Combustor part of combustor and combustor of gas turbine having such combustor part
The invention relates to a burner part (01) of a burner. The burner has a flow channel in which combustion air flows from upstream to downstream in a flow direction (05). In this case, the burner component (01) comprises a wall section (03) adjoining the flow channel and a plurality of nozzles (21,...
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| creator | VOGMANN DANIEL DEDERICHS STEFAN SCHMITZ UDO KALLURI, RAMSATISH SCHULTZ ANATOLE HUTH MICHAEL |
| description | The invention relates to a burner part (01) of a burner. The burner has a flow channel in which combustion air flows from upstream to downstream in a flow direction (05). In this case, the burner component (01) comprises a wall section (03) adjoining the flow channel and a plurality of nozzles (21, 22) arranged in the wall section (03); and a plurality of vortex generators (11) arranged on the wall section (03). In order to improve the distribution of the fuel in the combustion air, it is proposed that the vortex generator (11) has a ramp (12) which rises in the flow direction (05) and which is concavely curved.
本发明涉及一种燃烧器的燃烧器部件(01)。燃烧器具有流动通道，在所述流动通道中，助燃空气在流动方向(05)上从上游朝向下游流动。在此，燃烧器部件(01)包括：邻接于流动通道的壁部段(03)和多个设置在壁部段(03)中的喷嘴(21，22)；以及多个设置在壁部段(03)上的涡流发生器(11)。为了改进燃料在助燃空气中的分布提出，涡流发生器(11)具有在流动方向(05)上升高的斜面(12)，所述斜面凹形地拱曲。 |
| format | Patent |
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本发明涉及一种燃烧器的燃烧器部件(01)。燃烧器具有流动通道，在所述流动通道中，助燃空气在流动方向(05)上从上游朝向下游流动。在此，燃烧器部件(01)包括：邻接于流动通道的壁部段(03)和多个设置在壁部段(03)中的喷嘴(21，22)；以及多个设置在壁部段(03)上的涡流发生器(11)。为了改进燃料在助燃空气中的分布提出，涡流发生器(11)具有在流动方向(05)上升高的斜面(12)，所述斜面凹形地拱曲。</description><language>chi ; eng</language><subject>BLASTING ; BURNERS ; 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>2022</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=20221118&DB=EPODOC&CC=CN&NR=115362333A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221118&DB=EPODOC&CC=CN&NR=115362333A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>VOGMANN DANIEL</creatorcontrib><creatorcontrib>DEDERICHS STEFAN</creatorcontrib><creatorcontrib>SCHMITZ UDO</creatorcontrib><creatorcontrib>KALLURI, RAMSATISH</creatorcontrib><creatorcontrib>SCHULTZ ANATOLE</creatorcontrib><creatorcontrib>HUTH MICHAEL</creatorcontrib><title>Combustor part of combustor and combustor of gas turbine having such combustor part</title><description>The invention relates to a burner part (01) of a burner. The burner has a flow channel in which combustion air flows from upstream to downstream in a flow direction (05). In this case, the burner component (01) comprises a wall section (03) adjoining the flow channel and a plurality of nozzles (21, 22) arranged in the wall section (03); and a plurality of vortex generators (11) arranged on the wall section (03). In order to improve the distribution of the fuel in the combustion air, it is proposed that the vortex generator (11) has a ramp (12) which rises in the flow direction (05) and which is concavely curved.
本发明涉及一种燃烧器的燃烧器部件(01)。燃烧器具有流动通道，在所述流动通道中，助燃空气在流动方向(05)上从上游朝向下游流动。在此，燃烧器部件(01)包括：邻接于流动通道的壁部段(03)和多个设置在壁部段(03)中的喷嘴(21，22)；以及多个设置在壁部段(03)上的涡流发生器(11)。为了改进燃料在助燃空气中的分布提出，涡流发生器(11)具有在流动方向(05)上升高的斜面(12)，所述斜面凹形地拱曲。</description><subject>BLASTING</subject><subject>BURNERS</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAh2zs9NKi0uyS9SKEgsKlHIT1NIhosk5qUg8YBS6YnFCiWlRUmZeakKGYllmXnpCsWlyRlIikCG8DCwpiXmFKfyQmluBkU31xBnD93Ugvz41OKCxOTUvNSSeGc_Q0NTYzMjY2NjR2Ni1AAAgDA4tw</recordid><startdate>20221118</startdate><enddate>20221118</enddate><creator>VOGMANN DANIEL</creator><creator>DEDERICHS STEFAN</creator><creator>SCHMITZ UDO</creator><creator>KALLURI, RAMSATISH</creator><creator>SCHULTZ ANATOLE</creator><creator>HUTH MICHAEL</creator><scope>EVB</scope></search><sort><creationdate>20221118</creationdate><title>Combustor part of combustor and combustor of gas turbine having such combustor part</title><author>VOGMANN DANIEL ; DEDERICHS STEFAN ; SCHMITZ UDO ; KALLURI, RAMSATISH ; SCHULTZ ANATOLE ; HUTH MICHAEL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN115362333A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>BLASTING</topic><topic>BURNERS</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>VOGMANN DANIEL</creatorcontrib><creatorcontrib>DEDERICHS STEFAN</creatorcontrib><creatorcontrib>SCHMITZ UDO</creatorcontrib><creatorcontrib>KALLURI, RAMSATISH</creatorcontrib><creatorcontrib>SCHULTZ ANATOLE</creatorcontrib><creatorcontrib>HUTH MICHAEL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>VOGMANN DANIEL</au><au>DEDERICHS STEFAN</au><au>SCHMITZ UDO</au><au>KALLURI, RAMSATISH</au><au>SCHULTZ ANATOLE</au><au>HUTH MICHAEL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Combustor part of combustor and combustor of gas turbine having such combustor part</title><date>2022-11-18</date><risdate>2022</risdate><abstract>The invention relates to a burner part (01) of a burner. The burner has a flow channel in which combustion air flows from upstream to downstream in a flow direction (05). In this case, the burner component (01) comprises a wall section (03) adjoining the flow channel and a plurality of nozzles (21, 22) arranged in the wall section (03); and a plurality of vortex generators (11) arranged on the wall section (03). In order to improve the distribution of the fuel in the combustion air, it is proposed that the vortex generator (11) has a ramp (12) which rises in the flow direction (05) and which is concavely curved.
本发明涉及一种燃烧器的燃烧器部件(01)。燃烧器具有流动通道，在所述流动通道中，助燃空气在流动方向(05)上从上游朝向下游流动。在此，燃烧器部件(01)包括：邻接于流动通道的壁部段(03)和多个设置在壁部段(03)中的喷嘴(21，22)；以及多个设置在壁部段(03)上的涡流发生器(11)。为了改进燃料在助燃空气中的分布提出，涡流发生器(11)具有在流动方向(05)上升高的斜面(12)，所述斜面凹形地拱曲。</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | BLASTING BURNERS 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 part of combustor and combustor of gas turbine having such combustor part |
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