AXIAL COMPRESSOR AND ASSOCIATED OPERATING METHOD

PROBLEM TO BE SOLVED: To provide an axial compressor, especially for a gas turbine, for compressing a flow medium.SOLUTION: The compressor includes a plurality of compressor stator blades, which are assembled to form stator blade rows and fastened in each case on a stator blade carrier, and a plural...

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Hauptverfasser: HOELL HARALD, DUNGS SASCHA, BENKLER FRANCOIS
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creator HOELL HARALD
DUNGS SASCHA
BENKLER FRANCOIS
description PROBLEM TO BE SOLVED: To provide an axial compressor, especially for a gas turbine, for compressing a flow medium.SOLUTION: The compressor includes a plurality of compressor stator blades, which are assembled to form stator blade rows and fastened in each case on a stator blade carrier, and a plurality of compressor rotor blades, which are assembled to form rotor blade rows and fastened in each case on a compressor disk of a compressor shaft, wherein two consecutive compressor disks in each case enclose a hollow space lying between them, and wherein the last compressor disk, as seen in the flow direction of the flow medium, delimits a rear hollow space.
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BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; 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 ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; STEAM ENGINES ; WEAPONS</subject><creationdate>2012</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=20120524&amp;DB=EPODOC&amp;CC=JP&amp;NR=2012097748A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20120524&amp;DB=EPODOC&amp;CC=JP&amp;NR=2012097748A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HOELL HARALD</creatorcontrib><creatorcontrib>DUNGS SASCHA</creatorcontrib><creatorcontrib>BENKLER FRANCOIS</creatorcontrib><title>AXIAL COMPRESSOR AND ASSOCIATED OPERATING METHOD</title><description>PROBLEM TO BE SOLVED: To provide an axial compressor, especially for a gas turbine, for compressing a flow medium.SOLUTION: The compressor includes a plurality of compressor stator blades, which are assembled to form stator blade rows and fastened in each case on a stator blade carrier, and a plurality of compressor rotor blades, which are assembled to form rotor blade rows and fastened in each case on a compressor disk of a compressor shaft, wherein two consecutive compressor disks in each case enclose a hollow space lying between them, and wherein the last compressor disk, as seen in the flow direction of the flow medium, delimits a rear hollow space.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</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>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>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2012</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDBwjPB09FFw9vcNCHINDvYPUnD0c1FwBLKcPR1DXF0U_ANcgxxDPP3cFXxdQzz8XXgYWNMSc4pTeaE0N4OSm2uIs4duakF-fGpxQWJyal5qSbxXgJGBoZGBpbm5iYWjMVGKAH8dJtQ</recordid><startdate>20120524</startdate><enddate>20120524</enddate><creator>HOELL HARALD</creator><creator>DUNGS SASCHA</creator><creator>BENKLER FRANCOIS</creator><scope>EVB</scope></search><sort><creationdate>20120524</creationdate><title>AXIAL COMPRESSOR AND ASSOCIATED OPERATING METHOD</title><author>HOELL HARALD ; 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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
STEAM ENGINES
WEAPONS
title AXIAL COMPRESSOR AND ASSOCIATED OPERATING METHOD
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