Elevated-Temperature Al Alloys for Aircraft Structure
Elevated-temperature powder metallurgy (P/M) aluminum alloys are being developed to replace titanium aircraft structure materials for operation in the 300-600 F temperature range. Typical mechanical properties of P/M Al-Fe-Ce and Al-Fe-V-Si alloys are superior to those of conventional materials, and...
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| Veröffentlicht in: | J. Met.; (United States) 1988-05, Vol.40 (5), p.16-18 |
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| container_title | J. Met.; (United States) |
| container_volume | 40 |
| creator | Rainen, Richard A. Ekvall, John C. |
| description | Elevated-temperature powder metallurgy (P/M) aluminum alloys are being developed to replace titanium aircraft structure materials for operation in the 300-600 F temperature range. Typical mechanical properties of P/M Al-Fe-Ce and Al-Fe-V-Si alloys are superior to those of conventional materials, and cost savings of 50 to 70 percent have been projected for these alloys which can be fabricated and processed using methods similar to those used in the production of conventional aluminum. 5 references. |
| doi_str_mv | 10.1007/BF03258903 |
| format | Article |
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Typical mechanical properties of P/M Al-Fe-Ce and Al-Fe-V-Si alloys are superior to those of conventional materials, and cost savings of 50 to 70 percent have been projected for these alloys which can be fabricated and processed using methods similar to those used in the production of conventional aluminum. 5 references.</description><identifier>ISSN: 1047-4838</identifier><identifier>EISSN: 1543-1851</identifier><identifier>DOI: 10.1007/BF03258903</identifier><language>eng</language><publisher>United States</publisher><subject>AIRCRAFT ; ALLOYS ; ALUMINIUM ALLOYS ; ALUMINIUM BASE ALLOYS ; CERIUM ALLOYS ; COST ; HEAT RESISTANT MATERIALS ; HEAT RESISTING ALLOYS ; HIGH TEMPERATURE ; IRON ALLOYS ; LITHIUM ALLOYS ; MATERIALS ; MATERIALS SCIENCE ; MECHANICAL PROPERTIES ; METALLURGY ; POWDER METALLURGY ; RARE EARTH ALLOYS 360100 -- Metals & Alloys ; SILICON ALLOYS ; TITANIUM ALLOYS ; USES ; VANADIUM ALLOYS</subject><ispartof>J. 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Met.; (United States)</title><description>Elevated-temperature powder metallurgy (P/M) aluminum alloys are being developed to replace titanium aircraft structure materials for operation in the 300-600 F temperature range. Typical mechanical properties of P/M Al-Fe-Ce and Al-Fe-V-Si alloys are superior to those of conventional materials, and cost savings of 50 to 70 percent have been projected for these alloys which can be fabricated and processed using methods similar to those used in the production of conventional aluminum. 5 references.</description><subject>AIRCRAFT</subject><subject>ALLOYS</subject><subject>ALUMINIUM ALLOYS</subject><subject>ALUMINIUM BASE ALLOYS</subject><subject>CERIUM ALLOYS</subject><subject>COST</subject><subject>HEAT RESISTANT MATERIALS</subject><subject>HEAT RESISTING ALLOYS</subject><subject>HIGH TEMPERATURE</subject><subject>IRON ALLOYS</subject><subject>LITHIUM ALLOYS</subject><subject>MATERIALS</subject><subject>MATERIALS SCIENCE</subject><subject>MECHANICAL PROPERTIES</subject><subject>METALLURGY</subject><subject>POWDER METALLURGY</subject><subject>RARE EARTH ALLOYS 360100 -- Metals & Alloys</subject><subject>SILICON ALLOYS</subject><subject>TITANIUM ALLOYS</subject><subject>USES</subject><subject>VANADIUM ALLOYS</subject><issn>1047-4838</issn><issn>1543-1851</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1988</creationdate><recordtype>article</recordtype><recordid>eNpFkE1LAzEURYMoWKsbf8HgUoi-N_mYl2UtrQoFF9Z1iJkER6adkqRC_71TKggX7l0c7uIwdovwgADN49MSRK3IgDhjE1RScCSF5-MG2XBJgi7ZVc7fMMLS4ISpRR9-XAktX4fNLiRX9ilUs35MPxxyFYdUzbrkk4ulei9p74_ANbuIrs_h5q-n7GO5WM9f-Ort-XU-W3FfK104wmcrJCAarbQm0CTQSN8akk0LtTYKaymcaQNoLw2hU7GJGmtSmkKMYsruTr9DLp3NvivBf_lhuw2-WE2EjTYjdH-CfBpyTiHaXeo2Lh0sgj1asf9WxC9VKlFs</recordid><startdate>198805</startdate><enddate>198805</enddate><creator>Rainen, Richard A.