COMBINED AIR SWIRLER AND FUEL DISTRIBUTOR
A fuel mixture distribution system for a turbine engine assembly includes a combustor that includes a wall defining a combustion chamber, a fuel mixture distributor that includes a mixing chamber that extends along an axis between a closed end and an exit opening to the combustion chamber, the mixin...
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| creator | McCaldon, Kian |
| description | A fuel mixture distribution system for a turbine engine assembly includes a combustor that includes a wall defining a combustion chamber, a fuel mixture distributor that includes a mixing chamber that extends along an axis between a closed end and an exit opening to the combustion chamber, the mixing chamber shape being defined to achieve the desired mixing and prevent flashback at all operating conditions, and a plurality of fuel passages and a plurality of air passages that are disposed about a periphery of the mixing chamber within a common plane transverse to the axis. Each of the plurality of fuel passages and each of the plurality of air passages are angled to induce mixing of fuel and air within the mixing chamber prior to flowing through the exit opening into the combustion chamber. |
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Each of the plurality of fuel passages and each of the plurality of air passages are angled to induce mixing of fuel and air within the mixing chamber prior to flowing through the exit opening into the combustion chamber.</description><language>eng</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>2024</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=20240808&DB=EPODOC&CC=US&NR=2024263785A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240808&DB=EPODOC&CC=US&NR=2024263785A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>McCaldon, Kian</creatorcontrib><title>COMBINED AIR SWIRLER AND FUEL DISTRIBUTOR</title><description>A fuel mixture distribution system for a turbine engine assembly includes a combustor that includes a wall defining a combustion chamber, a fuel mixture distributor that includes a mixing chamber that extends along an axis between a closed end and an exit opening to the combustion chamber, the mixing chamber shape being defined to achieve the desired mixing and prevent flashback at all operating conditions, and a plurality of fuel passages and a plurality of air passages that are disposed about a periphery of the mixing chamber within a common plane transverse to the axis. 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Each of the plurality of fuel passages and each of the plurality of air passages are angled to induce mixing of fuel and air within the mixing chamber prior to flowing through the exit opening into the combustion chamber.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| 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 | COMBINED AIR SWIRLER AND FUEL DISTRIBUTOR |
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