Experimental and Numerical Investigations of the Fatigue Life of AA2024 Aluminium Alloy-Based Nanocomposite Reinforced by TiO2 Nanoparticles Under the Effect of Heat Treatment
Using aluminium metal matrix nanocomposites has recently gained increased attention in the industry due to their high strength and ductility. In this paper, TiO 2 nanoparticles in volume percentages of 5 wt. % were added to the AA2024 alloy using the stir casting method. Using a novel powder injecti...
Gespeichert in:
| Veröffentlicht in: | International Journal of Precision Engineering and Manufacturing, 25(1) 2024, 25(1), , pp.141-153 |
|---|---|
| Hauptverfasser: | , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 153 |
|---|---|
| container_issue | 1 |
| container_start_page | 141 |
| container_title | International Journal of Precision Engineering and Manufacturing, 25(1) |
| container_volume | 25 |
| creator | Mahan, Hamid M. Konovalov, S. V. Najm, Sherwan Mohammed Mihaela, Oleksik Trzepieciński, Tomasz |
| description | Using aluminium metal matrix nanocomposites has recently gained increased attention in the industry due to their high strength and ductility. In this paper, TiO
2
nanoparticles in volume percentages of 5 wt. % were added to the AA2024 alloy using the stir casting method. Using a novel powder injection system, TiO
2
nanoparticles with an average particle size of 30 ± 5 nm was added to the matrix. The influence of TiO
2
content on the fatigue life before and after heat treatment was studied. The results showed the fatigue properties of AA2024 with TiO
2
nanoparticles increased after heat treatment. The optimum improvement in fatigue properties was obtained at 5 wt. % TiO
2
after heat treatment, with an improving fatigue life in 14.71% compared with sample based. This is due to an increased number of fine precipitates besides its uniformly distributed after heat treatment. The fatigue life of the composite materials with added nanoparticles was investigated using a finite element-based ANSYS workbench. There was a good match between what happened in the experiments and what happened to the numerical fatigue strength. For the composite materials, the difference between the experimental and numerical values of fatigue strength was not greater than 4% for the matrix. The results also, indicated that, after ageing, the precipitate-free zone at the inter-dendritic zone disappeared or became smaller. However, after adding 5 wt. % of titanium and, also, performing heat treatment, it is not possible to precipitate the Al
2
CuMg precipitates, and, instead of it, the Al
3
TiCu and Al
7
TiCu phases precipitates have been formed. |
| doi_str_mv | 10.1007/s12541-023-00906-4 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_nrf_k</sourceid><recordid>TN_cdi_proquest_journals_2913704110</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2913704110</sourcerecordid><originalsourceid>FETCH-LOGICAL-c349t-9d40d55cd4fddb46a592becadf0d992040dd03148bcd8d6a0eed69f9fd95d67f3</originalsourceid><addsrcrecordid>eNp9UU1r3DAQNaWFhk3-QE-C3gpuZUn2ro5u2DQLSwNhcxayNNqqsSVXskv2V_UvdnZdyK0Xzdebp-G9ovhQ0c8VpesvuWK1qErKeEmppE0p3hRXjNK6FA1lbzFnXJTrWvL3xU3OvqO8Yg2vN81V8Wf7MkLyA4RJ90QHS77PAzYMVrvwG_Lkj3ryMWQSHZl-ALnD8jgD2XsH517bMsoEaft58MHPA2Z9PJVfdQYk0yGaOIwx-wnII_jgYjI46E7k4B_YBTDqNHnTQyZPwUK6_LJ1Dsx05r8HPZFDwvd85HXxzuk-w82_uCqe7raH2_ty__Btd9vuS8OFnEppBbV1baxw1nai0bVkHRhtHbVSMopTiyqITWfsxjaaAthGOumsrG2zdnxVfFp4Q3Lq2XgVtb_EY1TPSbWPh52qKGooGEfwxwU8pvhrRs3UzzingPcpJiu-pqJC7KpgC8qkmHMCp0YUXqcTEqmzkWoxUqGR6mKkErjEl6WM4HCE9Er9n62_W7iiSg</addsrcrecordid><sourcetype>Open Website</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2913704110</pqid></control><display><type>article</type><title>Experimental and Numerical Investigations of the Fatigue Life of AA2024 Aluminium Alloy-Based Nanocomposite Reinforced by TiO2 Nanoparticles Under the Effect of Heat Treatment</title><source>Springer Nature - Complete Springer Journals</source><creator>Mahan, Hamid M. ; Konovalov, S. V. ; Najm, Sherwan Mohammed ; Mihaela, Oleksik ; Trzepieciński, Tomasz</creator><creatorcontrib>Mahan, Hamid M. ; Konovalov, S. V. ; Najm, Sherwan Mohammed ; Mihaela, Oleksik ; Trzepieciński, Tomasz</creatorcontrib><description>Using aluminium metal matrix nanocomposites has recently gained increased attention in the industry due to their high strength and ductility. In this paper, TiO
2
