Provided is a combustor that is made compact and achieves NOx reduction. In the combustor ( 1 ) including a pilot nozzle ( 21 ) disposed along the central axis of the combustor ( 1 ) and performing diffusion combustion, a plurality of main nozzles ( 22 ) disposed on the outer peripheral side of the pilot nozzle ( 21 ) at intervals in the circumferential direction and performing premixing combustion, a single inner cylinder ( 2 a ) surrounding the pilot nozzle ( 21 ) and the main nozzles ( 22 ), and an outer cylinder approximately coaxially surrounding the outer side of the inner cylinder ( 2 a ) to form a compressed air passage ( 6 ) between the inner peripheral surface thereof and the outer peripheral surface of the inner cylinder and turning the flow direction of compressed air flowing in the compressed air passage ( 6 ) in approximately the opposite direction at the end of the inner cylinder ( 2 a ) to introduce the compressed air into the pilot nozzle ( 21 ), the compressed air passage ( 6 ) is provided with a flow rate controller that makes the flow rate on the combustor ( 1 ) inner peripheral side of the passage larger than that on the outer peripheral side. An example as the flow rate controller is a baffle plate 51 provided with holes 55, 56.
1. A combustor comprising: a pilot nozzle disposed along a central axis of the combustor and performing diffusion combustion; a plurality of main nozzles disposed on an outer peripheral side of the pilot nozzle at intervals in a circumferential direction and performing premixed combustion; a single inner cylinder surrounding the pilot nozzle and the main nozzles; and an outer cylinder approximately coaxially surrounding an outer side of the inner cylinder to form a compressed air passage between an inner peripheral surface thereof and an outer peripheral surface of the inner cylinder and turning a flow direction of compressed air flowing in the compressed air passage in approximately an opposite direction at an end of the inner cylinder to introduce the compressed air into the pilot nozzle,
wherein the compressed air passage is provided with a flow rate controller that makes a flow rate on an inner peripheral side to a position at which the compressed air passage is turned in approximately the opposite direction larger than that on an outer peripheral side,
wherein the flow rate controller is disposed on an upstream side, in a flow direction of the compressed air, of a center of the position at which the compressed air passage is turned in approximately the opposite direction,
wherein fuel is mixed on a downstream side of the flow rate controller in the flow direction of the compressed air,
wherein the compressed air passage is provided with a baffle plate functioning as the flow rate controller by blocking the passage, and
wherein the baffle plate is a ring-shaped flat plate, and the baffle plate is provided with a plurality of holes communicating between an upstream side and a downstream side, in the flow direction of the compressed air, of the baffle plate in the passage, wherein a diameter of the holes provided on the outer peripheral side is smaller than the diameter of the holes provided on the inner peripheral side.
2. The combustor according to claim 1 , wherein the baffle plate is disposed at a position, on the upstream side of the center of the position at which the passage is turned in approximately the opposite direction, with a distance from the center not longer than 15 times the diameter of the holes provided on the inner peripheral side.
3. The combustor according to claim 1 , wherein
the end of the inner cylinder is provided with an expanding portion gradually expanding outward in the radial direction toward the downstream end of the passage; and
the holes on the inner peripheral side are disposed farther toward an inner side in the radial direction than an edge of the expanding portion on an outer side in the radial direction.
4. The combustor according to claim 3 , wherein
the diameter of the holes on the inner peripheral side is formed so as not to be smaller than an expansion height of the expanding portion.
5. The combustor according to claim 1 , wherein
the distance between the centers of adjacent holes on the inner peripheral side is not smaller than 1.5 times the diameter of the holes on the inner peripheral side.
6. A combustor comprising: a pilot nozzle disposed along a central axis of the combustor and performing diffusion combustion; a plurality of main nozzles disposed on an outer peripheral side of the pilot nozzle at intervals in a circumferential direction and performing premixed combustion; a single inner cylinder surrounding the pilot nozzle and the main nozzles; and an outer cylinder approximately coaxially surrounding an outer side of the inner cylinder to form a compressed air passage between an inner peripheral surface thereof and an outer peripheral surface of the inner cylinder and turning a flow direction of compressed air flowing in the compressed air passage in approximately an opposite direction at an end of the inner cylinder to introduce the compressed air into the pilot nozzle,
wherein the compressed air passage is provided with a flow rate controller that makes a flow rate on an inner peripheral side to a position at which the compressed air passage is turned in approximately the opposite direction larger than that on an outer peripheral side,
wherein the flow rate controller is disposed on an upstream side, in a flow direction of the compressed air, of a center of a position at which the compressed air passage is turned in approximately the opposite direction,
wherein fuel is mixed on a downstream side of the flow rate controller in the flow direction of the compressed air,
wherein the compressed air passage is provided with a baffle plate functioning as the flow rate controller by blocking the passage; and
wherein the baffle plate is a ring-shaped flat plate, and the baffle plate is provided, on the inner peripheral side, with a slit communicating between the upstream side and the downstream side of the baffle plate in the flow direction of the compressed air, the slit is formed along the inner peripheral edge of the baffle plate as a gap with respect to the inner cylinder.
7. The combustor according to claim 1 , wherein
the compressed air passage is provided with a top hat nozzle at a position where the passage is turned in approximately the opposite direction.
8. The combustor according to claim 1 , wherein
the compressed air passage is provided with a turning vane facing an edge of the inner cylinder to guide fluid in the passage that turns in the opposite direction; and
the turning vane is provided, on a back side thereof, with a stirrer for stirring the flow of the fluid.
9. The combustor according to claim 8 , wherein
the turning vane is provided with a slit communicating between the back side and a front side of the turning vane at an end on a downstream side thereof.
10. The combustor according to claim 1 , wherein the baffle plate is disposed at the position, on the upstream side of the center of the position at which the passage is turned in approximately the opposite direction, with a distance from the center being at least 5 times the diameter of the holes provided on the inner peripheral side and not longer than 15 times the diameter of the holes provided on the inner peripheral side.
11. The combustor according to claim 1 , wherein said ring-shaped flat baffle plate has an annular planar surface on a downstream side of said baffle plate and said plurality of holes each have substantially uniform shapes across a width of said baffle plate with central axes of said plurality of holes extending substantially parallel to said flow direction of the compressed air and substantially perpendicular to said annular planar surface.
12. The combustor according to claim 6 , wherein said ring-shaped flat baffle plate has an annular planar surface on a downstream side of said baffle plate and said plurality of holes each have substantially uniform shapes across a width of said baffle plate with central axes of said plurality of holes extending substantially parallel to said flow direction of the compressed air and substantially perpendicular to said annular planar surface.