System and method for providing highly reactive fuels to a combustor
A system and related method for providing a highly reactive fuel to a combustor of a gas turbine are disclosed herein. The system includes a fuel supply system that is in fluid communication with a fuel supply. The fuel supply system includes multiple fuel circuits. Each fuel circuit individually feeds fuel to a corresponding fuel distribution manifold. The system further includes a steam injection system. The steam injection system includes at least one flow control valve that is in fluid communication with at least one of the fuel circuits. The flow control valve provides for fluid communication between a superheated steam source and the fuel circuit during both fueled operation and during non-fueled operation of the corresponding fuel circuit.
1. A system for modulating a modified Wobbe index of a highly reactive fuel, comprising:
a gas turbine having a combustor, a turbine downstream from the combustor, a gas fuel supply, a first fuel distribution manifold fluidly coupled between the gas fuel supply and the combustor and a second fuel distribution manifold fluidly coupled between the gas fuel supply and the combustor;
a first fuel circuit extending from a first stop valve downstream of the gas fuel supply to the first fuel distribution manifold;
a second fuel circuit extending from a second stop valve downstream of the gas fuel supply to the second fuel distribution manifold; and
a heat recovery steam generator disposed downstream from the turbine, the heat recovery steam generator connected directly to the first fuel circuit through a first flow control valve and connected directly to the second fuel circuit through a second flow control valve, wherein the heat recovery steam generator provides a first flow of steam to the first fuel distribution manifold via the first flow control valve and a second flow of steam to the second fuel distribution manifold via the second flow control valve.
2. The system as in claim 1 , wherein the first fuel distribution manifold and the first flow control valve are fluidly coupled to a first premix fuel circuit of the combustor.
3. The system as in claim 1 , wherein the second fuel distribution manifold and the second flow control valve are fluidly coupled to a second premix fuel circuit of the combustor.
4. The system as in claim 1 , further comprising a heat exchanger positioned between the gas fuel supply and the first fuel distribution manifold, wherein the heat exchanger is in thermal communication with the highly reactive fuel flowing from the gas fuel supply to the first fuel distribution manifold.
5. The system as in claim 1 , further comprising a heat exchanger positioned between the gas fuel supply and the second fuel distribution manifold, wherein the heat exchanger is in thermal communication with the highly reactive fuel flowing from the gas fuel supply to the second fuel distribution manifold.
6. The system as in claim 1 , further comprising a third fuel distribution manifold fluidly coupled between the gas fuel supply and the combustor and a third flow control valve positioned downstream from the gas fuel supply, wherein the heat recovery steam generator provides a third flow of steam to the third fuel distribution manifold via the third flow control valve.
7. The system as in claim 6 , wherein the third flow control valve is fluidly coupled to the third fuel distribution manifold at a location that is downstream from the gas fuel supply and upstream from the third fuel distribution manifold.
8. The system as in claim 6 , wherein the third fuel distribution manifold and the third flow control valve are fluidly coupled to a third premix fuel circuit of the combustor.
9. The system as in claim 6 , further comprising a heat exchanger positioned between the gas fuel supply and the third fuel distribution manifold, wherein the heat exchanger is in thermal communication with the highly reactive fuel flowing from the gas fuel supply to the third fuel distribution manifold.