Stellhebel für Turbinen-VTG
Die vorliegende Erfindung betrifft einen Hebel (10) für ein VTG-Leitgitter (1) einer Radialturbine (110). Der Hebel (10) umfasst einen Grundkörper (12), der einen gabelförmigen Koppelabschnitt (14) mit zwei Schenkeln (15) umfasst. An einer Innenseite (15a) von zumindest einem der Schenkel (15) ist e...
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| creator | Ramb, Thomas Kanoffsky, Nico |
| description | Die vorliegende Erfindung betrifft einen Hebel (10) für ein VTG-Leitgitter (1) einer Radialturbine (110). Der Hebel (10) umfasst einen Grundkörper (12), der einen gabelförmigen Koppelabschnitt (14) mit zwei Schenkeln (15) umfasst. An einer Innenseite (15a) von zumindest einem der Schenkel (15) ist ein verschleißfester Kontaktblock (16) angeordnet. Der verschleißfeste Kontaktblock (16) ist zum operativen Eingriff mit einem Verstellring (20) des VTG-Leitgitters (1) ausgebildet.
A lever for a VTG guide vane arrangement of a radial turbine with a main body with a fork-shaped coupling section with two limbs. A wear-resistant contact block is arranged on an inner side of at least one of the limbs. The wear-resistant contact block is designed for operative engagement with an adjusting ring of the VTG guide van arrangement, giving rise to the effect of increased wear resistance at least in the region of the engagement with the VTG guide vane arrangement. Furthermore, a VTG guide vane arrangement having such a lever, a radial turbine having such a VTG guide vane arrangement, and a supercharging device having such a radial turbine. |
| format | Patent |
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A lever for a VTG guide vane arrangement of a radial turbine with a main body with a fork-shaped coupling section with two limbs. A wear-resistant contact block is arranged on an inner side of at least one of the limbs. The wear-resistant contact block is designed for operative engagement with an adjusting ring of the VTG guide van arrangement, giving rise to the effect of increased wear resistance at least in the region of the engagement with the VTG guide vane arrangement. Furthermore, a VTG guide vane arrangement having such a lever, a radial turbine having such a VTG guide vane arrangement, and a supercharging device having such a radial turbine.</description><language>ger</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>2023</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=20230427&DB=EPODOC&CC=DE&NR=102022209202A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230427&DB=EPODOC&CC=DE&NR=102022209202A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Ramb, Thomas</creatorcontrib><creatorcontrib>Kanoffsky, Nico</creatorcontrib><title>Stellhebel für Turbinen-VTG</title><description>Die vorliegende Erfindung betrifft einen Hebel (10) für ein VTG-Leitgitter (1) einer Radialturbine (110). Der Hebel (10) umfasst einen Grundkörper (12), der einen gabelförmigen Koppelabschnitt (14) mit zwei Schenkeln (15) umfasst. An einer Innenseite (15a) von zumindest einem der Schenkel (15) ist ein verschleißfester Kontaktblock (16) angeordnet. Der verschleißfeste Kontaktblock (16) ist zum operativen Eingriff mit einem Verstellring (20) des VTG-Leitgitters (1) ausgebildet.
A lever for a VTG guide vane arrangement of a radial turbine with a main body with a fork-shaped coupling section with two limbs. A wear-resistant contact block is arranged on an inner side of at least one of the limbs. The wear-resistant contact block is designed for operative engagement with an adjusting ring of the VTG guide van arrangement, giving rise to the effect of increased wear resistance at least in the region of the engagement with the VTG guide vane arrangement. Furthermore, a VTG guide vane arrangement having such a lever, a radial turbine having such a VTG guide vane arrangement, and a supercharging device having such a radial turbine.</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>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJAJLknNyclITUrNUUg7vKdIIaS0KCkzLzVPNyzEnYeBNS0xpziVF0pzM6i6uYY4e-imFuTHpxYXJCan5qWWxLu4GhoYGRgZGRlYAilHQ2Ni1QEA1nslaQ</recordid><startdate>20230427</startdate><enddate>20230427</enddate><creator>Ramb, Thomas</creator><creator>Kanoffsky, Nico</creator><scope>EVB</scope></search><sort><creationdate>20230427</creationdate><title>Stellhebel für Turbinen-VTG</title><author>Ramb, Thomas ; Kanoffsky, Nico</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE102022209202A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ger</language><creationdate>2023</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>Ramb, Thomas</creatorcontrib><creatorcontrib>Kanoffsky, Nico</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Ramb, Thomas</au><au>Kanoffsky, Nico</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Stellhebel für Turbinen-VTG</title><date>2023-04-27</date><risdate>2023</risdate><abstract>Die vorliegende Erfindung betrifft einen Hebel (10) für ein VTG-Leitgitter (1) einer Radialturbine (110). Der Hebel (10) umfasst einen Grundkörper (12), der einen gabelförmigen Koppelabschnitt (14) mit zwei Schenkeln (15) umfasst. An einer Innenseite (15a) von zumindest einem der Schenkel (15) ist ein verschleißfester Kontaktblock (16) angeordnet. Der verschleißfeste Kontaktblock (16) ist zum operativen Eingriff mit einem Verstellring (20) des VTG-Leitgitters (1) ausgebildet.
A lever for a VTG guide vane arrangement of a radial turbine with a main body with a fork-shaped coupling section with two limbs. A wear-resistant contact block is arranged on an inner side of at least one of the limbs. The wear-resistant contact block is designed for operative engagement with an adjusting ring of the VTG guide van arrangement, giving rise to the effect of increased wear resistance at least in the region of the engagement with the VTG guide vane arrangement. Furthermore, a VTG guide vane arrangement having such a lever, a radial turbine having such a VTG guide vane arrangement, and a supercharging device having such a radial turbine.</abstract><oa>free_for_read</oa></addata></record> |
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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 | Stellhebel für Turbinen-VTG |
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