Gas turbine engine combustor with set of dilution channels
A combustor includes a domed wall, an annular liner, a combustion chamber, a set of fuel cups, and a set of dilution channels for each fuel cup of the set of fuel cups. The set of fuel cups are spaced circumferentially along the dome wall relative to the burner centerline. The set of dilution channe...
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| creator | BADUKE, PABTRA PANDURI, BHAVYA, NAIDU NARASIMHA CHIRANTHI RAMA NAIK PRADEEP BACCARO MICHAEL T ROY, ARIJIT, SINHA CHAKRABORTY, ARITRA UKANTI, PARUMARU PATRE AJOY PALLE, SIBUTOSH BENJAMIN MICHAEL A |
| description | A combustor includes a domed wall, an annular liner, a combustion chamber, a set of fuel cups, and a set of dilution channels for each fuel cup of the set of fuel cups. The set of fuel cups are spaced circumferentially along the dome wall relative to the burner centerline. The set of dilution channels terminate in a plurality of slots spaced about corresponding fuel cups of the set of fuel cups.
一种燃烧器，包括圆顶壁、环形衬套、燃烧室、一组燃料杯、以及用于该组燃料杯中的每个燃料杯的一组稀释通道。这组燃料杯相对于燃烧器中心线沿圆顶壁周向间隔开。该组稀释通道终止于绕该组燃料杯中的对应燃料杯间隔开的多个槽。 |
| format | Patent |
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一种燃烧器，包括圆顶壁、环形衬套、燃烧室、一组燃料杯、以及用于该组燃料杯中的每个燃料杯的一组稀释通道。这组燃料杯相对于燃烧器中心线沿圆顶壁周向间隔开。该组稀释通道终止于绕该组燃料杯中的对应燃料杯间隔开的多个槽。</description><language>chi ; eng</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>2024</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=20240621&DB=EPODOC&CC=CN&NR=118224615A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240621&DB=EPODOC&CC=CN&NR=118224615A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BADUKE, PABTRA</creatorcontrib><creatorcontrib>PANDURI, BHAVYA, NAIDU</creatorcontrib><creatorcontrib>NARASIMHA CHIRANTHI RAMA</creatorcontrib><creatorcontrib>NAIK PRADEEP</creatorcontrib><creatorcontrib>BACCARO MICHAEL T</creatorcontrib><creatorcontrib>ROY, ARIJIT, SINHA</creatorcontrib><creatorcontrib>CHAKRABORTY, ARITRA</creatorcontrib><creatorcontrib>UKANTI, PARUMARU</creatorcontrib><creatorcontrib>PATRE AJOY</creatorcontrib><creatorcontrib>PALLE, SIBUTOSH</creatorcontrib><creatorcontrib>BENJAMIN MICHAEL A</creatorcontrib><title>Gas turbine engine combustor with set of dilution channels</title><description>A combustor includes a domed wall, an annular liner, a combustion chamber, a set of fuel cups, and a set of dilution channels for each fuel cup of the set of fuel cups. The set of fuel cups are spaced circumferentially along the dome wall relative to the burner centerline. The set of dilution channels terminate in a plurality of slots spaced about corresponding fuel cups of the set of fuel cups.
一种燃烧器，包括圆顶壁、环形衬套、燃烧室、一组燃料杯、以及用于该组燃料杯中的每个燃料杯的一组稀释通道。这组燃料杯相对于燃烧器中心线沿圆顶壁周向间隔开。该组稀释通道终止于绕该组燃料杯中的对应燃料杯间隔开的多个槽。</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>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLByTyxWKCktSsrMS1VIzUsHUcn5uUmlxSX5RQrlmSUZCsWpJQr5aQopmTmlJZn5eQrJGYl5eak5xTwMrGmJOcWpvFCam0HRzTXE2UM3tSA_PrW4IDE5NS-1JN7Zz9DQwsjIxMzQ1NGYGDUAeZIvFg</recordid><startdate>20240621</startdate><enddate>20240621</enddate><creator>BADUKE, PABTRA</creator><creator>PANDURI, BHAVYA, NAIDU</creator><creator>NARASIMHA CHIRANTHI RAMA</creator><creator>NAIK PRADEEP</creator><creator>BACCARO MICHAEL T</creator><creator>ROY, ARIJIT, SINHA</creator><creator>CHAKRABORTY, ARITRA</creator><creator>UKANTI, PARUMARU</creator><creator>PATRE AJOY</creator><creator>PALLE, SIBUTOSH</creator><creator>BENJAMIN MICHAEL A</creator><scope>EVB</scope></search><sort><creationdate>20240621</creationdate><title>Gas turbine engine combustor with set of dilution channels</title><author>BADUKE, PABTRA ; PANDURI, BHAVYA, NAIDU ; NARASIMHA CHIRANTHI RAMA ; NAIK PRADEEP ; BACCARO MICHAEL T ; ROY, ARIJIT, SINHA ; CHAKRABORTY, ARITRA ; UKANTI, PARUMARU ; PATRE AJOY ; PALLE, SIBUTOSH ; BENJAMIN MICHAEL A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN118224615A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</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>BADUKE, PABTRA</creatorcontrib><creatorcontrib>PANDURI, BHAVYA, NAIDU</creatorcontrib><creatorcontrib>NARASIMHA CHIRANTHI RAMA</creatorcontrib><creatorcontrib>NAIK PRADEEP</creatorcontrib><creatorcontrib>BACCARO MICHAEL T</creatorcontrib><creatorcontrib>ROY, ARIJIT, SINHA</creatorcontrib><creatorcontrib>CHAKRABORTY, ARITRA</creatorcontrib><creatorcontrib>UKANTI, PARUMARU</creatorcontrib><creatorcontrib>PATRE AJOY</creatorcontrib><creatorcontrib>PALLE, SIBUTOSH</creatorcontrib><creatorcontrib>BENJAMIN MICHAEL A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BADUKE, PABTRA</au><au>PANDURI, BHAVYA, NAIDU</au><au>NARASIMHA CHIRANTHI RAMA</au><au>NAIK PRADEEP</au><au>BACCARO MICHAEL T</au><au>ROY, ARIJIT, SINHA</au><au>CHAKRABORTY, ARITRA</au><au>UKANTI, PARUMARU</au><au>PATRE AJOY</au><au>PALLE, SIBUTOSH</au><au>BENJAMIN MICHAEL A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Gas turbine engine combustor with set of dilution channels</title><date>2024-06-21</date><risdate>2024</risdate><abstract>A combustor includes a domed wall, an annular liner, a combustion chamber, a set of fuel cups, and a set of dilution channels for each fuel cup of the set of fuel cups. The set of fuel cups are spaced circumferentially along the dome wall relative to the burner centerline. The set of dilution channels terminate in a plurality of slots spaced about corresponding fuel cups of the set of fuel cups.
一种燃烧器，包括圆顶壁、环形衬套、燃烧室、一组燃料杯、以及用于该组燃料杯中的每个燃料杯的一组稀释通道。这组燃料杯相对于燃烧器中心线沿圆顶壁周向间隔开。该组稀释通道终止于绕该组燃料杯中的对应燃料杯间隔开的多个槽。</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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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 engine combustor with set of dilution channels |
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