PROCEDE DE FABRICATION D'UNE PIECE EN ALLIAGE D'ALUMINIUM

Procédé de fabrication d'une pièce (20) comportant une formation de couches métalliques (201...20n) successives, superposées les unes aux autres, chaque couche décrivant un motif défini à partir d'un modèle numérique, chaque couche étant formée par le dépôt d'un métal (15, 25), dit mé...

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Hauptverfasser: ODIEVRE, THIERRY, BES, BERNARD, LEDOUX, MARINE, CHEHAB, BECHIR, CHABRIOL, CHRISTOPHE
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creator ODIEVRE, THIERRY
BES, BERNARD
LEDOUX, MARINE
CHEHAB, BECHIR
CHABRIOL, CHRISTOPHE
description Procédé de fabrication d'une pièce (20) comportant une formation de couches métalliques (201...20n) successives, superposées les unes aux autres, chaque couche décrivant un motif défini à partir d'un modèle numérique, chaque couche étant formée par le dépôt d'un métal (15, 25), dit métal d'apport, le métal d'apport étant soumis, à une pression supérieure à 0.5 fois la pression atmosphérique, à un apport d'énergie de façon à entrer en fusion et à constituer ladite couche, le procédé étant caractérisé en ce que le métal d'apport est un alliage d'aluminium de la série 2xxx, comprenant les éléments d'alliage suivant : Cu, selon une fraction massique comprise entre 3 % et 7 % ; Mg, selon une fraction massique comprise entre 0.1 % et 0.8 %. The present invention relates to a process for manufacturing a part (20) comprising a formation of successive metal layers (201...20n), superimposed on one another, each layer describing a pattern defined from a numerical model, each layer being formed by the deposition of a metal (15, 25), referred to as filling metal, the filling metal being subjected, at a pressure greater than 0.5 times the atmospheric pressure, to an input of energy so as to melt and constitute said layer, the process being characterized in that the filling metal is an aluminium alloy of the 2xxx series, comprising the following alloying elements: - Cu, in a weight fraction of between 3% and 7%; - Mg, in a weight fraction of between 0.1% and 0.8%; - at least one element, or at least two elements or even at least three elements chosen from: * Mn, in a weight fraction of between 0.1% and 2%, preferably of at most 1% and in a preferred manner of at most 0.8%; * Ti, in a weight fraction of between 0.01% and 2%, preferably of at most 1% and in a preferred manner of at most 0.3%; * V, in a weight fraction of between 0.05% and 2%, preferably of at most 1% and in the preferred manner of at most 0.3%; * Zr, in a weight fraction of between 0.05% and 2%, preferably of at most 1% and in a preferred manner of at most 0.3%; * Cr, in a weight fraction of between 0.05% and 2%, preferably of at most 1% and in the preferred manner of at most 0.3%; and - optionally at least one element, or at least two elements or even at least three elements chosen from: * Ag, in a weight fraction of between 0.1% and 0.8%; * Li, in a weight fraction of between 0.1% and 2%, preferably 0.5% and 1.5%; * Zn, in a weight fraction of between 0.1% and 0.8%.
