Combustor
A combustor includes a cap assembly that extends radially across at least a portion of the combustor, wherein the cap assembly includes an upstream surface axially separated from a downstream surface, and a combustion chamber downstream from the cap assembly. A plurality of tubes extend from the upstream surface through the downstream surface of the cap assembly, and each tube provides fluid communication through the cap assembly to the combustion chamber. The downstream surface is sloped at an angle with respect to the upstream surface.
1. A combustor comprising:
a cap assembly that extends radially across at least a portion of the combustor, wherein the cap assembly comprises an upstream surface axially separated from a downstream surface along an axial centerline;
a combustion chamber downstream from the cap assembly;
a plurality of tubes that extend from the upstream surface through the downstream surface of the cap assembly, wherein each tube provides fluid communication through the cap assembly to the combustion chamber; and
wherein the entire downstream surface is sloped at an angle with respect to the upstream surface towards the axial centerline, and wherein the slope of the entire downstream surface is one of downstream or upstream from an outer perimeter of the cap assembly.
2. The combustor as in claim 1 , wherein the downstream surface is sloped downstream from an outer perimeter of the cap assembly.
3. The combustor as in claim 1 , wherein the downstream surface has a concave curvature.
4. The combustor as in claim 1 , wherein the downstream surface has a convex curvature.
5. The combustor as in claim 1 , wherein each tube comprises an outlet proximate to the downstream surface, and the outlet defines a non-circular cross-section.
6. The combustor as in claim 1 , further comprising a barrier that extends radially inside the cap assembly between the upstream and downstream surfaces to separate a fuel plenum from a fluid plenum inside the cap assembly.
7. The combustor as in claim 6 , further comprising a plurality of fluid ports through the downstream surface, wherein the plurality of fluid ports provides fluid communication from the fluid plenum through the downstream surface.
8. The combustor as in claim 6 , further comprising a plurality of fuel ports through the plurality of tubes, wherein the plurality of fuel ports provides fluid communication from the fuel plenum through the plurality of tubes.
9. The combustor as in claim 1 , further comprising a fuel nozzle substantially aligned with an axial centerline of the cap assembly, wherein the plurality of tubes circumferentially surround the fuel nozzle.
10. A combustor comprising:
a cap assembly that extends radially across at least a portion of the combustor, wherein the cap assembly comprises an upstream surface axially separated from a downstream surface along an axial centerline;
a combustion chamber downstream from the cap assembly; and
a plurality of tubes that extend from the upstream surface through the downstream surface of the cap assembly, wherein each tube comprises an inlet proximate to the upstream surface, an outlet proximate to the downstream surface, and the outlet is sloped at an angle with respect to the inlet, and wherein the entire downstream surface is sloped at an angle with respect to the upstream surface towards the axial centerline, and wherein the slope of the entire downstream surface is one of downstream or upstream from an outer perimeter of the cap assembly.
11. The combustor as in claim 10 , wherein each outlet s sloped downstream from an outer perimeter of the cap assembly.
12. The combustor as in claim 10 , wherein each outlet has a concave curvature.
13. The combustor as in claim 10 , wherein each outlet has a convex curvature.
14. The combustor as in claim 10 , wherein the downstream surface has a concave curvature.