TURBINENSCHAUFEL FÜR EINE TURBINE MIT EINEM KÜHLMITTELKANAL

The blade has a platform (16) for defining a flow channel in a turbine, where the platform has a coolant channel (20), which extends in the platform and guides the coolant. The coolant channel leads to two connection openings of the platform. An auxiliary component (24,26) is fastened at the platfor...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: GOLDSCHMIDT, DIRK, PICKERT, URSULA, MUENZER, JAN, OECHSNER, MATTHIAS, KUEPERKOCH, RUDOLF, BUCHAL, TOBIAS, KOCH, TORSTEN, MATTHEIS, THORSTEN, BOSTANJOGLO, GEORG, MUESGEN, RALF, VOSBERG, VOLKER, BERGANDER, KATHARINA, ESSER, WINFRIED
Format: Patent
Sprache:ger
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator GOLDSCHMIDT, DIRK
PICKERT, URSULA
MUENZER, JAN
OECHSNER, MATTHIAS
KUEPERKOCH, RUDOLF
BUCHAL, TOBIAS
KOCH, TORSTEN
MATTHEIS, THORSTEN
BOSTANJOGLO, GEORG
MUESGEN, RALF
VOSBERG, VOLKER
BERGANDER, KATHARINA
ESSER, WINFRIED
description The blade has a platform (16) for defining a flow channel in a turbine, where the platform has a coolant channel (20), which extends in the platform and guides the coolant. The coolant channel leads to two connection openings of the platform. An auxiliary component (24,26) is fastened at the platform, and has a connecting channel (28), which connects the openings with each other in a fluid-conductive manner. The platform extends transverse to a longitudinal extension of the blade along a main defining surface (30), and has front surfaces, which are arranged transverse to the extension.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_ATE459447TT1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ATE459447TT1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_ATE459447TT13</originalsourceid><addsrcrecordid>eNrjZLANCQ1y8vRz9Qt29nAMdXP1UXA7PCdIwRUopACVUvD1DAEL-Cp4H57j4QPkhrj6eDv6OfrwMLCmJeYUp_JCaW4GRTfXEGcP3dSC_PjU4oLE5NS81JJ4xxBXE1NLExPzkBBDY2LUAAAMaCw3</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>TURBINENSCHAUFEL FÜR EINE TURBINE MIT EINEM KÜHLMITTELKANAL</title><source>esp@cenet</source><creator>GOLDSCHMIDT, DIRK ; PICKERT, URSULA ; MUENZER, JAN ; OECHSNER, MATTHIAS ; KUEPERKOCH, RUDOLF ; BUCHAL, TOBIAS ; KOCH, TORSTEN ; MATTHEIS, THORSTEN ; BOSTANJOGLO, GEORG ; MUESGEN, RALF ; VOSBERG, VOLKER ; BERGANDER, KATHARINA ; ESSER, WINFRIED</creator><creatorcontrib>GOLDSCHMIDT, DIRK ; PICKERT, URSULA ; MUENZER, JAN ; OECHSNER, MATTHIAS ; KUEPERKOCH, RUDOLF ; BUCHAL, TOBIAS ; KOCH, TORSTEN ; MATTHEIS, THORSTEN ; BOSTANJOGLO, GEORG ; MUESGEN, RALF ; VOSBERG, VOLKER ; BERGANDER, KATHARINA ; ESSER, WINFRIED</creatorcontrib><description>The blade has a platform (16) for defining a flow channel in a turbine, where the platform has a coolant channel (20), which extends in the platform and guides the coolant. The coolant channel leads to two connection openings of the platform. An auxiliary component (24,26) is fastened at the platform, and has a connecting channel (28), which connects the openings with each other in a fluid-conductive manner. The platform extends transverse to a longitudinal extension of the blade along a main defining surface (30), and has front surfaces, which are arranged transverse to the extension.</description><language>ger</language><creationdate>2010</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=20100315&amp;DB=EPODOC&amp;CC=AT&amp;NR=E459447T1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25555,76308</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20100315&amp;DB=EPODOC&amp;CC=AT&amp;NR=E459447T1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GOLDSCHMIDT, DIRK</creatorcontrib><creatorcontrib>PICKERT, URSULA</creatorcontrib><creatorcontrib>MUENZER, JAN</creatorcontrib><creatorcontrib>OECHSNER, MATTHIAS</creatorcontrib><creatorcontrib>KUEPERKOCH, RUDOLF</creatorcontrib><creatorcontrib>BUCHAL, TOBIAS</creatorcontrib><creatorcontrib>KOCH, TORSTEN</creatorcontrib><creatorcontrib>MATTHEIS, THORSTEN</creatorcontrib><creatorcontrib>BOSTANJOGLO, GEORG</creatorcontrib><creatorcontrib>MUESGEN, RALF</creatorcontrib><creatorcontrib>VOSBERG, VOLKER</creatorcontrib><creatorcontrib>BERGANDER, KATHARINA</creatorcontrib><creatorcontrib>ESSER, WINFRIED</creatorcontrib><title>TURBINENSCHAUFEL FÜR