TURBOCHARGER WITH PREDETERMINED BREAKING POINT FOR AN INTERNAL COMBUSTION ENGINE
Disclosed is a turbocharger for an internal combustion engine, having a bearing housing. A turbocharger rotor is mounted to be rotatable in the bearing housing about the rotor axis of rotation of its rotor shaft, wherein a turbine wheel is arranged for conjoint rotation on the rotor shaft and in a t...
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| creator | Frankenstein, Dirk Böning, Ralf Ferling, Bruno Lehmayr, Bernhard Klaus, Michael |
| description | Disclosed is a turbocharger for an internal combustion engine, having a bearing housing. A turbocharger rotor is mounted to be rotatable in the bearing housing about the rotor axis of rotation of its rotor shaft, wherein a turbine wheel is arranged for conjoint rotation on the rotor shaft and in a turbine housing fixed on the bearing housing. Between the rotor shaft and the bearing housing, an oil seal for sealing the bearing housing with respect to the turbine housing is arranged between the turbine wheel and a radial bearing associated with the turbine wheel in order to seal the bearing housing with respect to the turbine housing. A predetermined breaking point is formed for the turbocharger rotor of the turbocharger which lies in a breaking point region and extends axially between the turbine wheel back and an axial end, facing the turbine wheel back, of the rotor-shaft oil seal. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2020056542A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2020056542A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2020056542A13</originalsourceid><addsrcrecordid>eNqNi7EKwjAQQLM4iPoPB85CrLZ7ml6ToL2U6xXHUiROooX6_9jBD3B6b3hvrVrpuYzWG3bIcAvioWWsUJCbQFhByWgugRy0MZBAHRkMwaLIZK5gY1P2nYRIgOSWY6tWj_E5p92PG7WvUaw_pOk9pHka7-mVPkPfZTrTOi_yc2aOp_-qL09NMCQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>TURBOCHARGER WITH PREDETERMINED BREAKING POINT FOR AN INTERNAL COMBUSTION ENGINE</title><source>esp@cenet</source><creator>Frankenstein, Dirk ; Böning, Ralf ; Ferling, Bruno ; Lehmayr, Bernhard ; Klaus, Michael</creator><creatorcontrib>Frankenstein, Dirk ; Böning, Ralf ; Ferling, Bruno ; Lehmayr, Bernhard ; Klaus, Michael</creatorcontrib><description>Disclosed is a turbocharger for an internal combustion engine, having a bearing housing. A turbocharger rotor is mounted to be rotatable in the bearing housing about the rotor axis of rotation of its rotor shaft, wherein a turbine wheel is arranged for conjoint rotation on the rotor shaft and in a turbine housing fixed on the bearing housing. Between the rotor shaft and the bearing housing, an oil seal for sealing the bearing housing with respect to the turbine housing is arranged between the turbine wheel and a radial bearing associated with the turbine wheel in order to seal the bearing housing with respect to the turbine housing. A predetermined breaking point is formed for the turbocharger rotor of the turbocharger which lies in a breaking point region and extends axially between the turbine wheel back and an axial end, facing the turbine wheel back, of the rotor-shaft oil seal.</description><language>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 ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INTERNAL-COMBUSTION PISTON ENGINES ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2020</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=20200220&DB=EPODOC&CC=US&NR=2020056542A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200220&DB=EPODOC&CC=US&NR=2020056542A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Frankenstein, Dirk</creatorcontrib><creatorcontrib>Böning, Ralf</creatorcontrib><creatorcontrib>Ferling, Bruno</creatorcontrib><creatorcontrib>Lehmayr, Bernhard</creatorcontrib><creatorcontrib>Klaus, Michael</creatorcontrib><title>TURBOCHARGER WITH PREDETERMINED BREAKING POINT FOR AN INTERNAL COMBUSTION ENGINE</title><description>Disclosed is a turbocharger for an internal combustion engine, having a bearing housing. A turbocharger rotor is mounted to be rotatable in the bearing housing about the rotor axis of rotation of its rotor shaft, wherein a turbine wheel is arranged for conjoint rotation on the rotor shaft and in a turbine housing fixed on the bearing housing. Between the rotor shaft and the bearing housing, an oil seal for sealing the bearing housing with respect to the turbine housing is arranged between the turbine wheel and a radial bearing associated with the turbine wheel in order to seal the bearing housing with respect to the turbine housing. A predetermined breaking point is formed for the turbocharger rotor of the turbocharger which lies in a breaking point region and extends axially between the turbine wheel back and an axial end, facing the turbine wheel back, of the rotor-shaft oil seal.</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>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>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNi7EKwjAQQLM4iPoPB85CrLZ7ml6ToL2U6xXHUiROooX6_9jBD3B6b3hvrVrpuYzWG3bIcAvioWWsUJCbQFhByWgugRy0MZBAHRkMwaLIZK5gY1P2nYRIgOSWY6tWj_E5p92PG7WvUaw_pOk9pHka7-mVPkPfZTrTOi_yc2aOp_-qL09NMCQ</recordid><startdate>20200220</startdate><enddate>20200220</enddate><creator>Frankenstein, Dirk</creator><creator>Böning, Ralf</creator><creator>Ferling, Bruno</creator><creator>Lehmayr, Bernhard</creator><creator>Klaus, Michael</creator><scope>EVB</scope></search><sort><creationdate>20200220</creationdate><title>TURBOCHARGER WITH PREDETERMINED BREAKING POINT FOR AN INTERNAL COMBUSTION ENGINE</title><author>Frankenstein, Dirk ; Böning, Ralf ; Ferling, Bruno ; Lehmayr, Bernhard ; Klaus, Michael</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2020056542A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2020</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>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>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Frankenstein, Dirk</creatorcontrib><creatorcontrib>Böning, Ralf</creatorcontrib><creatorcontrib>Ferling, Bruno</creatorcontrib><creatorcontrib>Lehmayr, Bernhard</creatorcontrib><creatorcontrib>Klaus, Michael</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Frankenstein, Dirk</au><au>Böning, Ralf</au><au>Ferling, Bruno</au><au>Lehmayr, Bernhard</au><au>Klaus, Michael</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBOCHARGER WITH PREDETERMINED BREAKING POINT FOR AN INTERNAL COMBUSTION ENGINE</title><date>2020-02-20</date><risdate>2020</risdate><abstract>Disclosed is a turbocharger for an internal combustion engine, having a bearing housing. A turbocharger rotor is mounted to be rotatable in the bearing housing about the rotor axis of rotation of its rotor shaft, wherein a turbine wheel is arranged for conjoint rotation on the rotor shaft and in a turbine housing fixed on the bearing housing. Between the rotor shaft and the bearing housing, an oil seal for sealing the bearing housing with respect to the turbine housing is arranged between the turbine wheel and a radial bearing associated with the turbine wheel in order to seal the bearing housing with respect to the turbine housing. A predetermined breaking point is formed for the turbocharger rotor of the turbocharger which lies in a breaking point region and extends axially between the turbine wheel back and an axial end, facing the turbine wheel back, of the rotor-shaft oil seal.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
| recordid | cdi_epo_espacenet_US2020056542A1 |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | TURBOCHARGER WITH PREDETERMINED BREAKING POINT FOR AN INTERNAL COMBUSTION ENGINE |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-16T09%3A38%3A29IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Frankenstein,%20Dirk&rft.date=2020-02-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2020056542A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |