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Development of Economical Sheet Titanium Alloy
The objective of this program was to develop an economical sheet titanium alloy. The approach was to build on the earlier work with emphasis on mill product economics consistent with formability, fabricability, and other properties required by the ultimate user. Including alloys from the earlier con...
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creator | Wardlaw,T L Rosenberg,H W Parris,W M |
description | The objective of this program was to develop an economical sheet titanium alloy. The approach was to build on the earlier work with emphasis on mill product economics consistent with formability, fabricability, and other properties required by the ultimate user. Including alloys from the earlier contracts, more than 60 compositions were evaluated. These were narrowed to three final compositions, Ti-8V-7Cr-3Al-4Sn-1Zr, Ti-8V-4Cr-2Mo-2Fe-3Al, and Ti-15V-3Cr-3Al-3Sn. Further work is recommended on all three. Each alloy exhibits good strip producibility potential while meeting the airframe industries' stated cold minimum bend requirements. Each alloy showed Erichsen cup draw depths exceeding 0.35 in. after simulated strip processing to about .040 in. gage. (Author) |
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The approach was to build on the earlier work with emphasis on mill product economics consistent with formability, fabricability, and other properties required by the ultimate user. Including alloys from the earlier contracts, more than 60 compositions were evaluated. These were narrowed to three final compositions, Ti-8V-7Cr-3Al-4Sn-1Zr, Ti-8V-4Cr-2Mo-2Fe-3Al, and Ti-15V-3Cr-3Al-3Sn. Further work is recommended on all three. Each alloy exhibits good strip producibility potential while meeting the airframe industries' stated cold minimum bend requirements. Each alloy showed Erichsen cup draw depths exceeding 0.35 in. after simulated strip processing to about .040 in. gage. (Author)</description><language>eng</language><subject>AIRFRAMES ; DEFORMATION ; IRON ALLOYS ; MATERIAL FORMING ; Metallurgy and Metallography ; STRAIN HARDENING ; Titanium alloy 3Al 3Cr 3Sn 15V ; Titanium alloy 3Al 4Cr 2Fe 2Mo 8V ; Titanium alloy 3Al 7Cr 4Sn 8V 1Zr ; VANADIUM ALLOYS</subject><creationdate>1973</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0775358$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Wardlaw,T L</creatorcontrib><creatorcontrib>Rosenberg,H W</creatorcontrib><creatorcontrib>Parris,W M</creatorcontrib><creatorcontrib>TITANIUM METALS CORP OF AMERICA HENDERSON NEV</creatorcontrib><title>Development of Economical Sheet Titanium Alloy</title><description>The objective of this program was to develop an economical sheet titanium alloy. The approach was to build on the earlier work with emphasis on mill product economics consistent with formability, fabricability, and other properties required by the ultimate user. Including alloys from the earlier contracts, more than 60 compositions were evaluated. These were narrowed to three final compositions, Ti-8V-7Cr-3Al-4Sn-1Zr, Ti-8V-4Cr-2Mo-2Fe-3Al, and Ti-15V-3Cr-3Al-3Sn. Further work is recommended on all three. Each alloy exhibits good strip producibility potential while meeting the airframe industries' stated cold minimum bend requirements. Each alloy showed Erichsen cup draw depths exceeding 0.35 in. after simulated strip processing to about .040 in. gage. (Author)</description><subject>AIRFRAMES</subject><subject>DEFORMATION</subject><subject>IRON ALLOYS</subject><subject>MATERIAL FORMING</subject><subject>Metallurgy and Metallography</subject><subject>STRAIN HARDENING</subject><subject>Titanium alloy 3Al 3Cr 3Sn 15V</subject><subject>Titanium alloy 3Al 4Cr 2Fe 2Mo 8V</subject><subject>Titanium alloy 3Al 7Cr 4Sn 8V 1Zr</subject><subject>VANADIUM ALLOYS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1973</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZNBzSS1LzckvyE3NK1HIT1NwTc7Py8_NTE7MUQjOSE0tUQjJLEnMyyzNVXDMycmv5GFgTUvMKU7lhdLcDDJuriHOHropJZnJ8cUlmXmpJfGOLgbm5qbGphbGBKQBPqwnbA</recordid><startdate>197312</startdate><enddate>197312</enddate><creator>Wardlaw,T L</creator><creator>Rosenberg,H W</creator><creator>Parris,W M</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>197312</creationdate><title>Development of Economical Sheet Titanium Alloy</title><author>Wardlaw,T L ; Rosenberg,H W ; Parris,W M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD07753583</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1973</creationdate><topic>AIRFRAMES</topic><topic>DEFORMATION</topic><topic>IRON ALLOYS</topic><topic>MATERIAL FORMING</topic><topic>Metallurgy and Metallography</topic><topic>STRAIN HARDENING</topic><topic>Titanium alloy 3Al 3Cr 3Sn 15V</topic><topic>Titanium alloy 3Al 4Cr 2Fe 2Mo 8V</topic><topic>Titanium alloy 3Al 7Cr 4Sn 8V 1Zr</topic><topic>VANADIUM ALLOYS</topic><toplevel>online_resources</toplevel><creatorcontrib>Wardlaw,T L</creatorcontrib><creatorcontrib>Rosenberg,H W</creatorcontrib><creatorcontrib>Parris,W M</creatorcontrib><creatorcontrib>TITANIUM METALS CORP OF AMERICA HENDERSON NEV</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Wardlaw,T L</au><au>Rosenberg,H W</au><au>Parris,W M</au><aucorp>TITANIUM METALS CORP OF AMERICA HENDERSON NEV</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Development of Economical Sheet Titanium Alloy</btitle><date>1973-12</date><risdate>1973</risdate><abstract>The objective of this program was to develop an economical sheet titanium alloy. 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source | DTIC Technical Reports |
subjects | AIRFRAMES DEFORMATION IRON ALLOYS MATERIAL FORMING Metallurgy and Metallography STRAIN HARDENING Titanium alloy 3Al 3Cr 3Sn 15V Titanium alloy 3Al 4Cr 2Fe 2Mo 8V Titanium alloy 3Al 7Cr 4Sn 8V 1Zr VANADIUM ALLOYS |
title | Development of Economical Sheet Titanium Alloy |
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