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Creep Aging Behavior of a Thermo-Mechanical Treated 7B04 Aluminum Alloy
Creep aging behavior of a pre-strain and under-age treated 7B04 aluminum alloy (7B04-P for short) was systematically investigated under different temperatures and applied stresses. A lot of dislocation tangles and η’/GPzs were formed in the Al matrix of the 7B04-P al alloy. With the increase in temp...
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Published in: | Metals (Basel ) 2023-01, Vol.13 (2), p.182 |
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creator | Lao, Shanfeng Zhan, Lihua Qian, Wei Xu, Yongqian Ma, Bolin Liu, Chuhui Huang, Minghui Yang, Youliang Chen, Kuigen Peng, Nanhui Gao, Tuanjie Xi, Hongfei |
description | Creep aging behavior of a pre-strain and under-age treated 7B04 aluminum alloy (7B04-P for short) was systematically investigated under different temperatures and applied stresses. A lot of dislocation tangles and η’/GPzs were formed in the Al matrix of the 7B04-P al alloy. With the increase in temperature and applied stress, the total creep strain and steady-state creep rate increased significantly. However, the mechanical properties of creep-aged 7B04-P al alloy are sensitive to temperature rather than applied stress. The age-hardening precipitates and grain boundaries change obviously when the temperature rises to 160 °C. Compare to the low temperature (less than 160 °C) creep-aged samples, the size of precipitates is much larger, the width of PFZ is broader, and the grain boundary precipitates are more discontinuous and coarsen. As expected, the electrical conductivity is improved after the high-temperature creep aging process at 160 °C. Last but not least, the creep deformation of 7B04-P al alloy almost retains that of AA7B04-T7451. Meanwhile, the mechanical properties after the creep aging process of 7B04-P al alloy are better than that of AA7B04-T7451. It can be suggested that the novel high-temperature creep age forming of the thermo-mechanical treated 7B04 aluminum alloy can enhance the forming efficiency and comprehensive properties for aerospace industries. |
doi_str_mv | 10.3390/met13020182 |
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A lot of dislocation tangles and η’/GPzs were formed in the Al matrix of the 7B04-P al alloy. With the increase in temperature and applied stress, the total creep strain and steady-state creep rate increased significantly. However, the mechanical properties of creep-aged 7B04-P al alloy are sensitive to temperature rather than applied stress. The age-hardening precipitates and grain boundaries change obviously when the temperature rises to 160 °C. Compare to the low temperature (less than 160 °C) creep-aged samples, the size of precipitates is much larger, the width of PFZ is broader, and the grain boundary precipitates are more discontinuous and coarsen. As expected, the electrical conductivity is improved after the high-temperature creep aging process at 160 °C. Last but not least, the creep deformation of 7B04-P al alloy almost retains that of AA7B04-T7451. Meanwhile, the mechanical properties after the creep aging process of 7B04-P al alloy are better than that of AA7B04-T7451. It can be suggested that the novel high-temperature creep age forming of the thermo-mechanical treated 7B04 aluminum alloy can enhance the forming efficiency and comprehensive properties for aerospace industries.