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Evaluation of properties and microstructure of non-heat treatable Al-Mg-Li-C-O alloys with variable Li concentration
Fine grained Al-Mg-Li-C alloys, with lithium concentrations from 0.7 to 1.5 wt-%, have been produced by a mechanical alloying-powder metallurgy route. An initial range of compositions was chosen for manufacture into 10 kg billets which were uniaxially forged into plate; subsequently two compositions...
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Published in: | Materials science and technology 2001-06, Vol.17 (6), p.645-650 |
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description | Fine grained Al-Mg-Li-C alloys, with lithium concentrations from 0.7 to 1.5 wt-%, have been produced by a mechanical alloying-powder metallurgy route. An initial range of compositions was chosen for manufacture into 10 kg billets which were uniaxially forged into plate; subsequently two compositions, alloy A (Al-3.7Mg-0.7Li-1.0C (wt-%) and alloy B (Al-4.4Mg-1.4Li-1.0C), were down-selected for a 20 kg scale-up exercise. Billets were forged at 300°C, using an 8:1 reduction ratio, which provided a sufficient level of work to develop properties, while avoiding excessive grain growth. Alloy B exhibited tensile properties (0.2% proof stress 450 MPa; ultimate tensile strength 510 MPa; strain to failure 6%) that exceeded the AECMA specification for AA 5091. Both alloys were confirmed as non-heat treatable and therefore exploitable in the as forged T1 condition. Microstructural analysis has confirmed that a fine grain size ( |
doi_str_mv | 10.1179/026708301101510500 |
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2
O
3
/Al
4
C
3
and MgO dispersoids provided significant Hall-Petch and Orowan strengthening, respectively, capable of increasing the 0.2% proof stress to 450 MPa. Although optimisation of thermomechanical practice is still required, these Al-Mg-Li-C alloys show considerable potential for aerospace, land, and space applications.</description><identifier>ISSN: 0267-0836</identifier><identifier>EISSN: 1743-2847</identifier><identifier>DOI: 10.1179/026708301101510500</identifier><identifier>CODEN: MSCTEP</identifier><language>eng</language><publisher>London, England: Taylor & Francis</publisher><subject>Applied sciences ; Elasticity. Plasticity ; Exact sciences and technology ; Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology ; Metal powders ; Metals. Metallurgy ; Powder metallurgy. Composite materials ; Production techniques</subject><ispartof>Materials science and technology, 2001-06, Vol.17 (6), p.645-650</ispartof><rights>2001 IOM Communications for the Institute of Materials 2001</rights><rights>2001 IOM Communications for the Institute of Materials</rights><rights>2001 INIST-CNRS</rights><rights>Copyright Institute of Materials Jun 2001</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c372t-dd379930da71953d46cfacab4d17cdb24b9336c7b4857ea0dcce7e98dd34559b3</citedby><cites>FETCH-LOGICAL-c372t-dd379930da71953d46cfacab4d17cdb24b9336c7b4857ea0dcce7e98dd34559b3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=1037273$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Vine, W.J.</creatorcontrib><creatorcontrib>Pitcher, P.D.</creatorcontrib><creatorcontrib>Tarrant, A.D.</creatorcontrib><title>Evaluation of properties and microstructure of non-heat treatable Al-Mg-Li-C-O alloys with variable Li concentration</title><title>Materials science and technology</title><description>Fine grained Al-Mg-Li-C alloys, with lithium concentrations from 0.7 to 1.5 wt-%, have been produced by a mechanical alloying-powder metallurgy route. An initial range of compositions was chosen for manufacture into 10 kg billets which were uniaxially forged into plate; subsequently two compositions, alloy A (Al-3.7Mg-0.7Li-1.0C (wt-%) and alloy B (Al-4.4Mg-1.4Li-1.0C), were down-selected for a 20 kg scale-up exercise. Billets were forged at 300°C, using an 8:1 reduction ratio, which provided a sufficient level of work to develop properties, while avoiding excessive grain growth. Alloy B exhibited tensile properties (0.2% proof stress 450 MPa; ultimate tensile strength 510 MPa; strain to failure 6%) that exceeded the AECMA specification for AA 5091. Both alloys were confirmed as non-heat treatable and therefore exploitable in the as forged T1 condition. Microstructural analysis has confirmed that a fine grain size (<1 µm) and nanoscale Al
2
O
