PROCESS FOR MAKING A METAL PART SUCH AS A TURBINE ENGINE BLADE REINFORCEMENT
A process for manufacturing a metal part such as a metal reinforcement for the blade of a turbine engine, comprising a step for manufacturing a three-dimensional metal structure made up of an insert which has properties which allow superplastic forming and diffusion welding to be carried out, and of...
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| creator | GODON, THIERRY PERROUX, ALAIN ROBERT YVES DAMBRINE, BRUNO JACQUES GERARD |
| description | A process for manufacturing a metal part such as a metal reinforcement for the blade of a turbine engine, comprising a step for manufacturing a three-dimensional metal structure made up of an insert which has properties which allow superplastic forming and diffusion welding to be carried out, and of multiple metal wires, each separate metal wire encircling a periphery of the insert, the metal structure forming a preform of the three-dimensional metal part; a step in which the three-dimensional metal structure is positioned in a forming tool; a hot-pressing step of the three-dimensional metal structure which causes agglomeration of the three-dimensional metal structure, so as to obtain the compact metal part.
La présente invention concerne un procédé de réalisation d'une pièce métallique telle qu'un renfort métallique d'aube de turbomachine comportant successivement : une étape réalisation d'une structure métallique tridimensionnelle (310) constituée par un insert (301) présentant dans propriétés permettant le formage superplastique et le soudage diffusion et par une pluralité de fils métalliques (302) encerclant la périphérie dudit insert (301), ladite structure métallique (310) formant une préforme de ladite pièce métallique (30); une étape de positionnement de ladite structure métallique (310) dans un outillage de forme : une étape de pressage à chaud de ladite structure métallique tridimensionnelle (310) provoquant l'agglomération de ladite structure métallique (310) de manière à obtenir ladite pièce métallique compacte. |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CA2828778C</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CA2828778C</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CA2828778C3</originalsourceid><addsrcrecordid>eNrjZPAJCPJ3dg0OVnDzD1LwdfT29HNXcFTwdQ1x9FEIcAwKUQgOdfZQcAwGCoaEBjl5-rkquPq5gygnH0cXV4UgV08_oFZnV19XvxAeBta0xJziVF4ozc0g7-Ya4uyhm1qQH59aXJCYnJqXWhLv7GhkYWRhbm7hbExYBQC-WyyV</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>PROCESS FOR MAKING A METAL PART SUCH AS A TURBINE ENGINE BLADE REINFORCEMENT</title><source>esp@cenet</source><creator>GODON, THIERRY ; PERROUX, ALAIN ROBERT YVES ; DAMBRINE, BRUNO JACQUES GERARD</creator><creatorcontrib>GODON, THIERRY ; PERROUX, ALAIN ROBERT YVES ; DAMBRINE, BRUNO JACQUES GERARD</creatorcontrib><description>A process for manufacturing a metal part such as a metal reinforcement for the blade of a turbine engine, comprising a step for manufacturing a three-dimensional metal structure made up of an insert which has properties which allow superplastic forming and diffusion welding to be carried out, and of multiple metal wires, each separate metal wire encircling a periphery of the insert, the metal structure forming a preform of the three-dimensional metal part; a step in which the three-dimensional metal structure is positioned in a forming tool; a hot-pressing step of the three-dimensional metal structure which causes agglomeration of the three-dimensional metal structure, so as to obtain the compact metal part.
