Gas turbine control method, storage medium storing gas turbine control program, gas turbine control device, and gas turbine facility
AssigneeMitsubishi Heavy Industries, Ltd.
InventorsMasayoshi HATTA, Kazuki MORIMOTO, Susumu WAKAZONO, Tomohiko YAMAMOTO
Life of this patent
Estimating the term…
Abstract
A control device includes a suction amount controller and a bleed flow controller. When an actual output is in a second output range from a second output to a third output less than the second output, the suction amount controller controls a suction amount so that the suction amount becomes constant even if the actual output decreases. The bleed flow controller controls a bleed flow so that the bleed flow gradually increases as the actual output decreases.
Claims16
A method of controlling a gas turbine including a compressor configured to compress air to generate the compressed air, a combustor configured to burn fuel in the compressed air to generate combustion gas, and a turbine driven by the combustion gas, the method of controlling the gas turbine comprising:
- a fuel control step of controlling a fuel flow rate so that the fuel flow rate of the fuel supplied to the combustor becomes a flow rate corresponding to a target output for the gas turbine;
- a suction amount control step of controlling a suction amount so that the suction amount, which is a flow rate of the air suctioned by the compressor, becomes a flow rate corresponding to an actual output of the gas turbine;
- and
- a bleed flow control step of controlling a bleed flow so that the bleed flow, which is a flow rate for externally exhausting a part of the compressed air from the compressor without involving the combustor, becomes a flow rate corresponding to the actual output,
- wherein the fuel flow rate is controlled so that the fuel flow rate gradually decreases as the target output decreases in the fuel control step,
- wherein the suction amount control step includes a first suction amount control step and a second suction amount control step,
- wherein the bleed flow control step includes a first bleed flow control step and a second bleed flow control step,
- wherein, when the actual output is in a first output range from a first output less than or equal to a rated output of the gas turbine to a second output that is an output less than the first output,
- the suction amount is controlled so that the suction amount gradually decreases as the actual output decreases in the first suction amount control step, and
- the bleed flow is controlled so that the bleed flow is maintained at 0 in the first bleed flow control step, and
- wherein, when the actual output is in a second output range from the second output to a third output that is an output less than the second output,
- the suction amount is controlled so that the suction amount gradually decreases as the actual output decreases or the suction amount becomes constant even if the actual output decreases in the second suction amount control step, and
- the bleed flow is controlled so that the bleed flow gradually increases as the actual output decreases and a ratio of the bleed flow to the suction amount becomes maximum when the actual output of the gas turbine becomes the third output in the second bleed flow control step.
A non-transitory computer-readable storage medium storing a control program for a gas turbine including a compressor configured to compress air to generate the compressed air, a combustor configured to burn fuel in the compressed air to generate combustion gas, a turbine driven by the combustion gas, a fuel line connected to the combustor so that the fuel is able to be supplied to the combustor, a fuel valve provided on the fuel line and configured to adjust a fuel flow rate that is a flow rate of the fuel flowing through the fuel line, a bypass line configured to externally exhaust a part of the compressed air from the compressor without involving the combustor, and a bypass valve provided on the bypass line and configured to adjust a bleed flow that is a flow rate of the compressed air flowing through the bypass line, wherein the compressor includes a suction amount adjuster having a vane capable of being opened and closed so that the suction amount that is a flow rate of air suctioned by the compressor is able to be adjusted, the control program causing a computer to perform:
- a fuel control step of determining the fuel flow rate in accordance with a target output for the gas turbine and indicating a valve opening degree to the fuel valve so that the determined fuel flow rate is reached;
- a suction amount control step of determining opening and closing angles of the vane in accordance with the actual output of the gas turbine and issuing an instruction to the suction amount adjuster so that the determined opening and closing angles of the vane are reached;
- and
- a bleed flow control step of determining a valve opening degree of the bypass valve in accordance with the actual output and issuing an instruction to the bypass valve so that the determined valve opening degree is reached,
- wherein the fuel flow rate is determined so that the fuel flow rate gradually decreases as the target output decreases and the valve opening degree is indicated to the fuel valve so that the determined fuel flow rate is reached in the fuel control step,
- wherein the suction amount control step includes a first suction amount control step and a second suction amount control step,
- wherein the bleed flow control step includes a first bleed flow control step and a second bleed flow control step.