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The present invention relates to a process for manufacturing a part (20) comprising a formation of successive metal layers (201...20n), superimposed on one another, each layer describing a pattern defined from a numerical model, each layer being formed by the deposition of a metal (15, 25), referred to as filling metal, the filling metal being subjected, at a pressure greater than 0.5 times the atmospheric pressure, to an input of energy so as to melt and constitute said layer, the process being characterized in that the filling metal is an aluminium alloy of the 2xxx series, comprising the following alloying elements: - Cu, in a weight fraction of between 3% and 7%; - Mg, in a weight fraction of between 0.1% and 0.8%; - at least one element, or at least two elements or even at least three elements chosen from: * Mn, in a weight fraction of between 0.1% and 2%, preferably of at most 1% and in a preferred manner of at most 0.8%; * Ti, in a weight fraction of between 0.01% and 2%, preferably of at most 1% and in a preferred manner of at most 0.3%; * V, in a weight fraction of between 0.05% and 2%, preferably of at most 1% and in the preferred manner of at most 0.3%; * Zr, in a weight fraction of between 0.05% and 2%, preferably of at most 1% and in a preferred manner of at most 0.3%; * Cr, in a weight fraction of between 0.05% and 2%, preferably of at most 1% and in the preferred manner of at most 0.3%; and - optionally at least one element, or at least two elements or even at least three elements chosen from: * Ag, in a weight fraction of between 0.1% and 0.8%; * Li, in a weight fraction of between 0.1% and 2%, preferably 0.5% and 1.5%; * Zn, in a weight fraction of between 0.1% and 0.8%.</description><language>fre</language><subject>ADDITIVE MANUFACTURING TECHNOLOGY ; ADDITIVE MANUFACTURING, i.e. MANUFACTURING OFTHREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVEAGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING,STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING ; ALLOYS ; CASTING ; CHEMISTRY ; FERROUS OR NON-FERROUS ALLOYS ; MAKING METALLIC POWDER ; MANUFACTURE OF ARTICLES FROM METALLIC POWDER ; METALLURGY ; PERFORMING OPERATIONS ; POWDER METALLURGY ; TRANSPORTING ; TREATMENT OF ALLOYS OR NON-FERROUS METALS ; WORKING METALLIC POWDER</subject><creationdate>2018</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20181019&amp;DB=EPODOC&amp;CC=FR&amp;NR=3065178A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20181019&amp;DB=EPODOC&amp;CC=FR&amp;NR=3065178A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ODIEVRE, THIERRY</creatorcontrib><creatorcontrib>BES, BERNARD</creatorcontrib><creatorcontrib>LEDOUX, MARINE</creatorcontrib><creatorcontrib>CHEHAB, BECHIR</creatorcontrib><creatorcontrib>CHABRIOL, CHRISTOPHE</creatorcontrib><title>PROCEDE DE FABRICATION D'UNE PIECE EN ALLIAGE D'ALUMINIUM</title><description>Procédé de fabrication d'une pièce (20) comportant une formation de couches métalliques (201...20n) successives, superposées les unes aux autres, chaque couche décrivant un motif défini à partir d'un modèle numérique, chaque couche étant formée par le dépôt d'un métal (15, 25), dit métal d'apport, le métal d'apport étant soumis, à une pression supérieure à 0.5 fois la pression atmosphérique, à un apport d'énergie de façon à entrer en fusion et à constituer ladite couche, le procédé étant caractérisé en ce que le métal d'apport est un alliage d'aluminium de la série 2xxx, comprenant les éléments d'alliage suivant : Cu, selon une fraction massique comprise entre 3 % et 7 % ; Mg, selon une fraction massique comprise entre 0.1 % et 0.8 %. The present invention relates to a process for manufacturing a part (20) comprising a formation of successive metal layers (201...20n), superimposed on one another, each layer describing a pattern defined from a numerical model, each layer being formed by the deposition of a metal (15, 25), referred to as filling metal, the filling metal being subjected, at a pressure greater than 0.5 times the atmospheric pressure, to an input of energy so as to melt and constitute said layer, the process being characterized in that the filling metal is an aluminium alloy of the 2xxx series, comprising the following alloying elements: - Cu, in a weight fraction of between 3% and 7%; - Mg, in a weight fraction of between 0.1% and 0.8%; - at least one element, or at least two elements or even at least three elements chosen from: * Mn, in a weight fraction of between 0.1% and 2%, preferably of at most 1% and in a preferred manner of at most 0.8%; * Ti, in a weight fraction of between 0.01% and 2%, preferably of at most 1% and in a preferred manner of at most 0.3%; 