La présente invention concerne un procédé de réalisation d'une pièce métallique telle qu'un renfort métallique d'aube de turbomachine comportant successivement : une étape réalisation d'une structure métallique tridimensionnelle (310) constituée par un insert (301) présentant dans propriétés permettant le formage superplastique et le soudage diffusion et par une pluralité de fils métalliques (302) encerclant la périphérie dudit insert (301), ladite structure métallique (310) formant une préforme de ladite pièce métallique (30); une étape de positionnement de ladite structure métallique (310) dans un outillage de forme : une étape de pressage à chaud de ladite structure métallique tridimensionnelle (310) provoquant l'agglomération de ladite structure métallique (310) de manière à obtenir ladite pièce métallique compacte.</description><language>eng ; fre</language><subject>AEROPLANES ; AIRCRAFT ; ALLOYS ; AVIATION ; BLASTING ; CHEMISTRY ; CLADDING OR PLATING BY SOLDERING OR WELDING ; COMBINED OPERATIONS ; COSMONAUTICS ; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ; ENGINE PLANTS IN GENERAL ; FERROUS OR NON-FERROUS ALLOYS ; HEATING ; HELICOPTERS ; LIGHTING ; MACHINE TOOLS ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; METALLURGY ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NON-POSITIVE DISPLACEMENT PUMPS ; OTHER WORKING OF METAL ; PERFORMING OPERATIONS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; SOLDERING OR UNSOLDERING ; STEAM ENGINES ; TRANSPORTING ; TREATMENT OF ALLOYS OR NON-FERROUS METALS ; UNIVERSAL MACHINE TOOLS ; WEAPONS ; WELDING ; WORKING BY LASER BEAM</subject><creationdate>2019</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=20190409&DB=EPODOC&CC=CA&NR=2828778C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190409&DB=EPODOC&CC=CA&NR=2828778C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GODON, THIERRY</creatorcontrib><creatorcontrib>PERROUX, ALAIN ROBERT YVES</creatorcontrib><creatorcontrib>DAMBRINE, BRUNO JACQUES GERARD</creatorcontrib><title>PROCESS FOR MAKING A METAL PART SUCH AS A TURBINE ENGINE BLADE REINFORCEMENT</title><description>A process for manufacturing a metal part such as a metal reinforcement for the blade of a turbine engine, comprising a step for manufacturing a three-dimensional metal structure made up of an insert which has properties which allow superplastic forming and diffusion welding to be carried out, and of multiple metal wires, each separate metal wire encircling a periphery of the insert, the metal structure forming a preform of the three-dimensional metal part; a step in which the three-dimensional metal structure is positioned in a forming tool; a hot-pressing step of the three-dimensional metal structure which causes agglomeration of the three-dimensional metal structure, so as to obtain the compact metal part.
La présente invention concerne un procédé de réalisation d'une pièce métallique telle qu'un renfort métallique d'aube de turbomachine comportant successivement : une étape réalisation d'une structure métallique tridimensionnelle (310) constituée par un insert (301) présentant dans propriétés permettant le formage superplastique et le soudage diffusion et par une pluralité de fils métalliques (302) encerclant la périphérie dudit insert (301), ladite structure métallique (310) formant une préforme de ladite pièce métallique (30); une étape de positionnement de ladite structure métallique (310) dans un outillage de forme : une étape de pressage à chaud de ladite structure métallique tridimensionnelle (310) provoquant l'agglomération de ladite structure métallique (310) de manière à obtenir ladite pièce métallique compacte.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ALLOYS</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>CHEMISTRY</subject><subject>CLADDING OR PLATING BY SOLDERING OR WELDING</subject><subject>COMBINED OPERATIONS</subject><subject>COSMONAUTICS</subject><subject>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>FERROUS OR NON-FERROUS ALLOYS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MACHINE TOOLS</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>METAL-WORKING NOT OTHERWISE PROVIDED FOR</subject><subject>METALLURGY</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>OTHER WORKING OF METAL</subject><subject>PERFORMING OPERATIONS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>SOLDERING OR UNSOLDERING</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><subject>UNIVERSAL MACHINE TOOLS</subject><subject>WEAPONS</subject><subject>WELDING</subject><subject>WORKING BY LASER