Mixer assembly for a gas turbine engine
A mixer assembly for a gas turbine engine is provided, including a main mixer with fuel injection holes located between at least one radial swirler and at least one axial swirler, wherein the fuel injected into the main mixer is atomized and dispersed by the air flowing through the radial swirler an...
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| creator | COHEN JEFFREY M FOTACHE CATALIN G DAI ZHONGTAO SMITH LANCE L HAUTMAN DONALD J |
| description | A mixer assembly for a gas turbine engine is provided, including a main mixer with fuel injection holes located between at least one radial swirler and at least one axial swirler, wherein the fuel injected into the main mixer is atomized and dispersed by the air flowing through the radial swirler and the axial swirler. |
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BLASTING ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN ; WEAPONS</subject><creationdate>2015</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=20150310&DB=EPODOC&CC=US&NR=8973368B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150310&DB=EPODOC&CC=US&NR=8973368B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>COHEN JEFFREY M</creatorcontrib><creatorcontrib>FOTACHE CATALIN G</creatorcontrib><creatorcontrib>DAI ZHONGTAO</creatorcontrib><creatorcontrib>SMITH LANCE L</creatorcontrib><creatorcontrib>HAUTMAN DONALD J</creatorcontrib><title>Mixer assembly for a gas turbine engine</title><description>A mixer assembly for a gas turbine engine is provided, including a main mixer with fuel injection holes located between at least one radial swirler and at least one axial swirler, wherein the fuel injected into the main mixer is atomized and dispersed by the air flowing through the radial swirler and the axial swirler.</description><subject>AIR</subject><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION PROCESSES</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFD3zaxILVJILC5OzU3KqVRIywdyFNITixVKSouSMvNSFVLz0oEUDwNrWmJOcSovlOZmUHBzDXH20E0tyI9PLS5ITE7NSy2JDw22sDQ3NjazcDIyJkIJADJQJ28</recordid><startdate>20150310</startdate><enddate>20150310</enddate><creator>COHEN JEFFREY M</creator><creator>FOTACHE CATALIN G</creator><creator>DAI ZHONGTAO</creator><creator>SMITH LANCE L</creator><creator>HAUTMAN DONALD J</creator><scope>EVB</scope></search><sort><creationdate>20150310</creationdate><title>Mixer assembly for a gas turbine engine</title><author>COHEN JEFFREY M ; 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| language | eng |
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| subjects | AIR BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN WEAPONS |
| title | Mixer assembly for a gas turbine engine |
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