Combustor can temperature control system
The present application provides a fuel delivery system for a combustor with reduced coherence and/or reduced combustion dynamics. The combustor can assembly may include a first manifold for delivering a first flow of fuel to a first set of fuel injectors and a second manifold for delivering a second flow of fuel to a second set of fuel injectors. The first flow of fuel may have a first temperature and the second flow of fuel may have a second temperature. The first temperature may be higher than the second temperature.
1. A fuel delivery system for a combustor with reduced coherence and/or reduced combustion dynamics, comprising:
a first manifold for delivering a first flow of fuel to a first set of fuel injectors;
wherein the first manifold comprises a fuel heater to heat the first flow of fuel; and
a second manifold for delivering a second flow of fuel to a second set of fuel injectors;
wherein the second manifold comprises a fuel blender in communication with a source flow at an ambient temperature and the heated first flow of fuel to create the second flow of fuel;
the first flow of fuel comprising a first temperature;
the second flow of fuel comprising a second temperature; and
wherein the first temperature is higher than the second temperature.
2. The fuel delivery system of claim 1 , wherein the first set of fuel injectors are positioned within a first combustor can and wherein the second set of fuel injectors are positioned within a second combustor can.
3. The fuel delivery system of claim 1 , wherein the first set of fuel injectors are positioned within a first combustor can and wherein the second set of fuel injectors are positioned within the first combustor can.
4. The fuel delivery system of claim 1 , further comprising a first manifold line in communication with the first manifold and a fuel source.
5. The fuel delivery system of claim 4 , wherein the first manifold line comprises the fuel heater thereon.
6. The fuel delivery system of claim 4 , further comprising a second manifold line in communication with the second manifold and the fuel source with the source flow at the ambient temperature.
7. The fuel delivery system of claim 6 , wherein the second manifold line comprises the fuel blender thereon.
8. The fuel delivery system of claim 7 , wherein the fuel blender comprises a tap off line in communication with the first flow of fuel such that the fuel blender blends the source flow at the ambient temperature and the first flow at the first temperature.
9. The fuel delivery system of claim 6 , further comprising a third manifold line in communication with a fuel source.
10. The fuel delivery system of claim 9 , wherein the third manifold line comprises a fuel blender thereon.
11. The fuel delivery system of claim 9 , wherein the third manifold line comprises a third flow of fuel therein at a third temperature and wherein the third temperature is less than or greater than the second temperature.
12. The fuel delivery system of claim 11 , further comprising a fourth manifold line in communication with a fuel source.
13. The fuel delivery system of claim 12 , wherein the fourth manifold line comprises a fuel blender thereon.
14. The fuel delivery system of claim 12 , wherein the fourth manifold line comprises a fourth flow of fuel therein at a fourth temperature and wherein the fourth temperature is less than or greater than the second temperature or the third temperature.
15. A fuel delivery system for a combustor can assembly with reduced coherence and/or combustion dynamics, comprising:
a first manifold for delivering a first flow of fuel to a first set of combustor cans;
a fuel heater in communication with the first manifold to heat the first flow of fuel;
a second manifold for delivering a second flow of fuel to a second set of combustor cans;
the second manifold in communication with a source flow at an ambient temperature; and
a fuel blender in communication with the ambient source flow of the second manifold and the heated first flow of fuel to create the second flow of fuel;
the first flow of fuel comprising a first temperature;
the second flow of fuel comprising a second temperature; and
wherein the first temperature is higher than the second temperature.
16. The fuel delivery system of claim 15 , further comprising a third manifold, wherein the third manifold comprises a third flow of fuel therein at a third temperature, and wherein the third temperature is less than or greater than the second temperature.
17. The fuel delivery system of claim 16 , further comprising a fourth manifold, wherein the fourth manifold comprises a fourth flow of fuel therein at a fourth temperature, and wherein the fourth temperature is less than or greater than the second temperature or the third temperature.