: 1527-2648</identifier><identifier>DOI: 10.1002/adem.200700110</identifier><language>eng</language><publisher>Weinheim: WILEY-VCH Verlag</publisher><subject>Al-Cu alloys ; Condensed matter: structure, mechanical and thermal properties ; Cross-disciplinary physics: materials science; rheology ; Equal channel angular pressing (ECAP) ; Exact sciences and technology ; Fatigue, brittleness, fracture, and cracks ; Materials science ; Mechanical and acoustical properties of condensed matter ; Mechanical properties of solids ; Other heat and thermomechanical treatments ; Physics ; Plastic deformation ; Treatment of materials and its effects on microstructure and properties</subject><ispartof>Advanced engineering materials, 2007-10, Vol.9 (10), p.860-866</ispartof><rights>Copyright © 2007 WILEY‐VCH Verlag GmbH & Co. KGaA, Weinheim</rights><rights>2007 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c4540-2f16e26e4af96e2a6b61afe24e8be3033533ffe924835db7c8554e18f684ac3e3</citedby><cites>FETCH-LOGICAL-c4540-2f16e26e4af96e2a6b61afe24e8be3033533ffe924835db7c8554e18f684ac3e3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1002%2Fadem.200700110$$EPDF$$P50$$Gwiley$$H</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1002%2Fadem.200700110$$EHTML$$P50$$Gwiley$$H</linktohtml><link.rule.ids>314,776,780,1411,27903,27904,45553,45554</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=19178658$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Fang, D. R.</creatorcontrib><creatorcontrib>Zhang, P.</creatorcontrib><creatorcontrib>Duan, Q. Q.</creatorcontrib><creatorcontrib>Wu, S. D.</creatorcontrib><creatorcontrib>Zhang, Z. F.</creatorcontrib><creatorcontrib>Li, J. J.</creatorcontrib><creatorcontrib>Zhao, N. Q.</creatorcontrib><title>Fatigue Behavior of Al-Cu Alloy Subjected to Different Numbers of ECAP Passes</title><title>Advanced engineering materials</title><addtitle>Adv. Eng. Mater</addtitle><description>The cast alloy Al‐0.63wt.% Cu was subjected to different number of equal channel angular pressing (ECAP) passes. Fatigue properties and shear bands on the surface of the alloy after fatigue were investigated. It is found that the ECAPed Al‐Cu alloy displays obvious cyclic softening. Meanwhile, multipass ECAP treatment can decrease the shape parameter of hysteresis loops, indicative of a large Bauschinger effect. It is shown that the shear bands orient at about 45° with respect to the cyclic load axis. The current research proves that there is no one‐to‐one relationship between the shear bands induced by fatigue and the shear plane of the last ECAP extrusion, and the orientation of shear bands under fatigue should be parallel to the maximum shear stress plane of the specimen. In addition, it is noted that fatigue cracks can also occur in the area away from shear bands at low number of ECAP passes.</description><subject>Al-Cu alloys</subject><subject>Condensed matter: structure, mechanical and thermal properties</subject><subject>Cross-disciplinary physics: materials science; rheology</subject><subject>Equal channel angular pressing (ECAP)</subject><subject>Exact sciences and technology</subject><subject>Fatigue, brittleness, fracture, and cracks</subject><subject>Materials science</subject><subject>Mechanical and acoustical properties of condensed matter</subject><subject>Mechanical properties of solids</subject><subject>Other heat and thermomechanical treatments</subject><subject>Physics</subject><subject>Plastic deformation</subject><subject>Treatment of materials and its effects on microstructure and properties</subject><issn>1438-1656</issn><issn>1527-2648</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2007</creationdate><recordtype>article</recordtype><recordid>eNqFkEtPwkAUhRujiYhuXXeju-K8O11CeWgCSMTHcjItd7RYKM60Kv_eYom6c3PvWXznnOR43jlGHYwQudILWHUIQiFCGKMDr4U5CQMimDysNaMywIKLY-_EueU3gmnLmwx1mT1X4PfgRb9nhfUL43fzIK7qmxdbf14lS0hLWPhl4fczY8DCuvSn1SoB63b0IO7O_Jl2Dtypd2R07uBs_9vew3BwH18H49vRTdwdBynjDAXEYAFEANMmqoUWicDaAGEgE6CIUk5pXRQRJilfJGEqOWeApRGS6ZQCbXuXTe7GFm8VuFKtMpdCnus1FJVTFElKIslqsNOAqS2cs2DUxmYrbbcKI7VbTe1WUz-r1YaLfbJ2qc6N1es0c7-uCIdScFlzUcN9ZDls_0lV3f5g8rcjaLyZK-Hzx6vtqxIhDbl6mo5U7zGeIzGdqDv6Bfsyi0s</recordid><startdate>200710</startdate><enddate>200710</enddate><creator>Fang, D. R.</creator><creator>Zhang, P.</creator><creator>Duan, Q. Q.</creator><creator>Wu, S. D.</creator><creator>Zhang, Z. F.</creator><creator>Li, J. J.</creator><creator>Zhao, N. Q.