Different effects of multiscale microstructure on fatigue crack growth path and rate in selective laser melted Ti6Al4V
During the selective laser melting (SLM) process of Ti6Al4V, a special structure can be formed with columnar prior β grains along the building direction and fully martensitic α′ within the β grain. To investigate the influence of such special structure on the fatigue crack growth (FCG) rate, Ti6Al4V...
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Veröffentlicht in: | Fatigue & fracture of engineering materials & structures 2022-09, Vol.45 (9), p.2457-2467 |
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description | During the selective laser melting (SLM) process of Ti6Al4V, a special structure can be formed with columnar prior β grains along the building direction and fully martensitic α′ within the β grain. To investigate the influence of such special structure on the fatigue crack growth (FCG) rate, Ti6Al4V specimens fabricated by SLM were heat‐treated at two different temperatures in this study. The columnar grains were retained, and the martensite was decomposed when heat‐treated below the β transus. It is found that all the SLM features were removed when heat‐treated above the β transus. FCG rate tests were subsequently performed at room temperature, and it was found that the prior β grains affected the macroscopic fracture morphology, but there was no discernible influence on the FCG rate. The morphology of the α phase affected the crack growth path and the FCG rate. Changes in the strength‐toughness relationship induced by heat treatment can help understand the decrease in the FCG rate.
Highlights
Heat treatments at two temperatures were used to eliminate SLM features.
The morphology of the α phase affected the fatigue crack growth path and rate.
The strength‐toughness relationship can help to understand the variation of FCG rate. |
doi_str_mv | 10.1111/ffe.13757 |
format | Article |
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Highlights
Heat treatments at two temperatures were used to eliminate SLM features.
The morphology of the α phase affected the fatigue crack growth path and rate.
The strength‐toughness relationship can help to understand the variation of FCG rate.</description><identifier>ISSN: 8756-758X</identifier><identifier>EISSN: 1460-2695</identifier><identifier>DOI: 10.1111/ffe.13757</identifier><language>eng</language><publisher>Oxford: Wiley Subscription Services, Inc</publisher><subject>Columnar structure ; Crack propagation ; fatigue crack growth rate ; Fatigue failure ; Fracture mechanics ; Grains ; Heat treating ; Heat treatment ; Laser beam melting ; Martensite ; microstructure ; Morphology ; Room temperature ; selective laser melting ; strength ; Ti6Al4V ; Titanium base alloys</subject><ispartof>Fatigue & fracture of engineering materials & structures, 2022-09, Vol.45 (9), p.2457-2467</ispartof><rights>2022 John Wiley & Sons Ltd.</rights><rights>2022 Wiley Publishing Ltd.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c2977-4e26c978f6b31814d2ecc82919d04551eae6b7787d51a9ae99e82cb1d1608b193</citedby><cites>FETCH-LOGICAL-c2977-4e26c978f6b31814d2ecc82919d04551eae6b7787d51a9ae99e82cb1d1608b193</cites><orcidid>0000-0002-5475-1470 ; 0000-0002-0907-2110</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1111%2Fffe.13757$$EPDF$$P50$$Gwiley$$H</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1111%2Fffe.13757$$EHTML$$P50$$Gwiley$$H</linktohtml><link.rule.ids>314,776,780,1411,27901,27902,45550,45551</link.rule.ids></links><search><creatorcontrib>Qi, Zhao</creatorcontrib><creatorcontrib>Wang, Bin</creatorcontrib><creatorcontrib>Zhang, Peng</creatorcontrib><creatorcontrib>Liu, Riu</creatorcontrib><creatorcontrib>Zhang, Zhenjun</creatorcontrib><creatorcontrib>Zhang, Zhefeng</creatorcontrib><title>Different effects of multiscale microstructure on fatigue crack growth path and rate in selective laser melted Ti6Al4V</title><title>Fatigue & fracture of engineering materials & structures</title><description>During the selective laser melting (SLM) process of Ti6Al4V, a special structure can be formed with columnar prior β grains along the building direction and fully martensitic α′ within the β grain. To investigate the influence of such special structure on the fatigue crack growth (FCG) rate, Ti6Al4V specimens fabricated by SLM were heat‐treated at two different temperatures in this study. The columnar grains were retained, and the martensite was decomposed when heat‐treated below the β transus. It is found that all the SLM features were removed when heat‐treated above the β transus. FCG rate tests were subsequently performed at room temperature, and it was found that the prior β grains affected the macroscopic fracture morphology, but there was no discernible influence on the FCG rate. The morphology of the α phase affected the crack growth path and the FCG rate. Changes in the strength‐toughness relationship induced by heat treatment can help understand the decrease in the FCG rate.
Highlights
Heat treatments at two temperatures were used to eliminate SLM features.
The morphology of the α phase affected the fatigue crack growth path and rate.
