Combustion device of a gas turbine
The combustion device (1) of a gas turbine comprises burners (2) connected to a front plate (5) of a combustion chamber (3). The front plate (5) comprises, spaced apart 5 from one another, a front sheet (8) and an impingement sheets (7) with aligned holes (11, 12) housing the burners (2). A piston r...
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 | TSCHUOR, REMIGI TROBJEVIC, BOGDAN BENZ, URS |
| description | The combustion device (1) of a gas turbine comprises burners (2) connected to a front plate (5) of a combustion chamber (3). The front plate (5) comprises, spaced apart 5 from one another, a front sheet (8) and an impingement sheets (7) with aligned holes (11, 12) housing the burners (2). A piston ring (15) is provided between the front sheet (8) and impingement sheet (7) to seal the holes (11, 12). The axial length of the border of the hole (11, 12) of the 10 front sheet (8) and/or impingement sheet (7) is longer than the thickness of the corresponding front sheet (8) and/or impingement sheet (7). (Fig. 3) Fig. 9 Fig. 1016Fg 8 157 |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_AU2011200401BB2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>AU2011200401BB2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_AU2011200401BB23</originalsourceid><addsrcrecordid>eNrjZFByzs9NKi0uyczPU0hJLctMTlXIT1NIVEhPLFYoKS1KysxL5WFgTUvMKU7lhdLcDCpuriHOHrqpBfnxqcUFicmpeakl8Y6hRgaGhkYGBiYGhk5ORsZEKgMAafEm1g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Combustion device of a gas turbine</title><source>esp@cenet</source><creator>TSCHUOR, REMIGI ; TROBJEVIC, BOGDAN ; BENZ, URS</creator><creatorcontrib>TSCHUOR, REMIGI ; TROBJEVIC, BOGDAN ; BENZ, URS</creatorcontrib><description>The combustion device (1) of a gas turbine comprises burners (2) connected to a front plate (5) of a combustion chamber (3). The front plate (5) comprises, spaced apart 5 from one another, a front sheet (8) and an impingement sheets (7) with aligned holes (11, 12) housing the burners (2). A piston ring (15) is provided between the front sheet (8) and impingement sheet (7) to seal the holes (11, 12). The axial length of the border of the hole (11, 12) of the 10 front sheet (8) and/or impingement sheet (7) is longer than the thickness of the corresponding front sheet (8) and/or impingement sheet (7). (Fig. 3) Fig. 9 Fig. 1016Fg 8 157</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION APPARATUS ; COMBUSTION ENGINES ; COMBUSTION PROCESSES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; 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=20150115&DB=EPODOC&CC=AU&NR=2011200401B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150115&DB=EPODOC&CC=AU&NR=2011200401B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TSCHUOR, REMIGI</creatorcontrib><creatorcontrib>TROBJEVIC, BOGDAN</creatorcontrib><creatorcontrib>BENZ, URS</creatorcontrib><title>Combustion device of a gas turbine</title><description>The combustion device (1) of a gas turbine comprises burners (2) connected to a front plate (5) of a combustion chamber (3). The front plate (5) comprises, spaced apart 5 from one another, a front sheet (8) and an impingement sheets (7) with aligned holes (11, 12) housing the burners (2). A piston ring (15) is provided between the front sheet (8) and impingement sheet (7) to seal the holes (11, 12). The axial length of the border of the hole (11, 12) of the 10 front sheet (8) and/or impingement sheet (7) is longer than the thickness of the corresponding front sheet (8) and/or impingement sheet (7). (Fig. 3) Fig. 9 Fig. 1016Fg 8 157</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION PROCESSES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFByzs9NKi0uyczPU0hJLctMTlXIT1NIVEhPLFYoKS1KysxL5WFgTUvMKU7lhdLcDCpuriHOHrqpBfnxqcUFicmpeakl8Y6hRgaGhkYGBiYGhk5ORsZEKgMAafEm1g</recordid><startdate>20150115</startdate><enddate>20150115</enddate><creator>TSCHUOR, REMIGI</creator><creator>TROBJEVIC, BOGDAN</creator><creator>BENZ, URS</creator><scope>EVB</scope></search><sort><creationdate>20150115</creationdate><title>Combustion device of a gas turbine</title><author>TSCHUOR, REMIGI ; TROBJEVIC, BOGDAN ; BENZ, URS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_AU2011200401BB23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION PROCESSES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>TSCHUOR, REMIGI</creatorcontrib><creatorcontrib>TROBJEVIC, BOGDAN</creatorcontrib><creatorcontrib>BENZ, URS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TSCHUOR, REMIGI</au><au>TROBJEVIC, BOGDAN</au><au>BENZ, URS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Combustion device of a gas turbine</title><date>2015-01-15</date><risdate>2015</risdate><abstract>The combustion device (1) of a gas turbine comprises burners (2) connected to a front plate (5) of a combustion chamber (3). The front plate (5) comprises, spaced apart 5 from one another, a front sheet (8) and an impingement sheets (7) with aligned holes (11, 12) housing the burners (2). A piston ring (15) is provided between the front sheet (8) and impingement sheet (7) to seal the holes (11, 12). The axial length of the border of the hole (11, 12) of the 10 front sheet (8) and/or impingement sheet (7) is longer than the thickness of the corresponding front sheet (8) and/or impingement sheet (7). (Fig. 3) Fig. 9 Fig. 1016Fg 8 157</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_epo_espacenet_AU2011200401BB2 |
| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | Combustion device of 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=2025-01-20T17%3A13%3A11IST&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=TSCHUOR,%20REMIGI&rft.date=2015-01-15&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EAU2011200401BB2%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 |