COMBUSTOR
Provided is a combustor including a support shaft, a wing portion provided on the support shaft and configured to swirl a first fluid around the support shaft, and a cover housing enclosing the support shaft and the wing portion and includes a space enlarging portion provided at a downstream of of t...
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| creator | JUNG SEUNGCHAI YANG SIWON KIM SINHYUN |
| description | Provided is a combustor including a support shaft, a wing portion provided on the support shaft and configured to swirl a first fluid around the support shaft, and a cover housing enclosing the support shaft and the wing portion and includes a space enlarging portion provided at a downstream of of the wing portion, where a distance of the space enlarging portion from an outer surface of the support shaft is different from distances of other portions of the cover housing from the outer surface of the support shaft. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2015211740A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2015211740A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2015211740A13</originalsourceid><addsrcrecordid>eNrjZOB09vd1Cg0O8Q_iYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXxocFGBoamRoaG5iYGjobGxKkCALd6HJA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>COMBUSTOR</title><source>esp@cenet</source><creator>JUNG SEUNGCHAI ; YANG SIWON ; KIM SINHYUN</creator><creatorcontrib>JUNG SEUNGCHAI ; YANG SIWON ; KIM SINHYUN</creatorcontrib><description>Provided is a combustor including a support shaft, a wing portion provided on the support shaft and configured to swirl a first fluid around the support shaft, and a cover housing enclosing the support shaft and the wing portion and includes a space enlarging portion provided at a downstream of of the wing portion, where a distance of the space enlarging portion from an outer surface of the support shaft is different from distances of other portions of the cover housing from the outer surface of the support shaft.</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>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=20150730&DB=EPODOC&CC=US&NR=2015211740A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150730&DB=EPODOC&CC=US&NR=2015211740A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JUNG SEUNGCHAI</creatorcontrib><creatorcontrib>YANG SIWON</creatorcontrib><creatorcontrib>KIM SINHYUN</creatorcontrib><title>COMBUSTOR</title><description>Provided is a combustor including a support shaft, a wing portion provided on the support shaft and configured to swirl a first fluid around the support shaft, and a cover housing enclosing the support shaft and the wing portion and includes a space enlarging portion provided at a downstream of of the wing portion, where a distance of the space enlarging portion from an outer surface of the support shaft is different from distances of other portions of the cover housing from the outer surface of the support shaft.</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZOB09vd1Cg0O8Q_iYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXxocFGBoamRoaG5iYGjobGxKkCALd6HJA</recordid><startdate>20150730</startdate><enddate>20150730</enddate><creator>JUNG SEUNGCHAI</creator><creator>YANG SIWON</creator><creator>KIM SINHYUN</creator><scope>EVB</scope></search><sort><creationdate>20150730</creationdate><title>COMBUSTOR</title><author>JUNG SEUNGCHAI ; YANG SIWON ; KIM SINHYUN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2015211740A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</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>JUNG SEUNGCHAI</creatorcontrib><creatorcontrib>YANG SIWON</creatorcontrib><creatorcontrib>KIM SINHYUN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JUNG SEUNGCHAI</au><au>YANG SIWON</au><au>KIM SINHYUN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMBUSTOR</title><date>2015-07-30</date><risdate>2015</risdate><abstract>Provided is a combustor including a support shaft, a wing portion provided on the support shaft and configured to swirl a first fluid around the support shaft, and a cover housing enclosing the support shaft and the wing portion and includes a space enlarging portion provided at a downstream of of the wing portion, where a distance of the space enlarging portion from an outer surface of the support shaft is different from distances of other portions of the cover housing from the outer surface of the support shaft.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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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 | COMBUSTOR |
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