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BES, BERNARD ; LEDOUX, MARINE ; CHEHAB, BECHIR ; CHABRIOL, CHRISTOPHE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR3065178A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</language><creationdate>2018</creationdate><topic>ADDITIVE MANUFACTURING TECHNOLOGY</topic><topic>ADDITIVE MANUFACTURING, i.e. MANUFACTURING OFTHREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVEAGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING,STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING</topic><topic>ALLOYS</topic><topic>CASTING</topic><topic>CHEMISTRY</topic><topic>FERROUS OR NON-FERROUS ALLOYS</topic><topic>MAKING METALLIC POWDER</topic><topic>MANUFACTURE OF ARTICLES FROM METALLIC POWDER</topic><topic>METALLURGY</topic><topic>PERFORMING OPERATIONS</topic><topic>POWDER METALLURGY</topic><topic>TRANSPORTING</topic><topic>TREATMENT OF ALLOYS OR NON-FERROUS METALS</topic><topic>WORKING METALLIC POWDER</topic><toplevel>online_resources</toplevel><creatorcontrib>ODIEVRE, THIERRY</creatorcontrib><creatorcontrib>BES, BERNARD</creatorcontrib><creatorcontrib>LEDOUX, MARINE</creatorcontrib><creatorcontrib>CHEHAB, BECHIR</creatorcontrib><creatorcontrib>CHABRIOL, CHRISTOPHE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ODIEVRE, THIERRY</au><au>BES, BERNARD</au><au>LEDOUX, MARINE</au><au>CHEHAB, BECHIR</au><au>CHABRIOL, CHRISTOPHE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PROCEDE DE FABRICATION D'UNE PIECE EN ALLIAGE D'ALUMINIUM</title><date>2018-10-19</date><risdate>2018</risdate><abstract>Procédé de fabrication d'une pièce (20) comportant une formation de couches métalliques (201...20n) successives, superposées les unes aux autres, chaque couche décrivant un motif défini à partir d'un modèle numérique, chaque couche étant formée par le dépôt d'un métal (15, 25), dit métal d'apport, le métal d'apport étant soumis, à une pression supérieure à 0.5 fois la pression atmosphérique, à un apport d'énergie de façon à entrer en fusion et à constituer ladite couche, le procédé étant caractérisé en ce que le métal d'apport est un alliage d'aluminium de la série 2xxx, comprenant les éléments d'alliage suivant : Cu, selon une fraction massique comprise entre 3 % et 7 % ; Mg, selon une fraction massique comprise entre 0.1 % et 0.8 %. The present invention relates to a process for manufacturing a part (20) comprising a formation of successive metal layers (201...20n), superimposed on one another, each layer describing a pattern defined from a numerical model, each layer being formed by the deposition of a metal (15, 25), referred to as filling metal, the filling metal being subjected, at a pressure greater than 0.5 times the atmospheric pressure, to an input of energy so as to melt and constitute said layer, the process being characterized in that the filling metal is an aluminium alloy of the 2xxx series, comprising the following alloying elements: - Cu, in a weight fraction of between 3% and 7%; - Mg, in a weight fraction of between 0.1% and 0.8%; - at least one element, or at least two elements or even at least three elements chosen from: * Mn, in a weight fraction of between 0.1% and 2%, preferably of at most 1% and in a preferred manner of at most 0.8%; * Ti, in a weight fraction of between 0.01% and 2%, preferably of at most 1% and in a preferred manner of at most 0.3%; * V, in a weight fraction of between 0.05% and 2%, preferably of at most 1% and in the preferred manner of at most 0.3%; * Zr, in a weight fraction of between 0.05% and 2%, preferably of at most 1% and in a preferred manner of at most 0.3%; * Cr, in a weight fraction of between 0.05% and 2%, preferably of at most 1% and in the preferred manner of at most 0.3%; and - optionally at least one element, or at least two elements or even at least three elements chosen from: * Ag, in a weight fraction of between 0.1% and 0.8%; * Li, in a weight fraction of between 0.1% and 2%, preferably 0.5% and 1.5%; * Zn, in a weight fraction of between 0.1% and 0.8%.</abstract><oa>free_for_read</oa></addata></record>
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subjects ADDITIVE MANUFACTURING TECHNOLOGY
ADDITIVE MANUFACTURING, i.e. MANUFACTURING OFTHREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVEAGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING,STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
ALLOYS
CASTING
CHEMISTRY
FERROUS OR NON-FERROUS ALLOYS
MAKING METALLIC POWDER
MANUFACTURE OF ARTICLES FROM METALLIC POWDER
METALLURGY
PERFORMING OPERATIONS
POWDER METALLURGY
TRANSPORTING
TREATMENT OF ALLOYS OR NON-FERROUS METALS
WORKING METALLIC POWDER
title PROCEDE DE FABRICATION D'UNE PIECE EN ALLIAGE D'ALUMINIUM
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