CORROSION-RESISTANT CLADDING FOR 7075-T6 ALUMINUM ALLOY
Corrosion of Clad 7075 aircraft alloy prompted the Air Force to sponsor an evaluation of differnt cladding compositions. The objective was to determine if these compositions offered better corrosion resistance than 7072, while providing adequate galvanic protection. Accelerated corrosion tests indic...
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creator | Lowe, Thomas A |
description | Corrosion of Clad 7075 aircraft alloy prompted the Air Force to sponsor an evaluation of differnt cladding compositions. The objective was to determine if these compositions offered better corrosion resistance than 7072, while providing adequate galvanic protection. Accelerated corrosion tests indicate that there are registered aluminum alloys that offer an improvement over 7072. Further work is needed to optimize a composition. |
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The objective was to determine if these compositions offered better corrosion resistance than 7072, while providing adequate galvanic protection. Accelerated corrosion tests indicate that there are registered aluminum alloys that offer an improvement over 7072. Further work is needed to optimize a composition.</description><language>eng</language><subject>ACCELERATED TESTING ; ALUMINUM ALLOY 7075 ; ALUMINUM ALLOYS ; CLADDING ; Coatings, Colorants and Finishes ; CORROSION INHIBITION ; ELECTROCHEMISTRY ; MAGNESIUM ALLOYS ; Properties of Metals and Alloys ; VOLTAGE ; ZINC ALLOYS</subject><creationdate>1967</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,777,882,27548,27549</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0823139$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Lowe, Thomas A</creatorcontrib><creatorcontrib>KAISER ALUMINUM AND CHEMICAL CORP SPOKANE WA DEPT OF METALLURGICAL RESEARCH</creatorcontrib><title>CORROSION-RESISTANT CLADDING FOR 7075-T6 ALUMINUM ALLOY</title><description>Corrosion of Clad 7075 aircraft alloy prompted the Air Force to sponsor an evaluation of differnt cladding compositions. The objective was to determine if these compositions offered better corrosion resistance than 7072, while providing adequate galvanic protection. Accelerated corrosion tests indicate that there are registered aluminum alloys that offer an improvement over 7072. Further work is needed to optimize a composition.</description><subject>ACCELERATED TESTING</subject><subject>ALUMINUM ALLOY 7075</subject><subject>ALUMINUM ALLOYS</subject><subject>CLADDING</subject><subject>Coatings, Colorants and Finishes</subject><subject>CORROSION INHIBITION</subject><subject>ELECTROCHEMISTRY</subject><subject>MAGNESIUM ALLOYS</subject><subject>Properties of Metals and Alloys</subject><subject>VOLTAGE</subject><subject>ZINC ALLOYS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1967</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZDB39g8K8g_29PfTDXIN9gwOcfQLUXD2cXRx8fRzV3DzD1IwNzA31Q0xU3D0CfX19Av1BTJ8_CN5GFjTEnOKU3mhNDeDjJtriLOHbkpJZnJ8cUlmXmpJvKOLgYWRsaGxpTEBaQCdYCUE</recordid><startdate>196705</startdate><enddate>196705</enddate><creator>Lowe, Thomas A</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>196705</creationdate><title>CORROSION-RESISTANT CLADDING FOR 7075-T6 ALUMINUM ALLOY</title><author>Lowe, Thomas A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD08231393</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1967</creationdate><topic>ACCELERATED TESTING</topic><topic>ALUMINUM ALLOY 7075</topic><topic>ALUMINUM ALLOYS</topic><topic>CLADDING</topic><topic>Coatings, Colorants and Finishes</topic><topic>CORROSION INHIBITION</topic><topic>ELECTROCHEMISTRY</topic><topic>MAGNESIUM ALLOYS</topic><topic>Properties of Metals and Alloys</topic><topic>VOLTAGE</topic><topic>ZINC ALLOYS</topic><toplevel>online_resources</toplevel><creatorcontrib>Lowe, Thomas A</creatorcontrib><creatorcontrib>KAISER ALUMINUM AND CHEMICAL CORP SPOKANE WA DEPT OF METALLURGICAL RESEARCH</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Lowe, Thomas A</au><aucorp>KAISER ALUMINUM AND CHEMICAL CORP SPOKANE WA DEPT OF METALLURGICAL RESEARCH</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>CORROSION-RESISTANT CLADDING FOR 7075-T6 ALUMINUM ALLOY</btitle><date>1967-05</date><risdate>1967</risdate><abstract>Corrosion of Clad 7075 aircraft alloy prompted the Air Force to sponsor an evaluation of differnt cladding compositions. The objective was to determine if these compositions offered better corrosion resistance than 7072, while providing adequate galvanic protection. Accelerated corrosion tests indicate that there are registered aluminum alloys that offer an improvement over 7072. Further work is needed to optimize a composition.</abstract><oa>free_for_read</oa></addata></record> |
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source | DTIC Technical Reports |
subjects | ACCELERATED TESTING ALUMINUM ALLOY 7075 ALUMINUM ALLOYS CLADDING Coatings, Colorants and Finishes CORROSION INHIBITION ELECTROCHEMISTRY MAGNESIUM ALLOYS Properties of Metals and Alloys VOLTAGE ZINC ALLOYS |
title | CORROSION-RESISTANT CLADDING FOR 7075-T6 ALUMINUM ALLOY |
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