- wherein, when the actual output is in a first output range from a first output less than or equal to a rated output of the gas turbine to a second output that is an output less than the first output,
- the opening and closing angles of the vane are determined so that the suction amount gradually decreases as the actual output decreases and the opening and closing angles of the vane are indicated to the suction amount adjuster in the first suction amount control step, and
- an instruction is issued to the bypass valve so that the bypass valve is closed in the first bleed flow control step, and
- wherein, when the actual output is in a second output range from the second output to a third output that is an output less than the second output,
- the opening and closing angles of the vane are determined so that the suction amount gradually decreases as the actual output decreases or the suction amount becomes constant even if the actual output decreases and the opening and closing angles of the vane are indicated to the suction amount adjuster in the second suction amount control step, and
- an instruction is issued to the bypass valve so that the bleed flow gradually increases as the actual output decreases and the bypass valve is fully opened when the actual output of the gas turbine becomes the third output in the second bleed flow control step.
A control device for a gas turbine including a compressor configured to compress air to generate the compressed air, a combustor configured to burn fuel in the compressed air to generate combustion gas, a turbine driven by the combustion gas, a fuel line connected to the combustor so that the fuel is able to be supplied to the combustor, a fuel valve provided on the fuel line and configured to adjust a fuel flow rate that is a flow rate of the fuel flowing into the fuel line, a bypass line configured to externally exhaust a part of the compressed air from the compressor without involving the combustor, and a bypass valve provided on the bypass line and configured to adjust a bleed flow that is a flow rate of the compressed air flowing through the bypass line, wherein the compressor includes a suction amount adjuster having a vane capable of being opened and closed so that the suction amount that is a flow rate of air suctioned by the compressor is able to be adjusted, the control device for the gas turbine comprising:
- a fuel controller configured to determine the fuel flow rate in accordance with a target output for the gas turbine and indicate a valve opening degree to the fuel valve so that the determined fuel flow rate is reached;
- a suction amount controller configured to determine opening and closing angles of the vane in accordance with the actual output of the gas turbine and issue an instruction to the suction amount adjuster so that the determined opening and closing angles of the vane are reached;
- and
- a bleed flow controller configured to determine a valve opening degree of the bypass valve in accordance with the actual output and issue an instruction to the bypass valve so that the determined valve opening degree is reached,
- wherein the fuel controller determines the fuel flow rate corresponding to the target output so that the fuel flow rate gradually decreases as the target output decreases and the valve opening degree is indicated to the fuel valve so that the determined fuel flow rate is reached,
- wherein the suction amount controller is able to perform a first suction amount control step and a second suction amount control step,
- wherein the bleed flow controller is able to perform a first bleed flow control step and a second bleed flow control step,
- wherein, when the actual output is in a first output range from a first output less than or equal to a rated output of the gas turbine to a second output that is an output less than the first output,
- the suction amount controller determines the opening and closing angles of the vane so that the suction amount gradually decreases as the actual output decreases and the opening and closing angles of the vane are indicated to the suction amount adjuster in the first suction amount control step, and
- the bleed flow controller issues an instruction to the bypass valve so that the bypass valve is closed in the first bleed flow control step, and
- wherein, when the actual output is in a second output range from the second output to a third output that is an output less than the second output,
- the suction amount controller determines the opening and closing angles of the vane so that the suction amount gradually decreases as the actual output decreases or the suction amount becomes constant even if the actual output decreases and the opening and closing angles of the vane are indicated to the suction amount adjuster in the second suction amount control step, and
- the bleed flow controller issues an instruction to the bypass valve so that the bleed flow gradually increases as the actual output decreases and the bypass valve is fully opened when the actual output of the gas turbine becomes the third output in the second bleed flow control step.
Dependencies are inferred from the claim text.