SYSTEM AND METHOD FOR CONTROLLED FUEL BLENDING IN GAS TURBINES

A system includes a gas turbine engine having a combustor, and a fuel blending system. The fuel blending system further includes a first fuel supply configured to supply a first fuel, a second fuel supply configured to supply a second fuel, a first fuel circuit, a second fuel circuit, and a controll...

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Hauptverfasser: TRUESDALE ALAN MEIER, KULKARNI ABHIJIT PRABHAKAR, POPOVIC PREDRAG, MENON ARVIND VENUGOPAL
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creator TRUESDALE ALAN MEIER
KULKARNI ABHIJIT PRABHAKAR
POPOVIC PREDRAG
MENON ARVIND VENUGOPAL
description A system includes a gas turbine engine having a combustor, and a fuel blending system. The fuel blending system further includes a first fuel supply configured to supply a first fuel, a second fuel supply configured to supply a second fuel, a first fuel circuit, a second fuel circuit, and a controller. The first fuel circuit may be configured to blend the first fuel and the second fuel to form a first to form a first fuel mixture. The second fuel circuit may be configured to blend the first fuel and the second fuel to form a second fuel mixture. The controller may be configured to regulate blending of the first fuel mixture and the second fuel mixture based on a measured operating parameter of the combustor.
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subjects 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
title SYSTEM AND METHOD FOR CONTROLLED FUEL BLENDING IN GAS TURBINES
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