Cooling of liquid fuel components to eliminate coking
A system for cooling at least one gas turbine liquid fuel component located in a high temperature environment to eliminate coking in the component is disclosed. The system includes a sleeve surrounding the liquid fuel component, a device for providing a current of cool air, and a conduit connected b...
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creator | IASILLO ROBERT JOSEPH KAPLAN HOWARD JAY O'DELL KEVIN JON JUNQUERA STEVEN PATRICK MILLER CHRISTOPHER DAVID ACQUAVELLA DAVID FRANCIS JOHNSON DAVID MARTIN HAMPSON GREGORY JAMES |
description | A system for cooling at least one gas turbine liquid fuel component located in a high temperature environment to eliminate coking in the component is disclosed. The system includes a sleeve surrounding the liquid fuel component, a device for providing a current of cool air, and a conduit connected between the cool air device and the sleeve to direct the current of cool air into the sleeve to cool the liquid fuel component. The system can also include a manifold connected to the conduit and a plurality of second conduits for connecting the manifold to a plurality of sleeves surrounding a plurality of liquid fuel components, each sleeve being connected to a corresponding second conduit. Each sleeve includes a plurality of spacing devices for centering the sleeve around the at least one liquid fuel component so as to form an annulus between the sleeve and the liquid fuel component through which the current of cool air flows. The system can alternatively use a supply of cool liquid pumped by a pump through a conduit adjacent to a liquid fuel component to cool the component. |
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The system includes a sleeve surrounding the liquid fuel component, a device for providing a current of cool air, and a conduit connected between the cool air device and the sleeve to direct the current of cool air into the sleeve to cool the liquid fuel component. The system can also include a manifold connected to the conduit and a plurality of second conduits for connecting the manifold to a plurality of sleeves surrounding a plurality of liquid fuel components, each sleeve being connected to a corresponding second conduit. Each sleeve includes a plurality of spacing devices for centering the sleeve around the at least one liquid fuel component so as to form an annulus between the sleeve and the liquid fuel component through which the current of cool air flows. The system can alternatively use a supply of cool liquid pumped by a pump through a conduit adjacent to a liquid fuel component to cool the component.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINEPLANTS ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NOT OTHERWISE PROVIDED FOR ; STEAM ENGINES ; USE OF WASTE HEAT OF COMBUSTION ENGINES ; WEAPONS</subject><creationdate>2006</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=20061010&DB=EPODOC&CC=US&NR=7117675B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20061010&DB=EPODOC&CC=US&NR=7117675B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>IASILLO ROBERT JOSEPH</creatorcontrib><creatorcontrib>KAPLAN HOWARD JAY</creatorcontrib><creatorcontrib>O'DELL KEVIN JON</creatorcontrib><creatorcontrib>JUNQUERA STEVEN PATRICK</creatorcontrib><creatorcontrib>MILLER CHRISTOPHER DAVID</creatorcontrib><creatorcontrib>ACQUAVELLA DAVID FRANCIS</creatorcontrib><creatorcontrib>JOHNSON DAVID MARTIN</creatorcontrib><creatorcontrib>HAMPSON GREGORY JAMES</creatorcontrib><title>Cooling of liquid fuel components to eliminate coking</title><description>A system for cooling at least one gas turbine liquid fuel component located in a high temperature environment to eliminate coking in the component is disclosed. The system includes a sleeve surrounding the liquid fuel component, a device for providing a current of cool air, and a conduit connected between the cool air device and the sleeve to direct the current of cool air into the sleeve to cool the liquid fuel component. The system can also include a manifold connected to the conduit and a plurality of second conduits for connecting the manifold to a plurality of sleeves surrounding a plurality of liquid fuel components, each sleeve being connected to a corresponding second conduit. Each sleeve includes a plurality of spacing devices for centering the sleeve around the at least one liquid fuel component so as to form an annulus between the sleeve and the liquid fuel component through which the current of cool air flows. The system can alternatively use a supply of cool liquid pumped by a pump through a conduit adjacent to a liquid fuel component to cool the component.