Combustor for a gas turbine engine including a collar surrounding a secondary fuel injector to define upstream and downstream purge paths
A combustor includes a premixer fuel injector that injects fuel into the combustor and ignites mixture of the fuel and compressed air to produce exhaust gas, a transition duct through which the exhaust gas passes, a secondary fuel injector disposed in an opening of the transition duct for providing further fuel to the exhaust gas, and a collar fixedly coupled to the transition duct and positioned to surround the secondary fuel injector. The collar cooperates with the secondary fuel injector to define an upstream purge path disposed on an upstream side of the opening and a downstream purge path disposed on a downstream side of the opening by a flow direction of the exhaust gas that each provides a flow communication between an exterior of the transition duct and an interior of the transition duct. The upstream purge path has a larger flow area than the downstream purge path.
1 . A combustor comprising:
a premixer fuel injector that injects a fuel into the combustor and ignites a mixture of the fuel and a compressed air to produce an exhaust gas;
a transition duct defining an interior through which the exhaust gas passes, the transition duct defining an opening therethrough, the opening having an upstream side and a downstream side defined by a flow direction of the exhaust gas;
a secondary fuel injector disposed in the opening that injects further fuel to the exhaust gas; and
a collar fixedly coupled to the transition duct and positioned to surround the secondary fuel injector, the collar having a first end positioned to an exterior of the transition duct, a second end fixed on the transition duct around the opening, and a wall therebetween, the collar cooperating with the secondary fuel injector to define an upstream purge path at least partially disposed on the upstream side and a downstream purge path at least partially disposed on the downstream side that each provides a flow communication between the exterior of the transition duct and the interior of the transition duct, the upstream purge path having a larger flow area than the downstream purge path,
wherein the second end of the collar has a non-planar shape that mates with a shape of the transition duct,
wherein the collar comprises a flap that extends from an inner surface of the collar and circumferentially around the inner surface, and wherein the flap divides an interior of the collar to a first cavity between the flap and the first end and a second cavity between the flap and the second end, and
wherein the collar comprises two ribs that extend from the inner surface of the collar and extend from a surface of the flap facing the second end of the collar, and wherein the upstream purge path and the downstream purge path are defined in the second cavity and are separated by the two ribs.
2 . The combustor of claim 1 , wherein the collar comprises a plurality of upstream apertures facing the upstream side of the opening and a plurality of downstream apertures facing the downstream side of the opening, and wherein the plurality of upstream apertures define the upstream purge path and the plurality of downstream apertures define the downstream purge path.
3 . The combustor of claim 2 , wherein a size of each upstream aperture of the plurality of upstream apertures is larger than a size of each downstream aperture of the plurality of downstream apertures.
4 . The combustor of claim 2 , wherein a total number of the plurality of the upstream apertures is more than a total number of the plurality of the downstream apertures.
5 . The combustor of claim 2 , wherein the plurality of upstream apertures and the plurality of downstream apertures extend through the wall and are oblique to the flow direction of the exhaust gas.
6 . The combustor of claim 1 , wherein the upstream purge path has a larger circumferential length around a perimeter of the collar than the downstream purge path.
7 . The combustor of claim 1 , wherein a surface of the flap facing the second end of the collar has a non-planar shape corresponding to the non-planar shape of the second end to form a constant circumferential cross-sectional area of the second cavity.
8 . The combustor of claim 1 , wherein the two ribs are disposed less than 180 degrees apart from each other at the downstream side.