EINE TURBINE MIT EINEM KÜHLMITTELKANAL</title><description>The blade has a platform (16) for defining a flow channel in a turbine, where the platform has a coolant channel (20), which extends in the platform and guides the coolant. The coolant channel leads to two connection openings of the platform. An auxiliary component (24,26) is fastened at the platform, and has a connecting channel (28), which connects the openings with each other in a fluid-conductive manner. The platform extends transverse to a longitudinal extension of the blade along a main defining surface (30), and has front surfaces, which are arranged transverse to the extension.</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2010</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLANCQ1y8vRz9Qt29nAMdXP1UXA7PCdIwRUopACVUvD1DAEL-Cp4H57j4QPkhrj6eDv6OfrwMLCmJeYUp_JCaW4GRTfXEGcP3dSC_PjU4oLE5NS81JJ4xxBXE1NLExPzkBBDY2LUAAAMaCw3</recordid><startdate>20100315</startdate><enddate>20100315</enddate><creator>GOLDSCHMIDT, DIRK</creator><creator>PICKERT, URSULA</creator><creator>MUENZER, JAN</creator><creator>OECHSNER, MATTHIAS</creator><creator>KUEPERKOCH, RUDOLF</creator><creator>BUCHAL, TOBIAS</creator><creator>KOCH, TORSTEN</creator><creator>MATTHEIS, THORSTEN</creator><creator>BOSTANJOGLO, GEORG</creator><creator>MUESGEN, RALF</creator><creator>VOSBERG, VOLKER</creator><creator>BERGANDER, KATHARINA</creator><creator>ESSER, WINFRIED</creator><scope>EVB</scope></search><sort><creationdate>20100315</creationdate><title>TURBINENSCHAUFEL FÜR EINE TURBINE MIT EINEM KÜHLMITTELKANAL</title><author>GOLDSCHMIDT, DIRK ; PICKERT, URSULA ; MUENZER, JAN ; OECHSNER, MATTHIAS ; KUEPERKOCH, RUDOLF ; BUCHAL, TOBIAS ; KOCH, TORSTEN ; MATTHEIS, THORSTEN ; BOSTANJOGLO, GEORG ; MUESGEN, RALF ; VOSBERG, VOLKER ; BERGANDER, KATHARINA ; ESSER, WINFRIED</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_ATE459447TT13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ger</language><creationdate>2010</creationdate><toplevel>online_resources</toplevel><creatorcontrib>GOLDSCHMIDT, DIRK</creatorcontrib><creatorcontrib>PICKERT, URSULA</creatorcontrib><creatorcontrib>MUENZER, JAN</creatorcontrib><creatorcontrib>OECHSNER, MATTHIAS</creatorcontrib><creatorcontrib>KUEPERKOCH, RUDOLF</creatorcontrib><creatorcontrib>BUCHAL, TOBIAS</creatorcontrib><creatorcontrib>KOCH, TORSTEN</creatorcontrib><creatorcontrib>MATTHEIS, THORSTEN</creatorcontrib><creatorcontrib>BOSTANJOGLO, GEORG</creatorcontrib><creatorcontrib>MUESGEN, RALF</creatorcontrib><creatorcontrib>VOSBERG, VOLKER</creatorcontrib><creatorcontrib>BERGANDER, KATHARINA</creatorcontrib><creatorcontrib>ESSER, WINFRIED</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GOLDSCHMIDT, DIRK</au><au>PICKERT, URSULA</au><au>MUENZER, JAN</au><au>OECHSNER, MATTHIAS</au><au>KUEPERKOCH, RUDOLF</au><au>BUCHAL, TOBIAS</au><au>KOCH, TORSTEN</au><au>MATTHEIS, THORSTEN</au><au>BOSTANJOGLO, GEORG</au><au>MUESGEN, RALF</au><au>VOSBERG, VOLKER</au><au>BERGANDER, KATHARINA</au><au>ESSER, WINFRIED</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBINENSCHAUFEL FÜR EINE TURBINE MIT EINEM KÜHLMITTELKANAL</title><date>2010-03-15</date><risdate>2010</risdate><abstract>The blade has a platform (16) for defining a flow channel in a turbine, where the platform has a coolant channel (20), which extends in the platform and guides the coolant. The coolant channel leads to two connection openings of the platform. An auxiliary component (24,26) is fastened at the platform, and has a connecting channel (28), which connects the openings with each other in a fluid-conductive manner. The platform extends transverse to a longitudinal extension of the blade along a main defining surface (30), and has front surfaces, which are arranged transverse to the extension.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language ger
recordid cdi_epo_espacenet_ATE459447TT1
source esp@cenet
title TURBINENSCHAUFEL FÜR EINE TURBINE MIT EINEM KÜHLMITTELKANAL
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-14T22%3A17%3A12IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=GOLDSCHMIDT,%20DIRK&rft.date=2010-03-15&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EATE459447TT1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true