Improvement of Al-Si Alloy Fatigue Strength by Means of Refining and Modification
The paper presents results of a study concerning an AlSi7Mg alloy and the effect of subjecting the liquid metal to four different processes: conventional refining with hexachloroethane; the same refining followed by modification with titanium, boron, and sodium; refining by purging with argon carrie...
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description | The paper presents results of a study concerning an AlSi7Mg alloy and the effect of subjecting the liquid metal to four different processes: conventional refining with hexachloroethane; the same refining followed by modification with titanium, boron, and sodium; refining by purging with argon carried out in parallel with modification with titanium and boron salts and strontium; and parallel refining with argon and modification with titanium, boron, and sodium salts. The effect of these four processes on compactness of the material, parameters of microstructure, and fatigue strength of AlSi7Mg alloy after heat treatment. It has been found that the highest compactness (the lowest porosity ratio value) and the most favorable values of the examined parameters of microstructure were demonstrated by the alloy obtained with the use of the process including parallel purging with argon and modification with salts of titanium, boron, and sodium. It has been found that in the fatigue cracking process observed in all the four variants of the liquid metal treatment, the crucial role in initiation of fatigue cracks was played by porosity. Application of the process consisting in refining by purging with argon parallel to modification with Ti, B, and Na salts allowed to refine the microstructure and reduce significantly porosity of the alloy extending thus the time of initiation and propagation of fatigue cracks. The ultimate effect consisted in a distinct increase of the fatigue limit value. |
doi_str_mv | 10.24425/afe.2019.129631 |
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The effect of these four processes on compactness of the material, parameters of microstructure, and fatigue strength of AlSi7Mg alloy after heat treatment. It has been found that the highest compactness (the lowest porosity ratio value) and the most favorable values of the examined parameters of microstructure were demonstrated by the alloy obtained with the use of the process including parallel purging with argon and modification with salts of titanium, boron, and sodium. It has been found that in the fatigue cracking process observed in all the four variants of the liquid metal treatment, the crucial role in initiation of fatigue cracks was played by porosity. Application of the process consisting in refining by purging with argon parallel to modification with Ti, B, and Na salts allowed to refine the microstructure and reduce significantly porosity of the alloy extending thus the time of initiation and propagation of fatigue cracks. The ultimate effect consisted in a distinct increase of the fatigue limit value.</description><identifier>ISSN: 1897-3310</identifier><identifier>EISSN: 2299-2944</identifier><identifier>DOI: 10.24425/afe.2019.129631</identifier><language>eng</language><publisher>Katowice: Polish Academy of Sciences</publisher><subject>Aluminum base alloys ; Argon ; Boron ; Crack initiation ; Crack propagation ; Fatigue cracking ; Fatigue cracks ; Fatigue failure ; Fatigue limit ; Fatigue strength ; Fracture mechanics ; Heat treatment ; Hexachloroethane ; Liquid metals ; Metal fatigue ; Microstructure ; Parameters ; Porosity ; Purging ; Silicon ; Sodium ; Sodium salts ; Titanium</subject><ispartof>Archives of foundry engineering, 2019-01, Vol.19 (4), p.61</ispartof><rights>2019. This work is licensed under http://creativecommons.org/licenses/by-nc-nd/3.0/ (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><citedby>FETCH-LOGICAL-c272t-ae56a657fe5c91731fcce8ddf838a2437b3c18c9dd8363280d5dabd1286f161f3</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Tupaj, M</creatorcontrib><creatorcontrib>Orłowicz, A W</creatorcontrib><creatorcontrib>Trytek, A</creatorcontrib><creatorcontrib>Mróz, M</creatorcontrib><title>Improvement of Al-Si Alloy Fatigue Strength by Means of Refining and Modification</title><title>Archives of foundry engineering</title><description>The paper presents results of a study concerning an AlSi7Mg alloy and the effect of subjecting the liquid metal to four different processes: conventional refining with hexachloroethane; the same refining followed by modification with titanium, boron, and sodium; refining by purging with argon carried out in parallel with modification with titanium and boron salts and strontium; and parallel refining with argon and modification with titanium, boron, and sodium salts. The effect of these four processes on compactness of the material, parameters of microstructure, and fatigue strength of AlSi7Mg alloy after heat treatment. It has been found that the highest compactness (the lowest porosity ratio value) and the most favorable values of the examined parameters of microstructure were demonstrated by the alloy obtained with the use of the process including parallel purging with argon and modification with salts of titanium, boron, and sodium. It has been found that in the fatigue cracking process observed in all the four variants of the liquid metal treatment, the crucial role in initiation of fatigue cracks was played by porosity. Application of the process consisting in refining by purging with argon parallel to modification with Ti, B, and Na salts allowed to refine the microstructure and reduce significantly porosity of the alloy extending thus the time of initiation and propagation of fatigue cracks. The ultimate effect consisted in a distinct increase of the fatigue limit value.