TURBOCHARGER HAVING SEALING SURFACES BETWEEN A NOZZLE RING AND A TURBINE HOUSING
The invention relates to a turbocharger, comprising a turbine for expanding a first medium and a compressor for compressing a second medium by using energy obtained in the turbine as the first mediumis expanded, wherein the turbine has a turbine housing (1) and a turbine rotor, wherein the compresso...
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| creator | REZANINA JAN SCHORER PAUL HOSSBACH BJORN WEISBROD TOBIAS BOZEK LUKAS |
| description | The invention relates to a turbocharger, comprising a turbine for expanding a first medium and a compressor for compressing a second medium by using energy obtained in the turbine as the first mediumis expanded, wherein the turbine has a turbine housing (1) and a turbine rotor, wherein the compressor has a compressor housing and a compressor rotor coupled to the turbine rotor by means of a shaft,wherein the turbine housing (1) and the compressor housing are each connected to a bearing housing (2) arranged between the same, in which bearing housing the shaft is supported, wherein the turbinehousing (1) and the bearing housing (2) are connected by means of a fastening device (5) in such a way that the fastening device is mounted on a flange (6) of the turbine housing (1) by means of a first section (7) and covers a flange (10) of the bearing housing (2) at least in some sections by means of a second section (9), and wherein at least one flange (11) of a nozzle ring (3) is clamped between the flange (6) of the t |
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eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; COMBUSTION ENGINES IN GENERAL ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INTERNAL-COMBUSTION PISTON ENGINES ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</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=20190716&DB=EPODOC&CC=CN&NR=110023590A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25551,76302</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190716&DB=EPODOC&CC=CN&NR=110023590A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>REZANINA JAN</creatorcontrib><creatorcontrib>SCHORER PAUL</creatorcontrib><creatorcontrib>HOSSBACH BJORN</creatorcontrib><creatorcontrib>WEISBROD TOBIAS</creatorcontrib><creatorcontrib>BOZEK LUKAS</creatorcontrib><title>TURBOCHARGER HAVING SEALING SURFACES BETWEEN A NOZZLE RING AND A TURBINE HOUSING</title><description>The invention relates to a turbocharger, comprising a turbine for expanding a first medium and a compressor for compressing a second medium by using energy obtained in the turbine as the first mediumis expanded, wherein the turbine has a turbine housing (1) and a turbine rotor, wherein the compressor has a compressor housing and a compressor rotor coupled to the turbine rotor by means of a shaft,wherein the turbine housing (1) and the compressor housing are each connected to a bearing housing (2) arranged between the same, in which bearing housing the shaft is supported, wherein the turbinehousing (1) and the bearing housing (2) are connected by means of a fastening device (5) in such a way that the fastening device is mounted on a flange (6) of the turbine housing (1) by means of a first section (7) and covers a flange (10) of the bearing housing (2) at least in some sections by means of a second section (9), and wherein at least one flange (11) of a nozzle ring (3) is clamped between the flange (6) of the t</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION ENGINES IN GENERAL</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>INTERNAL-COMBUSTION PISTON ENGINES</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAgICQ1y8nf2cAxydw1S8HAM8_RzVwh2dfQB06FBbo7OrsEKTq4h4a6ufgqOCn7-UVE-rgpBIGlHPxegCMgATz9XBQ__0GCgKA8Da1piTnEqL5TmZlB0cw1x9tBNLciPTy0uSExOzUstiXf2MzQ0MDAyNrU0cDQmRg0AZNAuzA</recordid><startdate>20190716</startdate><enddate>20190716</enddate><creator>REZANINA JAN</creator><creator>SCHORER PAUL</creator><creator>HOSSBACH BJORN</creator><creator>WEISBROD TOBIAS</creator><creator>BOZEK LUKAS</creator><scope>EVB</scope></search><sort><creationdate>20190716</creationdate><title>TURBOCHARGER HAVING SEALING SURFACES BETWEEN A NOZZLE RING AND A TURBINE HOUSING</title><author>REZANINA JAN ; SCHORER PAUL ; HOSSBACH BJORN ; WEISBROD TOBIAS ; BOZEK LUKAS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN110023590A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2019</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION ENGINES IN GENERAL</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>INTERNAL-COMBUSTION PISTON ENGINES</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>REZANINA JAN</creatorcontrib><creatorcontrib>SCHORER PAUL</creatorcontrib><creatorcontrib>HOSSBACH BJORN</creatorcontrib><creatorcontrib>WEISBROD TOBIAS</creatorcontrib><creatorcontrib>BOZEK LUKAS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>REZANINA JAN</au><au>SCHORER PAUL</au><au>HOSSBACH BJORN</au><au>WEISBROD TOBIAS</au><au>BOZEK LUKAS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBOCHARGER HAVING SEALING SURFACES BETWEEN A NOZZLE RING AND A TURBINE HOUSING</title><date>2019-07-16</date><risdate>2019</risdate><abstract>The invention relates to a turbocharger, comprising a turbine for expanding a first medium and a compressor for compressing a second medium by using energy obtained in the turbine as the first mediumis expanded, wherein the turbine has a turbine housing (1) and a turbine rotor, wherein the compressor has a compressor housing and a compressor rotor coupled to the turbine rotor by means of a shaft,wherein the turbine housing (1) and the compressor housing are each connected to a bearing housing (2) arranged between the same, in which bearing housing the shaft is supported, wherein the turbinehousing (1) and the bearing housing (2) are connected by means of a fastening device (5) in such a way that the fastening device is mounted on a flange (6) of the turbine housing (1) by means of a first section (7) and covers a flange (10) of the bearing housing (2) at least in some sections by means of a second section (9), and wherein at least one flange (11) of a nozzle ring (3) is clamped between the flange (6) of the t</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN110023590A |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | TURBOCHARGER HAVING SEALING SURFACES BETWEEN A NOZZLE RING AND A TURBINE HOUSING |
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