nanoparticles in volume percentages of 5 wt. % were added to the AA2024 alloy using the stir casting method. Using a novel powder injection system, TiO
2
nanoparticles with an average particle size of 30 ± 5 nm was added to the matrix. The influence of TiO
2
content on the fatigue life before and after heat treatment was studied. The results showed the fatigue properties of AA2024 with TiO
2
nanoparticles increased after heat treatment. The optimum improvement in fatigue properties was obtained at 5 wt. % TiO
2
after heat treatment, with an improving fatigue life in 14.71% compared with sample based. This is due to an increased number of fine precipitates besides its uniformly distributed after heat treatment. The fatigue life of the composite materials with added nanoparticles was investigated using a finite element-based ANSYS workbench. There was a good match between what happened in the experiments and what happened to the numerical fatigue strength. For the composite materials, the difference between the experimental and numerical values of fatigue strength was not greater than 4% for the matrix. The results also, indicated that, after ageing, the precipitate-free zone at the inter-dendritic zone disappeared or became smaller. However, after adding 5 wt. % of titanium and, also, performing heat treatment, it is not possible to precipitate the Al
2
CuMg precipitates, and, instead of it, the Al
3
TiCu and Al
7
TiCu phases precipitates have been formed.</description><identifier>ISSN: 2234-7593</identifier><identifier>EISSN: 2005-4602</identifier><identifier>EISSN: 2205-4602</identifier><identifier>DOI: 10.1007/s12541-023-00906-4</identifier><language>eng</language><publisher>Seoul: Korean Society for Precision Engineering</publisher><subject>Aluminum base alloys ; Composite materials ; Engineering ; Fatigue life ; Fatigue strength ; Finite element method ; Heat treating ; Heat treatment ; Industrial and Production Engineering ; Materials Science ; Metal matrix composites ; Nanocomposites ; Nanoparticles ; Precipitate free zone ; Precipitates ; Regular Paper ; Titanium ; Titanium dioxide ; 기계공학</subject><ispartof>International Journal of Precision Engineering and Manufacturing, 2024, 25(1), , pp.141-153</ispartof><rights>The Author(s) 2023</rights><rights>The Author(s) 2023. This work is published under http://creativecommons.org/licenses/by/4.0/ (the “License”). 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><cites>FETCH-LOGICAL-c349t-9d40d55cd4fddb46a592becadf0d992040dd03148bcd8d6a0eed69f9fd95d67f3</cites><orcidid>0000-0003-4809-8660 ; 0000-0003-3412-0716</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s12541-023-00906-4$$EPDF$$P50$$Gspringer$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s12541-023-00906-4$$EHTML$$P50$$Gspringer$$Hfree_for_read</linktohtml><link.rule.ids>314,776,780,27901,27902,41464,42533,51294</link.rule.ids><backlink>$$Uhttps://www.kci.go.kr/kciportal/ci/sereArticleSearch/ciSereArtiView.kci?sereArticleSearchBean.artiId=ART003043900$$DAccess content in National Research Foundation of Korea (NRF)$$Hfree_for_read</backlink></links><search><creatorcontrib>Mahan, Hamid M.</creatorcontrib><creatorcontrib>Konovalov, S. V.</creatorcontrib><creatorcontrib>Najm, Sherwan Mohammed</creatorcontrib><creatorcontrib>Mihaela, Oleksik</creatorcontrib><creatorcontrib>Trzepieciński, Tomasz</creatorcontrib><title>Experimental and Numerical Investigations of the Fatigue Life of AA2024 Aluminium Alloy-Based Nanocomposite Reinforced by TiO2 Nanoparticles Under the Effect of Heat Treatment</title><title>International Journal of Precision Engineering and Manufacturing, 25(1)</title><addtitle>Int. J. Precis. Eng. Manuf</addtitle><description>Using aluminium metal matrix nanocomposites has recently gained increased attention in the industry due to their high strength and ductility. In this paper, TiO
2
nanoparticles in volume percentages of 5 wt. % were added to the AA2024 alloy using the stir casting method. Using a novel powder injection system, TiO
2
nanoparticles with an average particle size of 30 ± 5 nm was added to the matrix. The influence of TiO
2
content on the fatigue life before and after heat treatment was studied. The results showed the fatigue properties of AA2024 with TiO
2
nanoparticles increased after heat treatment. The optimum improvement in fatigue properties was obtained at 5 wt. % TiO
2
