SEAL SYSTEM FOR A GAS TURBINE

The disclosure pertains to a seal system for a passage between a turbine stator (49, 50) and a turbine rotor (47, 48), comprising: a first arm (6) extending radially outwards from the turbine rotor (47, 48) and toward the first seal (8) arranged on the stator (49, 50), and terminating short of the f...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: SIMON-DELGADO, CARLOS, WIDMER, MARC, FILKORN, GUENTER, DIDION, CHRISTOPH, SCHAEFER, MARTIN
Format: Patent
Sprache:eng ; fre
Schlagworte:
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 SIMON-DELGADO, CARLOS
WIDMER, MARC
FILKORN, GUENTER
DIDION, CHRISTOPH
SCHAEFER, MARTIN
description The disclosure pertains to a seal system for a passage between a turbine stator (49, 50) and a turbine rotor (47, 48), comprising: a first arm (6) extending radially outwards from the turbine rotor (47, 48) and toward the first seal (8) arranged on the stator (49, 50), and terminating short of the first seal (8) thereby creating a first gap (9) between the first seal (8) and the first arm(6). The seal system further comprises a second seal (12) arranged on the turbine stator (49, 50), and a second arm (10) extending axially from the turbine rotor (47, 48) towards the second seal base (11), and terminating short of the second seal (12) thereby creating a second gap (13) between the second seal (12) and the second arm (10). The disclosure further refers to a gas turbine comprising such a seal system.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CA2875408A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CA2875408A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CA2875408A13</originalsourceid><addsrcrecordid>eNrjZJANdnX0UQiODA5x9VVw8w9ScFRwdwxWCAkNcvL0c-VhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfHOjkYW5qYmBhaOhsZEKAEANl8gVA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>SEAL SYSTEM FOR A GAS TURBINE</title><source>esp@cenet</source><creator>SIMON-DELGADO, CARLOS ; WIDMER, MARC ; FILKORN, GUENTER ; DIDION, CHRISTOPH ; SCHAEFER, MARTIN</creator><creatorcontrib>SIMON-DELGADO, CARLOS ; WIDMER, MARC ; FILKORN, GUENTER ; DIDION, CHRISTOPH ; SCHAEFER, MARTIN</creatorcontrib><description>The disclosure pertains to a seal system for a passage between a turbine stator (49, 50) and a turbine rotor (47, 48), comprising: a first arm (6) extending radially outwards from the turbine rotor (47, 48) and toward the first seal (8) arranged on the stator (49, 50), and terminating short of the first seal (8) thereby creating a first gap (9) between the first seal (8) and the first arm(6). The seal system further comprises a second seal (12) arranged on the turbine stator (49, 50), and a second arm (10) extending axially from the turbine rotor (47, 48) towards the second seal base (11), and terminating short of the second seal (12) thereby creating a second gap (13) between the second seal (12) and the second arm (10). The disclosure further refers to a gas turbine comprising such a seal system.</description><language>eng ; fre</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2015</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=20150620&amp;DB=EPODOC&amp;CC=CA&amp;NR=2875408A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20150620&amp;DB=EPODOC&amp;CC=CA&amp;NR=2875408A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SIMON-DELGADO, CARLOS</creatorcontrib><creatorcontrib>WIDMER, MARC</creatorcontrib><creatorcontrib>FILKORN, GUENTER</creatorcontrib><creatorcontrib>DIDION, CHRISTOPH</creatorcontrib><creatorcontrib>SCHAEFER, MARTIN</creatorcontrib><title>SEAL SYSTEM FOR A GAS TURBINE</title><description>The disclosure pertains to a seal system for a passage between a turbine stator (49, 50) and a turbine rotor (47, 48), comprising: a first arm (6) extending radially outwards from the turbine rotor (47, 48) and toward the first seal (8) arranged on the stator (49, 50), and terminating short of the first seal (8) thereby creating a first gap (9) between the first seal (8) and the first arm(6). The seal system further comprises a second seal (12) arranged on the turbine stator (49, 50), and a second arm (10) extending axially from the turbine rotor (47, 48) towards the second seal base (11), and terminating short of the second seal (12) thereby creating a second gap (13) between the second seal (12) and the second arm (10). The disclosure further refers to a gas turbine comprising such a seal system.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJANdnX0UQiODA5x9VVw8w9ScFRwdwxWCAkNcvL0c-VhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfHOjkYW5qYmBhaOhsZEKAEANl8gVA</recordid><startdate>20150620</startdate><enddate>20150620</enddate><creator>SIMON-DELGADO, CARLOS</creator><creator>WIDMER, MARC</creator><creator>FILKORN, GUENTER</creator><creator>DIDION, CHRISTOPH</creator><creator>SCHAEFER, MARTIN</creator><scope>EVB</scope></search><sort><creationdate>20150620</creationdate><title>SEAL SYSTEM FOR A GAS TURBINE</title><author>SIMON-DELGADO, CARLOS ; WIDMER, MARC ; FILKORN, GUENTER ; DIDION, CHRISTOPH ; SCHAEFER, MARTIN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2875408A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2015</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</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>SIMON-DELGADO, CARLOS</creatorcontrib><creatorcontrib>WIDMER, MARC</creatorcontrib><creatorcontrib>FILKORN, GUENTER</creatorcontrib><creatorcontrib>DIDION, CHRISTOPH</creatorcontrib><creatorcontrib>SCHAEFER, MARTIN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SIMON-DELGADO, CARLOS</au><au>WIDMER, MARC</au><au>FILKORN, GUENTER</au><au>DIDION, CHRISTOPH</au><au>SCHAEFER, MARTIN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SEAL SYSTEM FOR A GAS TURBINE</title><date>2015-06-20</date><risdate>2015</risdate><abstract>The disclosure pertains to a seal system for a passage between a turbine stator (49, 50) and a turbine rotor (47, 48), comprising: a first arm (6) extending radially outwards from the turbine rotor (47, 48) and toward the first seal (8) arranged on the stator (49, 50), and terminating short of the first seal (8) thereby creating a first gap (9) between the first seal (8) and the first arm(6). The seal system further comprises a second seal (12) arranged on the turbine stator (49, 50), and a second arm (10) extending axially from the turbine rotor (47, 48) towards the second seal base (11), and terminating short of the second seal (12) thereby creating a second gap (13) between the second seal (12) and the second arm (10). The disclosure further refers to a gas turbine comprising such a seal system.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre
recordid cdi_epo_espacenet_CA2875408A1
source esp@cenet
subjects BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
title SEAL SYSTEM FOR A GAS TURBINE
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T05%3A42%3A10IST&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=SIMON-DELGADO,%20CARLOS&rft.date=2015-06-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECA2875408A1%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