Operation of a gas turbine to lower load and MEL
AssigneeSiemens Energy Global GmbH & Co. KG
InventorKai Voit
Life of this patent
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Abstract
A method of operating a gas turbine, wherein a compressor for the gas turbine has adjustable guide vanes at the inlet of the compressor, wherein the compressed air by the compressor is mixed with fuel in order to burn the mixture inside a combustor, wherein the addition of fuel has a given fuel rate, wherein the gas tur is controlled from a high load to a given house load. At a first step the adjustable guide vanes are continuously closing and the fuel rate is also accordingly reduced and then in a second and final step starting at a turning point the adjustable guide vanes are not further closed, but the fuel rate is further reduced until the given house load is reached, so that a given exhaust flow is maintained.
Claims13
A method of operating a gas turbine in a combined cycle power plant, wherein a compressor for the gas turbine has adjustable guide vanes at an inlet of the compressor, wherein compressed air by the compressor is mixed with fuel for combustion inside a combustor, wherein an addition of fuel has a given fuel rate at steady state of the gas turbine, wherein the gas turbine is controlled from a full load or from a base load, down to a given house load, the method comprising:
- in a first step, closing the adjustable guide vanes continuously and reducing the fuel rate, and
- in a second step starting at a turning point, halting the closing of the adjustable guide vanes at the turning point and reducing the fuel rate further after halting the closing of the adjustable guide vanes until the given house load is reached, so that a given exhaust flow is maintained, wherein the turning point is at a given load, which is defined by the given house load in percent plus a difference in percent, wherein the difference is 5% up to 20%.
A method of operating a gas turbine in a combined cycle power plant, wherein a compressor for the gas turbine has adjustable guide vanes at an inlet of the compressor, wherein compressed air by the compressor is mixed with fuel for combustion inside a combustor, wherein an addition of fuel has a given fuel rate at steady state of the gas turbine, wherein the gas turbine is controlled from a full load or from a base load, down to a given house load, the method comprising:
- closing the adjustable guide vanes continuously while simultaneously reducing the fuel rate continuously in a first step at a first fuel reduction rate, the first fuel reduction rate being constant throughout the entire first step;
- and
- holding the adjustable guide vanes in a fixed position while constantly reducing the fuel rate during a second step at a second fuel reduction rate, wherein the second fuel reduction rate is constant throughout the entire second step, the second step occurring immediately after the first step,
- wherein the second fuel reduction rate is at least 10% greater than the first fuel reduction rate.
Dependencies are inferred from the claim text.