COWL DAMPER FOR COMBUSTOR
A combustor for a turbomachine engine. The combustor includes a combustion chamber, and a cowl having an annular shape that is symmetric around a centerline axis of the turbomachine engine. The cowl includes a hollow cavity that is in fluid communication with the combustion chamber. The hollow cavit...
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| creator | Ganiger, Ravindra Shankar Kim, Kwanwoo Vukanti, Perumallu Mohan, Sripathi Nath, Hiranya |
| description | A combustor for a turbomachine engine. The combustor includes a combustion chamber, and a cowl having an annular shape that is symmetric around a centerline axis of the turbomachine engine. The cowl includes a hollow cavity that is in fluid communication with the combustion chamber. The hollow cavity is a damper that reduces combustion dynamics of the combustor. |
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The combustor includes a combustion chamber, and a cowl having an annular shape that is symmetric around a centerline axis of the turbomachine engine. The cowl includes a hollow cavity that is in fluid communication with the combustion chamber. The hollow cavity is a damper that reduces combustion dynamics of the combustor.</description><language>eng</language><subject>BLASTING ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; 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=20240425&DB=EPODOC&CC=US&NR=2024133555A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240425&DB=EPODOC&CC=US&NR=2024133555A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Ganiger, Ravindra Shankar</creatorcontrib><creatorcontrib>Kim, Kwanwoo</creatorcontrib><creatorcontrib>Vukanti, Perumallu</creatorcontrib><creatorcontrib>Mohan, Sripathi</creatorcontrib><creatorcontrib>Nath, Hiranya</creatorcontrib><title>COWL DAMPER FOR COMBUSTOR</title><description>A combustor for a turbomachine engine. The combustor includes a combustion chamber, and a cowl having an annular shape that is symmetric around a centerline axis of the turbomachine engine. The cowl includes a hollow cavity that is in fluid communication with the combustion chamber. The hollow cavity is a damper that reduces combustion dynamics of the combustor.</description><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>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB09g_3UXBx9A1wDVJw8w9ScPb3dQoNDvEP4mFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgZGJobGxqampo6GxsSpAgCPMyDj</recordid><startdate>20240425</startdate><enddate>20240425</enddate><creator>Ganiger, Ravindra Shankar</creator><creator>Kim, Kwanwoo</creator><creator>Vukanti, Perumallu</creator><creator>Mohan, Sripathi</creator><creator>Nath, Hiranya</creator><scope>EVB</scope></search><sort><creationdate>20240425</creationdate><title>COWL DAMPER FOR COMBUSTOR</title><author>Ganiger, Ravindra Shankar ; Kim, Kwanwoo ; Vukanti, Perumallu ; Mohan, Sripathi ; Nath, Hiranya</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2024133555A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2024</creationdate><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION PROCESSES</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Ganiger, Ravindra Shankar</creatorcontrib><creatorcontrib>Kim, Kwanwoo</creatorcontrib><creatorcontrib>Vukanti, Perumallu</creatorcontrib><creatorcontrib>Mohan, Sripathi</creatorcontrib><creatorcontrib>Nath, Hiranya</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Ganiger, Ravindra Shankar</au><au>Kim, Kwanwoo</au><au>Vukanti, Perumallu</au><au>Mohan, Sripathi</au><au>Nath, Hiranya</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COWL DAMPER FOR COMBUSTOR</title><date>2024-04-25</date><risdate>2024</risdate><abstract>A combustor for a turbomachine engine. The combustor includes a combustion chamber, and a cowl having an annular shape that is symmetric around a centerline axis of the turbomachine engine. The cowl includes a hollow cavity that is in fluid communication with the combustion chamber. The hollow cavity is a damper that reduces combustion dynamics of the combustor.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | COWL DAMPER FOR COMBUSTOR |
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