Methods and apparatus for injecting fluids into a turbine engine
A method facilitates operating a gas turbine engine (10). The method comprises supplying steam to a nozzle (50), supplying primary fuel to the nozzle, discharging the steam into a combustor (16) from a plurality of circumferentially-spaced steam outlets (106) defined in a tip (100) of the nozzle, an...
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| creator | FORTUNA, DOUGHAL MARTI DURBIN, MARK HELD, TIMOTHY J DURSTOCK, DANIEL COOPER, JAMES N DANIS, ALLEN M |
| description | A method facilitates operating a gas turbine engine (10). The method comprises supplying steam to a nozzle (50), supplying primary fuel to the nozzle, discharging the steam into a combustor (16) from a plurality of circumferentially-spaced steam outlets (106) defined in a tip (100) of the nozzle, and discharging the primary fuel into the combustor from at least one outlet (104) that is spaced circumferentially between the steam outlets. |
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The method comprises supplying steam to a nozzle (50), supplying primary fuel to the nozzle, discharging the steam into a combustor (16) from a plurality of circumferentially-spaced steam outlets (106) defined in a tip (100) of the nozzle, and discharging the primary fuel into the combustor from at least one outlet (104) that is spaced circumferentially between the steam outlets.</description><language>eng ; fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; AIR SUPPLY ; BLASTING ; BURNERS ; COMBUSTION APPARATUS ; COMBUSTION ENGINES ; COMBUSTION PROCESSES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; DRAUGHT-INDUCING ; 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 ; SUPPLYING NON-COMBUSTIBLE LIQUID OR GAS ; WEAPONS</subject><creationdate>2014</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=20140108&DB=EPODOC&CC=EP&NR=1783342A3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140108&DB=EPODOC&CC=EP&NR=1783342A3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>FORTUNA, DOUGHAL MARTI</creatorcontrib><creatorcontrib>DURBIN, MARK</creatorcontrib><creatorcontrib>HELD, TIMOTHY J</creatorcontrib><creatorcontrib>DURSTOCK, DANIEL</creatorcontrib><creatorcontrib>COOPER, JAMES N</creatorcontrib><creatorcontrib>DANIS, ALLEN M</creatorcontrib><title>Methods and apparatus for injecting fluids into a turbine engine</title><description>A method facilitates operating a gas turbine engine (10). The method comprises supplying steam to a nozzle (50), supplying primary fuel to the nozzle, discharging the steam into a combustor (16) from a plurality of circumferentially-spaced steam outlets (106) defined in a tip (100) of the nozzle, and discharging the primary fuel into the combustor from at least one outlet (104) that is spaced circumferentially between the steam outlets.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIR SUPPLY</subject><subject>BLASTING</subject><subject>BURNERS</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>DRAUGHT-INDUCING</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>SUPPLYING NON-COMBUSTIBLE LIQUID OR GAS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHDwTS3JyE8pVkjMS1FILChILEosKS1WSMsvUsjMy0pNLsnMS1dIyynNBCrJzCvJV0hUKCktSsrMS1VIzUsHUjwMrGmJOcWpvFCam0HBzTXE2UM3tSA_PrW4IDE5NS-1JN41wNDcwtjYxMjR2JgIJQBi_zDW</recordid><startdate>20140108</startdate><enddate>20140108</enddate><creator>FORTUNA, DOUGHAL MARTI</creator><creator>DURBIN, MARK</creator><creator>HELD, TIMOTHY J</creator><creator>DURSTOCK, DANIEL</creator><creator>COOPER, JAMES N</creator><creator>DANIS, ALLEN M</creator><scope>EVB</scope></search><sort><creationdate>20140108</creationdate><title>Methods and apparatus for injecting fluids into a turbine engine</title><author>FORTUNA, DOUGHAL MARTI ; DURBIN, MARK ; HELD, TIMOTHY J ; DURSTOCK, DANIEL ; COOPER, JAMES N ; DANIS, ALLEN M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP1783342A33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2014</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIR SUPPLY</topic><topic>BLASTING</topic><topic>BURNERS</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>DRAUGHT-INDUCING</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>SUPPLYING NON-COMBUSTIBLE LIQUID OR GAS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>FORTUNA, DOUGHAL MARTI</creatorcontrib><creatorcontrib>DURBIN, MARK</creatorcontrib><creatorcontrib>HELD, TIMOTHY J</creatorcontrib><creatorcontrib>DURSTOCK, DANIEL</creatorcontrib><creatorcontrib>COOPER, JAMES N</creatorcontrib><creatorcontrib>DANIS, ALLEN M</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>FORTUNA, DOUGHAL MARTI</au><au>DURBIN, MARK</au><au>HELD, TIMOTHY J</au><au>DURSTOCK, DANIEL</au><au>COOPER, JAMES N</au><au>DANIS, ALLEN M</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Methods and apparatus for injecting fluids into a turbine engine</title><date>2014-01-08</date><risdate>2014</risdate><abstract>A method facilitates operating a gas turbine engine (10). The method comprises supplying steam to a nozzle (50), supplying primary fuel to the nozzle, discharging the steam into a combustor (16) from a plurality of circumferentially-spaced steam outlets (106) defined in a tip (100) of the nozzle, and discharging the primary fuel into the combustor from at least one outlet (104) that is spaced circumferentially between the steam outlets.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS AIR SUPPLY BLASTING BURNERS COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS DRAUGHT-INDUCING 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 SUPPLYING NON-COMBUSTIBLE LIQUID OR GAS WEAPONS |
| title | Methods and apparatus for injecting fluids into a turbine engine |
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