A multiple fuel delivery system (100) for use with a gas turbine engine includes a first fuel tank (110) with a first fuel (120) therein, a second fuel tank (170) with a second fuel (180) therein, a mixing chamber (130), and a flow divider (250) downstream...

Liquid fuel assist ignition system (1) for providing a fuel-air mixture to a gas turbine in its start-up phase, comprising a high pressure tank (2), a vacuum pump (3) connected to the high pressure tank (2), a liquid fuel inlet (4) connected to the high pr...

An operation control method for a gas turbine comprising the steps of: making a molten salt map in a liquid phase state by calculating a dew point and a solidus temperature of molten salt for causing high-temperature corrosion on high-temperature component...

An operational control system of a gas turbine which is driven using mainly ammonia as fuel, wherein in a deteriorated combustibility operating region where the combustibility of ammonia deteriorates compared with the time of normal operation of the gas tu...