Burner arrangement
View Patent ↗A burner arrangement is provided. The burner arrangement includes a support and at least two fuel nozzles attached to the support in the direction of flow, with each fuel nozzle including a support-side section which includes a contact surface on the support side with which it rests on a supporting surface of the support, with at least two fuel nozzle tips embodied in one piece extending out from the support-side section in the direction of flow and the support-side contact surface including at least two extension parts projecting in the direction of the support, with the extension parts each embodying a channel through which fuel is fed in each case to the fuel nozzle tips through passages which are arranged in the support-side contact surface of the support-side section.
1. A burner arrangement, comprising:
a support; and
at least two fuel nozzles attached to the support in a flow direction,
wherein each fuel nozzle includes a support-side section which has a contact surface on a support side, wherein the contact surface rests against a supporting surface of the support,
wherein each fuel nozzle comprises at least two fuel nozzle tips, the least two fuel nozzle tips extending outwards in the flow direction from the support-side section of the fuel nozzle,
wherein the contact surface of the support-side section includes at least two extension parts projecting in a direction of the support, and
wherein the at least two extension parts each embody a channel through which fuel is supplied to the at least two fuel nozzle tips through a plurality of passages connected downstream from the at least two extension parts in the flow direction, which are arranged in the support-side contact surface of the support-side section.
2. The burner arrangement as claimed in claim 1 , wherein the at least two extension parts are an oil channel and a gas channel respectively.
3. The burner arrangement as claimed in claim 2 , wherein a further oil channel is present.
4. The burner arrangement as claimed in claim 3 , wherein each of the respective oil channels supplies one fuel nozzle tip of the at least two fuel nozzle tips with oil.
5. The burner arrangement as claimed in claim 1 , wherein the at least two extension parts are connected to make a positive or non-positive fit with the plurality of passages in the support-side of the support-side section of the at least two fuel nozzles.
6. The burner arrangement as claimed in claim 1 ,
wherein the at lest two extension parts each comprise a remote end against the direction of flow, each remote end comprising a first attachment element, and
wherein the at least two extension parts are attached to the support using the first attachment elements.
7. The burner arrangement as claimed in claim 1 , wherein at least the at least two fuel nozzle tips of the support-side section and the support side contact surface with the plurality of passages are embodied as a casting.
8. The burner arrangement as claimed in claim 1 , wherein the at least two extension parts with the plurality of passages are welded in the support-side section of the at least two fuel nozzles.
9. The burner arrangement as claimed in claim 1 , wherein the as least two extension parts are embodied in one piece.
10. The burner arrangement as claimed in claim 1 , wherein the support-side contact surface includes an opening for attaching the support-side contact surface to the supporting surface of the support.
11. The burner arrangement as claimed in claim 10 , wherein at least six openings are provided in the support side contact surface, openings being distributed over an entire support-side contact surface.
12. A gas turbine, comprising:
a burner arrangement, comprising:
a support; and
at least two fuel nozzles attached to the support in a flow direction,
wherein each fuel nozzle includes a support-side section which has a contact surface on a support side, wherein the contact surface rests against a supporting surface of the support,
wherein each fuel nozzle comprises at least two fuel nozzle tips, the least two fuel nozzle tips extending outwards in the flow direction from the support-side section of the fuel nozzle,
wherein the contact surface of the support -side section includes at least two extension parts projecting in a direction of the support, and
wherein the at least two extension parts each embody a channel through which fuel is supplied to the at least two fuel nozzle tips through a plurality of passages connected downstream from the at least two extension parts in the flow direction, which are arranged in the support-side contact surface of the support-side section.