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Influence of forming method on the tensile and fatigue properties of Ti–6Al–4V sheet for helicopter erosion shield applications
► Two difference forming methods SPF and HSF have been studied. ► The forming method has been shown to have a direct bearing on mechanical properties. ► HSF has been shown exhibit higher static and fatigue properties. ► The factor responsible for the reported differences is primarily microstructural...
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Published in: | Materials in engineering 2012, Vol.33, p.254-263 |
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description | ► Two difference forming methods SPF and HSF have been studied. ► The forming method has been shown to have a direct bearing on mechanical properties. ► HSF has been shown exhibit higher static and fatigue properties. ► The factor responsible for the reported differences is primarily microstructural.
The effect that different forming methods (i.e. hot and super-plastic forming) have on the static, microstructural and fatigue properties of Ti–6Al–4V sheet has been studied. From the test data it is clear that the type of forming method used can have an influence on the resultant static and fatigue properties. Although manufacturing differences used by each forming method preclude direct comparison to be made between forming techniques it would appear high cycle fatigue (HCF) and 0.2% proof stress of Hot Stretch Formed (HSF) annealed Ti–6Al–4V was shown to be on average 20% and 10% higher respectively than that produced by Super Plastic Forming (SPF). Based on the results contained within this paper it would appear that the factors responsible for the observed differences were primarily microstructural, in which the higher the forming temperature employed, the coarser the primary alpha grain size and the lower the resultant static and dynamic properties. |
doi_str_mv | 10.1016/j.matdes.2011.07.011 |
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The effect that different forming methods (i.e. hot and super-plastic forming) have on the static, microstructural and fatigue properties of Ti–6Al–4V sheet has been studied. From the test data it is clear that the type of forming method used can have an influence on the resultant static and fatigue properties. Although manufacturing differences used by each forming method preclude direct comparison to be made between forming techniques it would appear high cycle fatigue (HCF) and 0.2% proof stress of Hot Stretch Formed (HSF) annealed Ti–6Al–4V was shown to be on average 20% and 10% higher respectively than that produced by Super Plastic Forming (SPF). Based on the results contained within this paper it would appear that the factors responsible for the observed differences were primarily microstructural, in which the higher the forming temperature employed, the coarser the primary alpha grain size and the lower the resultant static and dynamic properties.</description><identifier>ISSN: 0261-3069</identifier><identifier>DOI: 10.1016/j.matdes.2011.07.011</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>A. Non-ferrous metals and alloys ; C. Forming ; E. Fatigue ; Fatigue (materials) ; Forming ; Grain size ; High cycle fatigue ; Microstructure ; Proof stress ; Resultants ; Titanium base alloys</subject><ispartof>Materials in engineering, 2012, Vol.33, p.254-263</ispartof><rights>2011 Elsevier Ltd</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c338t-edcaae353d7a7ba76d56e74731552d7c74b84d06effb644247cb5b2bff2a63cf3</citedby><cites>FETCH-LOGICAL-c338t-edcaae353d7a7ba76d56e74731552d7c74b84d06effb644247cb5b2bff2a63cf3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,4009,27902,27903,27904</link.rule.ids></links><search><creatorcontrib>Davies, D.P.</creatorcontrib><creatorcontrib>Jenkins, S.L.</creatorcontrib><title>Influence of forming method on the tensile and fatigue properties of Ti–6Al–4V sheet for helicopter erosion shield applications</title><title>Materials in engineering</title><description>► Two difference forming methods SPF and HSF have been studied. ► The forming method has been shown to have a direct bearing on mechanical properties. ► HSF has been shown exhibit higher static and fatigue properties. ► The factor responsible for the reported differences is primarily microstructural.
