Combustion chamber for gas turbine
The combustion chamber arrangement has a combustion chamber wall (1) encompassing the combustion chamber, which encloses a flow channel in the area of the combustion chamber outlet for hot gases formed inside the combustion chamber. A combustion chamber wall edge (4) is constructed in profiled manne...
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| creator | Magni, Fulvio Poyyapakkam, Madhavan Narasimhan Ince, Nadir |
| description | The combustion chamber arrangement has a combustion chamber wall (1) encompassing the combustion chamber, which encloses a flow channel in the area of the combustion chamber outlet for hot gases formed inside the combustion chamber. A combustion chamber wall edge (4) is constructed in profiled manner, such that by this a profile (17), with an overflow of the combustion chamber wall edge by a cooling air in the annular space region (13) is guided axially through the flow channels (12), where an inhibitory diffuser effect arises. |
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A combustion chamber wall edge (4) is constructed in profiled manner, such that by this a profile (17), with an overflow of the combustion chamber wall edge by a cooling air in the annular space region (13) is guided axially through the flow channels (12), where an inhibitory diffuser effect arises.</description><language>eng ; fre ; ger</language><subject>BLASTING ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; ENGINE PLANTS IN GENERAL ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2018</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=20180711&DB=EPODOC&CC=EP&NR=2189723B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180711&DB=EPODOC&CC=EP&NR=2189723B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Magni, Fulvio</creatorcontrib><creatorcontrib>Poyyapakkam, Madhavan Narasimhan</creatorcontrib><creatorcontrib>Ince, Nadir</creatorcontrib><title>Combustion chamber for gas turbine</title><description>The combustion chamber arrangement has a combustion chamber wall (1) encompassing the combustion chamber, which encloses a flow channel in the area of the combustion chamber outlet for hot gases formed inside the combustion chamber. A combustion chamber wall edge (4) is constructed in profiled manner, such that by this a profile (17), with an overflow of the combustion chamber wall edge by a cooling air in the annular space region (13) is guided axially through the flow channels (12), where an inhibitory diffuser effect arises.</description><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION PROCESSES</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFByzs9NKi0uyczPU0jOSMxNSi1SSMsvUkhPLFYoKS1KysxL5WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BRoYWluZGxk6GxkQoAQBnkSWj</recordid><startdate>20180711</startdate><enddate>20180711</enddate><creator>Magni, Fulvio</creator><creator>Poyyapakkam, Madhavan Narasimhan</creator><creator>Ince, Nadir</creator><scope>EVB</scope></search><sort><creationdate>20180711</creationdate><title>Combustion chamber for gas turbine</title><author>Magni, Fulvio ; Poyyapakkam, Madhavan Narasimhan ; Ince, Nadir</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2189723B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</creationdate><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION PROCESSES</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Magni, Fulvio</creatorcontrib><creatorcontrib>Poyyapakkam, Madhavan Narasimhan</creatorcontrib><creatorcontrib>Ince, Nadir</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Magni, Fulvio</au><au>Poyyapakkam, Madhavan Narasimhan</au><au>Ince, Nadir</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Combustion chamber for gas turbine</title><date>2018-07-11</date><risdate>2018</risdate><abstract>The combustion chamber arrangement has a combustion chamber wall (1) encompassing the combustion chamber, which encloses a flow channel in the area of the combustion chamber outlet for hot gases formed inside the combustion chamber. A combustion chamber wall edge (4) is constructed in profiled manner, such that by this a profile (17), with an overflow of the combustion chamber wall edge by a cooling air in the annular space region (13) is guided axially through the flow channels (12), where an inhibitory diffuser effect arises.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | Combustion chamber for gas turbine |
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