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...
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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 |
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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&date=20211130&DB=EPODOC&CC=CN&NR=113718179A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20211130&DB=EPODOC&CC=CN&NR=113718179A$$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> |
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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 |
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