THERMALLY-COUPLED FUEL MANIFOLD
A fuel manifold apparatus includes an annular array of fuel nozzles interconnected by a plurality of manifold tubes (32), wherein each manifold tube (32) includes at least two fuel passages (84, 86, 88) integrally formed therein, the fuel passages (84, 86, 88) being configured for conduction heat tr...
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creator | WOLFE, JARED MATTHEW |
description | A fuel manifold apparatus includes an annular array of fuel nozzles interconnected by a plurality of manifold tubes (32), wherein each manifold tube (32) includes at least two fuel passages (84, 86, 88) integrally formed therein, the fuel passages (84, 86, 88) being configured for conduction heat transfer therebetween. |
format | Patent |
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fre</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION APPARATUS ; COMBUSTION ENGINES ; COMBUSTION PROCESSES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; 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 ; WEAPONS</subject><creationdate>2016</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=20161014&DB=EPODOC&CC=CA&NR=2926072A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20161014&DB=EPODOC&CC=CA&NR=2926072A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WOLFE, JARED MATTHEW</creatorcontrib><title>THERMALLY-COUPLED FUEL MANIFOLD</title><description>A fuel manifold apparatus includes an annular array of fuel nozzles interconnected by a plurality of manifold tubes (32), wherein each manifold tube (32) includes at least two fuel passages (84, 86, 88) integrally formed therein, the fuel passages (84, 86, 88) being configured for conduction heat transfer therebetween.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</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>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>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJAP8XAN8nX08YnUdfYPDfBxdVFwC3X1UfB19PN08_dx4WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8c6ORpZGZgbmRo6GxkQoAQCXSSEl</recordid><startdate>20161014</startdate><enddate>20161014</enddate><creator>WOLFE, JARED MATTHEW</creator><scope>EVB</scope></search><sort><creationdate>20161014</creationdate><title>THERMALLY-COUPLED FUEL MANIFOLD</title><author>WOLFE, JARED MATTHEW</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2926072A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2016</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</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>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>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>WOLFE, JARED MATTHEW</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WOLFE, JARED MATTHEW</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>THERMALLY-COUPLED FUEL MANIFOLD</title><date>2016-10-14</date><risdate>2016</risdate><abstract>A fuel manifold apparatus includes an annular array of fuel nozzles interconnected by a plurality of manifold tubes (32), wherein each manifold tube (32) includes at least two fuel passages (84, 86, 88) integrally formed therein, the fuel passages (84, 86, 88) being configured for conduction heat transfer therebetween.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre |
recordid | cdi_epo_espacenet_CA2926072A1 |
source | esp@cenet |
subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS 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 WEAPONS |
title | THERMALLY-COUPLED FUEL MANIFOLD |
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