Micromixer Heat Shield
Methods and systems are provided for operating a turbine engine. The combustor includes a combustor wall defining a combustion zone (210) and a fuel nozzle (200). The fuel nozzle includes a forward face (220), an aft face (230) downstream from the forward face and adjacent to the combustion zone, a...
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creator | BARKER, CARL ROBERT JOHNSON, THOMAS EDWARD |
description | Methods and systems are provided for operating a turbine engine. The combustor includes a combustor wall defining a combustion zone (210) and a fuel nozzle (200). The fuel nozzle includes a forward face (220), an aft face (230) downstream from the forward face and adjacent to the combustion zone, a plurality of mixing tubes (320) extending between the forward face and the aft face, an outer sleeve (240) positioned radially outward of the plurality of mixing tubes, a heat shield (260) positioned radially inward of the outer sleeve, and a baffle plate (300) between the forward face and the aft face. At least one of the plurality of mixing tubes includes a sidewall (350) that includes an injection opening (360) defined therethrough. The baffle plate is oriented to channel fuel between the plurality of mixing tubes and between the baffle plate and the aft face prior to the fuel being channeled through the injection opening. |
format | Patent |
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The fuel nozzle includes a forward face (220), an aft face (230) downstream from the forward face and adjacent to the combustion zone, a plurality of mixing tubes (320) extending between the forward face and the aft face, an outer sleeve (240) positioned radially outward of the plurality of mixing tubes, a heat shield (260) positioned radially inward of the outer sleeve, and a baffle plate (300) between the forward face and the aft face. At least one of the plurality of mixing tubes includes a sidewall (350) that includes an injection opening (360) defined therethrough. The baffle plate is oriented to channel fuel between the plurality of mixing tubes and between the baffle plate and the aft face prior to the fuel being channeled through the injection opening.</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>2013</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=20130220&DB=EPODOC&CC=EP&NR=2559947A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20130220&DB=EPODOC&CC=EP&NR=2559947A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BARKER, CARL ROBERT</creatorcontrib><creatorcontrib>JOHNSON, THOMAS EDWARD</creatorcontrib><title>Micromixer Heat Shield</title><description>Methods and systems are provided for operating a turbine engine. The combustor includes a combustor wall defining a combustion zone (210) and a fuel nozzle (200). The fuel nozzle includes a forward face (220), an aft face (230) downstream from the forward face and adjacent to the combustion zone, a plurality of mixing tubes (320) extending between the forward face and the aft face, an outer sleeve (240) positioned radially outward of the plurality of mixing tubes, a heat shield (260) positioned radially inward of the outer sleeve, and a baffle plate (300) between the forward face and the aft face. At least one of the plurality of mixing tubes includes a sidewall (350) that includes an injection opening (360) defined therethrough. The baffle plate is oriented to channel fuel between the plurality of mixing tubes and between the baffle plate and the aft face prior to the fuel being channeled through the injection opening.</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>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBDzzUwuys_NrEgtUvBITSxRCM7ITM1J4WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BRqamlpYm5o5GxkQoAQBJZSDz</recordid><startdate>20130220</startdate><enddate>20130220</enddate><creator>BARKER, CARL ROBERT</creator><creator>JOHNSON, THOMAS EDWARD</creator><scope>EVB</scope></search><sort><creationdate>20130220</creationdate><title>Micromixer Heat Shield</title><author>BARKER, CARL ROBERT ; JOHNSON, THOMAS EDWARD</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2559947A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2013</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>BARKER, CARL ROBERT</creatorcontrib><creatorcontrib>JOHNSON, THOMAS EDWARD</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BARKER, CARL ROBERT</au><au>JOHNSON, THOMAS EDWARD</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Micromixer Heat Shield</title><date>2013-02-20</date><risdate>2013</risdate><abstract>Methods and systems are provided for operating a turbine engine. The combustor includes a combustor wall defining a combustion zone (210) and a fuel nozzle (200). The fuel nozzle includes a forward face (220), an aft face (230) downstream from the forward face and adjacent to the combustion zone, a plurality of mixing tubes (320) extending between the forward face and the aft face, an outer sleeve (240) positioned radially outward of the plurality of mixing tubes, a heat shield (260) positioned radially inward of the outer sleeve, and a baffle plate (300) between the forward face and the aft face. At least one of the plurality of mixing tubes includes a sidewall (350) that includes an injection opening (360) defined therethrough. The baffle plate is oriented to channel fuel between the plurality of mixing tubes and between the baffle plate and the aft face prior to the fuel being channeled through the injection opening.</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 | Micromixer Heat Shield |
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