Systems for Supplying Liquid Fuel to a Combustion System, in Particular a Gas Turbine, including a Device for Generating an Emulsion and for Distributing the Emulsion Flow Rate
Liquid fuel supply system (12) for a combustion system (14), in particular a gas turbine, including at least one storage tank (16) for liquid fuel supplying at least one injector (34) connected to a combustion chamber (32) of the combustion system (14), said liquid fuel supply system (12) including...
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| creator | Glaser, Paul Burchell Amancherla, Sundar Aboujaib, Maher Suleiman, Baha Montagne, Pierre |
| description | Liquid fuel supply system (12) for a combustion system (14), in particular a gas turbine, including at least one storage tank (16) for liquid fuel supplying at least one injector (34) connected to a combustion chamber (32) of the combustion system (14), said liquid fuel supply system (12) including a first piping section (18) disposed downstream of the tank (16) and a second piping section (20) disposed downstream of the first piping section (18) and upstream of fuel nozzle (34) in each combustion chamber (32), said first piping section (18) including at least one pressurizing means (22), and at least one injecting point or entering (24) for a water-soluble product, and the second piping section (20) including a mixing and distribution flow device (26) configured to create an emulsion and distributing the emulsion flow rate to at least one piping (28) connected to said nozzle (34). |
| format | Patent |
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Suleiman, Baha ; Montagne, Pierre</creator><creatorcontrib>Glaser, Paul Burchell ; Amancherla, Sundar ; Aboujaib, Maher ; Suleiman, Baha ; Montagne, Pierre</creatorcontrib><description>Liquid fuel supply system (12) for a combustion system (14), in particular a gas turbine, including at least one storage tank (16) for liquid fuel supplying at least one injector (34) connected to a combustion chamber (32) of the combustion system (14), said liquid fuel supply system (12) including a first piping section (18) disposed downstream of the tank (16) and a second piping section (20) disposed downstream of the first piping section (18) and upstream of fuel nozzle (34) in each combustion chamber (32), said first piping section (18) including at least one pressurizing means (22), and at least one injecting point or entering (24) for a water-soluble product, and the second piping section (20) including a mixing and distribution flow device (26) configured to create an emulsion and distributing the emulsion flow rate to at least one piping (28) connected to said nozzle (34).</description><language>eng</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>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=20190411&DB=EPODOC&CC=US&NR=2019107049A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190411&DB=EPODOC&CC=US&NR=2019107049A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Glaser, Paul Burchell</creatorcontrib><creatorcontrib>Amancherla, Sundar</creatorcontrib><creatorcontrib>Aboujaib, Maher</creatorcontrib><creatorcontrib>Suleiman, Baha</creatorcontrib><creatorcontrib>Montagne, Pierre</creatorcontrib><title>Systems for Supplying Liquid Fuel to a Combustion System, in Particular a Gas Turbine, including a Device for Generating an Emulsion and for Distributing the Emulsion Flow Rate</title><description>Liquid fuel supply system (12) for a combustion system (14), in particular a gas turbine, including at least one storage tank (16) for liquid fuel supplying at least one injector (34) connected to a combustion chamber (32) of the combustion system (14), said liquid fuel supply system (12) including a first piping section (18) disposed downstream of the tank (16) and a second piping section (20) disposed downstream of the first piping section (18) and upstream of fuel nozzle (34) in each combustion chamber (32), said first piping section (18) including at least one pressurizing means (22), and at least one injecting point or entering (24) for a water-soluble product, and the second piping section (20) including a mixing and distribution flow device (26) configured to create an emulsion and distributing the emulsion flow rate to at least one piping (28) connected to said nozzle (34).</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjcGKwkAQRHPxsKz-Q8NeV0h0QXJc1OjBgxj3LJ2k1YbJTJzpVvwrP1ETBa97Kqh6VfUR3fJrEKoD7J2HXJvGXNkeYMUn5QoyJQPiAGHq6kKDsLPwbHwDW1ijFy7VoH8gCwywVV-wpTYsjVbtFMKMzlxS97AgSx6l8y3MazWhnURbdfGMg3gutAPkSG8iM-4CGxTqR709mkCDl35GX9l8O10OqXE7Cg2WjwvZ_eWjOEmTeBL_pL_J-H_UHXsSWmk</recordid><startdate>20190411</startdate><enddate>20190411</enddate><creator>Glaser, Paul Burchell</creator><creator>Amancherla, Sundar</creator><creator>Aboujaib, Maher</creator><creator>Suleiman, Baha</creator><creator>Montagne, Pierre</creator><scope>EVB</scope></search><sort><creationdate>20190411</creationdate><title>Systems for Supplying Liquid Fuel to a Combustion System, in Particular a Gas Turbine, including a Device for Generating an Emulsion and for Distributing the Emulsion Flow Rate</title><author>Glaser, Paul Burchell ; Amancherla, Sundar ; Aboujaib, Maher ; Suleiman, Baha ; Montagne, Pierre</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2019107049A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2019</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>Glaser, Paul Burchell</creatorcontrib><creatorcontrib>Amancherla, Sundar</creatorcontrib><creatorcontrib>Aboujaib, Maher</creatorcontrib><creatorcontrib>Suleiman, Baha</creatorcontrib><creatorcontrib>Montagne, Pierre</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Glaser, Paul Burchell</au><au>Amancherla, Sundar</au><au>Aboujaib, Maher</au><au>Suleiman, Baha</au><au>Montagne, Pierre</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Systems for Supplying Liquid Fuel to a Combustion System, in Particular a Gas Turbine, including a Device for Generating an Emulsion and for Distributing the Emulsion Flow Rate</title><date>2019-04-11</date><risdate>2019</risdate><abstract>Liquid fuel supply system (12) for a combustion system (14), in particular a gas turbine, including at least one storage tank (16) for liquid fuel supplying at least one injector (34) connected to a combustion chamber (32) of the combustion system (14), said liquid fuel supply system (12) including a first piping section (18) disposed downstream of the tank (16) and a second piping section (20) disposed downstream of the first piping section (18) and upstream of fuel nozzle (34) in each combustion chamber (32), said first piping section (18) including at least one pressurizing means (22), and at least one injecting point or entering (24) for a water-soluble product, and the second piping section (20) including a mixing and distribution flow device (26) configured to create an emulsion and distributing the emulsion flow rate to at least one piping (28) connected to said nozzle (34).</abstract><oa>free_for_read</oa></addata></record> |
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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 | Systems for Supplying Liquid Fuel to a Combustion System, in Particular a Gas Turbine, including a Device for Generating an Emulsion and for Distributing the Emulsion Flow Rate |
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