Multi-stage radial compressor unit comprising gas removal during a compressor stage

The invention relates to a radial compressor unit for compressing gas having several compressor stages (11), wherein each compressor stage (11) comprises an impeller (18) having rotor blades (23), a flow channel (24) arranged downstream of the impeller (18) as viewed in the flow direction of the gas...

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Hauptverfasser: BUECHE DIRK, MISCHO BOB, KLEYNHANS GEORGE
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creator BUECHE DIRK
MISCHO BOB
KLEYNHANS GEORGE
description The invention relates to a radial compressor unit for compressing gas having several compressor stages (11), wherein each compressor stage (11) comprises an impeller (18) having rotor blades (23), a flow channel (24) arranged downstream of the impeller (18) as viewed in the flow direction of the gas to be compressed, having a diffusor section (25), a deflection section (26), and a recirculation section (27) having guide blades (28). The gas compressed in a compressor stage (11) can be removed as cooling gas for cooling a component to be cooled, and can be conveyed in the direction of the component to be cooled, wherein the cooling gas can be removed adjacent to an intermediate wall (32) of the compressor stage from the deflection section (26) and/or the recirculation section (27) of the flow channel (24) of the compressor stage (11).
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The gas compressed in a compressor stage (11) can be removed as cooling gas for cooling a component to be cooled, and can be conveyed in the direction of the component to be cooled, wherein the cooling gas can be removed adjacent to an intermediate wall (32) of the compressor stage from the deflection section (26) and/or the recirculation section (27) of the flow channel (24) of the compressor stage (11).</description><language>chi ; eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; WEAPONS</subject><creationdate>2014</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=20141210&amp;DB=EPODOC&amp;CC=CN&amp;NR=104204535A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20141210&amp;DB=EPODOC&amp;CC=CN&amp;NR=104204535A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BUECHE DIRK</creatorcontrib><creatorcontrib>MISCHO BOB</creatorcontrib><creatorcontrib>KLEYNHANS GEORGE</creatorcontrib><title>Multi-stage radial compressor unit comprising gas removal during a compressor stage</title><description>The invention relates to a radial compressor unit for compressing gas having several compressor stages (11), wherein each compressor stage (11) comprises an impeller (18) having rotor blades (23), a flow channel (24) arranged downstream of the impeller (18) as viewed in the flow direction of the gas to be compressed, having a diffusor section (25), a deflection section (26), and a recirculation section (27) having guide blades (28). 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language chi ; eng
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
WEAPONS
title Multi-stage radial compressor unit comprising gas removal during a compressor stage
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