THIMBLE FAN FOR COMBUSTION SYSTEM
PROBLEM TO BE SOLVED: To protect an upstream part of a combustion liner from flame or heat. SOLUTION: The present application discloses a combustor liner 100. The combustor liner 100 comprises a large number of air mixing holes 110 and a large number of thimble fans 140 positioned thereon. A method...
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| creator | BERRY JONATHAN D KARIM HASAN DEFOREST RUSSELL |
| description | PROBLEM TO BE SOLVED: To protect an upstream part of a combustion liner from flame or heat. SOLUTION: The present application discloses a combustor liner 100. The combustor liner 100 comprises a large number of air mixing holes 110 and a large number of thimble fans 140 positioned thereon. A method for operating a fuel nozzle in the combustor liner having a large number of the air mixing holes includes a step for arranging a number of inclination slots on the upstream side of a first line of the air mixing holes on the combustor liner, a step for burning fuel flows from the fuel nozzle in the combustor liner, and a step for guiding air flows via the inclination slots so as to separate the burnt fuel flows from a wall of the combustor liner. COPYRIGHT: (C)2011,JPO&INPIT |
| format | Patent |
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The combustor liner 100 comprises a large number of air mixing holes 110 and a large number of thimble fans 140 positioned thereon. A method for operating a fuel nozzle in the combustor liner having a large number of the air mixing holes includes a step for arranging a number of inclination slots on the upstream side of a first line of the air mixing holes on the combustor liner, a step for burning fuel flows from the fuel nozzle in the combustor liner, and a step for guiding air flows via the inclination slots so as to separate the burnt fuel flows from a wall of the combustor liner. COPYRIGHT: (C)2011,JPO&INPIT</description><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>2010</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=20101111&DB=EPODOC&CC=JP&NR=2010256005A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20101111&DB=EPODOC&CC=JP&NR=2010256005A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BERRY JONATHAN D</creatorcontrib><creatorcontrib>KARIM HASAN</creatorcontrib><creatorcontrib>DEFOREST RUSSELL</creatorcontrib><title>THIMBLE FAN FOR COMBUSTION SYSTEM</title><description>PROBLEM TO BE SOLVED: To protect an upstream part of a combustion liner from flame or heat. SOLUTION: The present application discloses a combustor liner 100. The combustor liner 100 comprises a large number of air mixing holes 110 and a large number of thimble fans 140 positioned thereon. A method for operating a fuel nozzle in the combustor liner having a large number of the air mixing holes includes a step for arranging a number of inclination slots on the upstream side of a first line of the air mixing holes on the combustor liner, a step for burning fuel flows from the fuel nozzle in the combustor liner, and a step for guiding air flows via the inclination slots so as to separate the burnt fuel flows from a wall of the combustor liner. 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SOLUTION: The present application discloses a combustor liner 100. The combustor liner 100 comprises a large number of air mixing holes 110 and a large number of thimble fans 140 positioned thereon. A method for operating a fuel nozzle in the combustor liner having a large number of the air mixing holes includes a step for arranging a number of inclination slots on the upstream side of a first line of the air mixing holes on the combustor liner, a step for burning fuel flows from the fuel nozzle in the combustor liner, and a step for guiding air flows via the inclination slots so as to separate the burnt fuel flows from a wall of the combustor liner. COPYRIGHT: (C)2011,JPO&INPIT</abstract><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 | THIMBLE FAN FOR COMBUSTION SYSTEM |
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