Operation control method for gas turbine and operation controller for gas turbine
View Patent ↗An operation control method for a gas turbine includes making a molten salt map of molten salt for causing high-temperature corrosion on high-temperature components of the turbine due to impurities using a thermodynamic equilibrium calculation on the basis of the impurities contained in low-quality fuel and operation data of the gas turbine, indicating a surface temperature and a pressure of the high-temperature components of the turbine on the molten salt map , predicting a lifetime of the high-temperature components of the gas turbine by estimating a corrosion rate thereof, and controlling the flow rate of the low-quality fuel supplied to a combustor so that an area of surface temperature and pressure regions of the high-temperature components superposing on the region of molten salt in the liquid phase on the molten salt map is reduced.
1. An operation control method for a gas turbine for burning low-quality fuel containing high-temperature corrosive impurities, comprising the steps of:
making a molten salt map showing the dew point and solidus temperatures of a molten salt in a liquid phase state as a function of pressure, the molten salt being selected on a basis of impurities contained in the low-quality fuel and operation data of the gas turbine, by calculating a dew point and a solidus temperature of molten salt resulting from combustion of the low-quality fuel and causing high-temperature corrosion on high-temperature components of the gas turbine through which high-temperature combustion gas flows using a thermodynamic equilibrium calculation,
calculating and indicating a surface temperature and a pressure of the high-temperature components of the gas turbine superposed on the molten salt map to determine a superposition state of the surface temperature and the pressure on a region of molten salt in a liquid phase,
predicting a lifetime of the high-temperature components of the gas turbine by estimating a corrosion rate of the high-temperature components, and
controlling a flow rate of the low-quality fuel supplied to a combustor on the basis of the prediction of the lifetime of the high-temperature components so that an area of surface temperature and pressure regions of the high-temperature components of the gas turbine superposed on the region of molten salt in the liquid phase on the molten salt map is reduced.
2. The operation control method for a gas turbine according to claim 1 , wherein:
the calculation for the molten salt map preparation, on the basis of the impurities contained in fuel data of the low-quality fuel and the operation data, prepares the molten salt map composed of a gas phase, a liquid phase, and a solid phase by calculating a dew point and a solidus temperature of an alkaline sulfate and a vanadium compound for causing high-temperature corrosion on the high-temperature components composing the gas turbine through which high-temperature combustion gas flows down due to the impurities using the thermodynamic equilibrium calculation.
3. The operation control method for a gas turbine according to claim 1 , wherein:
the calculation for corrosion region determination shows the surface temperature and the pressure of the high-temperature components calculated using design data of the high-temperature components of the gas turbine on the molten salt map made by the calculation for the molten salt map preparation and determines whether the surface temperature and the pressure superpose on the region of molten salt in the liquid phase or not.
4. The operation control method for a gas turbine according to claim 1 , wherein:
the calculation for corrosion damage prediction estimates the corrosion rate of the high-temperature components of the gas turbine using material data and periodic inspection data and predicts the lifetime of the high-temperature components.
5. The operation control method for a gas turbine according to claim 1 , wherein:
the calculation for operation condition optimization, on the basis of the prediction of the lifetime of the high-temperature components calculated in corrosion damage prediction, controls the flow rate of the low-quality fuel supplied to the combustor of the gas turbine device so as to reduce so that an area of surface temperature and pressure regions of movable blades and static blades, which are the high-temperature components of the gas turbine, superposing on the region of molten salt in the liquid phase on the molten salt map is reduced.
6. The operation control method for a gas turbine according to claim 4 , wherein:
the calculation for the corrosion damage prediction performs the prediction of the lifetime of the high-temperature components on the basis of a molten salt generation quantity in the combustion gas.
7. The operation control method for a gas turbine according to claim 1 , wherein:
in the calculation for the molten salt map preparation, impurity concentration in the combustion gas in a calculation of a molten salt generation quantity performed by the thermodynamic equilibrium calculation is a concentration of sodium, potassium and sulfur.
8. The operation control method for a gas turbine according to claim 1 , wherein:
in the calculation for the molten salt map preparation, impurity concentration in the combustion gas in a calculation of a molten salt generation quantity performed by the thermodynamic equilibrium calculation is a concentration of sodium, potassium, sulfur, and vanadium.
9. An operation controller for a gas turbine for burning low-quality fuel containing high-temperature corrosive impurities, comprising:
a calculator for molten salt map preparation for making a molten salt map showing the dew point and solidus temperatures of a molten salt in a liquid phase state as a function of pressure, the molten salt being selected on a basis of impurities contained in the low-quality fuel and operation data, by calculating a dew point and a solidus temperature of molten salt resulting from combustion of the low-quality fuel and causing high-temperature corrosion on high-temperature components of the gas turbine through which high-temperature combustion gas flows using a thermodynamic equilibrium calculation,
a calculator for corrosion region determination for calculating and indicating a surface temperature and a pressure of the high-temperature components of the gas turbine superposed on the molten salt map made by the calculator for molten salt map preparation to determine a superposition state of the surface temperature and the pressure on a region of molten salt in a liquid phase,
a calculator for corrosion damage prediction for predicting a lifetime of the high-temperature components of the gas turbine by estimating a corrosion rate of the high-temperature components, and
a calculator for operational condition optimization and outputting a command signal for controlling a flow rate of the low-quality fuel supplied to a combustor on the basis of the prediction of the lifetime of the high-temperature components so that an area of surface temperature and pressure regions of the high-temperature components of the gas turbine superposed on the region of molten salt in the liquid phase on the molten salt map is reduced.
10. The operation controller for a gas turbine according to claim 9 , wherein:
the calculator for molten salt map preparation, on the basis of impurities contained in fuel data of the low-quality fuel installed in an input data device and operation data, prepares the molten salt map composed of a gas phase, a liquid phase, and a solid phase by calculating a dew point and a solidus temperature of an alkaline sulfate or molten salt of a vanadium compound for causing high-temperature corrosion on the high-temperature components of the turbine through which high-temperature combustion gas flows down due to the impurities using the thermodynamic equilibrium calculation.
11. The operation controller for a gas turbine according to claim 9 , wherein:
the calculator for corrosion region determination shows the surface temperature and the pressure of the high-temperature components calculated using design data of the high-temperature components of the gas turbine installed in an input data device on the molten salt map made by the calculator for molten salt map preparation and determines whether the surface temperature and the pressure superpose on the region of molten salt in the liquid phase or not.
12. The operation controller for a gas turbine according to claim 9 , wherein:
the calculator for corrosion damage prediction estimates the corrosion rate of the high-temperature components of the gas turbine using material data and periodic inspection data installed in an input data device and predicts the lifetime of the high-temperature components.
13. The operation controller for a gas turbine according to claim 9 , wherein:
the calculator for operation condition optimization, on the basis of the prediction of the lifetime of the high-temperature components calculated by the calculator for corrosion damage prediction, controls the flow rate of the low-quality fuel supplied to the combustor of the gas turbine device so as to reduce so that an area of surface temperature and pressure regions of movable blades and static blades which are the high-temperature components of the gas turbine superposing on the region of molten salt in the liquid phase on the molten salt map is reduced.
14. The operation controller for a gas turbine according to claim 12 , wherein:
the calculator for corrosion damage prediction performs the prediction for the lifetime of the high-temperature components on the basis of a molten salt generation quantity in the combustion gas.