Aircraft structural member made of an Al-Cu-Mg alloy
The invention relates to a work-hardened product, particularly a rolled, extruded or forged product, made of an alloy with the following composition (% by weight): Cu 3.8-4.3; Mg 1.25-1.45; Mn 0.2-0.5; Zn 0.4-1.3; Fe
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creator | BES BERNARD WARNER TIMOTHY DIF RONAN RIBES HERVE |
description | The invention relates to a work-hardened product, particularly a rolled, extruded or forged product, made of an alloy with the following composition (% by weight): Cu 3.8-4.3; Mg 1.25-1.45; Mn 0.2-0.5; Zn 0.4-1.3; Fe |
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Cold strain-hardening can be achieved by controlled tension and/or cold transformation, for example rolling, die forging or drawing. 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Cold strain-hardening can be achieved by controlled tension and/or cold transformation, for example rolling, die forging or drawing. This cladded metal plate type product is a suitable element to be used as aircraft fuselage skin.</description><subject>ALLOYS</subject><subject>CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS</subject><subject>CHEMISTRY</subject><subject>FERROUS OR NON-FERROUS ALLOYS</subject><subject>METALLURGY</subject><subject>TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDBxzCxKLkpMK1EoLikqTS4pLUrMUchNzU1KLVLITUxJVchPU0jMU3DM0XUu1fVNV0jMycmv5GFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8aHB5paWxibmJk5GxkQoAQCGCSuv</recordid><startdate>20110809</startdate><enddate>20110809</enddate><creator>BES BERNARD</creator><creator>WARNER TIMOTHY</creator><creator>DIF RONAN</creator><creator>RIBES HERVE</creator><scope>EVB</scope></search><sort><creationdate>20110809</creationdate><title>Aircraft structural member made of an Al-Cu-Mg alloy</title><author>BES BERNARD ; WARNER TIMOTHY ; DIF RONAN ; RIBES HERVE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US7993474B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2011</creationdate><topic>ALLOYS</topic><topic>CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS</topic><topic>CHEMISTRY</topic><topic>FERROUS OR NON-FERROUS ALLOYS</topic><topic>METALLURGY</topic><topic>TREATMENT OF ALLOYS OR NON-FERROUS METALS</topic><toplevel>online_resources</toplevel><creatorcontrib>BES BERNARD</creatorcontrib><creatorcontrib>WARNER TIMOTHY</creatorcontrib><creatorcontrib>DIF RONAN</creatorcontrib><creatorcontrib>RIBES HERVE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BES BERNARD</au><au>WARNER TIMOTHY</au><au>DIF RONAN</au><au>RIBES HERVE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft structural member made of an Al-Cu-Mg alloy</title><date>2011-08-09</date><risdate>2011</risdate><abstract>The invention relates to a work-hardened product, particularly a rolled, extruded or forged product, made of an alloy with the following composition (% by weight): Cu 3.8-4.3; Mg 1.25-1.45; Mn 0.2-0.5; Zn 0.4-1.3; Fe<0.15; Si<0.15; Zr 0.05; Ag<0.01, other elements <0.05 each and <0.15 total, remainder Al, treated by dissolution, quenching and cold strain-hardening, with a permanent deformation of between 0.5% and 15%, and preferably between 1.5% and 3.5%. Cold strain-hardening can be achieved by controlled tension and/or cold transformation, for example rolling, die forging or drawing. This cladded metal plate type product is a suitable element to be used as aircraft fuselage skin.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | ALLOYS CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS CHEMISTRY FERROUS OR NON-FERROUS ALLOYS METALLURGY TREATMENT OF ALLOYS OR NON-FERROUS METALS |
title | Aircraft structural member made of an Al-Cu-Mg alloy |
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