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINEPLANTS</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>NOT OTHERWISE PROVIDED FOR</subject><subject>STEAM ENGINES</subject><subject>USE OF WASTE HEAT OF COMBUSTION ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2006</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB1zs_PycxLV8hPU8jJLCzNTFFIK03NUUjOzy3Iz0vNKylWKMlXSM3JzM3MSyxJBYpnA1XzMLCmJeYUp_JCaW4GBTfXEGcP3dSC_PjU4oLE5NS81JL40GBzQ0NzM3NTJyNjIpQAABOGLQI</recordid><startdate>20061010</startdate><enddate>20061010</enddate><creator>IASILLO ROBERT JOSEPH</creator><creator>KAPLAN HOWARD JAY</creator><creator>O'DELL KEVIN JON</creator><creator>JUNQUERA STEVEN PATRICK</creator><creator>MILLER CHRISTOPHER DAVID</creator><creator>ACQUAVELLA DAVID FRANCIS</creator><creator>JOHNSON DAVID MARTIN</creator><creator>HAMPSON GREGORY JAMES</creator><scope>EVB</scope></search><sort><creationdate>20061010</creationdate><title>Cooling of liquid fuel components to eliminate coking</title><author>IASILLO ROBERT JOSEPH ; KAPLAN HOWARD JAY ; O'DELL KEVIN JON ; JUNQUERA STEVEN PATRICK ; MILLER CHRISTOPHER DAVID ; ACQUAVELLA DAVID FRANCIS ; JOHNSON DAVID MARTIN ; HAMPSON GREGORY JAMES</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US7117675B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2006</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINEPLANTS</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>NOT OTHERWISE PROVIDED FOR</topic><topic>STEAM ENGINES</topic><topic>USE OF WASTE HEAT OF COMBUSTION ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>IASILLO ROBERT JOSEPH</creatorcontrib><creatorcontrib>KAPLAN HOWARD JAY</creatorcontrib><creatorcontrib>O'DELL KEVIN JON</creatorcontrib><creatorcontrib>JUNQUERA STEVEN PATRICK</creatorcontrib><creatorcontrib>MILLER CHRISTOPHER DAVID</creatorcontrib><creatorcontrib>ACQUAVELLA DAVID FRANCIS</creatorcontrib><creatorcontrib>JOHNSON DAVID MARTIN</creatorcontrib><creatorcontrib>HAMPSON GREGORY JAMES</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>IASILLO ROBERT JOSEPH</au><au>KAPLAN HOWARD JAY</au><au>O'DELL KEVIN JON</au><au>JUNQUERA STEVEN PATRICK</au><au>MILLER CHRISTOPHER DAVID</au><au>ACQUAVELLA DAVID FRANCIS</au><au>JOHNSON DAVID MARTIN</au><au>HAMPSON GREGORY JAMES</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Cooling of liquid fuel components to eliminate coking</title><date>2006-10-10</date><risdate>2006</risdate><abstract>A system for cooling at least one gas turbine liquid fuel component located in a high temperature environment to eliminate coking in the component is disclosed. The system includes a sleeve surrounding the liquid fuel component, a device for providing a current of cool air, and a conduit connected between the cool air device and the sleeve to direct the current of cool air into the sleeve to cool the liquid fuel component. The system can also include a manifold connected to the conduit and a plurality of second conduits for connecting the manifold to a plurality of sleeves surrounding a plurality of liquid fuel components, each sleeve being connected to a corresponding second conduit. Each sleeve includes a plurality of spacing devices for centering the sleeve around the at least one liquid fuel component so as to form an annulus between the sleeve and the liquid fuel component through which the current of cool air flows. The system can alternatively use a supply of cool liquid pumped by a pump through a conduit adjacent to a liquid fuel component to cool the component.</abstract><oa>free_for_read</oa></addata></record> |
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recordid | cdi_epo_espacenet_US7117675B2 |
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subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINEPLANTS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NOT OTHERWISE PROVIDED FOR STEAM ENGINES USE OF WASTE HEAT OF COMBUSTION ENGINES WEAPONS |
title | Cooling of liquid fuel components to eliminate coking |
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