Turbine for internal combustion engine

The invention relates to a turbine (1) for an internal combustion engine. The turbine comprises a shaft (2) and a rolling bearing (3) for supporting the shaft (2). The rolling bearing (3) has at least one inner ring (4a, 4b), at least one outer ring (5) and rolling bodies (6a, 6b) arranged spatially...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: POHRER BENJAMIN, HULLIN GREGOR, GEBAUER PETER, SCHREIBER BENEDIKT
Format: Patent
Sprache:chi ; eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator POHRER BENJAMIN
HULLIN GREGOR
GEBAUER PETER
SCHREIBER BENEDIKT
description The invention relates to a turbine (1) for an internal combustion engine. The turbine comprises a shaft (2) and a rolling bearing (3) for supporting the shaft (2). The rolling bearing (3) has at least one inner ring (4a, 4b), at least one outer ring (5) and rolling bodies (6a, 6b) arranged spatially between the at least one inner ring (4a, 4b) and the at least one outer ring (5). At least the at least one inner ring (4a, 4b) is constructed from a steel alloy. The steel alloy has at least 5.8 to up to 6.2% by weight of nickel, at least 4.8 to up to 5.2% by weight of chromium, at least 2.0 to up to 2.4% by weight of aluminum, at least 0.6 to up to 0.8% by weight of molybdenum, and at least 0.45 to up to 0.55% by weight of vanadium. 本发明涉及一种用于内燃机的涡轮机(1),所述涡轮机包括轴(2)和用于支承所述轴(2)的滚动轴承(3),其中,所述滚动轴承(3)具有至少一个内圈(4a、4b)、至少一个外圈(5)以及在空间上布置在所述至少一个内圈(4a、4b)和所述至少一个外圈(5)之间的滚动体(6a、6b),其中,至少所述至少一个内圈(4a、4b)由钢合金构造,其中,所述钢合金具有至少5.8至最高6.2重量%的镍、至少4.8至最高5.2重量%的铬、至少2.0至最高2.4重量%的铝、至少0.6至最高0.8重量%的钼和至少0.45至最高0.55重量%的钒。
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN113718179A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN113718179A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN113718179A3</originalsourceid><addsrcrecordid>eNrjZFALKS1KysxLVUjLL1LIzCtJLcpLzFFIzs9NKi0uyczPU0jNSwdK8zCwpiXmFKfyQmluBkU31xBnD93Ugvz41OKCxOTUvNSSeGc_Q0Njc0MLQ3NLR2Ni1AAAhyEnzw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Turbine for internal combustion engine</title><source>esp@cenet</source><creator>POHRER BENJAMIN ; HULLIN GREGOR ; GEBAUER PETER ; SCHREIBER BENEDIKT</creator><creatorcontrib>POHRER BENJAMIN ; HULLIN GREGOR ; GEBAUER PETER ; SCHREIBER BENEDIKT</creatorcontrib><description>The invention relates to a turbine (1) for an internal combustion engine. The turbine comprises a shaft (2) and a rolling bearing (3) for supporting the shaft (2). The rolling bearing (3) has at least one inner ring (4a, 4b), at least one outer ring (5) and rolling bodies (6a, 6b) arranged spatially between the at least one inner ring (4a, 4b) and the at least one outer ring (5). At least the at least one inner ring (4a, 4b) is constructed from a steel alloy. The steel alloy has at least 5.8 to up to 6.2% by weight of nickel, at least 4.8 to up to 5.2% by weight of chromium, at least 2.0 to up to 2.4% by weight of aluminum, at least 0.6 to up to 0.8% by weight of molybdenum, and at least 0.45 to up to 0.55% by weight of vanadium. 本发明涉及一种用于内燃机的涡轮机(1),所述涡轮机包括轴(2)和用于支承所述轴(2)的滚动轴承(3),其中,所述滚动轴承(3)具有至少一个内圈(4a、4b)、至少一个外圈(5)以及在空间上布置在所述至少一个内圈(4a、4b)和所述至少一个外圈(5)之间的滚动体(6a、6b),其中,至少所述至少一个内圈(4a、4b)由钢合金构造,其中,所述钢合金具有至少5.8至最高6.2重量%的镍、至少4.8至最高5.2重量%的铬、至少2.0至最高2.4重量%的铝、至少0.6至最高0.8重量%的钼和至少0.45至最高0.55重量%的钒。</description><language>chi ; eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; ALLOYS ; BLASTING ; CHEMISTRY ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; FERROUS OR NON-FERROUS ALLOYS ; GAS-TURBINE PLANTS ; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS ; MECHANICAL ENGINEERING ; METALLURGY ; METALLURGY OF IRON ; MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS ; TREATMENT OF ALLOYS OR NON-FERROUS METALS ; WEAPONS</subject><creationdate>2021</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&amp;date=20211130&amp;DB=EPODOC&amp;CC=CN&amp;NR=113718179A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20211130&amp;DB=EPODOC&amp;CC=CN&amp;NR=113718179A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>POHRER BENJAMIN</creatorcontrib><creatorcontrib>HULLIN GREGOR</creatorcontrib><creatorcontrib>GEBAUER PETER</creatorcontrib><creatorcontrib>SCHREIBER BENEDIKT</creatorcontrib><title>Turbine for internal combustion engine</title><description>The invention relates to a turbine (1) for an internal combustion engine. The turbine comprises a shaft (2) and a rolling bearing (3) for supporting the shaft (2). The rolling bearing (3) has at least one inner ring (4a, 4b), at least one outer ring (5) and rolling bodies (6a, 6b) arranged spatially between the at least one inner ring (4a, 4b) and the at least one outer ring (5). At least the at least one inner ring (4a, 4b) is constructed from a steel alloy. The steel alloy has at least 5.8 to up to 6.2% by weight of nickel, at least 4.8 to up to 5.2% by weight of chromium, at least 2.0 to up to 2.4% by weight of aluminum, at least 0.6 to up to 0.8% by weight of molybdenum, and at least 0.45 to up to 0.55% by weight of vanadium. 