VAPORIZING LIQUID FUEL
The liquid fuel evaporation system for gas turbine engines has a "heat pipe" in the form of a closed container of non-condensible gas which pre-heats the incoming fuel and leads to more efficient combustion, with the object of reducing the carbon-monoxide and oxides of nitrogen passing thr...
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| creator | GEOFFREY ANTHONY HARROW WALTER DEREK MILLS |
| description | The liquid fuel evaporation system for gas turbine engines has a "heat pipe" in the form of a closed container of non-condensible gas which pre-heats the incoming fuel and leads to more efficient combustion, with the object of reducing the carbon-monoxide and oxides of nitrogen passing through the exhaust. The fuel inlet pipes (36) are situated over a trough-like conductor tube (37) leading to the central duct (30). A typical air/fuel ratio is 20/1. Extra cooling is provided for the "heat pipe" to control the pressure within the sealed container. |
| format | Patent |
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The fuel inlet pipes (36) are situated over a trough-like conductor tube (37) leading to the central duct (30). A typical air/fuel ratio is 20/1. Extra cooling is provided for the "heat pipe" to control the pressure within the sealed container.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; COMBUSTION ENGINES IN GENERAL ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INTERNAL-COMBUSTION PISTON ENGINES ; LIGHTING ; MECHANICAL ENGINEERING ; SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF ; WEAPONS</subject><creationdate>1976</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=19760311&DB=EPODOC&CC=AU&NR=7310674A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19760311&DB=EPODOC&CC=AU&NR=7310674A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GEOFFREY ANTHONY HARROW</creatorcontrib><creatorcontrib>WALTER DEREK MILLS</creatorcontrib><title>VAPORIZING LIQUID FUEL</title><description>The liquid fuel evaporation system for gas turbine engines has a "heat pipe" in the form of a closed container of non-condensible gas which pre-heats the incoming fuel and leads to more efficient combustion, with the object of reducing the carbon-monoxide and oxides of nitrogen passing through the exhaust. 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The fuel inlet pipes (36) are situated over a trough-like conductor tube (37) leading to the central duct (30). A typical air/fuel ratio is 20/1. Extra cooling is provided for the "heat pipe" to control the pressure within the sealed container.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MECHANICAL ENGINEERING SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF WEAPONS |
| title | VAPORIZING LIQUID FUEL |
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