Burner arrangement having a peripheral staging concept
A burner arrangement has a plurality of mixing channels which extend parallel to the main axis of the burner arrangement and are arranged in at least two concentric circles, in which mixing channels fuel and discharge air from the compressor are mixed during the operation of the burner arrangement. The mixing channels are grouped together into fuel stages so as to produce an irregular staging in the peripheral direction of the burner arrangement.
1. A burner arrangement of a gas turbine combustor, comprising:
a plurality of mixing channels, which extend parallel to a main axis of the burner arrangement and are arranged in at least two concentric circles, in the plurality of mixing channels fuel and discharge air from a compressor are mixed during operation of the burner arrangement,
wherein the plurality of mixing channels are grouped together into fuel stages, wherein a fuel stage of the fuel stages comprises a portion of the plurality of mixing channels with a common fuel supply, which are controlled jointly during operation, and irregular staging in a circumferential direction of the burner arrangement is obtained in respect of a geometric distribution of the plurality of mixing channels associated with each of the fuel stages, wherein the fuel stage comprises different number of the plurality of mixing channels than in a different fuel stage of the fuel stages, wherein the common fuel supply in the fuel stage is different than a common fuel supply in the different fuel stage of the fuel stages,
wherein the fuel stage comprises at least two subgroups, wherein each subgroup of the at least two subgroups comprises at least two directly adjacent mixing channels of the plurality of mixing channels in two different circles of the at least two concentric circles, wherein each subgroup of the at least two subgroups comprises different number of the plurality of mixing channels in each of the two different circles.
2. The burner arrangement as claimed in claim 1 , further comprising:
a centrally arranged pilot burner.
3. The burner arrangement as claimed in claim 1 ,
wherein a first number of the plurality of mixing channels in a circle of the at least two concentric circles within one subgroup of the at least two subgroups is no more than twice a second number of the plurality of mixing channels in another circle of the at least two concentric circles of the one subgroup.
4. The burner arrangement as claimed in claim 1 ,
wherein the subgroups in at least one of the fuel stages have different numbers of the plurality of mixing channels from each other.
5. The burner arrangement as claimed in claim 1 ,
wherein a first number of the plurality of mixing channels in one of the fuel stages exceeds a second number of the plurality of mixing channels of another of the fuel stages different from the one of the fuel stages by no more than 50%.