3
/Al
4
C
3
and MgO dispersoids provided significant Hall-Petch and Orowan strengthening, respectively, capable of increasing the 0.2% proof stress to 450 MPa. Although optimisation of thermomechanical practice is still required, these Al-Mg-Li-C alloys show considerable potential for aerospace, land, and space applications.</description><subject>Applied sciences</subject><subject>Elasticity. Plasticity</subject><subject>Exact sciences and technology</subject><subject>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</subject><subject>Metal powders</subject><subject>Metals. Metallurgy</subject><subject>Powder metallurgy. 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Plasticity</topic><topic>Exact sciences and technology</topic><topic>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</topic><topic>Metal powders</topic><topic>Metals. Metallurgy</topic><topic>Powder metallurgy. Composite materials</topic><topic>Production techniques</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Vine, W.J.</creatorcontrib><creatorcontrib>Pitcher, P.D.</creatorcontrib><creatorcontrib>Tarrant, A.D.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>ProQuest Central (Corporate)</collection><collection>Engineered Materials Abstracts</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>Science Database (Alumni Edition)</collection><collection>STEM Database</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni) (purchase pre-March 2016)</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 (subscription)</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>ProQuest Central Student</collection><collection>SciTech Premium Collection</collection><collection>Materials Research Database</collection><collection>Materials Science Database</collection><collection>ProQuest Science Journals</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 Basic</collection><collection>SIRS Editorial</collection><collection>Aluminium Industry Abstracts</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Materials science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Vine, W.J.</au><au>Pitcher, P.D.</au><au>Tarrant, A.D.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Evaluation of properties and microstructure of non-heat treatable Al-Mg-Li-C-O alloys with variable Li concentration</atitle><jtitle>Materials science and technology</jtitle><date>2001-06</date><risdate>2001</risdate><volume>17</volume><issue>6</issue><spage>645</spage><epage>650</epage><pages>645-650</pages><issn>0267-0836</issn><eissn>1743-2847</eissn><coden>MSCTEP</coden><abstract>Fine grained Al-Mg-Li-C alloys, with lithium concentrations from 0.7 to 1.5 wt-%, have been produced by a mechanical alloying-powder metallurgy route. An initial range of compositions was chosen for manufacture into 10 kg billets which were uniaxially forged into plate; subsequently two compositions, alloy A (Al-3.7Mg-0.7Li-1.0C (wt-%) and alloy B (Al-4.4Mg-1.4Li-1.0C), were down-selected for a 20 kg scale-up exercise. Billets were forged at 300°C, using an 8:1 reduction ratio, which provided a sufficient level of work to develop properties, while avoiding excessive grain growth. Alloy B exhibited tensile properties (0.2% proof stress 450 MPa; ultimate tensile strength 510 MPa; strain to failure 6%) that exceeded the AECMA specification for AA 5091. Both alloys were confirmed as non-heat treatable and therefore exploitable in the as forged T1 condition. Microstructural analysis has confirmed that a fine grain size (<1 µm) and nanoscale Al
2
O
3
/Al
4
C
3
and MgO dispersoids provided significant Hall-Petch and Orowan strengthening, respectively, capable of increasing the 0.2% proof stress to 450 MPa. Although optimisation of thermomechanical practice is still required, these Al-Mg-Li-C alloys show considerable potential for aerospace, land, and space applications.</abstract><cop>London, England</cop><pub>Taylor & Francis</pub><doi>10.1179/026708301101510500</doi><tpages>6</tpages></addata></record> |
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subjects | Applied sciences Elasticity. Plasticity Exact sciences and technology Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology Metal powders Metals. Metallurgy Powder metallurgy. Composite materials Production techniques |
title | Evaluation of properties and microstructure of non-heat treatable Al-Mg-Li-C-O alloys with variable Li concentration |
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