</creator><creator>Ekvall, John C.</creator><scope>AAYXX</scope><scope>CITATION</scope><scope>OTOTI</scope></search><sort><creationdate>198805</creationdate><title>Elevated-Temperature Al Alloys for Aircraft Structure</title><author>Rainen, Richard A. ; Ekvall, John C.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c256t-10bd340119656680683194cd9847d026951243a9de06c4981a5f7f6128568eff3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1988</creationdate><topic>AIRCRAFT</topic><topic>ALLOYS</topic><topic>ALUMINIUM ALLOYS</topic><topic>ALUMINIUM BASE ALLOYS</topic><topic>CERIUM ALLOYS</topic><topic>COST</topic><topic>HEAT RESISTANT MATERIALS</topic><topic>HEAT RESISTING ALLOYS</topic><topic>HIGH TEMPERATURE</topic><topic>IRON ALLOYS</topic><topic>LITHIUM ALLOYS</topic><topic>MATERIALS</topic><topic>MATERIALS SCIENCE</topic><topic>MECHANICAL PROPERTIES</topic><topic>METALLURGY</topic><topic>POWDER METALLURGY</topic><topic>RARE EARTH ALLOYS 360100 -- Metals & Alloys</topic><topic>SILICON ALLOYS</topic><topic>TITANIUM ALLOYS</topic><topic>USES</topic><topic>VANADIUM ALLOYS</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Rainen, Richard A.</creatorcontrib><creatorcontrib>Ekvall, John C.</creatorcontrib><creatorcontrib>Lockheed Aeronautical Systems Co., Sunland, CA (USA)</creatorcontrib><collection>CrossRef</collection><collection>OSTI.GOV</collection><jtitle>J. Met.; (United States)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Rainen, Richard A.</au><au>Ekvall, John C.</au><aucorp>Lockheed Aeronautical Systems Co., Sunland, CA (USA)</aucorp><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Elevated-Temperature Al Alloys for Aircraft Structure</atitle><jtitle>J. Met.; (United States)</jtitle><date>1988-05</date><risdate>1988</risdate><volume>40</volume><issue>5</issue><spage>16</spage><epage>18</epage><pages>16-18</pages><issn>1047-4838</issn><eissn>1543-1851</eissn><abstract>Elevated-temperature powder metallurgy (P/M) aluminum alloys are being developed to replace titanium aircraft structure materials for operation in the 300-600 F temperature range. Typical mechanical properties of P/M Al-Fe-Ce and Al-Fe-V-Si alloys are superior to those of conventional materials, and cost savings of 50 to 70 percent have been projected for these alloys which can be fabricated and processed using methods similar to those used in the production of conventional aluminum. 5 references.</abstract><cop>United States</cop><doi>10.1007/BF03258903</doi><tpages>3</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1047-4838 |
| ispartof | J. Met.; (United States), 1988-05, Vol.40 (5), p.16-18 |
| issn | 1047-4838 1543-1851 |
| language | eng |
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| source | SpringerLink |
| subjects | AIRCRAFT ALLOYS ALUMINIUM ALLOYS ALUMINIUM BASE ALLOYS CERIUM ALLOYS COST HEAT RESISTANT MATERIALS HEAT RESISTING ALLOYS HIGH TEMPERATURE IRON ALLOYS LITHIUM ALLOYS MATERIALS MATERIALS SCIENCE MECHANICAL PROPERTIES METALLURGY POWDER METALLURGY RARE EARTH ALLOYS 360100 -- Metals & Alloys SILICON ALLOYS TITANIUM ALLOYS USES VANADIUM ALLOYS |
| title | Elevated-Temperature Al Alloys for Aircraft Structure |
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