</description><identifier>ISSN: 2075-4701</identifier><identifier>EISSN: 2075-4701</identifier><identifier>DOI: 10.3390/met13020182</identifier><language>eng</language><publisher>Basel: MDPI AG</publisher><subject>Aerospace industry ; Age hardening ; Aging (artificial) ; Aircraft ; Al-Zn-Mg-Cu alloy ; Alloys ; Aluminum ; Aluminum alloys ; Aluminum base alloys ; Corrosion resistance ; creep aging forming ; Creep rate ; Creep strength ; Deformation ; dislocation ; Electrical conductivity ; Electrical resistivity ; Grain boundaries ; High temperature ; Hot rolling ; Investigations ; Low temperature ; Mechanical properties ; Microstructure ; Morphology ; precipitate phase ; Precipitates ; Specialty metals industry ; Steady state creep ; Strain ; Strain hardening ; TEM</subject><ispartof>Metals (Basel ), 2023-01, Vol.13 (2), p.182</ispartof><rights>COPYRIGHT 2023 MDPI AG</rights><rights>2023 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c403t-92d84dab054edd00429224a97536404770cbf2df2214b805863438b992d3c6a13</citedby><cites>FETCH-LOGICAL-c403t-92d84dab054edd00429224a97536404770cbf2df2214b805863438b992d3c6a13</cites><orcidid>0000-0001-9419-4149 ; 0000-0002-0401-8019</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.proquest.com/docview/2779533958/fulltextPDF?pq-origsite=primo$$EPDF$$P50$$Gproquest$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://www.proquest.com/docview/2779533958?pq-origsite=primo$$EHTML$$P50$$Gproquest$$Hfree_for_read</linktohtml><link.rule.ids>314,780,784,25753,27924,27925,37012,44590,75126</link.rule.ids></links><search><creatorcontrib>Lao, Shanfeng</creatorcontrib><creatorcontrib>Zhan, Lihua</creatorcontrib><creatorcontrib>Qian, Wei</creatorcontrib><creatorcontrib>Xu, Yongqian</creatorcontrib><creatorcontrib>Ma, Bolin</creatorcontrib><creatorcontrib>Liu, Chuhui</creatorcontrib><creatorcontrib>Huang, Minghui</creatorcontrib><creatorcontrib>Yang, Youliang</creatorcontrib><creatorcontrib>Chen, Kuigen</creatorcontrib><creatorcontrib>Peng, Nanhui</creatorcontrib><creatorcontrib>Gao, Tuanjie</creatorcontrib><creatorcontrib>Xi, Hongfei</creatorcontrib><title>Creep Aging Behavior of a Thermo-Mechanical Treated 7B04 Aluminum Alloy</title><title>Metals (Basel )</title><description>Creep aging behavior of a pre-strain and under-age treated 7B04 aluminum alloy (7B04-P for short) was systematically investigated under different temperatures and applied stresses. A lot of dislocation tangles and η’/GPzs were formed in the Al matrix of the 7B04-P al alloy. With the increase in temperature and applied stress, the total creep strain and steady-state creep rate increased significantly. However, the mechanical properties of creep-aged 7B04-P al alloy are sensitive to temperature rather than applied stress. The age-hardening precipitates and grain boundaries change obviously when the temperature rises to 160 °C. Compare to the low temperature (less than 160 °C) creep-aged samples, the size of precipitates is much larger, the width of PFZ is broader, and the grain boundary precipitates are more discontinuous and coarsen. As expected, the electrical conductivity is improved after the high-temperature creep aging process at 160 °C. Last but not least, the creep deformation of 7B04-P al alloy almost retains that of AA7B04-T7451. Meanwhile, the mechanical properties after the creep aging process of 7B04-P al alloy are better than that of AA7B04-T7451. It can be suggested that the novel high-temperature creep age forming of the thermo-mechanical treated 7B04 aluminum alloy can enhance the forming efficiency and comprehensive properties for aerospace industries.</description><subject>Aerospace industry</subject><subject>Age hardening</subject><subject>Aging (artificial)</subject><subject>Aircraft</subject><subject>Al-Zn-Mg-Cu alloy</subject><subject>Alloys</subject><subject>Aluminum</subject><subject>Aluminum alloys</subject><subject>Aluminum base alloys</subject><subject>Corrosion resistance</subject><subject>creep aging forming</subject><subject>Creep rate</subject><subject>Creep strength</subject><subject>Deformation</subject><subject>dislocation</subject><subject>Electrical conductivity</subject><subject>Electrical resistivity</subject><subject>Grain boundaries</subject><subject>High temperature</subject><subject>Hot rolling</subject><subject>Investigations</subject><subject>Low temperature</subject><subject>Mechanical