本发明涉及一种用于内燃机的涡轮机(1),所述涡轮机包括轴(2)和用于支承所述轴(2)的滚动轴承(3),其中,所述滚动轴承(3)具有至少一个内圈(4a、4b)、至少一个外圈(5)以及在空间上布置在所述至少一个内圈(4a、4b)和所述至少一个外圈(5)之间的滚动体(6a、6b),其中,至少所述至少一个内圈(4a、4b)由钢合金构造,其中,所述钢合金具有至少5.8至最高6.2重量%的镍、至少4.8至最高5.2重量%的铬、至少2.0至最高2.4重量%的铝、至少0.6至最高0.8重量%的钼和至少0.45至最高0.55重量%的钒。</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>ALLOYS</subject><subject>BLASTING</subject><subject>CHEMISTRY</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>FERROUS OR NON-FERROUS ALLOYS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS</subject><subject>MECHANICAL ENGINEERING</subject><subject>METALLURGY</subject><subject>METALLURGY OF IRON</subject><subject>MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS</subject><subject>TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFALKS1KysxLVUjLL1LIzCtJLcpLzFFIzs9NKi0uyczPU0jNSwdK8zCwpiXmFKfyQmluBkU31xBnD93Ugvz41OKCxOTUvNSSeGc_Q0Njc0MLQ3NLR2Ni1AAAhyEnzw</recordid><startdate>20211130</startdate><enddate>20211130</enddate><creator>POHRER BENJAMIN</creator><creator>HULLIN GREGOR</creator><creator>GEBAUER PETER</creator><creator>SCHREIBER BENEDIKT</creator><scope>EVB</scope></search><sort><creationdate>20211130</creationdate><title>Turbine for internal combustion engine</title><author>POHRER BENJAMIN ; HULLIN GREGOR ; GEBAUER PETER ; SCHREIBER BENEDIKT</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN113718179A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>ALLOYS</topic><topic>BLASTING</topic><topic>CHEMISTRY</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>FERROUS OR NON-FERROUS ALLOYS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS</topic><topic>MECHANICAL ENGINEERING</topic><topic>METALLURGY</topic><topic>METALLURGY OF IRON</topic><topic>MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS</topic><topic>TREATMENT OF ALLOYS OR NON-FERROUS METALS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>POHRER BENJAMIN</creatorcontrib><creatorcontrib>HULLIN GREGOR</creatorcontrib><creatorcontrib>GEBAUER PETER</creatorcontrib><creatorcontrib>SCHREIBER BENEDIKT</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>POHRER BENJAMIN</au><au>HULLIN GREGOR</au><au>GEBAUER PETER</au><au>SCHREIBER BENEDIKT</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Turbine for internal combustion engine</title><date>2021-11-30</date><risdate>2021</risdate><abstract>The invention relates to a turbine (1) for an internal combustion engine. The turbine comprises a shaft (2) and a rolling bearing (3) for supporting the shaft (2). The rolling bearing (3) has at least one inner ring (4a, 4b), at least one outer ring (5) and rolling bodies (6a, 6b) arranged spatially between the at least one inner ring (4a, 4b) and the at least one outer ring (5). At least the at least one inner ring (4a, 4b) is constructed from a steel alloy. The steel alloy has at least 5.8 to up to 6.2% by weight of nickel, at least 4.8 to up to 5.2% by weight of chromium, at least 2.0 to up to 2.4% by weight of aluminum, at least 0.6 to up to 0.8% by weight of molybdenum, and at least 0.45 to up to 0.55% by weight of vanadium. 本发明涉及一种用于内燃机的涡轮机(1),所述涡轮机包括轴(2)和用于支承所述轴(2)的滚动轴承(3),其中,所述滚动轴承(3)具有至少一个内圈(4a、4b)、至少一个外圈(5)以及在空间上布置在所述至少一个内圈(4a、4b)和所述至少一个外圈(5)之间的滚动体(6a、6b),其中,至少所述至少一个内圈(4a、4b)由钢合金构造,其中,所述钢合金具有至少5.8至最高6.2重量%的镍、至少4.8至最高5.2重量%的铬、至少2.0至最高2.4重量%的铝、至少0.6至最高0.8重量%的钼和至少0.45至最高0.55重量%的钒。</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN113718179A
source esp@cenet
subjects AIR INTAKES FOR JET-PROPULSION PLANTS
ALLOYS
BLASTING
CHEMISTRY
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
FERROUS OR NON-FERROUS ALLOYS
GAS-TURBINE PLANTS
GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS
MECHANICAL ENGINEERING
METALLURGY
METALLURGY OF IRON
MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS
TREATMENT OF ALLOYS OR NON-FERROUS METALS
WEAPONS
title Turbine for 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=2025-01-16T08%3A08%3A40IST&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=POHRER%20BENJAMIN&rft.date=2021-11-30&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN113718179A%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