VARIABLE GEOMETRY TURBOCHARGER
In a variable geometry turbocharger, with a turbine housing having a standar d inlet for exhaust gas and an outlet to the exhaust system of the engine, a volute connected to the inlet and an integral outer nozzle, a plurality of vanes having rotation posts extending from a first surface substantiall...
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creator | SLUPSKI, KEVIN ARNOLD, STEVEN DON MARTIN, STEVEN P KANIGOWSKI, VOYTEK |
description | In a variable geometry turbocharger, with a turbine housing having a standar d inlet for exhaust gas and an outlet to the exhaust system of the engine, a volute connected to the inlet and an integral outer nozzle, a plurality of vanes having rotation posts extending from a first surface substantially parallel to the outer nozzle wall to provide the variable nozzle; the posts received in circumferentially spaced apertures in the outer nozzle wall; the vanes having actuation tabs extending from the opposite surfaces of the vanes; a unison ring engaged between the centre housing and the vanes and having a plurality of profiled slots equal in numb er to the vanes; the slots oriented obliquely to a circumference of the unison ring and receive t he tabs; the profiled surfaces of the slots engage the substantially flat sides of the tabs on different surfaces during the translation to provide optimum control and wear reduction; a radial slot wit h crank shaft having a pin engaging the radial slot to actuate the unison ring, the crank shaft moveable continuously from a first position to a second position to cause the pin to translate in the radial slot; an integral hydraulic actuator providing the actuation mechanism for the crank shaft. |
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the posts received in circumferentially spaced apertures in the outer nozzle wall; the vanes having actuation tabs extending from the opposite surfaces of the vanes; a unison ring engaged between the centre housing and the vanes and having a plurality of profiled slots equal in numb er to the vanes; the slots oriented obliquely to a circumference of the unison ring and receive t he tabs; the profiled surfaces of the slots engage the substantially flat sides of the tabs on different surfaces during the translation to provide optimum control and wear reduction; a radial slot wit h crank shaft having a pin engaging the radial slot to actuate the unison ring, the crank shaft moveable continuously from a first position to a second position to cause the pin to translate in the radial slot; an integral hydraulic actuator providing the actuation mechanism for the crank shaft.</S DOAB></description><language>eng ; fre</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>2008</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=20081202&DB=EPODOC&CC=CA&NR=2349917C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20081202&DB=EPODOC&CC=CA&NR=2349917C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SLUPSKI, KEVIN</creatorcontrib><creatorcontrib>ARNOLD, STEVEN DON</creatorcontrib><creatorcontrib>MARTIN, STEVEN P</creatorcontrib><creatorcontrib>KANIGOWSKI, VOYTEK</creatorcontrib><title>VARIABLE GEOMETRY TURBOCHARGER</title><description>In a variable geometry turbocharger, with a turbine housing having a standar d inlet for exhaust gas and an outlet to the exhaust system of the engine, a volute connected to the inlet and an integral outer nozzle, a plurality of vanes having rotation posts extending from a first surface substantially parallel to the outer nozzle wall to provide the variable nozzle; the posts received in circumferentially spaced apertures in the outer nozzle wall; the vanes having actuation tabs extending from the opposite surfaces of the vanes; a unison ring engaged between the centre housing and the vanes and having a plurality of profiled slots equal in numb er to the vanes; the slots oriented obliquely to a circumference of the unison ring and receive t he tabs; the profiled surfaces of the slots engage the substantially flat sides of the tabs on different surfaces during the translation to provide optimum control and wear reduction; a radial slot wit h crank shaft having a pin engaging the radial slot to actuate the unison ring, the crank shaft moveable continuously from a first position to a second position to cause the pin to translate in the radial slot; an integral hydraulic actuator providing the actuation mechanism for the crank shaft.</S DOAB></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>2008</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJALcwzydHTycVVwd_X3dQ0JilQICQ1y8nf2cAxydw3iYWBNS8wpTuWF0twM8m6uIc4euqkF-fGpxQWJyal5qSXxzo5GxiaWlobmzsaEVQAAQjkgqw</recordid><startdate>20081202</startdate><enddate>20081202</enddate><creator>SLUPSKI, KEVIN</creator><creator>ARNOLD, STEVEN DON</creator><creator>MARTIN, STEVEN P</creator><creator>KANIGOWSKI, VOYTEK</creator><scope>EVB</scope></search><sort><creationdate>20081202</creationdate><title>VARIABLE GEOMETRY TURBOCHARGER</title><author>SLUPSKI, KEVIN ; ARNOLD, STEVEN DON ; MARTIN, STEVEN P ; KANIGOWSKI, VOYTEK</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2349917C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2008</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>SLUPSKI, KEVIN</creatorcontrib><creatorcontrib>ARNOLD, STEVEN DON</creatorcontrib><creatorcontrib>MARTIN, STEVEN P</creatorcontrib><creatorcontrib>KANIGOWSKI, VOYTEK</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SLUPSKI, KEVIN</au><au>ARNOLD, STEVEN DON</au><au>MARTIN, STEVEN P</au><au>KANIGOWSKI, VOYTEK</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>VARIABLE GEOMETRY TURBOCHARGER</title><date>2008-12-02</date><risdate>2008</risdate><abstract>In a variable geometry turbocharger, with a turbine housing having a standar d inlet for exhaust gas and an outlet to the exhaust system of the engine, a volute connected to the inlet and an integral outer nozzle, a plurality of vanes having rotation posts extending from a first surface substantially parallel to the outer nozzle wall to provide the variable nozzle; the posts received in circumferentially spaced apertures in the outer nozzle wall; the vanes having actuation tabs extending from the opposite surfaces of the vanes; a unison ring engaged between the centre housing and the vanes and having a plurality of profiled slots equal in numb er to the vanes; the slots oriented obliquely to a circumference of the unison ring and receive t he tabs; the profiled surfaces of the slots engage the substantially flat sides of the tabs on different surfaces during the translation to provide optimum control and wear reduction; a radial slot wit h crank shaft having a pin engaging the radial slot to actuate the unison ring, the crank shaft moveable continuously from a first position to a second position to cause the pin to translate in the radial slot; an integral hydraulic actuator providing the actuation mechanism for the crank shaft.</S DOAB></abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre |
recordid | cdi_epo_espacenet_CA2349917C |
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 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 | VARIABLE GEOMETRY TURBOCHARGER |
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