after heat treatment, with an improving fatigue life in 14.71% compared with sample based. This is due to an increased number of fine precipitates besides its uniformly distributed after heat treatment. The fatigue life of the composite materials with added nanoparticles was investigated using a finite element-based ANSYS workbench. There was a good match between what happened in the experiments and what happened to the numerical fatigue strength. For the composite materials, the difference between the experimental and numerical values of fatigue strength was not greater than 4% for the matrix. The results also, indicated that, after ageing, the precipitate-free zone at the inter-dendritic zone disappeared or became smaller. However, after adding 5 wt. % of titanium and, also, performing heat treatment, it is not possible to precipitate the Al
2
CuMg precipitates, and, instead of it, the Al
3
TiCu and Al
7
TiCu phases precipitates have been formed.</description><subject>Aluminum base alloys</subject><subject>Composite materials</subject><subject>Engineering</subject><subject>Fatigue life</subject><subject>Fatigue strength</subject><subject>Finite element method</subject><subject>Heat treating</subject><subject>Heat treatment</subject><subject>Industrial and Production Engineering</subject><subject>Materials Science</subject><subject>Metal matrix composites</subject><subject>Nanocomposites</subject><subject>Nanoparticles</subject><subject>Precipitate free zone</subject><subject>Precipitates</subject><subject>Regular Paper</subject><subject>Titanium</subject><subject>Titanium dioxide</subject><subject>기계공학</subject><issn>2234-7593</issn><issn>2005-4602</issn><issn>2205-4602</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>C6C</sourceid><recordid>eNp9UU1r3DAQNaWFhk3-QE-C3gpuZUn2ro5u2DQLSwNhcxayNNqqsSVXskv2V_UvdnZdyK0Xzdebp-G9ovhQ0c8VpesvuWK1qErKeEmppE0p3hRXjNK6FA1lbzFnXJTrWvL3xU3OvqO8Yg2vN81V8Wf7MkLyA4RJ90QHS77PAzYMVrvwG_Lkj3ryMWQSHZl-ALnD8jgD2XsH517bMsoEaft58MHPA2Z9PJVfdQYk0yGaOIwx-wnII_jgYjI46E7k4B_YBTDqNHnTQyZPwUK6_LJ1Dsx05r8HPZFDwvd85HXxzuk-w82_uCqe7raH2_ty__Btd9vuS8OFnEppBbV1baxw1nai0bVkHRhtHbVSMopTiyqITWfsxjaaAthGOumsrG2zdnxVfFp4Q3Lq2XgVtb_EY1TPSbWPh52qKGooGEfwxwU8pvhrRs3UzzingPcpJiu-pqJC7KpgC8qkmHMCp0YUXqcTEqmzkWoxUqGR6mKkErjEl6WM4HCE9Er9n62_W7iiSg</recordid><startdate>2024</startdate><enddate>2024</enddate><creator>Mahan, Hamid M.</creator><creator>Konovalov, S. V.</creator><creator>Najm, Sherwan Mohammed</creator><creator>Mihaela, Oleksik</creator><creator>Trzepieciński, Tomasz</creator><general>Korean Society for Precision Engineering</general><general>Springer Nature B.V</general><general>한국정밀공학회</general><scope>C6C</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>ACYCR</scope><orcidid>https://orcid.org/0000-0003-4809-8660</orcidid><orcidid>https://orcid.org/0000-0003-3412-0716</orcidid></search><sort><creationdate>2024</creationdate><title>Experimental and Numerical Investigations of the Fatigue Life of AA2024 Aluminium Alloy-Based Nanocomposite Reinforced by TiO2 Nanoparticles Under the Effect of Heat Treatment</title><author>Mahan, Hamid M. ; Konovalov, S. V. ; Najm, Sherwan Mohammed ; Mihaela, Oleksik ; Trzepieciński, Tomasz</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c349t-9d40d55cd4fddb46a592becadf0d992040dd03148bcd8d6a0eed69f9fd95d67f3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Aluminum base alloys</topic><topic>Composite materials</topic><topic>Engineering</topic><topic>Fatigue life</topic><topic>Fatigue strength</topic><topic>Finite element method</topic><topic>Heat treating</topic><topic>Heat treatment</topic><topic>Industrial and Production Engineering</topic><topic>Materials Science</topic><topic>Metal matrix composites</topic><topic>Nanocomposites</topic><topic>Nanoparticles</topic><topic>Precipitate free zone</topic><topic>Precipitates</topic><topic>Regular Paper</topic><topic>Titanium</topic><topic>Titanium dioxide</topic><topic>기계공학</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Mahan, Hamid M.</creatorcontrib><creatorcontrib>Konovalov, S. V.</creatorcontrib><creatorcontrib>Najm, Sherwan Mohammed</creatorcontrib><creatorcontrib>Mihaela, Oleksik</creatorcontrib><creatorcontrib>Trzepieciński, Tomasz</creatorcontrib><collection>Springer Nature OA Free Journals</collection><collection>CrossRef</collection><collection>Korean Citation Index</collection><jtitle>International Journal of Precision Engineering and Manufacturing, 25(1)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Mahan, Hamid M.