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Ambient Temperature Properties of PM (Powder Metal) Aluminum-Titanium Alloys
The structure and properties of dispersion strengthened aluminum 4 and 6 weight percent titanium powder alloys were investigated as candidate materials for high temperature performance. Alloy rod was extruded from vacuum hot pressed billets of helium gas atomized, mechanically alloyed, and atomized...
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creator | Frazier, William E Koczak, Michael J |
description | The structure and properties of dispersion strengthened aluminum 4 and 6 weight percent titanium powder alloys were investigated as candidate materials for high temperature performance. Alloy rod was extruded from vacuum hot pressed billets of helium gas atomized, mechanically alloyed, and atomized plus mechanically alloyed powder. Microstructure and mechanical properties were fully characterized to assess the effect of disperoids on alloy strength, ductility, notch toughness, and modulus. The alloys exhibited low density (2.8g/ cm3), high modulus (85 GPa), good ductility (12%), and strength equivalent to Al-Fe-Ce alloys, e.g., 120 MPa at 250-300 C.
Prepared in collaboration with Drexel Univ., Philadelphia, PA. |
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Prepared in collaboration with Drexel Univ., Philadelphia, PA.</description><language>eng</language><subject>ALLOYS ; ALUMINUM ALLOYS ; BILLETS ; CERIUM ALLOYS ; DUCTILITY ; GASES ; HELIUM ; HIGH TEMPERATURE ; HOT PRESSING ; IRON ALLOYS ; LOW DENSITY ; MECHANICAL PROPERTIES ; Metallurgy and Metallography ; MICROSTRUCTURE ; NOTCH TOUGHNESS ; PE62234N ; POWDER ALLOYS ; POWDER METALS ; RODS ; STRENGTH(GENERAL) ; TEMPERATURE ; TITANIUM ALLOYS ; VACUUM</subject><creationdate>1988</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>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA205997$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Frazier, William E</creatorcontrib><creatorcontrib>Koczak, Michael J</creatorcontrib><creatorcontrib>NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIR VEHICLE AND CREW SYSTEMS TECHNOLOGY DEPT</creatorcontrib><title>Ambient Temperature Properties of PM (Powder Metal) Aluminum-Titanium Alloys</title><description>The structure and properties of dispersion strengthened aluminum 4 and 6 weight percent titanium powder alloys were investigated as candidate materials for high temperature performance. Alloy rod was extruded from vacuum hot pressed billets of helium gas atomized, mechanically alloyed, and atomized plus mechanically alloyed powder. Microstructure and mechanical properties were fully characterized to assess the effect of disperoids on alloy strength, ductility, notch toughness, and modulus. The alloys exhibited low density (2.8g/ cm3), high modulus (85 GPa), good ductility (12%), and strength equivalent to Al-Fe-Ce alloys, e.g., 120 MPa at 250-300 C.
Prepared in collaboration with Drexel Univ., Philadelphia, PA.</description><subject>ALLOYS</subject><subject>ALUMINUM ALLOYS</subject><subject>BILLETS</subject><subject>CERIUM ALLOYS</subject><subject>DUCTILITY</subject><subject>GASES</subject><subject>HELIUM</subject><subject>HIGH TEMPERATURE</subject><subject>HOT PRESSING</subject><subject>IRON ALLOYS</subject><subject>LOW DENSITY</subject><subject>MECHANICAL PROPERTIES</subject><subject>Metallurgy and Metallography</subject><subject>MICROSTRUCTURE</subject><subject>NOTCH TOUGHNESS</subject><subject>PE62234N</subject><subject>POWDER ALLOYS</subject><subject>POWDER METALS</subject><subject>RODS</subject><subject>STRENGTH(GENERAL)</subject><subject>TEMPERATURE</subject><subject>TITANIUM ALLOYS</subject><subject>VACUUM</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1988</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZPBxzE3KTM0rUQhJzS1ILUosKS1KVQgoygeySzJTixXy0xQCfBU0AvLLU1KLFHxTSxJzNBUcc0pzM_NKc3VDMksS8zJLc4EiOfmVxTwMrGmJOcWpvFCam0HGzTXE2UM3pSQzOb64JDMvtSTe0cXRyMDU0tLcmIA0ADCOMkU</recordid><startdate>198806</startdate><enddate>198806</enddate><creator>Frazier, William E</creator><creator>Koczak, Michael J</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>198806</creationdate><title>Ambient Temperature Properties of PM (Powder Metal) Aluminum-Titanium Alloys</title><author>Frazier, William E ; Koczak, Michael J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA2059973</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1988</creationdate><topic>ALLOYS</topic><topic>ALUMINUM ALLOYS</topic><topic>BILLETS</topic><topic>CERIUM ALLOYS</topic><topic>DUCTILITY</topic><topic>GASES</topic><topic>HELIUM</topic><topic>HIGH TEMPERATURE</topic><topic>HOT PRESSING</topic><topic>IRON ALLOYS</topic><topic>LOW DENSITY</topic><topic>MECHANICAL PROPERTIES</topic><topic>Metallurgy and Metallography</topic><topic>MICROSTRUCTURE</topic><topic>NOTCH TOUGHNESS</topic><topic>PE62234N</topic><topic>POWDER ALLOYS</topic><topic>POWDER METALS</topic><topic>RODS</topic><topic>STRENGTH(GENERAL)</topic><topic>TEMPERATURE</topic><topic>TITANIUM ALLOYS</topic><topic>VACUUM</topic><toplevel>online_resources</toplevel><creatorcontrib>Frazier, William E</creatorcontrib><creatorcontrib>Koczak, Michael J</creatorcontrib><creatorcontrib>NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIR VEHICLE AND CREW SYSTEMS TECHNOLOGY DEPT</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Frazier, William E</au><au>Koczak, Michael J</au><aucorp>NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIR VEHICLE AND CREW SYSTEMS TECHNOLOGY DEPT</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Ambient Temperature Properties of PM (Powder Metal) Aluminum-Titanium Alloys</btitle><date>1988-06</date><risdate>1988</risdate><abstract>The structure and properties of dispersion strengthened aluminum 4 and 6 weight percent titanium powder alloys were investigated as candidate materials for high temperature performance. Alloy rod was extruded from vacuum hot pressed billets of helium gas atomized, mechanically alloyed, and atomized plus mechanically alloyed powder. Microstructure and mechanical properties were fully characterized to assess the effect of disperoids on alloy strength, ductility, notch toughness, and modulus. The alloys exhibited low density (2.8g/ cm3), high modulus (85 GPa), good ductility (12%), and strength equivalent to Al-Fe-Ce alloys, e.g., 120 MPa at 250-300 C.
Prepared in collaboration with Drexel Univ., Philadelphia, PA.</abstract><oa>free_for_read</oa></addata></record> |
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source | DTIC Technical Reports |
subjects | ALLOYS ALUMINUM ALLOYS BILLETS CERIUM ALLOYS DUCTILITY GASES HELIUM HIGH TEMPERATURE HOT PRESSING IRON ALLOYS LOW DENSITY MECHANICAL PROPERTIES Metallurgy and Metallography MICROSTRUCTURE NOTCH TOUGHNESS PE62234N POWDER ALLOYS POWDER METALS RODS STRENGTH(GENERAL) TEMPERATURE TITANIUM ALLOYS VACUUM |
title | Ambient Temperature Properties of PM (Powder Metal) Aluminum-Titanium Alloys |
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