Combustor fuel supply assembly and related method

A system includes a turbine fuel supply system (40). The turbine fuel supply system includes a first turbine fuel mixer (52) configured to mix a first liquid fuel (42) and a first deaerated water (15) to generate a first fuel mixture. The first fuel mixture is configured to combust in a combustor (1...

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Bibliographische Detailangaben
Hauptverfasser:	ZHANG, HUA, BEADIE, DOUGLAS FRANK, CODRON, FABIEN THIBAULT, ROSS, WILLIAM THOMAS, MYERS, GEOFFREY DAVID
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A system includes a turbine fuel supply system (40). The turbine fuel supply system includes a first turbine fuel mixer (52) configured to mix a first liquid fuel (42) and a first deaerated water (15) to generate a first fuel mixture. The first fuel mixture is configured to combust in a combustor (16) of a gas turbine engine (10). The turbine fuel supply system also includes a deaerated water flow path (70) configured to route the first deaerated water (15) to the first turbine fuel mixer (52) and a liquid fuel flow path configured to route the first liquid fuel to the first turbine fuel mixer (52).