</creator><general>WILEY-VCH Verlag</general><general>WILEY‐VCH Verlag</general><general>Wiley-VCH</general><scope>BSCLL</scope><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>200710</creationdate><title>Fatigue Behavior of Al-Cu Alloy Subjected to Different Numbers of ECAP Passes</title><author>Fang, D. R. ; Zhang, P. ; Duan, Q. Q. ; Wu, S. D. ; Zhang, Z. F. ; Li, J. J. ; Zhao, N. Q.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c4540-2f16e26e4af96e2a6b61afe24e8be3033533ffe924835db7c8554e18f684ac3e3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2007</creationdate><topic>Al-Cu alloys</topic><topic>Condensed matter: structure, mechanical and thermal properties</topic><topic>Cross-disciplinary physics: materials science; rheology</topic><topic>Equal channel angular pressing (ECAP)</topic><topic>Exact sciences and technology</topic><topic>Fatigue, brittleness, fracture, and cracks</topic><topic>Materials science</topic><topic>Mechanical and acoustical properties of condensed matter</topic><topic>Mechanical properties of solids</topic><topic>Other heat and thermomechanical treatments</topic><topic>Physics</topic><topic>Plastic deformation</topic><topic>Treatment of materials and its effects on microstructure and properties</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Fang, D. R.</creatorcontrib><creatorcontrib>Zhang, P.</creatorcontrib><creatorcontrib>Duan, Q. Q.</creatorcontrib><creatorcontrib>Wu, S. D.</creatorcontrib><creatorcontrib>Zhang, Z. F.</creatorcontrib><creatorcontrib>Li, J. J.</creatorcontrib><creatorcontrib>Zhao, N. Q.</creatorcontrib><collection>Istex</collection><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Advanced engineering materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Fang, D. R.</au><au>Zhang, P.</au><au>Duan, Q. Q.</au><au>Wu, S. D.</au><au>Zhang, Z. F.</au><au>Li, J. J.</au><au>Zhao, N. Q.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Fatigue Behavior of Al-Cu Alloy Subjected to Different Numbers of ECAP Passes</atitle><jtitle>Advanced engineering materials</jtitle><addtitle>Adv. Eng. Mater</addtitle><date>2007-10</date><risdate>2007</risdate><volume>9</volume><issue>10</issue><spage>860</spage><epage>866</epage><pages>860-866</pages><issn>1438-1656</issn><eissn>1527-2648</eissn><abstract>The cast alloy Al‐0.63wt.% Cu was subjected to different number of equal channel angular pressing (ECAP) passes. Fatigue properties and shear bands on the surface of the alloy after fatigue were investigated. It is found that the ECAPed Al‐Cu alloy displays obvious cyclic softening. Meanwhile, multipass ECAP treatment can decrease the shape parameter of hysteresis loops, indicative of a large Bauschinger effect. It is shown that the shear bands orient at about 45° with respect to the cyclic load axis. The current research proves that there is no one‐to‐one relationship between the shear bands induced by fatigue and the shear plane of the last ECAP extrusion, and the orientation of shear bands under fatigue should be parallel to the maximum shear stress plane of the specimen. In addition, it is noted that fatigue cracks can also occur in the area away from shear bands at low number of ECAP passes.</abstract><cop>Weinheim</cop><pub>WILEY-VCH Verlag</pub><doi>10.1002/adem.200700110</doi><tpages>7</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1438-1656 |
| ispartof | Advanced engineering materials, 2007-10, Vol.9 (10), p.860-866 |
| issn | 1438-1656 1527-2648 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_30832984 |
| source | Wiley Online Library Journals Frontfile Complete |
| subjects | Al-Cu alloys Condensed matter: structure, mechanical and thermal properties Cross-disciplinary physics: materials science rheology Equal channel angular pressing (ECAP) Exact sciences and technology Fatigue, brittleness, fracture, and cracks Materials science Mechanical and acoustical properties of condensed matter Mechanical properties of solids Other heat and thermomechanical treatments Physics Plastic deformation Treatment of materials and its effects on microstructure and properties |
| title | Fatigue Behavior of Al-Cu Alloy Subjected to Different Numbers of ECAP Passes |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-24T20%3A57%3A04IST&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=Fatigue%20Behavior%20of%20Al-Cu%20Alloy%20Subjected%20to%20Different%20Numbers%20of%20ECAP%20Passes&rft.jtitle=Advanced%20engineering%20materials&rft.au=Fang,%20D.%E2%80%89R.&rft.date=2007-10&rft.volume=9&rft.issue=10&rft.spage=860&rft.epage=866&rft.pages=860-866&rft.issn=1438-1656&rft.eissn=1527-2648&rft_id=info:doi/10.1002/adem.200700110&rft_dat=%3Cproquest_cross%3E30832984%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=30832984&rft_id=info:pmid/&rfr_iscdi=true |