Brazing of titanium-aluminium intermetallic alloy to nickel based superalloy using an interposed layer of nickel, notably for the production of aircraft engine components
The fixing on the surface of a first component (1) of a first metal of a second metal (4) by melting a solder (3) adapted to the second metal. The first metal is an intermetallic alloy such as titanium-aluminium and a layer of nickel (2) is interposed between the first component and the solder. An i...
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| creator | HOFFMANN CARINE JOSSO PIERRE BACOS MARIE PIERRE NAVEOS SERGE |
| description | The fixing on the surface of a first component (1) of a first metal of a second metal (4) by melting a solder (3) adapted to the second metal. The first metal is an intermetallic alloy such as titanium-aluminium and a layer of nickel (2) is interposed between the first component and the solder. An independent claim is also included for a composite metal component obtained by this method.
Une couche de nickel (2) interposée entre une pièce (1) en aluminiure de titane et une feuille de brasure (3) permet de braser cette pièce (1) à un autre matériau métallique (4) sans que l'aluminium diffuse de l'une vers l'autre, et d'obtenir ainsi une liaison stable ayant une bonne résistance mécanique.Application à l'assemblage de pièces de moteurs aéronautiques en aluminiure de titane et en un superalliage à base de nickel. |
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Une couche de nickel (2) interposée entre une pièce (1) en aluminiure de titane et une feuille de brasure (3) permet de braser cette pièce (1) à un autre matériau métallique (4) sans que l'aluminium diffuse de l'une vers l'autre, et d'obtenir ainsi une liaison stable ayant une bonne résistance mécanique.Application à l'assemblage de pièces de moteurs aéronautiques en aluminiure de titane et en un superalliage à base de nickel.</description><edition>7</edition><language>eng ; fre</language><subject>CLADDING OR PLATING BY SOLDERING OR WELDING ; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC ; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS ; MACHINE TOOLS ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; PERFORMING OPERATIONS ; SOLDERING OR UNSOLDERING ; TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION ; TECHNICAL SUBJECTS COVERED BY FORMER USPC ; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS ; TRANSPORTING ; WELDING ; WORKING BY LASER BEAM</subject><creationdate>2005</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&date=20050128&DB=EPODOC&CC=FR&NR=2857892A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20050128&DB=EPODOC&CC=FR&NR=2857892A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HOFFMANN CARINE</creatorcontrib><creatorcontrib>JOSSO PIERRE</creatorcontrib><creatorcontrib>BACOS MARIE PIERRE</creatorcontrib><creatorcontrib>NAVEOS SERGE</creatorcontrib><title>Brazing of titanium-aluminium intermetallic alloy to nickel based superalloy using an interposed layer of nickel, notably for the production of aircraft engine components</title><description>The fixing on the surface of a first component (1) of a first metal of a second metal (4) by melting a solder (3) adapted to the second metal. The first metal is an intermetallic alloy such as titanium-aluminium and a layer of nickel (2) is interposed between the first component and the solder. An independent claim is also included for a composite metal component obtained by this method.
Une couche de nickel (2) interposée entre une pièce (1) en aluminiure de titane et une feuille de brasure (3) permet de braser cette pièce (1) à un autre matériau métallique (4) sans que l'aluminium diffuse de l'une vers l'autre, et d'obtenir ainsi une liaison stable ayant une bonne résistance mécanique.Application à l'assemblage de pièces de moteurs aéronautiques en aluminiure de titane et en un superalliage à base de nickel.</description><subject>CLADDING OR PLATING BY SOLDERING OR WELDING</subject><subject>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</subject><subject>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</subject><subject>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</subject><subject>MACHINE TOOLS</subject><subject>METAL-WORKING NOT OTHERWISE PROVIDED FOR</subject><subject>PERFORMING OPERATIONS</subject><subject>SOLDERING OR UNSOLDERING</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</subject><subject>TRANSPORTING</subject><subject>WELDING</subject><subject>WORKING BY LASER BEAM</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2005</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjEEOQUEQRP_GQnCHPgALRLBEiLXYSxv96ZjfPZnpWXxHckom3wFsqip5VdWv3tuIL5Y7aA3GhsK5maDPDZcELEaxIUPv2cFXtQVTEHZP8nDFRDdIOVDsUE7lCqXbBS3YY0ux3HejMYgaXn0LtUawB0GIesvOWKW0kKOLWBuQ3FkInDZBhcTSsOrV6BONfj6o4LA_744TCnqhFNCRkF0Op9lqsVytZ5vp_I_KB_7jWb0</recordid><startdate>20050128</startdate><enddate>20050128</enddate><creator>HOFFMANN CARINE</creator><creator>JOSSO PIERRE</creator><creator>BACOS MARIE PIERRE</creator><creator>NAVEOS SERGE</creator><scope>EVB</scope></search><sort><creationdate>20050128</creationdate><title>Brazing of titanium-aluminium intermetallic alloy to nickel based superalloy using an interposed layer of nickel, notably for the production of aircraft engine components</title><author>HOFFMANN CARINE ; JOSSO PIERRE ; BACOS MARIE PIERRE ; NAVEOS SERGE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR2857892A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2005</creationdate><topic>CLADDING OR PLATING BY SOLDERING OR WELDING</topic><topic>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</topic><topic>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</topic><topic>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</topic><topic>MACHINE TOOLS</topic><topic>METAL-WORKING NOT OTHERWISE PROVIDED FOR</topic><topic>PERFORMING OPERATIONS</topic><topic>SOLDERING OR UNSOLDERING</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</topic><topic>TRANSPORTING</topic><topic>WELDING</topic><topic>WORKING BY LASER BEAM</topic><toplevel>online_resources</toplevel><creatorcontrib>HOFFMANN CARINE</creatorcontrib><creatorcontrib>JOSSO PIERRE</creatorcontrib><creatorcontrib>BACOS MARIE PIERRE</creatorcontrib><creatorcontrib>NAVEOS SERGE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HOFFMANN CARINE</au><au>JOSSO PIERRE</au><au>BACOS MARIE PIERRE</au><au>NAVEOS SERGE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Brazing of titanium-aluminium intermetallic alloy to nickel based superalloy using an interposed layer of nickel, notably for the production of aircraft engine components</title><date>2005-01-28</date><risdate>2005</risdate><abstract>The fixing on the surface of a first component (1) of a first metal of a second metal (4) by melting a solder (3) adapted to the second metal. The first metal is an intermetallic alloy such as titanium-aluminium and a layer of nickel (2) is interposed between the first component and the solder. An independent claim is also included for a composite metal component obtained by this method.
Une couche de nickel (2) interposée entre une pièce (1) en aluminiure de titane et une feuille de brasure (3) permet de braser cette pièce (1) à un autre matériau métallique (4) sans que l'aluminium diffuse de l'une vers l'autre, et d'obtenir ainsi une liaison stable ayant une bonne résistance mécanique.Application à l'assemblage de pièces de moteurs aéronautiques en aluminiure de titane et en un superalliage à base de nickel.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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| subjects | CLADDING OR PLATING BY SOLDERING OR WELDING CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS SOLDERING OR UNSOLDERING TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TRANSPORTING WELDING WORKING BY LASER BEAM |
| title | Brazing of titanium-aluminium intermetallic alloy to nickel based superalloy using an interposed layer of nickel, notably for the production of aircraft engine components |
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