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...
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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&date=20150620&DB=EPODOC&CC=CA&NR=2875408A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150620&DB=EPODOC&CC=CA&NR=2875408A1$$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> |
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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 |
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