Exhaust gas liner used for gas turbine, and gas turbine with the same
An exhaust gas liner (18) for a gas turbine comprises an annular inner shell (21) and an annular outer shell (19), which are arranged concentrically around a machine axis of said gas turbine to define an annular exhaust gas channel in between, whereby said inner shell (21) and/or said outer shell (1...
Gespeichert in:
| Hauptverfasser: | , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng |
| 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 | MLADEN MATAN JUERGEN PACHOLLECK MIRJANA MIHELIC PEDJA MILANKOVIC IGOR MIHALIC CHRISTIAN JOERG KREUTLE |
| description | An exhaust gas liner (18) for a gas turbine comprises an annular inner shell (21) and an annular outer shell (19), which are arranged concentrically around a machine axis of said gas turbine to define an annular exhaust gas channel in between, whereby said inner shell (21) and/or said outer shell (19) are composed of a plurality of liner segments (22, 23; 26, 27; 28), which are attached to a support structure. To compensate thermal expansion and achieving resistance against dynamic loads said liner segments (22, 23; 26, 27; 28) are fixed to said support structure at certain fixation spots (29a-c; 30a-c), which are distributed over the area of said liner segments (22, 23; 26, 27; 28), such that said liner segments (22, 23; 26, 27; 28) are clamped to said support structure through a whole engine thermal cycle without hindering thermal expansion. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN105298562A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN105298562A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN105298562A3</originalsourceid><addsrcrecordid>eNrjZHB1rchILC0uUUhPLFbIycxLLVIoLU5NUUjLLwILlZQWJQFFdRQS81KQBRTKM0syFEoyUhWKE3NTeRhY0xJzilN5oTQ3g6Kba4izh25qQX58anFBYnJqXmpJvLOfoYGpkaWFqZmRozExagCHXzJR</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Exhaust gas liner used for gas turbine, and gas turbine with the same</title><source>esp@cenet</source><creator>MLADEN MATAN ; JUERGEN PACHOLLECK ; MIRJANA MIHELIC ; PEDJA MILANKOVIC ; IGOR MIHALIC ; CHRISTIAN JOERG KREUTLE</creator><creatorcontrib>MLADEN MATAN ; JUERGEN PACHOLLECK ; MIRJANA MIHELIC ; PEDJA MILANKOVIC ; IGOR MIHALIC ; CHRISTIAN JOERG KREUTLE</creatorcontrib><description>An exhaust gas liner (18) for a gas turbine comprises an annular inner shell (21) and an annular outer shell (19), which are arranged concentrically around a machine axis of said gas turbine to define an annular exhaust gas channel in between, whereby said inner shell (21) and/or said outer shell (19) are composed of a plurality of liner segments (22, 23; 26, 27; 28), which are attached to a support structure. To compensate thermal expansion and achieving resistance against dynamic loads said liner segments (22, 23; 26, 27; 28) are fixed to said support structure at certain fixation spots (29a-c; 30a-c), which are distributed over the area of said liner segments (22, 23; 26, 27; 28), such that said liner segments (22, 23; 26, 27; 28) are clamped to said support structure through a whole engine thermal cycle without hindering thermal expansion.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC ; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS ; TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE ; WEAPONS</subject><creationdate>2016</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=20160203&DB=EPODOC&CC=CN&NR=105298562A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160203&DB=EPODOC&CC=CN&NR=105298562A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MLADEN MATAN</creatorcontrib><creatorcontrib>JUERGEN PACHOLLECK</creatorcontrib><creatorcontrib>MIRJANA MIHELIC</creatorcontrib><creatorcontrib>PEDJA MILANKOVIC</creatorcontrib><creatorcontrib>IGOR MIHALIC</creatorcontrib><creatorcontrib>CHRISTIAN JOERG KREUTLE</creatorcontrib><title>Exhaust gas liner used for gas turbine, and gas turbine with the same</title><description>An exhaust gas liner (18) for a gas turbine comprises an annular inner shell (21) and an annular outer shell (19), which are arranged concentrically around a machine axis of said gas turbine to define an annular exhaust gas channel in between, whereby said inner shell (21) and/or said outer shell (19) are composed of a plurality of liner segments (22, 23; 26, 27; 28), which are attached to a support structure. To compensate thermal expansion and achieving resistance against dynamic loads said liner segments (22, 23; 26, 27; 28) are fixed to said support structure at certain fixation spots (29a-c; 30a-c), which are distributed over the area of said liner segments (22, 23; 26, 27; 28), such that said liner segments (22, 23; 26, 27; 28) are clamped to said support structure through a whole engine thermal cycle without hindering thermal expansion.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</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>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</subject><subject>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</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>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</subject><subject>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHB1rchILC0uUUhPLFbIycxLLVIoLU5NUUjLLwILlZQWJQFFdRQS81KQBRTKM0syFEoyUhWKE3NTeRhY0xJzilN5oTQ3g6Kba4izh25qQX58anFBYnJqXmpJvLOfoYGpkaWFqZmRozExagCHXzJR</recordid><startdate>20160203</startdate><enddate>20160203</enddate><creator>MLADEN MATAN</creator><creator>JUERGEN PACHOLLECK</creator><creator>MIRJANA MIHELIC</creator><creator>PEDJA MILANKOVIC</creator><creator>IGOR MIHALIC</creator><creator>CHRISTIAN JOERG KREUTLE</creator><scope>EVB</scope></search><sort><creationdate>20160203</creationdate><title>Exhaust gas liner used for gas turbine, and gas turbine with the same</title><author>MLADEN MATAN ; JUERGEN PACHOLLECK ; MIRJANA MIHELIC ; PEDJA MILANKOVIC ; IGOR MIHALIC ; CHRISTIAN JOERG KREUTLE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN105298562A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2016</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</topic><topic>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</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>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</topic><topic>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>MLADEN MATAN</creatorcontrib><creatorcontrib>JUERGEN PACHOLLECK</creatorcontrib><creatorcontrib>MIRJANA MIHELIC</creatorcontrib><creatorcontrib>PEDJA MILANKOVIC</creatorcontrib><creatorcontrib>IGOR MIHALIC</creatorcontrib><creatorcontrib>CHRISTIAN JOERG KREUTLE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MLADEN MATAN</au><au>JUERGEN PACHOLLECK</au><au>MIRJANA MIHELIC</au><au>PEDJA MILANKOVIC</au><au>IGOR MIHALIC</au><au>CHRISTIAN JOERG KREUTLE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Exhaust gas liner used for gas turbine, and gas turbine with the same</title><date>2016-02-03</date><risdate>2016</risdate><abstract>An exhaust gas liner (18) for a gas turbine comprises an annular inner shell (21) and an annular outer shell (19), which are arranged concentrically around a machine axis of said gas turbine to define an annular exhaust gas channel in between, whereby said inner shell (21) and/or said outer shell (19) are composed of a plurality of liner segments (22, 23; 26, 27; 28), which are attached to a support structure. To compensate thermal expansion and achieving resistance against dynamic loads said liner segments (22, 23; 26, 27; 28) are fixed to said support structure at certain fixation spots (29a-c; 30a-c), which are distributed over the area of said liner segments (22, 23; 26, 27; 28), such that said liner segments (22, 23; 26, 27; 28) are clamped to said support structure through a whole engine thermal cycle without hindering thermal expansion.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_epo_espacenet_CN105298562A |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS |
| title | Exhaust gas liner used for gas turbine, and gas turbine with the same |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-12T02%3A55%3A40IST&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=MLADEN%20MATAN&rft.date=2016-02-03&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN105298562A%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 |