TURBULATOR GEOMETRY FOR A COMBUSTION LINER
A heat transfer mechanism is provided comprising a plurality of turbulators located along a surface of a body, such as a combustion liner. The turbulators have a first side with a first ramp angle, a second side with a second ramp angle, a height, and a base width, where the base width is a function...
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| creator | BACILE, John MARTLING, Vincent C XIAO, Zenhua FOLKERS, Daniel L |
| description | A heat transfer mechanism is provided comprising a plurality of turbulators located along a surface of a body, such as a combustion liner. The turbulators have a first side with a first ramp angle, a second side with a second ramp angle, a height, and a base width, where the base width is a function of the height and where the turbulators are spaced an axial distance apart that is a function of the turbulator height.
Mécanisme de transfert de chaleur comprenant une pluralité de turbulateurs situés le long d'une surface d'un corps, tel qu'une chemise de combustion. Les turbulateurs comportent un premier côté présentant un premier angle de rampe, un second côté présentant un second angle de rampe, une hauteur et une largeur de base, la largeur de base étant fonction de la hauteur et les turbulateurs étant espacés les uns des autres d'une distance axiale qui est fonction de la hauteur de turbulateur. |
| format | Patent |
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Mécanisme de transfert de chaleur comprenant une pluralité de turbulateurs situés le long d'une surface d'un corps, tel qu'une chemise de combustion. Les turbulateurs comportent un premier côté présentant un premier angle de rampe, un second côté présentant un second angle de rampe, une hauteur et une largeur de base, la largeur de base étant fonction de la hauteur et les turbulateurs étant espacés les uns des autres d'une distance axiale qui est fonction de la hauteur de turbulateur.</description><language>eng ; fre</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>2020</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=20200507&DB=EPODOC&CC=WO&NR=2020092916A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200507&DB=EPODOC&CC=WO&NR=2020092916A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BACILE, John</creatorcontrib><creatorcontrib>MARTLING, Vincent C</creatorcontrib><creatorcontrib>XIAO, Zenhua</creatorcontrib><creatorcontrib>FOLKERS, Daniel L</creatorcontrib><title>TURBULATOR GEOMETRY FOR A COMBUSTION LINER</title><description>A heat transfer mechanism is provided comprising a plurality of turbulators located along a surface of a body, such as a combustion liner. The turbulators have a first side with a first ramp angle, a second side with a second ramp angle, a height, and a base width, where the base width is a function of the height and where the turbulators are spaced an axial distance apart that is a function of the turbulator height.
Mécanisme de transfert de chaleur comprenant une pluralité de turbulateurs situés le long d'une surface d'un corps, tel qu'une chemise de combustion. Les turbulateurs comportent un premier côté présentant un premier angle de rampe, un second côté présentant un second angle de rampe, une hauteur et une largeur de base, la largeur de base étant fonction de la hauteur et les turbulateurs étant espacés les uns des autres d'une distance axiale qui est fonction de la hauteur de turbulateur.</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>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAKCQ1yCvVxDPEPUnB39fd1DQmKVHADchwVnP19nUKDQzz9_RR8PP1cg3gYWNMSc4pTeaE0N4Oym2uIs4duakF-fGpxQWJyal5qSXy4v5GBkYGBpZGloZmjoTFxqgD90yXE</recordid><startdate>20200507</startdate><enddate>20200507</enddate><creator>BACILE, John</creator><creator>MARTLING, Vincent C</creator><creator>XIAO, Zenhua</creator><creator>FOLKERS, Daniel L</creator><scope>EVB</scope></search><sort><creationdate>20200507</creationdate><title>TURBULATOR GEOMETRY FOR A COMBUSTION LINER</title><author>BACILE, John ; MARTLING, Vincent C ; XIAO, Zenhua ; FOLKERS, Daniel L</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2020092916A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2020</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>BACILE, John</creatorcontrib><creatorcontrib>MARTLING, Vincent C</creatorcontrib><creatorcontrib>XIAO, Zenhua</creatorcontrib><creatorcontrib>FOLKERS, Daniel L</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BACILE, John</au><au>MARTLING, Vincent C</au><au>XIAO, Zenhua</au><au>FOLKERS, Daniel L</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBULATOR GEOMETRY FOR A COMBUSTION LINER</title><date>2020-05-07</date><risdate>2020</risdate><abstract>A heat transfer mechanism is provided comprising a plurality of turbulators located along a surface of a body, such as a combustion liner. The turbulators have a first side with a first ramp angle, a second side with a second ramp angle, a height, and a base width, where the base width is a function of the height and where the turbulators are spaced an axial distance apart that is a function of the turbulator height.
Mécanisme de transfert de chaleur comprenant une pluralité de turbulateurs situés le long d'une surface d'un corps, tel qu'une chemise de combustion. Les turbulateurs comportent un premier côté présentant un premier angle de rampe, un second côté présentant un second angle de rampe, une hauteur et une largeur de base, la largeur de base étant fonction de la hauteur et les turbulateurs étant espacés les uns des autres d'une distance axiale qui est fonction de la hauteur de turbulateur.</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 | TURBULATOR GEOMETRY FOR A COMBUSTION LINER |
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