Method and device for compensating variations in fuel composition in a gas turbine system
View Patent ↗The invention relates to a method for compensating variations in fuel composition in a gas turbine system consisting of at least two parallel-operated burner stages, wherein the fuel supply to at least two of the burner stages is adjusted in response to variations in fuel composition, wherein the fuel split between the burner stages, i.e. the relative increase in speed of the fuel supplied to the burner stages, is adjusted to a target value or maintained at a target value during adjustment of the fuel supply. The target value can, for example be a constant or a function of one or several variables. More particularly, the gas turbine system can comprise a pilot burner stage and a main burner stage. When the fuel supply is adjusted, the fuel split between the pilot burner stage and the main burner stage is adjusted to a target value or maintained at a target value.
1. A gas turbine system comprising:
a control device for adjusting a fuel supply in a gas turbine system having a plurality of burner stages operated in parallel in which a plurality of fuel control valves are allocated to the burner stages and a regulator is allocated to the fuel control valves to compensate for variations in a fuel composition, the control device including an analyzer for analyzing the fuel composition, a computing unit for calculating a current Wobbe index of the fuel composition based on the analysis, and an updating unit for adjusting the regulator and the fuel control valves based on the calculated current Wobbe index to keep the fuel supply split between the burner stages at a constant target value;
a fuel line through which a fuel flows, including a branching point on the fuel line for branching off a part of the fuel and for introducing the branched off fuel into a branch line as an analysis sample flow; and
the analyzer positioned to receive the analysis sample flow, wherein a distance between the branching point and the fuel control valves is sufficiently elongated to allow:
the analyzer to fully analyze the fuel composition of the sample flow,
the computing unit to fully calculate the current Wobbe index, and
the updating unit to fully adjust the regulator and the fuel control valves before the fuel reaches the fuel control valves.
2. The control device as claimed in claim 1 , wherein the computing unit is physically separated from the regulator.
3. The control device as claimed in claim 1 , wherein the computing unit is integrated into the regulator.
4. The control device as claimed in claim 1 , wherein the updating unit is physically separated from the regulator.
5. The control device as claimed in claim 1 , wherein the updating unit is integrated into the regulator.
6. A gas turbine system, comprising:
a plurality of burner stages operated in parallel in which a plurality of fuel control valves are allocated to the burner stages and a regulator is allocated to the fuel control valves; and
a control device for adjusting a fuel supply in the gas turbine system to keep the fuel supply split between the burner stages at a constant target value to compensate for variations in a fuel composition, comprising:
an analyzer for analyzing the fuel composition,
a computing unit for calculating a current Wobbe index of the fuel composition based on the analysis, and
an updating unit for adjusting the regulator and the fuel control valves based on the calculated current Wobbe index, wherein the gas turbine system comprises:
a fuel line through which a fuel flows;
a branching point on the fuel line for branching off a part of the fuel and for introducing the branched off fuel as an analysis sample flow; and
a branch line which feeds the analysis sample flow to the analyzer of the control device,
wherein a distance between the branching point and the fuel control valves is sufficiently elongated to allow:
the analyzer to fully analyze the fuel composition of the sample flow,
the computing unit to fully calculate the current Wobbe index, and
the updating unit to fully adjust the regulator and the fuel control valves before the fuel reaches the fuel control valves.
7. The gas turbine system as claimed in claim 6 , wherein the gas turbine system comprises a pilot burner stage and a main burner stage.