Fuel distribution system for a gas turbine with multistage burner arrangement
View Patent ↗A fuel distribution system for a gas turbine with multistage burner arrangement is provided having at least one distribution line that branches off from a common fuel feed line and leads to a burner stage, and at least one element is provided in each distribution line for the specific influencing of the fuel mass flow. In such a fuel distribution system simplified controlling is made possible by a control valve being arranged in each case in one section of the distribution lines as an element for the specific influencing of the fuel mass flow, and in that a restrictor, which is preset in a fixed manner, is arranged in each case in the remaining distribution lines as an element for the specific influencing of the fuel mass flow.
1. A fuel distribution system, for a gas turbine with multistage burner arrangement having at least three stages, each stage comprising a plurality of burners connected by a common burner fuel ring, the plurality of burners being specific to the individual stage, the system comprising a plurality of distribution lines that branch directly off from a common fuel feed line and extend to each of the burner rings of each stage; in each of the distribution lines, a respective single element that provides the only specific influencing of the fuel mass flow is provided for each of the distribution lines; a control valve is arranged in a section of only one of the distribution lines as the element for the specific influencing of the fuel mass flow; and in each of the remaining distribution lines a restrictor, which is preset in a fixed manner, is arranged as the single element for the specific influencing of the fuel mass flow.
2. The fuel distribution system as claimed in claim 1 , wherein the single control valve is arranged in the distribution line which leads to a first burner stage.
3. The fuel distribution system as claimed in claim 1 , wherein the restrictors in the remaining distribution lines are selected so that respective fuel portions of the individual burner stages are adjusted to a fuel ratio which is favorable for a load range of the gas turbine.
4. The fuel distribution system as claimed in claim 1 , wherein the control valve is controlled by a control unit.