DISQUE DE TURBINE MONOBLOC
The monoblock bladed disc for turbine, comprises a central hub, a periphery blade, a first radial wing (2a), and a second radial wing (2b) between the hub and blades spaced axially on each other to allow the blades in an internal cavity. The first radial wing includes axial holes to communicate with...
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| creator | ESCURE DIDIER RENE ANDRE VIGNEAU JOEL OLIVIER ALFRED ABEL LARDELLIER ALAIN MARIE JOSEPH |
| description | The monoblock bladed disc for turbine, comprises a central hub, a periphery blade, a first radial wing (2a), and a second radial wing (2b) between the hub and blades spaced axially on each other to allow the blades in an internal cavity. The first radial wing includes axial holes to communicate with the cavity, and is connected to external sealing rings (5, 6). The blades have hollow cavity to contact the interior blades. The disc with radial fins is present inside the cavity. The first wing or the second wing is connected to an attachment flange of the disc to gas turbine motor. Independent claims are included for: (1) a method of manufacturing the monoblock bladed disc; and (2) a turbomachine. |
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The first radial wing includes axial holes to communicate with the cavity, and is connected to external sealing rings (5, 6). The blades have hollow cavity to contact the interior blades. The disc with radial fins is present inside the cavity. The first wing or the second wing is connected to an attachment flange of the disc to gas turbine motor. Independent claims are included for: (1) a method of manufacturing the monoblock bladed disc; and (2) a turbomachine.</description><language>fre</language><subject>BLASTING ; CLADDING OR PLATING BY SOLDERING OR WELDING ; COMBINED OPERATIONS ; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ; ENGINE PLANTS IN GENERAL ; HEATING ; INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS ; INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 ; LIGHTING ; MACHINE TOOLS ; MACHINES OR ENGINES IN GENERAL ; MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES,RIVETS, BOLTS OR WHEELS ; MECHANICAL ENGINEERING ; MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; OTHER WORKING OF METAL ; PERFORMING OPERATIONS ; PUNCHING METAL ; SOLDERING OR UNSOLDERING ; STEAM ENGINES ; TRANSPORTING ; UNIVERSAL MACHINE TOOLS ; WEAPONS ; WELDING ; WORKING BY LASER BEAM</subject><creationdate>2012</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=20121116&DB=EPODOC&CC=FR&NR=2901305B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20121116&DB=EPODOC&CC=FR&NR=2901305B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ESCURE DIDIER RENE ANDRE</creatorcontrib><creatorcontrib>VIGNEAU JOEL OLIVIER ALFRED ABEL</creatorcontrib><creatorcontrib>LARDELLIER ALAIN MARIE JOSEPH</creatorcontrib><title>DISQUE DE TURBINE MONOBLOC</title><description>The monoblock bladed disc for turbine, comprises a central hub, a periphery blade, a first radial wing (2a), and a second radial wing (2b) between the hub and blades spaced axially on each other to allow the blades in an internal cavity. The first radial wing includes axial holes to communicate with the cavity, and is connected to external sealing rings (5, 6). The blades have hollow cavity to contact the interior blades. The disc with radial fins is present inside the cavity. The first wing or the second wing is connected to an attachment flange of the disc to gas turbine motor. Independent claims are included for: (1) a method of manufacturing the monoblock bladed disc; and (2) a turbomachine.</description><subject>BLASTING</subject><subject>CLADDING OR PLATING BY SOLDERING OR WELDING</subject><subject>COMBINED OPERATIONS</subject><subject>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</subject><subject>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</subject><subject>LIGHTING</subject><subject>MACHINE TOOLS</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES,RIVETS, BOLTS OR WHEELS</subject><subject>MECHANICAL ENGINEERING</subject><subject>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</subject><subject>METAL-WORKING NOT OTHERWISE PROVIDED FOR</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>OTHER WORKING OF METAL</subject><subject>PERFORMING OPERATIONS</subject><subject>PUNCHING METAL</subject><subject>SOLDERING OR UNSOLDERING</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</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>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJBy8QwODHVVcHFVCAkNcvL0c1Xw9ffzd_Lxd-ZhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfFuQUaWBobGBqZOhsZEKAEA69kfvw</recordid><startdate>20121116</startdate><enddate>20121116</enddate><creator>ESCURE DIDIER RENE ANDRE</creator><creator>VIGNEAU JOEL OLIVIER ALFRED ABEL</creator><creator>LARDELLIER ALAIN MARIE JOSEPH</creator><scope>EVB</scope></search><sort><creationdate>20121116</creationdate><title>DISQUE DE TURBINE MONOBLOC</title><author>ESCURE DIDIER RENE ANDRE ; VIGNEAU JOEL OLIVIER ALFRED ABEL ; LARDELLIER ALAIN MARIE JOSEPH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR2901305B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</language><creationdate>2012</creationdate><topic>BLASTING</topic><topic>CLADDING OR PLATING BY SOLDERING OR WELDING</topic><topic>COMBINED OPERATIONS</topic><topic>CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</topic><topic>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</topic><topic>LIGHTING</topic><topic>MACHINE TOOLS</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES,RIVETS, BOLTS OR WHEELS</topic><topic>MECHANICAL ENGINEERING</topic><topic>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</topic><topic>METAL-WORKING NOT OTHERWISE PROVIDED FOR</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>OTHER WORKING OF METAL</topic><topic>PERFORMING OPERATIONS</topic><topic>PUNCHING METAL</topic><topic>SOLDERING OR UNSOLDERING</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>UNIVERSAL MACHINE TOOLS</topic><topic>WEAPONS</topic><topic>WELDING</topic><topic>WORKING BY LASER BEAM</topic><toplevel>online_resources</toplevel><creatorcontrib>ESCURE DIDIER RENE ANDRE</creatorcontrib><creatorcontrib>VIGNEAU JOEL OLIVIER ALFRED ABEL</creatorcontrib><creatorcontrib>LARDELLIER ALAIN MARIE JOSEPH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ESCURE DIDIER RENE ANDRE</au><au>VIGNEAU JOEL OLIVIER ALFRED ABEL</au><au>LARDELLIER ALAIN MARIE JOSEPH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DISQUE DE TURBINE MONOBLOC</title><date>2012-11-16</date><risdate>2012</risdate><abstract>The monoblock bladed disc for turbine, comprises a central hub, a periphery blade, a first radial wing (2a), and a second radial wing (2b) between the hub and blades spaced axially on each other to allow the blades in an internal cavity. The first radial wing includes axial holes to communicate with the cavity, and is connected to external sealing rings (5, 6). The blades have hollow cavity to contact the interior blades. The disc with radial fins is present inside the cavity. The first wing or the second wing is connected to an attachment flange of the disc to gas turbine motor. Independent claims are included for: (1) a method of manufacturing the monoblock bladed disc; and (2) a turbomachine.</abstract><oa>free_for_read</oa></addata></record> |
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| language | fre |
| recordid | cdi_epo_espacenet_FR2901305B1 |
| source | esp@cenet |
| subjects | BLASTING CLADDING OR PLATING BY SOLDERING OR WELDING COMBINED OPERATIONS CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES,RIVETS, BOLTS OR WHEELS MECHANICAL ENGINEERING MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OTHER WORKING OF METAL PERFORMING OPERATIONS PUNCHING METAL SOLDERING OR UNSOLDERING STEAM ENGINES TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS WELDING WORKING BY LASER BEAM |
| title | DISQUE DE TURBINE MONOBLOC |
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