</description><subject>Aluminum base alloys</subject><subject>Argon</subject><subject>Boron</subject><subject>Crack initiation</subject><subject>Crack propagation</subject><subject>Fatigue cracking</subject><subject>Fatigue cracks</subject><subject>Fatigue failure</subject><subject>Fatigue limit</subject><subject>Fatigue strength</subject><subject>Fracture mechanics</subject><subject>Heat treatment</subject><subject>Hexachloroethane</subject><subject>Liquid metals</subject><subject>Metal fatigue</subject><subject>Microstructure</subject><subject>Parameters</subject><subject>Porosity</subject><subject>Purging</subject><subject>Silicon</subject><subject>Sodium</subject><subject>Sodium salts</subject><subject>Titanium</subject><issn>1897-3310</issn><issn>2299-2944</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNotjk1Lw0AYhBdRMNTePS543ph93-zXsRSrhRbR6rls9iOmpBttEqH_3ojOYebyMDOE3PIih7IEcW9jyKHgJudgJPILkgEYw8CU5SXJuDaKIfLimsz7_lBMElLqEjLysj5-nrrvcAxpoF2ki5btmsnb7kxXdmjqMdDdcAqpHj5odabbYFP_C76G2KQm1dQmT7edb2LjJr5LN-Qq2rYP8_-ckffVw9vyiW2eH9fLxYY5UDAwG4S0UqgYhDNcIY_OBe191KgtlKgqdFw7471GiaALL7ytPActI5c84ozc_fVO_7_G0A_7Qzee0jS5ByEEAiAq_AGlOlH5</recordid><startdate>20190101</startdate><enddate>20190101</enddate><creator>Tupaj, M</creator><creator>Orłowicz, A W</creator><creator>Trytek, A</creator><creator>Mróz, M</creator><general>Polish Academy of Sciences</general><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>DWQXO</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>M7S</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20190101</creationdate><title>Improvement of Al-Si Alloy Fatigue Strength by Means of Refining and Modification</title><author>Tupaj, M ; Orłowicz, A W ; Trytek, A ; Mróz, M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c272t-ae56a657fe5c91731fcce8ddf838a2437b3c18c9dd8363280d5dabd1286f161f3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Aluminum base alloys</topic><topic>Argon</topic><topic>Boron</topic><topic>Crack initiation</topic><topic>Crack propagation</topic><topic>Fatigue cracking</topic><topic>Fatigue cracks</topic><topic>Fatigue failure</topic><topic>Fatigue limit</topic><topic>Fatigue strength</topic><topic>Fracture mechanics</topic><topic>Heat treatment</topic><topic>Hexachloroethane</topic><topic>Liquid metals</topic><topic>Metal fatigue</topic><topic>Microstructure</topic><topic>Parameters</topic><topic>Porosity</topic><topic>Purging</topic><topic>Silicon</topic><topic>Sodium</topic><topic>Sodium salts</topic><topic>Titanium</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Tupaj, M</creatorcontrib><creatorcontrib>Orłowicz, A W</creatorcontrib><creatorcontrib>Trytek, A</creatorcontrib><creatorcontrib>Mróz, M</creatorcontrib><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><jtitle>Archives of foundry engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Tupaj, M</au><au>Orłowicz, A W</au><au>Trytek, A</au><au>Mróz, M</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Improvement of Al-Si Alloy Fatigue Strength by Means of Refining and Modification</atitle><jtitle>Archives of foundry engineering</jtitle><date>2019-01-01</date><risdate>2019</risdate><volume>19</volume><issue>4</issue><spage>61</spage><pages>61-</pages><issn>1897-3310</issn><eissn>2299-2944</eissn><abstract>The paper presents results of a study concerning an AlSi7Mg alloy and the effect of subjecting the liquid metal to four different processes: conventional refining with hexachloroethane; the same refining followed by modification with titanium, boron, and sodium; refining by purging with argon carried out in parallel with modification with titanium and boron salts and strontium; and parallel refining with argon and modification with titanium, boron, and sodium salts. The effect of these four processes on compactness of the material, parameters of microstructure, and fatigue strength of AlSi7Mg alloy after heat treatment. It has been found that the highest compactness (the lowest porosity ratio value) and the most favorable values of the examined parameters of microstructure were demonstrated by the alloy obtained with the use of the process including parallel purging with argon and modification with salts of titanium, boron, and sodium. It has been found that in the fatigue cracking process observed in all the four variants of the liquid metal treatment, the crucial role in initiation of fatigue cracks was played by porosity. Application of the process consisting in refining by purging with argon parallel to modification with Ti, B, and Na salts allowed to refine the microstructure and reduce significantly porosity of the alloy extending thus the time of initiation and propagation of fatigue cracks. The ultimate effect consisted in a distinct increase of the fatigue limit value.</abstract><cop>Katowice</cop><pub>Polish Academy of Sciences</pub><doi>10.24425/afe.2019.129631</doi><oa>free_for_read</oa></addata></record> |
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source | Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals; Alma/SFX Local Collection |
subjects | Aluminum base alloys Argon Boron Crack initiation Crack propagation Fatigue cracking Fatigue cracks Fatigue failure Fatigue limit Fatigue strength Fracture mechanics Heat treatment Hexachloroethane Liquid metals Metal fatigue Microstructure Parameters Porosity Purging Silicon Sodium Sodium salts Titanium |
title | Improvement of Al-Si Alloy Fatigue Strength by Means of Refining and Modification |
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