9 . A combustor comprising:
a transition duct defining an interior through which a flow of combustion gas passes in a flow direction, the transition duct defining an opening therethrough, the opening having an upstream side and a downstream side defined by the flow direction;
a primary fuel injector;
a secondary fuel injector at least partially disposed within the opening to inject fuel into the flow of combustion gas; and
a collar having a first end and a second end, wherein the second end is fixedly coupled to the transition duct and positioned to surround the opening, the collar cooperating with the secondary fuel injector to define an upstream purge path at least partially disposed on the upstream side of the opening and a downstream purge path at least partially disposed on the downstream side of the opening that each provides a flow communication between an exterior of the transition duct and the interior of the transition duct, the upstream purge path having a larger flow area than the downstream purge path, wherein the second end of the collar has a smooth non-planar shape that mates with a shape of the transition duct,
wherein the collar comprises a flap that extends from an inner surface of the collar and circumferentially around the inner surface, and wherein the flap divides an interior of the collar to a first cavity between the flap and the first end and a second cavity between the flap and the second end, and
wherein the collar comprises two ribs that extend from the inner surface of the collar and extend from a surface of the flap facing the second end of the collar, and wherein the upstream purge path and the downstream purge path are defined in the second cavity and are separated by the two ribs.
10 . The combustor of claim 9 , wherein the collar comprises a plurality of upstream apertures facing the upstream side of the opening and a plurality of downstream apertures facing the downstream side of the opening, and wherein the plurality of upstream apertures define the upstream purge path and the plurality of downstream apertures define the downstream purge path.
11 . The combustor of claim 10 , wherein a size of each upstream aperture of the plurality of upstream apertures is larger than a size of each downstream aperture of the plurality of downstream apertures.
12 . The combustor of claim 10 , wherein a total number of the plurality of upstream apertures is more than a total number of the plurality of downstream apertures.
13 . The combustor of claim 10 , wherein the plurality of upstream apertures and the plurality of downstream apertures extend through the collar and are oblique to the flow direction of the combustion gas.
14 . The combustor of claim 9 , wherein the upstream purge path has a larger circumferential length around a perimeter of the collar than the downstream purge path.
15 . The combustor of claim 9 , wherein the first end is positioned to the exterior of the transition duct and the second end is fixed on the transition duct.
16 . The combustor of claim 9 , wherein a surface of the flap facing the second end of the collar has a non-planar shape corresponding to the non-planar shape of the second end to form a constant circumferential cross-sectional area of the second cavity.
17 . The combustor of claim 9 , wherein the two ribs are disposed less than 180 degrees apart from each other at the downstream side.
18 . A combustor comprising:
a transition duct defining an interior through which a flow of combustion gas passes in a flow direction, the transition duct defining an opening therethrough, the opening having an upstream side and a downstream side defined by the flow direction;
a primary fuel injector;
a secondary fuel injector at least partially disposed within the opening to inject fuel into the flow of combustion gas; and
a collar having a first end and a second end, wherein the second end is fixedly coupled to the transition duct and positioned to surround the opening, the collar cooperating with the secondary fuel injector to define an upstream purge path at least partially disposed on the upstream side of the opening and a downstream purge path at least partially disposed on the downstream side of the opening that each provides a flow communication between an exterior of the transition duct and the interior of the transition duct, the upstream purge path having a larger flow area than the downstream purge path,
wherein the collar comprises a plurality of upstream apertures facing the upstream side of the opening and a plurality of downstream apertures facing the downstream side of the opening, and
wherein the plurality of upstream apertures define the upstream purge path and the plurality of downstream apertures define the downstream purge path,
wherein a size of each upstream aperture of the plurality of upstream apertures is larger than a size of each downstream aperture of the plurality of downstream apertures,
wherein a total number of the plurality of upstream apertures is more than a total number of the plurality of downstream apertures,
wherein the upstream purge path has a larger circumferential length around a perimeter of the collar than the downstream purge path, and
wherein the upstream purge path and the downstream purge path are separated by two ribs disposed in an inner surface of the collar,
wherein the second end of the collar has a non-planar shape that mates with a shape of the transition duct,
wherein the collar comprises a flap that extends from an inner surface of the collar and circumferentially around the inner surface, and wherein the flap divides an interior of the collar to a first cavity between the flap and the first end and a second cavity between the flap and the second end, and
wherein the two ribs extend from the inner surface of the collar and extend from a surface of the flap facing the second end of the collar, and wherein the upstream purge path and the downstream purge path are defined in the second cavity and are separated by the two ribs.
19 . The combustor of claim 1 , wherein the second end of the collar has a hyperbolic paraboloid shape.