GAS TURBINE ENGINE WITH RESONATOR RINGS
A gas turbine engine has a resonator ring (10) that is formed by two circumferentially extending rings. The first and second circumferentially extending rings (30, 31) have located within them baffles (20). Both the first ring (30) and the second ring (31) are able to mitigate acoustic frequencies g...
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| creator | DYSZKIEWICZ, Wojciech CASSAR, Daniel CRANE, John M RAJARAM, Rajesh TERDALKAR, Sachin |
| description | A gas turbine engine has a resonator ring (10) that is formed by two circumferentially extending rings. The first and second circumferentially extending rings (30, 31) have located within them baffles (20). Both the first ring (30) and the second ring (31) are able to mitigate acoustic frequencies generated by the gas turbine engine. |
| format | Patent |
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The first and second circumferentially extending rings (30, 31) have located within them baffles (20). Both the first ring (30) and the second ring (31) are able to mitigate acoustic frequencies generated by the gas turbine engine.</description><language>eng ; fre ; ger</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>2019</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=20190410&DB=EPODOC&CC=EP&NR=3465008A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190410&DB=EPODOC&CC=EP&NR=3465008A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DYSZKIEWICZ, Wojciech</creatorcontrib><creatorcontrib>CASSAR, Daniel</creatorcontrib><creatorcontrib>CRANE, John M</creatorcontrib><creatorcontrib>RAJARAM, Rajesh</creatorcontrib><creatorcontrib>TERDALKAR, Sachin</creatorcontrib><title>GAS TURBINE ENGINE WITH RESONATOR RINGS</title><description>A gas turbine engine has a resonator ring (10) that is formed by two circumferentially extending rings. 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Both the first ring (30) and the second ring (31) are able to mitigate acoustic frequencies generated by the gas turbine engine.</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB3dwxWCAkNcvL0c1Vw9XMHUeGeIR4KQa7B_n6OIf5BCkGefu7BPAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXA2MTM1MDAwtHQmAglAKDZI3A</recordid><startdate>20190410</startdate><enddate>20190410</enddate><creator>DYSZKIEWICZ, Wojciech</creator><creator>CASSAR, Daniel</creator><creator>CRANE, John M</creator><creator>RAJARAM, Rajesh</creator><creator>TERDALKAR, Sachin</creator><scope>EVB</scope></search><sort><creationdate>20190410</creationdate><title>GAS TURBINE ENGINE WITH RESONATOR RINGS</title><author>DYSZKIEWICZ, Wojciech ; CASSAR, Daniel ; CRANE, John M ; RAJARAM, Rajesh ; TERDALKAR, Sachin</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3465008A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</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>DYSZKIEWICZ, Wojciech</creatorcontrib><creatorcontrib>CASSAR, Daniel</creatorcontrib><creatorcontrib>CRANE, John M</creatorcontrib><creatorcontrib>RAJARAM, Rajesh</creatorcontrib><creatorcontrib>TERDALKAR, Sachin</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DYSZKIEWICZ, Wojciech</au><au>CASSAR, Daniel</au><au>CRANE, John M</au><au>RAJARAM, Rajesh</au><au>TERDALKAR, Sachin</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE ENGINE WITH RESONATOR RINGS</title><date>2019-04-10</date><risdate>2019</risdate><abstract>A gas turbine engine has a resonator ring (10) that is formed by two circumferentially extending rings. 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| language | eng ; fre ; ger |
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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 | GAS TURBINE ENGINE WITH RESONATOR RINGS |
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