</au><au>Konovalov, S. V.</au><au>Najm, Sherwan Mohammed</au><au>Mihaela, Oleksik</au><au>Trzepieciński, Tomasz</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental and Numerical Investigations of the Fatigue Life of AA2024 Aluminium Alloy-Based Nanocomposite Reinforced by TiO2 Nanoparticles Under the Effect of Heat Treatment</atitle><jtitle>International Journal of Precision Engineering and Manufacturing, 25(1)</jtitle><stitle>Int. J. Precis. Eng. Manuf</stitle><date>2024</date><risdate>2024</risdate><volume>25</volume><issue>1</issue><spage>141</spage><epage>153</epage><pages>141-153</pages><issn>2234-7593</issn><eissn>2005-4602</eissn><eissn>2205-4602</eissn><abstract>Using aluminium metal matrix nanocomposites has recently gained increased attention in the industry due to their high strength and ductility. In this paper, TiO
2
nanoparticles in volume percentages of 5 wt. % were added to the AA2024 alloy using the stir casting method. Using a novel powder injection system, TiO
2
nanoparticles with an average particle size of 30 ± 5 nm was added to the matrix. The influence of TiO
2
content on the fatigue life before and after heat treatment was studied. The results showed the fatigue properties of AA2024 with TiO
2
nanoparticles increased after heat treatment. The optimum improvement in fatigue properties was obtained at 5 wt. % TiO
2
after heat treatment, with an improving fatigue life in 14.71% compared with sample based. This is due to an increased number of fine precipitates besides its uniformly distributed after heat treatment. The fatigue life of the composite materials with added nanoparticles was investigated using a finite element-based ANSYS workbench. There was a good match between what happened in the experiments and what happened to the numerical fatigue strength. For the composite materials, the difference between the experimental and numerical values of fatigue strength was not greater than 4% for the matrix. The results also, indicated that, after ageing, the precipitate-free zone at the inter-dendritic zone disappeared or became smaller. However, after adding 5 wt. % of titanium and, also, performing heat treatment, it is not possible to precipitate the Al
2
CuMg precipitates, and, instead of it, the Al
3
TiCu and Al
7
TiCu phases precipitates have been formed.</abstract><cop>Seoul</cop><pub>Korean Society for Precision Engineering</pub><doi>10.1007/s12541-023-00906-4</doi><tpages>13</tpages><orcidid>https://orcid.org/0000-0003-4809-8660</orcidid><orcidid>https://orcid.org/0000-0003-3412-0716</orcidid><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 2234-7593 |
| ispartof | International Journal of Precision Engineering and Manufacturing, 2024, 25(1), , pp.141-153 |
| issn | 2234-7593 2005-4602 2205-4602 |
| language | eng |
| recordid | cdi_proquest_journals_2913704110 |
| source | Springer Nature - Complete Springer Journals |
| subjects | Aluminum base alloys Composite materials Engineering Fatigue life Fatigue strength Finite element method Heat treating Heat treatment Industrial and Production Engineering Materials Science Metal matrix composites Nanocomposites Nanoparticles Precipitate free zone Precipitates Regular Paper Titanium Titanium dioxide 기계공학 |
| title | Experimental and Numerical Investigations of the Fatigue Life of AA2024 Aluminium Alloy-Based Nanocomposite Reinforced by TiO2 Nanoparticles Under the Effect of Heat Treatment |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-14T12%3A35%3A31IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_nrf_k&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Experimental%20and%20Numerical%20Investigations%20of%20the%20Fatigue%20Life%20of%20AA2024%20Aluminium%20Alloy-Based%20Nanocomposite%20Reinforced%20by%20TiO2%20Nanoparticles%20Under%20the%20Effect%20of%20Heat%20Treatment&rft.jtitle=International%20Journal%20of%20Precision%20Engineering%20and%20Manufacturing,%2025(1)&rft.au=Mahan,%20Hamid%20M.&rft.date=2024&rft.volume=25&rft.issue=1&rft.spage=141&rft.epage=153&rft.pages=141-153&rft.issn=2234-7593&rft.eissn=2005-4602&rft_id=info:doi/10.1007/s12541-023-00906-4&rft_dat=%3Cproquest_nrf_k%3E2913704110%3C/proquest_nrf_k%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2913704110&rft_id=info:pmid/&rfr_iscdi=true |