SYSTEM AND METHOD FOR OPERATING A COMBUSTOR WITH MULTIPLE LIQUID FUELS

The systems and methods presented herein are configured to transition from a first liquid fuel (38a) supplied to a combustor (14) of a gas turbine system (10) to a second liquid fuel (38b) supplied to the combustor (14) utilizing a fuel pump (42) configured to supply both fuels (38a, 38b) from the f...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	TEJEDA, Ely, Edgardo, SCHORNICK, Joe, Floyd, GRAZIANO TORRES, Rene, CASTILLO, Jesus, Daniel, HUYNH, Tuy, Cam, BABIUCH, Miroslaw, Pawel
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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