Combustor with fuel injector pegs for reducing combustion pressure oscillations
View Patent ↗A combustor includes a combustor external cylinder, a tubular combustor basket installed in the combustor external cylinder, a compressed air channel defined between the combustor external cylinder and the combustor basket, and a plurality of fuel nozzles installed in the combustor basket. Compressed air flowing along the compressed air channel is approximately reversed in the flow direction at an end of the combustor basket, and is introduced into the plurality of fuel nozzles. Fuel injection pegs made up of an upstream side fuel injection peg injecting upstream side fuel and a downstream side fuel injection peg injecting downstream side fuel, are installed in the compressed air channel. Concentration fluctuation of the upstream side fuel caused by pressure fluctuation in the combustor is configured so as to reduce a peak of concentration fluctuation of the downstream side fuel at a combustion start position of the combustor.
1. A combustor comprising:
a combustor external cylinder;
a tubular combustor basket installed in the combustor external cylinder;
a compressed air channel defined between an inner circumferential surface of the combustor external cylinder and an outer circumferential surface of the combustor basket;
a plurality of fuel nozzles installed in the combustor basket, extending approximately in parallel with a central axis of the combustor basket, and injecting fuel for premixing combustion from at least one thereof; and
an airflow introduction part configured to introduce compressed air flowing in a direction along the compressed air channel into the plurality of fuel nozzles so that the compressed air is approximately reversed in the flow direction at an end of the combustor basket, wherein
fuel injection pegs, each of which is made up of an upstream side fuel injection peg injecting upstream side fuel and a downstream side fuel injection peg provided in the downstream side of the upstream side fuel injection peg and injecting downstream side fuel, are installed in the compressed air channel, and
concentration fluctuation of the upstream side fuel caused by pressure fluctuation in the combustor is configured so as to reduce a peak of concentration fluctuation of the downstream side fuel at a combustion start position of the combustor,
wherein, with respect to a direction from the upstream side fuel injection peg to the downstream side fuel injection peg, the downstream side fuel injection peg forms an acute angle with respect to the combustor external cylinder and an obtuse angle with respect to the tubular combustor basket.
2. The combustor according to claim 1 , wherein a distance between the upstream side fuel injection peg and the downstream side fuel injection peg is set so that a phase of the concentration fluctuation of the upstream side fuel is opposite to a phase of the concentration fluctuation of the downstream side fuel at a position where the upstream side fuel reaches the downstream side fuel injection peg.
3. The combustor according to claim 1 , wherein a concentration of fuel gas mixed by the fuel injection pegs is set so as to be lower than an inflammability limiting concentration.
4. The combustor according to claim 1 , wherein the plurality of fuel nozzles include a pilot nozzle installed on a central axis of the combustor basket, and premixing nozzles extending approximately in parallel with the pilot nozzle and installed in the combustor basket at intervals at which central angles thereof are equal to one another.
5. The combustor according to claim 1 , wherein the at least one of the plurality of fuel nozzles is provided with both a fuel injection hole for premixing combustion and a fuel injection hole for diffusion combustion.
6. The combustor according to claim 2 , wherein a concentration of fuel gas mixed by the fuel injection pegs is set so as to be lower than an inflammability limiting concentration.
7. The combustor according to claim 2 , wherein the plurality of fuel nozzles include a pilot nozzle installed on a central axis of the combustor basket, and premixing nozzles extending approximately in parallel with the pilot nozzle and installed in the combustor basket at intervals at which central angles thereof are equal to one another.
8. The combustor according to claim 3 , wherein the plurality of fuel nozzles include a pilot nozzle installed on a central axis of the combustor basket, and premixing nozzles extending approximately in parallel with the pilot nozzle and installed in the combustor basket at intervals at which central angles thereof are equal to one another.
9. The combustor according to claim 6 , wherein the plurality of fuel nozzles include a pilot nozzle installed on a central axis of the combustor basket, and premixing nozzles extending approximately in parallel with the pilot nozzle and installed in the combustor basket at intervals at which central angles thereof are equal to one another.
10. The combustor according to claim 2 , wherein the at least one of the plurality of fuel nozzles is provided with both a fuel injection hole for premixing combustion and a fuel injection hole for diffusion combustion.
11. The combustor according to claim 3 , wherein the at least one of the plurality of fuel nozzles is provided with both a fuel injection hole for premixing combustion and a fuel injection hole for diffusion combustion.
12. The combustor according to claim 6 , wherein the at least one of the plurality of fuel nozzles is provided with both a fuel injection hole for premixing combustion and a fuel injection hole for diffusion combustion.