Combustor and method for supplying fuel to a combustor
A combustor includes an end cap having upstream and downstream surfaces and a cap shield surrounding the upstream and downstream surfaces. First and second sets of premixer tubes extend from the upstream surface through the downstream surface. A first fuel conduit supplies fuel to the first set of premixer tubes. A casing circumferentially surrounds the cap shield to define an annular passage, and a second fuel conduit supplies fuel through the annular passage to the second set of premixer tubes. A method for supplying fuel to a combustor includes flowing a working fluid through first and second sets of premixer tubes, flowing a first fuel into the first set of premixer tubes, and flowing a second fuel through an annular passage surrounding the end cap and into the second set of premixer tubes.
1. A combustor, comprising:
a. an end cap that extends radially across at least a portion of the combustor, wherein the end cap comprises an upstream surface axially separated from a downstream surface and a cap shield circumferentially surrounding the upstream and downstream surfaces;
b. a first set of premixer tubes extending from the upstream surface through the downstream surface to provide fluid communication through the end cap;
c. a first fuel conduit in fluid communication with the first set of premixer tubes to supply fuel to the first set of premixer tubes;
d. a second set of premixer tubes extending from the upstream surface through the downstream surface to provide fluid communication through the end cap;
e. a casing circumferentially surrounding at least a portion of the cap shield to define an annular passage between the cap shield and the casing;
f. a second fuel conduit in fluid communication with the second set of premixer tubes to supply fuel through the annular passage to the second set of premixer tubes
g. a barrier disposed between the upstream and downstream surfaces, wherein the barrier at least partially defines a fuel plenum and an air plenum inside the end cap; and
h. a divider disposed within the end cap separating fuel flows to the first and second sets of premix tubes.
2. The combustor as in claim 1 , wherein the first fuel conduit supplies fuel through the annular passage to the first set of premixer tubes.
3. The combustor as in claim 1 , wherein the second set of premixer tubes surrounds the first set of premixer tubes.
4. The combustor as in claim 1 , further comprising an expansion joint between the upstream and downstream surfaces.
5. The combustor as in claim 1 , further comprising at least one of an airfoil or vane surrounding at least a portion of the second fuel conduit in the annular passage.
6. The combustor as in claim 1 , further comprising an air port through the cap shield, wherein the air port provides fluid communication from the annular passage, through the cap shield, and into the air plenum.
7. The combustor as in claim 1 , further comprising a shroud circumferentially surrounding the first fuel conduit, wherein the shroud provides fluid communication through the end cap.
8. The combustor as in claim 7 , further comprising a swirler vane between the shroud and the first fuel conduit.
9. A combustor, comprising:
a. an end cap that extends radially across at least a portion of the combustor, wherein the end cap comprises an upstream surface axially separated from a downstream surface and a cap shield circumferentially surrounding the upstream and downstream surfaces;
b. a first fuel conduit in fluid communication with the end cap;
c. a first set of premixer tubes extending from the upstream surface through the downstream surface to provide fluid communication through the end cap;
d. a second set of premixer tubes extending from the upstream surface through the downstream surface to provide fluid communication through the end cap;
e. a casing circumferentially surrounding at least a portion of the end cap to define an annular passage between the end cap and the casing;
f. a second fuel conduit in fluid communication with the second set of premixer tubes to supply fuel through the annular passage to the second set of premixer tubes
g. a barrier disposed between the upstream and downstream surfaces, wherein the barrier at least partially defines a fuel plenum and an air plenum inside the end cap; and
h. a divider disposed within the end cap separating fuel flows to the first and second sets of premix tubes.
10. The combustor as in claim 9 , wherein the first fuel conduit supplies fuel to the first set of premixer tubes.
11. The combustor as in claim 9 , wherein the second set of premixer tubes surrounds the first set of premixer tubes.
12. The combustor as in claim 9 , further comprising at least one of an airfoil or vane surrounding the second fuel conduit in the annular passage.
13. The combustor as in claim 9 , further comprising an expansion joint between the upstream and downstream surfaces.
14. The combustor as in claim 9 , further comprising a third fuel conduit in fluid communication with the first set of premixer tubes, wherein the third fuel conduit supplies fuel through the annular passage to the first set of premixer tubes.
15. The combustor as in claim 9 , further comprising an air port through the cap shield, wherein the air port provides fluid communication from the annular passage, through the cap shield, and into the air plenum.
16. The combustor as in claim 9 , further comprising a shroud circumferentially surrounding the first fuel conduit, wherein the shroud provides fluid communication through the end cap.