Combustor and gas turbine including the same
View Patent ↗A combustor and a gas turbine capable of uniformly supplying air into a burner are provided. The combustor may include a burner including a tubular nozzle casing, a head plate coupled to an end of the nozzle casing, and a plurality of nozzles to inject fuel and air, and a duct assembly coupled to the burner, a mixture of the fuel and the air being burned in the duct assembly to produce combustion gas. Each of the nozzles may include outer nozzles and an inner nozzle installed inside the outer nozzles, each of the outer nozzles may include a nozzle tube configured to provide a channel through which air and fuel flow and a nozzle shroud configured to surround the nozzle tube, and a flow distribution member may be installed between the head plate and the nozzle shroud to distribute a flow rate of air introduced into the outer nozzle.
1. A combustor comprising:
a burner including a nozzle casing, a head plate coupled to an end of the nozzle casing, and a plurality of nozzles to inject fuel and air; and
a duct assembly coupled to the burner, the fuel being burned in the duct assembly to produce combustion gas,
wherein each of the nozzles comprises outer nozzles and an inner nozzle installed inside the outer nozzles,
each of the outer nozzles comprises a nozzle tube configured to provide a channel through which air and fuel flow, and a nozzle shroud configured to surround the nozzle tube, and
a flow distribution member is installed between the head plate and the nozzle shroud to distribute a flow rate of air introduced into the outer nozzle,
wherein the flow distribution member is spaced apart from the nozzle shroud to define a first distribution channel between the flow distribution member and the nozzle shroud, and the flow distribution member is spaced apart from the head plate to define a second distribution channel between the flow distribution member and the head plate, and
wherein a flow guide member having a curved guide surface is installed at a corner in which the nozzle casing meets the head plate, and the second distribution channel is defined between the flow guide member and the flow distribution member.
2. The combustor according to claim 1 , wherein a volume of the second distribution channel is larger than a volume of the first distribution channel.
3. The combustor according to claim 1 , wherein a gap between the nozzle shroud and an extension line, extending toward a central axis of the outer nozzle from an upper end of the flow distribution member, is larger than a gap between the extension line and the nozzle casing.
4. The combustor according to claim 1 , wherein the flow distribution member comprises an induction plate and a distribution plate obliquely bent from an inner end of the induction plate.
5. The combustor according to claim 4 , wherein a first angle formed by the induction plate and a reference axis parallel to the head plate is greater than a second angle formed by the distribution plate and the reference axis.
6. The combustor according to claim 4 , wherein the flow distribution member further comprises a guide plate extending from the induction plate in a direction of introduced air.
7. The combustor according to claim 6 , wherein the guide plate is inclined toward a center of the burner with respect to a direction parallel to a central axis of the outer nozzle.
8. The combustor according to claim 6 , wherein a gap between an upper end of the guide plate and the nozzle casing is larger than a gap between the upper end of the guide plate and the nozzle shroud.
9. The combustor according to claim 1 , wherein the flow distribution member comprises a plurality of guide ribs protruding therefrom, each of the guide ribs extending in a direction of flow of air.
10. A combustor comprising:
a burner including a nozzle casing, a head plate coupled to an end of the nozzle casing, and a plurality of nozzles to inject fuel and air; and
a duct assembly coupled to the burner, the fuel being burned in the duct assembly to produce combustion gas,
wherein each of the nozzles comprises outer nozzles and an inner nozzle installed inside the outer nozzles,
each of the outer nozzles comprises a nozzle tube configured to provide a channel through which air and fuel flow, and a nozzle shroud configured to surround the nozzle tube, and
a flow distribution member is installed between the head plate and the nozzle shroud to distribute a flow rate of air introduced into the outer nozzle,
wherein the flow distribution member comprises a first flow distribution member and a second flow distribution member spaced apart from the first flow distribution member with a gap therebetween, and
the first flow distribution member is disposed between the nozzle shroud and the second flow distribution member, and the second flow distribution member is disposed between the nozzle casing and the first flow distribution member.
11. The combustor according to claim 10 , wherein
the first flow distribution member comprises a first induction plate inclined with respect to a direction of introduced air, a first distribution plate bent from an inner end of the first induction plate, and a first guide plate extending from an outer end of the first induction plate in the direction of introduced air, and
the second flow distribution member comprises a second induction plate inclined with respect to the direction of introduced air, a second distribution plate bent from an inner end of the second induction plate, and a second guide plate extending from an outer end of the second induction plate in the direction of introduced air.
12. The combustor according to claim 11 , wherein a gap between an upper end of the first guide plate and the nozzle shroud is smaller than a gap between the upper end of the first guide plate and an upper end of the second guide plate.
13. The combustor according to claim 11 , wherein a gap between the first guide plate and the second guide plate gradually decreases toward the head plate.
14. A gas turbine comprising:
a compressor configured to compress air introduced from an outside;
a combustor configured to mix fuel with the air compressed by the compressor and combust a mixture of the fuel and the compressed air; and
a turbine including a plurality of turbine blades configured to be rotated by combustion gas produced by the combustor,
wherein the combustor comprises:
a burner including a plurality of nozzles to inject fuel and air; and
a duct assembly coupled to the burner, the mixture of the fuel and the compressed air being burned in the duct assembly to produce the combustion gas,
wherein each of the nozzles comprises outer nozzles and an inner nozzle installed inside the outer nozzles,
each of the outer nozzles comprises a nozzle tube configured to provide a channel through which air and fuel flow, and a nozzle shroud configured to surround the nozzle tube, and
a flow distribution member is installed between the head plate and the nozzle shroud to distribute a flow rate of air introduced into the outer nozzle,
wherein the flow distribution member is spaced apart from the nozzle shroud to define a first distribution channel between the flow distribution member and the nozzle shroud, and the flow distribution member is spaced apart from the head plate to define a second distribution channel between the flow distribution member and the head plate, and
wherein a flow guide member having a curved guide surface is installed at a corner in which the nozzle casing meets the head plate, and the second distribution channel is defined between the flow guide member and the flow distribution member.
15. The gas turbine according to claim 14 , wherein a volume of the second distribution channel is larger than a volume of the first distribution channel.