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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Bibliographische Detailangaben
Hauptverfasser:	GEOFFREY ANTHONY HARROW, WALTER DEREK MILLS
Format:	Patent
Sprache:	eng
Schlagworte:	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
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Beschreibung
Zusammenfassung:	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.