Gas turbine system
Provided is a gas turbine system, including: an ammonia tank; a combustor connected to the ammonia tank; an exhaust flow passage connected to the combustor; a turbine provided in the exhaust flow passage; a cracked-gas reservoir connected to the combustor; and an ammonia cracking catalyst, which is arranged on a downstream side of the turbine in the exhaust flow passage, and is connected to the ammonia tank and the cracked-gas reservoir.
1. A gas turbine system comprising:
an ammonia tank;
a combustor connected to the ammonia tank;
an exhaust flow passage connected to the combustor;
a turbine provided in the exhaust flow passage;
a cracked-gas reservoir connected to the combustor;
an ammonia cracking catalyst, which is arranged on a downstream side of the turbine in the exhaust flow passage, and is connected to the ammonia tank and the cracked-gas reservoir; and
a controller,
wherein the controller of the gas turbine system is configured to, during an operation of the gas turbine system, determine whether or not a temperature of the ammonia cracking catalyst has become equal to or higher than a reference temperature and, when the gas turbine system has determined that the temperature of the ammonia cracking catalyst has become equal to or higher than the reference temperature, control so that ammonia is supplied from the ammonia tank to the ammonia cracking catalyst, and
wherein the controller of the gas turbine system is configured to, during an operation of the gas turbine system, (i) control a supply amount of ammonia from the ammonia tank to the ammonia cracking catalyst so that pressure in the cracked-gas reservoir becomes equal to a reference pressure, (ii) not stop the gas turbine system and continue supply of ammonia from the ammonia tank to the ammonia cracking catalyst when the pressure in the cracked-gas reservoir is lower than the reference pressure, and (iii) stop the gas turbine system when the pressure in the cracked-gas reservoir has become equal to or higher than the reference pressure, and
wherein the controller of the gas turbine system is configured to, at the time of activation of the gas turbine system, control so that supply of ammonia from the ammonia tank to the combustor is started after supply of a cracked gas from the cracked-gas reservoir to the combustor is started.
2. The gas turbine system according to claim 1 , wherein a cooling device is provided in a flow passage that connects the ammonia cracking catalyst and the cracked-gas reservoir to each other.
3. The gas turbine system according to claim 2 ,
wherein the cooling device is a first heat exchanger provided in a flow passage that connects the ammonia cracking catalyst and the cracked-gas reservoir to each other, and
wherein a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other passes through the first heat exchanger.
4. The gas turbine system according to claim 3 ,
wherein a second heat exchanger is provided on a downstream side of the ammonia cracking catalyst in the exhaust flow passage, and
wherein a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other passes through the second heat exchanger.
5. The gas turbine system according to claim 4 ,
wherein a first flow rate control valve is provided in a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other, and
wherein the controller is configured to control the first flow rate control valve so that ammonia is supplied from the ammonia tank to the ammonia cracking catalyst during an operation of the gas turbine system.
6. The gas turbine system according to claim 5 ,
wherein a second flow rate control valve is provided in a flow passage that connects the cracked-gas reservoir and the combustor to each other,
wherein a third flow rate control valve is provided in a flow passage that connects the ammonia tank and the combustor to each other, and
wherein the controller controls the second flow rate control valve and the third flow rate control valve so that supply of the ammonia from the ammonia tank to the combustor is started after supply of the cracked gas from the cracked-gas reservoir to the combustor is started at the time of activation of the gas turbine system.
7. The gas turbine system according to claim 3 ,
wherein a first flow rate control valve is provided in a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other, and
wherein the controller is configured to control the first flow rate control valve so that ammonia is supplied from the ammonia tank to the ammonia cracking catalyst during an operation of the gas turbine system.
8. The gas turbine system according to claim 7 ,
wherein a second flow rate control valve is provided in a flow passage that connects the cracked-gas reservoir and the combustor to each other,
wherein a third flow rate control valve is provided in a flow passage that connects the ammonia tank and the combustor to each other, and
wherein the controller controls the second flow rate control valve and the third flow rate control valve so that supply of the ammonia from the ammonia tank to the combustor is started after supply of the cracked gas from the cracked-gas reservoir to the combustor is started at the time of activation of the gas turbine system.