BEAM</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPAJCPJ3dg0OVnDzD1LwdfT29HNXcFTwdQ1x9FEIcAwKUQgOdfZQcAwGCoaEBjl5-rkquPq5gygnH0cXV4UgV08_oFZnV19XvxAeBta0xJziVF4ozc0g7-Ya4uyhm1qQH59aXJCYnJqXWhLv7GhkYWRhbm7hbExYBQC-WyyV</recordid><startdate>20190409</startdate><enddate>20190409</enddate><creator>GODON, THIERRY</creator><creator>PERROUX, ALAIN ROBERT YVES</creator><creator>DAMBRINE, BRUNO JACQUES GERARD</creator><scope>EVB</scope></search><sort><creationdate>20190409</creationdate><title>PROCESS FOR MAKING A METAL PART SUCH AS A TURBINE ENGINE BLADE REINFORCEMENT</title><author>GODON, THIERRY ; PERROUX, ALAIN ROBERT YVES ; DAMBRINE, BRUNO JACQUES GERARD</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2828778C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2019</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ALLOYS</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>CHEMISTRY</topic><topic>CLADDING OR PLATING BY SOLDERING OR WELDING</topic><topic>COMBINED OPERATIONS</topic><topic>COSMONAUTICS</topic><topic>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>FERROUS OR NON-FERROUS ALLOYS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MACHINE TOOLS</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>METAL-WORKING NOT OTHERWISE PROVIDED FOR</topic><topic>METALLURGY</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>OTHER WORKING OF METAL</topic><topic>PERFORMING OPERATIONS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>SOLDERING OR UNSOLDERING</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>TREATMENT OF ALLOYS OR NON-FERROUS METALS</topic><topic>UNIVERSAL MACHINE TOOLS</topic><topic>WEAPONS</topic><topic>WELDING</topic><topic>WORKING BY LASER BEAM</topic><toplevel>online_resources</toplevel><creatorcontrib>GODON, THIERRY</creatorcontrib><creatorcontrib>PERROUX, ALAIN ROBERT YVES</creatorcontrib><creatorcontrib>DAMBRINE, BRUNO JACQUES GERARD</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GODON, THIERRY</au><au>PERROUX, ALAIN ROBERT YVES</au><au>DAMBRINE, BRUNO JACQUES GERARD</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PROCESS FOR MAKING A METAL PART SUCH AS A TURBINE ENGINE BLADE REINFORCEMENT</title><date>2019-04-09</date><risdate>2019</risdate><abstract>A process for manufacturing a metal part such as a metal reinforcement for the blade of a turbine engine, comprising a step for manufacturing a three-dimensional metal structure made up of an insert which has properties which allow superplastic forming and diffusion welding to be carried out, and of multiple metal wires, each separate metal wire encircling a periphery of the insert, the metal structure forming a preform of the three-dimensional metal part; a step in which the three-dimensional metal structure is positioned in a forming tool; a hot-pressing step of the three-dimensional metal structure which causes agglomeration of the three-dimensional metal structure, so as to obtain the compact metal part.
La présente invention concerne un procédé de réalisation d'une pièce métallique telle qu'un renfort métallique d'aube de turbomachine comportant successivement : une étape réalisation d'une structure métallique tridimensionnelle (310) constituée par un insert (301) présentant dans propriétés permettant le formage superplastique et le soudage diffusion et par une pluralité de fils métalliques (302) encerclant la périphérie dudit insert (301), ladite structure métallique (310) formant une préforme de ladite pièce métallique (30); une étape de positionnement de ladite structure métallique (310) dans un outillage de forme : une étape de pressage à chaud de ladite structure métallique tridimensionnelle (310) provoquant l'agglomération de ladite structure métallique (310) de manière à obtenir ladite pièce métallique compacte.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT ALLOYS AVIATION BLASTING CHEMISTRY CLADDING OR PLATING BY SOLDERING OR WELDING COMBINED OPERATIONS COSMONAUTICS CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ENGINE PLANTS IN GENERAL FERROUS OR NON-FERROUS ALLOYS HEATING HELICOPTERS LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR METALLURGY NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS OTHER WORKING OF METAL PERFORMING OPERATIONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS SOLDERING OR UNSOLDERING STEAM ENGINES TRANSPORTING TREATMENT OF ALLOYS OR NON-FERROUS METALS UNIVERSAL MACHINE TOOLS WEAPONS WELDING WORKING BY LASER BEAM |
| title | PROCESS FOR MAKING A METAL PART SUCH AS A TURBINE ENGINE BLADE REINFORCEMENT |
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