Inlet air cooling system and inlet air cooling method for gas turbine
An inlet air cooling system used in a gas turbine for supplying power to a refrigerant compressor for compressing refrigerant in a natural gas liquefaction plant includes: an inlet air cooler for cooling inlet air of the gas turbine; chiller motors used for a chiller for cooling coolant supplied to the inlet air cooler; a first variable speed driver for supplying electric power to each of the one or more chiller motors; and an electric generator driven by the gas turbine, wherein the electric generator is electrically connected to the first variable speed driver, and electric power generated by the electric generator can be supplied to each of the chiller motors from the first variable speed driver without using a main power line of an electric power system, which enables efficient electric power supply to the motors via the variable speed driver.
1. An inlet air cooling system used in a gas turbine for supplying power to a refrigerant compressor for compressing refrigerant in a natural gas liquefaction plant, comprising:
an evaporator for cooling inlet air of the gas turbine by evaporative cooling;
a chiller for cooling coolant supplied to the evaporator by a refrigeration cycle, the chiller including one or more chiller motors;
a first variable speed driver for supplying electric power to each of the one or more chiller motors; and
an electric generator driven by the gas turbine,
wherein the electric generator is electrically connected to the first variable speed driver, and electric power generated by the electric generator is allowed to be supplied to each of the one or more chiller motors from the first variable speed driver without using a main power line of an electric power system,
wherein the electric generator functions as a starter motor for starting the gas turbine, and
wherein the gas turbine inlet air cooling system further comprises a second variable speed driver for supplying electric power from the main power line to the electric generator which functions as the starter motor.
2. The gas turbine inlet air cooling system according to claim 1 , wherein at least part of the electric power generated by the electric generator is supplied from the second variable speed driver to the main power line.
3. The gas turbine inlet air cooling system according to claim 1 , wherein at least part of the electric power generated by the electric generator is supplied from the first variable speed driver to the main power line.
4. The gas turbine inlet air cooling system according to claim 1 , wherein the chiller motor comprises at least one selected from the group consisting of a chiller compressor motor for driving a chiller compressor used in the chiller; a first pump motor for driving a first pump for moving the coolant cooled by the chiller to the evaporator; and a second pump motor for driving a second pump for moving heating medium to a cooling tower, wherein heat exchange is performed between the heating medium and the coolant in a condenser used in the chiller.
5. The gas turbine inlet air cooling system according to claim 1 , wherein the refrigerant compressor includes a propane compressor and a mixed refrigerant compressor for compressing propane refrigerant and a mixed refrigerant, respectively, for a C3-MR process used in the natural gas liquefaction plant.
6. An inlet air cooling method used in a gas turbine for supplying power to a refrigerant compressor for compressing refrigerant in a natural gas liquefaction plant, comprising:
an inlet air cooling step for cooling inlet air of the gas turbine by an evaporator;
a chilling step for cooling coolant used in the inlet air cooling step by a refrigeration cycle; and
a generating step for driving an electric generator by the gas turbine to generate electric power; and
an electric power supplying step in which electric power generated by the electric generator is supplied to one or more motors used in the chilling step from a first variable speed river without using a main power line of an electric power system,
wherein the electric generator functions as a starter motor for starting the gas turbine, and
wherein the gas turbine inlet air cooling system further comprises a second variable speed driver for supplying electric power from the main power line to the electric generator which functions as the starter motor.