COMBUSTOR FRONT ASSEMBLY FOR A GAS TURBINE
A combustor front assembly for a gas turbine power plant, wherein the combustor front assembly is provided with at least a through hole for allowing the gas flow to come into a combustion chamber, the combustor front assembly comprising: - a combustor front plate having at least a through hole and p...
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| creator | BEG, Marijan SIEWERT, Piotr BENZ, Urs BELINA, Ivo CVITAK, Branko |
| description | A combustor front assembly for a gas turbine power plant, wherein the combustor front assembly is provided with at least a through hole for allowing the gas flow to come into a combustion chamber, the combustor front assembly comprising:
- a combustor front plate having at least a through hole and provided with an outer surface outside the combustor chamber;
- at least a combustor front segment having a through hole and coupled with the outer surface of the combustor front plate so that the through hole of the front segment is aligned with the through hole of the front plate;
wherein
the combustor front segment is clamped in position and forced against the outer surface of the combustor front plate. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3299720A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3299720A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3299720A13</originalsourceid><addsrcrecordid>eNrjZNBy9vd1Cg0O8Q9ScAvy9wtRcAwOdvV18olUcAMKOSq4OwYrhIQGOXn6ufIwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUknjXAGMjS0tzIwNHQ2MilAAACwYkPA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>COMBUSTOR FRONT ASSEMBLY FOR A GAS TURBINE</title><source>esp@cenet</source><creator>BEG, Marijan ; SIEWERT, Piotr ; BENZ, Urs ; BELINA, Ivo ; CVITAK, Branko</creator><creatorcontrib>BEG, Marijan ; SIEWERT, Piotr ; BENZ, Urs ; BELINA, Ivo ; CVITAK, Branko</creatorcontrib><description>A combustor front assembly for a gas turbine power plant, wherein the combustor front assembly is provided with at least a through hole for allowing the gas flow to come into a combustion chamber, the combustor front assembly comprising:
- a combustor front plate having at least a through hole and provided with an outer surface outside the combustor chamber;
- at least a combustor front segment having a through hole and coupled with the outer surface of the combustor front plate so that the through hole of the front segment is aligned with the through hole of the front plate;
wherein
the combustor front segment is clamped in position and forced against the outer surface of the combustor front plate.</description><language>eng ; fre ; ger</language><subject>BLASTING ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2018</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=20180328&DB=EPODOC&CC=EP&NR=3299720A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180328&DB=EPODOC&CC=EP&NR=3299720A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BEG, Marijan</creatorcontrib><creatorcontrib>SIEWERT, Piotr</creatorcontrib><creatorcontrib>BENZ, Urs</creatorcontrib><creatorcontrib>BELINA, Ivo</creatorcontrib><creatorcontrib>CVITAK, Branko</creatorcontrib><title>COMBUSTOR FRONT ASSEMBLY FOR A GAS TURBINE</title><description>A combustor front assembly for a gas turbine power plant, wherein the combustor front assembly is provided with at least a through hole for allowing the gas flow to come into a combustion chamber, the combustor front assembly comprising:
- a combustor front plate having at least a through hole and provided with an outer surface outside the combustor chamber;
- at least a combustor front segment having a through hole and coupled with the outer surface of the combustor front plate so that the through hole of the front segment is aligned with the through hole of the front plate;
wherein
the combustor front segment is clamped in position and forced against the outer surface of the combustor front plate.</description><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION PROCESSES</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNBy9vd1Cg0O8Q9ScAvy9wtRcAwOdvV18olUcAMKOSq4OwYrhIQGOXn6ufIwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUknjXAGMjS0tzIwNHQ2MilAAACwYkPA</recordid><startdate>20180328</startdate><enddate>20180328</enddate><creator>BEG, Marijan</creator><creator>SIEWERT, Piotr</creator><creator>BENZ, Urs</creator><creator>BELINA, Ivo</creator><creator>CVITAK, Branko</creator><scope>EVB</scope></search><sort><creationdate>20180328</creationdate><title>COMBUSTOR FRONT ASSEMBLY FOR A GAS TURBINE</title><author>BEG, Marijan ; SIEWERT, Piotr ; BENZ, Urs ; BELINA, Ivo ; CVITAK, Branko</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3299720A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</creationdate><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION PROCESSES</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>BEG, Marijan</creatorcontrib><creatorcontrib>SIEWERT, Piotr</creatorcontrib><creatorcontrib>BENZ, Urs</creatorcontrib><creatorcontrib>BELINA, Ivo</creatorcontrib><creatorcontrib>CVITAK, Branko</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BEG, Marijan</au><au>SIEWERT, Piotr</au><au>BENZ, Urs</au><au>BELINA, Ivo</au><au>CVITAK, Branko</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMBUSTOR FRONT ASSEMBLY FOR A GAS TURBINE</title><date>2018-03-28</date><risdate>2018</risdate><abstract>A combustor front assembly for a gas turbine power plant, wherein the combustor front assembly is provided with at least a through hole for allowing the gas flow to come into a combustion chamber, the combustor front assembly comprising:
- a combustor front plate having at least a through hole and provided with an outer surface outside the combustor chamber;
- at least a combustor front segment having a through hole and coupled with the outer surface of the combustor front plate so that the through hole of the front segment is aligned with the through hole of the front plate;
wherein
the combustor front segment is clamped in position and forced against the outer surface of the combustor front plate.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| source | esp@cenet |
| subjects | BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | COMBUSTOR FRONT ASSEMBLY 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=2025-02-11T03%3A31%3A14IST&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=BEG,%20Marijan&rft.date=2018-03-28&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3299720A1%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 |