Gas turbine premix burner
The pre-mixing burner has an annular channel for supplying air and fuel and a spin generator arranged in the channel. The spin generator comprises multiple flow guiding elements distributed around the periphery of the channel cross-section. The radial inner channel wall (43) and radial outer channel...
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| creator | Clemen, Carsten |
| description | The pre-mixing burner has an annular channel for supplying air and fuel and a spin generator arranged in the channel. The spin generator comprises multiple flow guiding elements distributed around the periphery of the channel cross-section. The radial inner channel wall (43) and radial outer channel wall (44) are provided with concave, annular groove-like recesses (45,46) in area of the flow guiding elements. The cross-sectional area of the radially inner or radially outer recesses is equal to or smaller than a sum of the thicknesses of the flow guiding elements. |
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The radial inner channel wall (43) and radial outer channel wall (44) are provided with concave, annular groove-like recesses (45,46) in area of the flow guiding elements. The cross-sectional area of the radially inner or radially outer recesses is equal to or smaller than a sum of the thicknesses of the flow guiding elements.</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>2019</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=20191009&DB=EPODOC&CC=EP&NR=2626634B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191009&DB=EPODOC&CC=EP&NR=2626634B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Clemen, Carsten</creatorcontrib><title>Gas turbine premix burner</title><description>The pre-mixing burner has an annular channel for supplying air and fuel and a spin generator arranged in the channel. The spin generator comprises multiple flow guiding elements distributed around the periphery of the channel cross-section. The radial inner channel wall (43) and radial outer channel wall (44) are provided with concave, annular groove-like recesses (45,46) in area of the flow guiding elements. The cross-sectional area of the radially inner or radially outer recesses is equal to or smaller than a sum of the thicknesses of the flow guiding elements.</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB0TyxWKCktSsrMS1UoKErNzaxQSCotykst4mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BRmZGZmbGJk6GxkQoAQDXviI7</recordid><startdate>20191009</startdate><enddate>20191009</enddate><creator>Clemen, Carsten</creator><scope>EVB</scope></search><sort><creationdate>20191009</creationdate><title>Gas turbine premix burner</title><author>Clemen, Carsten</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2626634B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</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>Clemen, Carsten</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Clemen, Carsten</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Gas turbine premix burner</title><date>2019-10-09</date><risdate>2019</risdate><abstract>The pre-mixing burner has an annular channel for supplying air and fuel and a spin generator arranged in the channel. The spin generator comprises multiple flow guiding elements distributed around the periphery of the channel cross-section. The radial inner channel wall (43) and radial outer channel wall (44) are provided with concave, annular groove-like recesses (45,46) in area of the flow guiding elements. The cross-sectional area of the radially inner or radially outer recesses is equal to or smaller than a sum of the thicknesses of the flow guiding elements.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| 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 | Gas turbine premix burner |
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