Combustor replacement method and gas turbine plant
A combustor replacement method and a gas turbine plant capable of efficiently replacing a combustor using an existing facility. The combustor replacement method includes a step of separating, from a plurality of fuel supply systems, a first combustor that includes a plurality of nozzle systems connected to any of the plurality of fuel supply systems and supplied with fuel from the connected fuel supply systems, and removing the first combustor from a gas turbine plant. The method includes a step of attaching a second combustor that includes fewer nozzle systems than the first combustor to the gas turbine plant, and a step of providing communication between the fuel supply systems connected to the same nozzle system of the second combustor by a coupling pipe, and coupling the fuel supply systems and the second combustor.
1. A combustor replacement method for replacing a combustor of a gas turbine in a gas turbine plant including the combustor and a plurality of fuel supply systems that supplies fuel to the combustor, the method comprising the steps of:
separating, from the plurality of fuel supply systems, a first combustor that comprises a plurality of first nozzle systems connected to any of the plurality of fuel supply systems and supplied with the fuel from the connected fuel supply systems, and removing the first combustor from the gas turbine plant;
attaching a second combustor to the gas turbine plant, the second combustor comprises a plurality of second nozzle systems, wherein the number of second nozzle systems of the second combustor is fewer than the number of first nozzle systems of the first combustor; and
providing communication by a coupling pipe between one fuel supply system and another fuel supply system of the plurality of fuel supply systems connected to the plurality of second nozzle systems, and coupling the fuel supply systems and the second combustor.
2. The combustor replacement method according to claim 1 , wherein
the fuel supply systems comprise a plurality of manifolds and a plurality of branch pipes that connect the plurality of manifolds and the coupling pipe, and
the coupling pipe connects the plurality of branch pipes and the plurality of second nozzle systems.
3. The combustor replacement method according to claim 2 , further comprising a step of providing communication between the fuel supply systems by an upstream side coupling pipe on an upstream side of the manifolds connected to the plurality of second nozzle systems.
4. The combustor replacement method according to claim 3 , wherein the upstream side coupling pipe is disposed in the vicinity of the manifolds.
5. The combustor replacement method according to claim 3 , wherein
the fuel supply systems each comprise a regulating valve that regulates supply of the fuel on an upstream side of the manifold, and
the upstream side coupling pipe is disposed between the manifold and the regulating valve.
6. The combustor replacement method according to claim 3 , wherein the upstream side coupling pipe comprises an on-off valve disposed thereon.
7. The combustor replacement method according to claim 1 , further comprising the steps of:
removing respective manifolds of the fuel supply systems connected to the plurality of second nozzle systems; and
providing a common manifold in the fuel supply systems connected to the plurality of second nozzle systems,
wherein the coupling pipe is a first coupling pipe, and
wherein a second coupling pipe is provided on an upstream side of the manifold.