Fuel injection assembly having a boss with a serpentine cooling passage
Fuel injection assemblies and combustors are provided. The fuel injection assembly includes a fuel injector that is configured to couple to an outer sleeve of the combustor. The fuel injection assembly further comprises a boss that is spaced apart from the fuel injector and is configured to couple to a combustion liner of the combustor. The boss includes a flange portion, an annular wall portion extending from the flange portion, and an interior surface. The boss defines a serpentine cooling passage that extends from an inlet on the flange portion to an outlet on the interior surface.
1 . A fuel injection assembly for a combustor of a gas turbine, the fuel injection assembly comprising:
a fuel injector configured to couple to an outer sleeve of the combustor; and
a boss configured to couple to a combustion liner of the combustor, the boss comprising a flange portion extending to an annular edge, an annular wall portion extending from the flange portion, and an interior surface, the boss defining a serpentine cooling passage extending from an inlet on the flange portion to an outlet on the interior surface, the serpentine cooling passage including an inlet portion and an outlet portion, wherein the inlet portion diverges away from the outlet portion as the inlet portion extends from the inlet towards the annular edge, and wherein the outlet portion converges towards the inlet portion as the outlet portion extends away from the annular edge towards the outlet.
2 . The fuel injection assembly as in claim 1 , further comprising an insert coupled to the boss such that a cooling gap is defined between the boss and the insert.
3 . The fuel injection assembly as in claim 2 , wherein the inlet of the serpentine cooling passage is fluidly coupled to a low pressure air source, and wherein the outlet of the serpentine cooling passage is fluidly coupled to the cooling gap.
4 . The fuel injection assembly as in claim 1 , wherein the serpentine cooling passage includes the inlet portion, the outlet portion, and a C-shaped portion fluidly connecting the inlet portion and the outlet portion, wherein the C-shaped portion is spaced apart from the annular edge, wherein the inlet portion extends from the inlet towards the annular edge, and the outlet portion extends away from the annular edge to the outlet.
5 . The fuel injection assembly as in claim 1 , wherein the flange portion of the boss includes a radially outer surface, and wherein the inlet of the serpentine cooling passage is defined on the radially outer surface proximate the annular wall portion.
6 . The fuel injection assembly as in claim 1 , wherein the serpentine cooling passage is a first serpentine cooling passage in a plurality of serpentine cooling passages defined in the boss, the plurality of serpentine cooling passages being spaced apart from one another.
7 . The fuel injection assembly as in claim 1 , wherein the annular wall portion includes a first end segment, a second end segment, and side segments extending between the first end segment and the second end segment, and wherein the boss comprises a first blocking flange extending from the first end segment and a second blocking flange extending from the second end segment.
8 . The fuel injection assembly as in claim 1 , wherein the inlet and the outlet have different non-circular shapes.
9 . A combustor comprising:
at least one fuel nozzle;
a combustion liner extending downstream from the at least one fuel nozzle;
an outer sleeve spaced apart from and surrounding the combustion liner such that an annulus is defined therebetween; and
a fuel injection assembly disposed downstream from the at least one fuel nozzle, the fuel injection assembly comprising:
a fuel injector coupled to the outer sleeve of the combustor; and
a boss coupled to the combustion liner of the combustor, the boss comprising a flange portion extending to an annular edge, an annular wall portion extending from the flange portion, and an interior surface, the boss defining a serpentine cooling passage extending from an inlet on the flange portion to an outlet on the interior surface, the serpentine cooling passage including an inlet portion and an outlet portion, wherein the inlet portion diverges away from the outlet portion as the inlet portion extends from the inlet towards the annular edge, and wherein the outlet portion converges towards the inlet portion as the outlet portion extends away from the annular edge towards the outlet.
10 . The combustor as in claim 9 , further comprising an insert coupled to the boss such that a cooling gap is defined between the boss and the insert.
11 . The combustor as in claim 10 , wherein the inlet of the serpentine cooling passage is fluidly coupled to a low pressure air source, and wherein the outlet of the serpentine cooling passage is fluidly coupled to the cooling gap.
12 . The combustor as in claim 9 , wherein the serpentine cooling passage includes the inlet portion, the outlet portion, and a C-shaped portion fluidly connecting the inlet portion and the outlet portion; and wherein the inlet portion extends from the inlet towards the annular edge, and the outlet portion extends away from the annular edge to the outlet.
13 . The combustor as in claim 12 , wherein the serpentine cooling passage is a first serpentine cooling passage in a plurality of serpentine cooling passages defined in the boss, the plurality of serpentine cooling passages being spaced apart from one another; wherein the plurality of serpentine cooling passages includes a second serpentine cooling passage having a second inlet portion and a second outlet portion; and wherein the second inlet portion is generally parallel to the second outlet portion.
14 . The combustor as in claim 9 , wherein the annular wall portion includes a first end segment, a second end segment, and side segments extending between the first end segment and the second end segment, and wherein the boss comprises a first blocking flange extending from the first end segment and a second blocking flange extending from the second end segment.
15 . A fuel injection assembly for a combustor of a gas turbine, the fuel injection assembly comprising:
a fuel injector configured to couple to an outer sleeve of the combustor; and
a boss spaced apart from the fuel injector and configured to couple to a combustion liner of the combustor, the boss comprising a flange portion, an annular wall portion extending from the flange portion, and an interior surface, the boss defining a serpentine cooling passage extending from an inlet on the flange portion to an outlet on the interior surface, wherein the flange portion of the boss extends to an annular edge, wherein the serpentine cooling passage includes an inlet portion, an outlet portion, and a C-shaped portion fluidly connecting the inlet portion and the outlet portion, wherein the inlet portion extends from the inlet towards the annular edge, and the outlet portion extends away from the annular edge to the outlet, wherein the inlet portion diverges away from the outlet portion as the inlet portion extends from the inlet towards the annular edge, and wherein the outlet portion converges towards the inlet portion as the outlet portion extends away from the annular edge towards the outlet.