The effect that different forming methods (i.e. hot and super-plastic forming) have on the static, microstructural and fatigue properties of Ti–6Al–4V sheet has been studied. From the test data it is clear that the type of forming method used can have an influence on the resultant static and fatigue properties. Although manufacturing differences used by each forming method preclude direct comparison to be made between forming techniques it would appear high cycle fatigue (HCF) and 0.2% proof stress of Hot Stretch Formed (HSF) annealed Ti–6Al–4V was shown to be on average 20% and 10% higher respectively than that produced by Super Plastic Forming (SPF). Based on the results contained within this paper it would appear that the factors responsible for the observed differences were primarily microstructural, in which the higher the forming temperature employed, the coarser the primary alpha grain size and the lower the resultant static and dynamic properties.</description><subject>A. Non-ferrous metals and alloys</subject><subject>C. Forming</subject><subject>E. Fatigue</subject><subject>Fatigue (materials)</subject><subject>Forming</subject><subject>Grain size</subject><subject>High cycle fatigue</subject><subject>Microstructure</subject><subject>Proof stress</subject><subject>Resultants</subject><subject>Titanium base alloys</subject><issn>0261-3069</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2012</creationdate><recordtype>article</recordtype><recordid>eNp9kD1OxDAQhVOAxO8NKNxRbbBjx95tkFYrflZCogFay7HHxKskDrYXiQ6JI3BDToKjUNPMK-a9TzOvKC4ILgkm_GpX9ioZiGWFCSmxKLMcFMe44mRBMV8dFScx7jAmgpDquPjaDrbbw6ABeYusD70bXlEPqfUG-QGlFlCCIboOkBoMsiq51z2gMfgRQnIQp9yT-_n85usuT_aCYguQJhZqoXPajwkCguCjy8DYOugMUuOYVxnmh3hWHFrVRTj_09Pi-fbmaXO_eHi8227WDwtN6TItwGilgNbUCCUaJbipOQgmKKnryggtWLNkBnOwtuGMVUzopm6qxtpKcaotPS0uZ24-_m0PMcneRQ1dpwbw-yhXnC4ZW1GWnWx26nx1DGDlGFyvwockWE41y52ca5ZTzRILmSXHrucY5C_eHQQZtZu6NS6ATtJ49z_gF-pjjyc</recordid><startdate>2012</startdate><enddate>2012</enddate><creator>Davies, D.P.</creator><creator>Jenkins, S.L.</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>H8D</scope><scope>JG9</scope><scope>L7M</scope></search><sort><creationdate>2012</creationdate><title>Influence of forming method on the tensile and fatigue properties of Ti–6Al–4V sheet for helicopter erosion shield applications</title><author>Davies, D.P. ; Jenkins, S.L.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c338t-edcaae353d7a7ba76d56e74731552d7c74b84d06effb644247cb5b2bff2a63cf3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2012</creationdate><topic>A. Non-ferrous metals and alloys</topic><topic>C. Forming</topic><topic>E. Fatigue</topic><topic>Fatigue (materials)</topic><topic>Forming</topic><topic>Grain size</topic><topic>High cycle fatigue</topic><topic>Microstructure</topic><topic>Proof stress</topic><topic>Resultants</topic><topic>Titanium base alloys</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Davies, D.P.</creatorcontrib><creatorcontrib>Jenkins, S.L.</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Materials in engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Davies, D.P.</au><au>Jenkins, S.L.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Influence of forming method on the tensile and fatigue properties of Ti–6Al–4V sheet for helicopter erosion shield applications</atitle><jtitle>Materials in engineering</jtitle><date>2012</date><risdate>2012</risdate><volume>33</volume><spage>254</spage><epage>263</epage><pages>254-263</pages><issn>0261-3069</issn><abstract>► Two difference forming methods SPF and HSF have been studied. ► The forming method has been shown to have a direct bearing on mechanical properties. ► HSF has been shown exhibit higher static and fatigue properties. ► The factor responsible for the reported differences is primarily microstructural.
The effect that different forming methods (i.e. hot and super-plastic forming) have on the static, microstructural and fatigue properties of Ti–6Al–4V sheet has been studied. From the test data it is clear that the type of forming method used can have an influence on the resultant static and fatigue properties. Although manufacturing differences used by each forming method preclude direct comparison to be made between forming techniques it would appear high cycle fatigue (HCF) and 0.2% proof stress of Hot Stretch Formed (HSF) annealed Ti–6Al–4V was shown to be on average 20% and 10% higher respectively than that produced by Super Plastic Forming (SPF). Based on the results contained within this paper it would appear that the factors responsible for the observed differences were primarily microstructural, in which the higher the forming temperature employed, the coarser the primary alpha grain size and the lower the resultant static and dynamic properties.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.matdes.2011.07.011</doi><tpages>10</tpages></addata></record> |
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subjects | A. Non-ferrous metals and alloys C. Forming E. Fatigue Fatigue (materials) Forming Grain size High cycle fatigue Microstructure Proof stress Resultants Titanium base alloys |
title | Influence of forming method on the tensile and fatigue properties of Ti–6Al–4V sheet for helicopter erosion shield applications |
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