The strength‐toughness relationship can help to understand the variation of FCG rate.</description><subject>Columnar structure</subject><subject>Crack propagation</subject><subject>fatigue crack growth rate</subject><subject>Fatigue failure</subject><subject>Fracture mechanics</subject><subject>Grains</subject><subject>Heat treating</subject><subject>Heat treatment</subject><subject>Laser beam melting</subject><subject>Martensite</subject><subject>microstructure</subject><subject>Morphology</subject><subject>Room temperature</subject><subject>selective laser melting</subject><subject>strength</subject><subject>Ti6Al4V</subject><subject>Titanium base alloys</subject><issn>8756-758X</issn><issn>1460-2695</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp1kD1PwzAQhi0EEqUw8A8sMTGktfPhj7EqFJAqsRTEZjnOpbikSbGdVv33uISVG-5ueN73dC9Ct5RMaKxpXcOEZrzgZ2hEc0aSlMniHI0EL1jCC_Fxia683xBCWZ5lI7R_sFHioA0Y4mKCx12Nt30TrDe6Aby1xnU-uN6E3gHuWlzrYNc9YOO0-cJr1x3CJ97p2HRbYacDYNtiD010s3vAjfbg8BaaABVeWTZr8vdrdFHrxsPN3xyjt8Xjav6cLF-fXuazZWJSyXmSQ8qM5KJmZUYFzasUjBGppLIieVFQ0MBKzgWvCqqlBilBpKakFWVElFRmY3Q3-O5c992DD2rT9a6NJ1UMhudSspRE6n6gTq96B7XaObvV7qgoUadYVYxG_cYa2enAHmwDx_9BtVg8DoofjWJ6Ig</recordid><startdate>202209</startdate><enddate>202209</enddate><creator>Qi, Zhao</creator><creator>Wang, Bin</creator><creator>Zhang, Peng</creator><creator>Liu, Riu</creator><creator>Zhang, Zhenjun</creator><creator>Zhang, Zhefeng</creator><general>Wiley Subscription Services, Inc</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope><orcidid>https://orcid.org/0000-0002-5475-1470</orcidid><orcidid>https://orcid.org/0000-0002-0907-2110</orcidid></search><sort><creationdate>202209</creationdate><title>Different effects of multiscale microstructure on fatigue crack growth path and rate in selective laser melted Ti6Al4V</title><author>Qi, Zhao ; Wang, Bin ; Zhang, Peng ; Liu, Riu ; Zhang, Zhenjun ; Zhang, Zhefeng</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2977-4e26c978f6b31814d2ecc82919d04551eae6b7787d51a9ae99e82cb1d1608b193</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Columnar structure</topic><topic>Crack propagation</topic><topic>fatigue crack growth rate</topic><topic>Fatigue failure</topic><topic>Fracture mechanics</topic><topic>Grains</topic><topic>Heat treating</topic><topic>Heat treatment</topic><topic>Laser beam melting</topic><topic>Martensite</topic><topic>microstructure</topic><topic>Morphology</topic><topic>Room temperature</topic><topic>selective laser melting</topic><topic>strength</topic><topic>Ti6Al4V</topic><topic>Titanium base alloys</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Qi, Zhao</creatorcontrib><creatorcontrib>Wang, Bin</creatorcontrib><creatorcontrib>Zhang, Peng</creatorcontrib><creatorcontrib>Liu, Riu</creatorcontrib><creatorcontrib>Zhang, Zhenjun</creatorcontrib><creatorcontrib>Zhang, Zhefeng</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Fatigue & fracture of engineering materials & structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Qi, Zhao</au><au>Wang, Bin</au><au>Zhang, Peng</au><au>Liu, Riu</au><au>Zhang, Zhenjun</au><au>Zhang, Zhefeng</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Different effects of multiscale microstructure on fatigue crack growth path and rate in selective laser melted Ti6Al4V</atitle><jtitle>Fatigue & fracture of engineering materials & structures</jtitle><date>2022-09</date><risdate>2022</risdate><volume>45</volume><issue>9</issue><spage>2457</spage><epage>2467</epage><pages>2457-2467</pages><issn>8756-758X</issn><eissn>1460-2695</eissn><abstract>During the selective laser melting (SLM) process of Ti6Al4V, a special structure can be formed with columnar prior β grains along the building direction and fully martensitic α′ within the β grain. To investigate the influence of such special structure on the fatigue crack growth (FCG) rate, Ti6Al4V specimens fabricated by SLM were heat‐treated at two different temperatures in this study. The columnar grains were retained, and the martensite was decomposed when heat‐treated below the β transus. It is found that all the SLM features were removed when heat‐treated above the β transus. FCG rate tests were subsequently performed at room temperature, and it was found that the prior β grains affected the macroscopic fracture morphology, but there was no discernible influence on the FCG rate. The morphology of the α phase affected the crack growth path and the FCG rate. Changes in the strength‐toughness relationship induced by heat treatment can help understand the decrease in the FCG rate.
Highlights
Heat treatments at two temperatures were used to eliminate SLM features.
The morphology of the α phase affected the fatigue crack growth path and rate.
The strength‐toughness relationship can help to understand the variation of FCG rate.</abstract><cop>Oxford</cop><pub>Wiley Subscription Services, Inc</pub><doi>10.1111/ffe.13757</doi><tpages>11</tpages><orcidid>https://orcid.org/0000-0002-5475-1470</orcidid><orcidid>https://orcid.org/0000-0002-0907-2110</orcidid></addata></record> |
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source | Wiley Online Library Journals Frontfile Complete |
subjects | Columnar structure Crack propagation fatigue crack growth rate Fatigue failure Fracture mechanics Grains Heat treating Heat treatment Laser beam melting Martensite microstructure Morphology Room temperature selective laser melting strength Ti6Al4V Titanium base alloys |
title | Different effects of multiscale microstructure on fatigue crack growth path and rate in selective laser melted Ti6Al4V |
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