COMBUSTION CONTROLLER FOR GAS TURBINE
PURPOSE:To enable the maintaining of a low NOx burning at a high efficiency by allowing stable combustion with a low NOx in a full load range while premixed combustion with a plurality of main burners is kept with a better balance even when a backfire occurs. CONSTITUTION:In a combustion apparatus o...
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| creator | OGA SHINICHI KITAJIMA JUNICHI KIMURA TAKEKIYO KAJITA SHINICHI |
| description | PURPOSE:To enable the maintaining of a low NOx burning at a high efficiency by allowing stable combustion with a low NOx in a full load range while premixed combustion with a plurality of main burners is kept with a better balance even when a backfire occurs. CONSTITUTION:In a combustion apparatus of a gas turbine in which a plurality of main burners 8 are arranged in the perimeter of a pilot burner 7 provided at the center of a combustion chamber, a fuel supply controller is provided to accomplish a pre mixed combustion with a pilot burner 7 by supplying a quantity of a fuel equivalent to that to be supplied to the main burners 8 to the pilot burner 7 when a backfire occurs in one of the burners 8. |
| format | Patent |
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CONSTITUTION:In a combustion apparatus of a gas turbine in which a plurality of main burners 8 are arranged in the perimeter of a pilot burner 7 provided at the center of a combustion chamber, a fuel supply controller is provided to accomplish a pre mixed combustion with a pilot burner 7 by supplying a quantity of a fuel equivalent to that to be supplied to the main burners 8 to the pilot burner 7 when a backfire occurs in one of the burners 8.</description><edition>5</edition><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION APPARATUS ; COMBUSTION ENGINES ; COMBUSTION PROCESSES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>1993</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=19931207&DB=EPODOC&CC=JP&NR=H05322169A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19931207&DB=EPODOC&CC=JP&NR=H05322169A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>OGA SHINICHI</creatorcontrib><creatorcontrib>KITAJIMA JUNICHI</creatorcontrib><creatorcontrib>KIMURA TAKEKIYO</creatorcontrib><creatorcontrib>KAJITA SHINICHI</creatorcontrib><title>COMBUSTION CONTROLLER FOR GAS TURBINE</title><description>PURPOSE:To enable the maintaining of a low NOx burning at a high efficiency by allowing stable combustion with a low NOx in a full load range while premixed combustion with a plurality of main burners is kept with a better balance even when a backfire occurs. CONSTITUTION:In a combustion apparatus of a gas turbine in which a plurality of main burners 8 are arranged in the perimeter of a pilot burner 7 provided at the center of a combustion chamber, a fuel supply controller is provided to accomplish a pre mixed combustion with a pilot burner 7 by supplying a quantity of a fuel equivalent to that to be supplied to the main burners 8 to the pilot burner 7 when a backfire occurs in one of the burners 8.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION PROCESSES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1993</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB19vd1Cg0O8fT3U3D29wsJ8vfxcQ1ScPMPUnB3DFYICQ1y8vRz5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8V4BHgamxkZGhmaWjsbEqAEAutQjqA</recordid><startdate>19931207</startdate><enddate>19931207</enddate><creator>OGA SHINICHI</creator><creator>KITAJIMA JUNICHI</creator><creator>KIMURA TAKEKIYO</creator><creator>KAJITA SHINICHI</creator><scope>EVB</scope></search><sort><creationdate>19931207</creationdate><title>COMBUSTION CONTROLLER FOR GAS TURBINE</title><author>OGA SHINICHI ; KITAJIMA JUNICHI ; KIMURA TAKEKIYO ; KAJITA SHINICHI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JPH05322169A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1993</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION PROCESSES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>OGA SHINICHI</creatorcontrib><creatorcontrib>KITAJIMA JUNICHI</creatorcontrib><creatorcontrib>KIMURA TAKEKIYO</creatorcontrib><creatorcontrib>KAJITA SHINICHI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>OGA SHINICHI</au><au>KITAJIMA JUNICHI</au><au>KIMURA TAKEKIYO</au><au>KAJITA SHINICHI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMBUSTION CONTROLLER FOR GAS TURBINE</title><date>1993-12-07</date><risdate>1993</risdate><abstract>PURPOSE:To enable the maintaining of a low NOx burning at a high efficiency by allowing stable combustion with a low NOx in a full load range while premixed combustion with a plurality of main burners is kept with a better balance even when a backfire occurs. CONSTITUTION:In a combustion apparatus of a gas turbine in which a plurality of main burners 8 are arranged in the perimeter of a pilot burner 7 provided at the center of a combustion chamber, a fuel supply controller is provided to accomplish a pre mixed combustion with a pilot burner 7 by supplying a quantity of a fuel equivalent to that to be supplied to the main burners 8 to the pilot burner 7 when a backfire occurs in one of the burners 8.</abstract><edition>5</edition><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | COMBUSTION CONTROLLER FOR GAS TURBINE |
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