9. The gas turbine system according to claim 2 ,
wherein a second heat exchanger is provided on a downstream side of the ammonia cracking catalyst in the exhaust flow passage, and
wherein a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other passes through the second heat exchanger.
10. The gas turbine system according to claim 9 ,
wherein a first flow rate control valve is provided in a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other, and
wherein the controller is configured to control the first flow rate control valve so that ammonia is supplied from the ammonia tank to the ammonia cracking catalyst during an operation of the gas turbine system.
11. The gas turbine system according to claim 10 ,
wherein a second flow rate control valve is provided in a flow passage that connects the cracked-gas reservoir and the combustor to each other,
wherein a third flow rate control valve is provided in a flow passage that connects the ammonia tank and the combustor to each other, and
wherein the controller controls the second flow rate control valve and the third flow rate control valve so that supply of the ammonia from the ammonia tank to the combustor is started after supply of the cracked gas from the cracked-gas reservoir to the combustor is started at the time of activation of the gas turbine system.
12. The gas turbine system according to claim 2 ,
wherein a first flow rate control valve is provided in a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other, and
wherein the controller is configured to control the first flow rate control valve so that ammonia is supplied from the ammonia tank to the ammonia cracking catalyst during an operation of the gas turbine system.
13. The gas turbine system according to claim 12 ,
wherein a second flow rate control valve is provided in a flow passage that connects the cracked-gas reservoir and the combustor to each other,
wherein a third flow rate control valve is provided in a flow passage that connects the ammonia tank and the combustor to each other, and
wherein the controller controls the second flow rate control valve and the third flow rate control valve so that supply of the ammonia from the ammonia tank to the combustor is started after supply of the cracked gas from the cracked-gas reservoir to the combustor is started at the time of activation of the gas turbine system.
14. The gas turbine system according to claim 1 ,
wherein a second heat exchanger is provided on a downstream side of the ammonia cracking catalyst in the exhaust flow passage, and
wherein a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other passes through the second heat exchanger.
15. The gas turbine system according to claim 14 ,
wherein a first flow rate control valve is provided in a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other, and
wherein the controller is configured to control the first flow rate control valve so that ammonia is supplied from the ammonia tank to the ammonia cracking catalyst during an operation of the gas turbine system.
16. The gas turbine system according to claim 15 ,
wherein a second flow rate control valve is provided in a flow passage that connects the cracked-gas reservoir and the combustor to each other,
wherein a third flow rate control valve is provided in a flow passage that connects the ammonia tank and the combustor to each other, and
wherein the controller controls the second flow rate control valve and the third flow rate control valve so that supply of the ammonia from the ammonia tank to the combustor is started after supply of the cracked gas from the cracked-gas reservoir to the combustor is started at the time of activation of the gas turbine system.
17. The gas turbine system according to claim 1 ,
wherein a first flow rate control valve is provided in a flow passage that connects the ammonia tank and the ammonia cracking catalyst to each other, and
wherein the controller is configured to control the first flow rate control valve so that ammonia is supplied from the ammonia tank to the ammonia cracking catalyst during an operation of the gas turbine system.
18. The gas turbine system according to claim 17 ,
wherein a second flow rate control valve is provided in a flow passage that connects the cracked-gas reservoir and the combustor to each other,
wherein a third flow rate control valve is provided in a flow passage that connects the ammonia tank and the combustor to each other, and
wherein the controller controls the second flow rate control valve and the third flow rate control valve so that supply of the ammonia from the ammonia tank to the combustor is started after supply of the cracked gas from the cracked-gas reservoir to the combustor is started at the time of activation of the gas turbine system.
19. The gas turbine system according to claim 18 , wherein the controller includes a central processing unit, a read-only memory, and a random-access memory.
20. The gas turbine system according to claim 1 , wherein the controller includes a central processing unit, a read-only memory, and a random-access memory.