properties</subject><subject>Microstructure</subject><subject>Morphology</subject><subject>precipitate phase</subject><subject>Precipitates</subject><subject>Specialty metals industry</subject><subject>Steady state creep</subject><subject>Strain</subject><subject>Strain hardening</subject><subject>TEM</subject><issn>2075-4701</issn><issn>2075-4701</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>PIMPY</sourceid><sourceid>DOA</sourceid><recordid>eNpNUU1L5EAQDcsKinryDwQ8SrT6K905joPrCoqX8dxUf830kKRnO5kF_729GxGrDvV4vPcoqqrqisAtYx3cDX4mDCgQRX9UZxSkaLgE8vMbPq0up2kPpRRtoevOqsd19v5Qr7Zx3Nb3fod_Y8p1CjXWm53PQ2pevN3hGC329SZ7nL2r5T3wetUfhzgehwL69H5RnQTsJ3_5Oc-rt18Pm_Xv5vn18Wm9em4sBzY3HXWKOzQguHcOgNOOUo6dFKzlwKUEawJ1gVLCjQKhWsaZMl3xMdsiYefV05LrEu71IccB87tOGPV_IuWtxjxH23utsBWItLVeBG6CUQGZs6hMawhhwpSs6yXrkNOfo59mvU_HPJb1NZWyE-WqQhXV7aLaYgmNY0hzRlva-SHaNPoQC7-SnBHVLoabxWBzmqbsw9eaBPS_T-lvn2IfZNCCUQ</recordid><startdate>20230101</startdate><enddate>20230101</enddate><creator>Lao, Shanfeng</creator><creator>Zhan, Lihua</creator><creator>Qian, Wei</creator><creator>Xu, Yongqian</creator><creator>Ma, Bolin</creator><creator>Liu, Chuhui</creator><creator>Huang, Minghui</creator><creator>Yang, Youliang</creator><creator>Chen, Kuigen</creator><creator>Peng, Nanhui</creator><creator>Gao, Tuanjie</creator><creator>Xi, Hongfei</creator><general>MDPI AG</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8BQ</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>JG9</scope><scope>KB.</scope><scope>PDBOC</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>DOA</scope><orcidid>https://orcid.org/0000-0001-9419-4149</orcidid><orcidid>https://orcid.org/0000-0002-0401-8019</orcidid></search><sort><creationdate>20230101</creationdate><title>Creep Aging Behavior of a Thermo-Mechanical Treated 7B04 Aluminum Alloy</title><author>Lao, Shanfeng ; 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A lot of dislocation tangles and η’/GPzs were formed in the Al matrix of the 7B04-P al alloy. With the increase in temperature and applied stress, the total creep strain and steady-state creep rate increased significantly. However, the mechanical properties of creep-aged 7B04-P al alloy are sensitive to temperature rather than applied stress. The age-hardening precipitates and grain boundaries change obviously when the temperature rises to 160 °C. Compare to the low temperature (less than 160 °C) creep-aged samples, the size of precipitates is much larger, the width of PFZ is broader, and the grain boundary precipitates are more discontinuous and coarsen. As expected, the electrical conductivity is improved after the high-temperature creep aging process at 160 °C. Last but not least, the creep deformation of 7B04-P al alloy almost retains that of AA7B04-T7451. Meanwhile, the mechanical properties after the creep aging process of 7B04-P al alloy are better than that of AA7B04-T7451. It can be suggested that the novel high-temperature creep age forming of the thermo-mechanical treated 7B04 aluminum alloy can enhance the forming efficiency and comprehensive properties for aerospace industries.</abstract><cop>Basel</cop><pub>MDPI AG</pub><doi>10.3390/met13020182</doi><orcidid>https://orcid.org/0000-0001-9419-4149</orcidid><orcidid>https://orcid.org/0000-0002-0401-8019</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Aerospace industry Age hardening Aging (artificial) Aircraft Al-Zn-Mg-Cu alloy Alloys Aluminum Aluminum alloys Aluminum base alloys Corrosion resistance creep aging forming Creep rate Creep strength Deformation dislocation Electrical conductivity Electrical resistivity Grain boundaries High temperature Hot rolling Investigations Low temperature Mechanical properties Microstructure Morphology precipitate phase Precipitates Specialty metals industry Steady state creep Strain Strain hardening TEM |
title | Creep Aging Behavior of a Thermo-Mechanical Treated 7B04 Aluminum Alloy |
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