Compressor in particular for turbocharger
A compressor comprising an impeller (1) and diffuser (3) with a number of diffuser vanes (13) wherein the diffuser is located downstream of the impeller (1) in a flow direction (F) of a fluid compressed by the compressor is provided. Each diffuser vane (13) has a leading edge (21) which faces the fl...
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| creator | ROACH, PAUL DR |
| description | A compressor comprising an impeller (1) and diffuser (3) with a number of diffuser vanes (13) wherein the diffuser is located downstream of the impeller (1) in a flow direction (F) of a fluid compressed by the compressor is provided. Each diffuser vane (13) has a leading edge (21) which faces the flow direction (F) and which includes a cut back region (19). The cut back region is locally inclined to the flow direction (F) by an angle ± of not more than 65 degrees. |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP1873402A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP1873402A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP1873402A13</originalsourceid><addsrcrecordid>eNrjZNB0zs8tKEotLs4vUsjMUyhILCrJTC7NSSxSSAOKlJQWJeUnZyQWpacW8TCwpiXmFKfyQmluBgU31xBnD93Ugvz41OKCxOTUvNSSeNcAQwtzYxMDI0dDYyKUAADhASi0</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Compressor in particular for turbocharger</title><source>esp@cenet</source><creator>ROACH, PAUL DR</creator><creatorcontrib>ROACH, PAUL DR</creatorcontrib><description>A compressor comprising an impeller (1) and diffuser (3) with a number of diffuser vanes (13) wherein the diffuser is located downstream of the impeller (1) in a flow direction (F) of a fluid compressed by the compressor is provided. Each diffuser vane (13) has a leading edge (21) which faces the flow direction (F) and which includes a cut back region (19). The cut back region is locally inclined to the flow direction (F) by an angle ± of not more than 65 degrees.</description><language>eng ; fre ; ger</language><subject>BLASTING ; HEATING ; INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS ; INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 ; LIGHTING ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; 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=20080102&DB=EPODOC&CC=EP&NR=1873402A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20080102&DB=EPODOC&CC=EP&NR=1873402A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ROACH, PAUL DR</creatorcontrib><title>Compressor in particular for turbocharger</title><description>A compressor comprising an impeller (1) and diffuser (3) with a number of diffuser vanes (13) wherein the diffuser is located downstream of the impeller (1) in a flow direction (F) of a fluid compressed by the compressor is provided. Each diffuser vane (13) has a leading edge (21) which faces the flow direction (F) and which includes a cut back region (19). The cut back region is locally inclined to the flow direction (F) by an angle ± of not more than 65 degrees.</description><subject>BLASTING</subject><subject>HEATING</subject><subject>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</subject><subject>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2008</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB0zs8tKEotLs4vUsjMUyhILCrJTC7NSSxSSAOKlJQWJeUnZyQWpacW8TCwpiXmFKfyQmluBgU31xBnD93Ugvz41OKCxOTUvNSSeNcAQwtzYxMDI0dDYyKUAADhASi0</recordid><startdate>20080102</startdate><enddate>20080102</enddate><creator>ROACH, PAUL DR</creator><scope>EVB</scope></search><sort><creationdate>20080102</creationdate><title>Compressor in particular for turbocharger</title><author>ROACH, PAUL DR</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP1873402A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2008</creationdate><topic>BLASTING</topic><topic>HEATING</topic><topic>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</topic><topic>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ROACH, PAUL DR</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ROACH, PAUL DR</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Compressor in particular for turbocharger</title><date>2008-01-02</date><risdate>2008</risdate><abstract>A compressor comprising an impeller (1) and diffuser (3) with a number of diffuser vanes (13) wherein the diffuser is located downstream of the impeller (1) in a flow direction (F) of a fluid compressed by the compressor is provided. Each diffuser vane (13) has a leading edge (21) which faces the flow direction (F) and which includes a cut back region (19). The cut back region is locally inclined to the flow direction (F) by an angle ± of not more than 65 degrees.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | BLASTING HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS |
| title | Compressor in particular for turbocharger |
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