Control apparatus for gas turbine and start up method for gas turbine
An electronic control apparatus is applied to a gas turbine including a cylindrical combustor, a plurality of fuel injection valves, and an ignition plug. Air compressed by a compressor is supplied to the combustor. The plurality of fuel injection valves are aligned in a circumferential direction in the combustor and are capable of injecting fuel into the combustor. The ignition plug is provided in the combustor and is capable of igniting a fuel-mixture within the combustor. The electronic control apparatus controls the operation of the plurality of fuel injection valves so that when the gas turbine is started up, fuel injection opening times of the # 6 and # 12 fuel injection valves which are positioned far from the ignition plug are later than fuel injection opening times of the # 1 and # 7 fuel injection valves which are positioned close to the ignition plug.
1. A control apparatus applied to a gas turbine, the gas turbine includes:
a combustor in which air compressed by a compressor is supplied, the combustor having a combustion chamber, a shape of the combustion chamber being cylindrical;
a plurality of fuel injection valves aligned in a circumferential direction in the combustor, the plurality of fuel injection valves being capable of injecting fuel into the combustor; and
an ignition device provided in the combustor, the ignition device being capable of igniting a fuel-air mixture within the combustor,
the control apparatus comprising:
a control device which controls the operation of the plurality of fuel injection valves so that when the gas turbine is started up, fuel injection opening times of the fuel injection valves positioned far from the ignition device are later than fuel injection opening times of the fuel injection valves positioned close to the ignition device; and
a temperature detection device which is disposed in the periphery of the fuel injection valve closest to the ignition device among the plurality of the fuel injection valves and detects a temperature within the combustor, wherein
the control device controls the fuel injection valve closest to the ignition device to inject the fuel, and then when a temperature detected by the temperature detection device becomes equal to or greater than a prescribed determination temperature in a state in which fuel is being injected from the fuel injection valve closest to the ignition device, the control device controls the fuel injection valves other than the fuel injection valve closest to the ignition device to inject the fuel.
2. The control apparatus according to claim 1 , wherein the control device controls the operation of the plurality of fuel injection valves so that the fuel injection valves between the fuel injection valve closest to the ignition device and the fuel injection valve farthest from the ignition device are sequentially opened at prescribed intervals from the fuel injection valve closest to the ignition device toward the fuel injection valve farthest from the fuel injection device.
3. A control apparatus applied to a gas turbine, the gas turbine includes:
a combustor in which air compressed by a compressor is supplied, the combustor having a combustion chamber, a shape of the combustion chamber being cylindrical;
a plurality of fuel injection valves aligned in a circumferential direction in the combustor, the plurality of fuel injection valves being capable of injecting fuel into the combustor; and
an ignition device provided in the combustor, the ignition device being capable of igniting a fuel-air mixture within the combustor,
the control apparatus comprising:
a control device which controls the operation of the plurality of fuel injection valves so that when the gas turbine is started up, fuel injection opening times of the fuel injection valves positioned far from the ignition device are later than fuel injection opening times of the fuel injection valves positioned close to the ignition device, wherein
delay times are set for each fuel injection valve, the delay times depending on a distance from the ignition device, and
when an elapsed time from when fuel from the fuel injection valve closest to the ignition device is injected becomes equal to or greater than a delay time of one of the fuel injection valves, the control device injects fuel from the fuel injection valve for which that delay time is set.
4. The control apparatus according to claim 3 , wherein the delay times are times at which a flame generated by fuel injected from the fuel injection valve closest to the ignition device is predicted to reach each fuel injection valve.
5. The control apparatus according to claim 3 , wherein the control device controls the operation of the plurality of fuel injection valves so that the fuel injection valves between the fuel injection valve closest to the ignition device and the fuel injection valve farthest from the ignition device are sequentially opened at prescribed intervals from the fuel injection valve closest to the ignition device toward the fuel injection valve farthest from the fuel injection device.
6. A start up method applied to a gas turbine, the gas turbine includes:
a combustor in which air compressed by a compressor is supplied, the combustor having a combustion chamber, a shape of the combustion chamber being cylindrical;
a plurality of fuel injection valves aligned in a circumferential direction in the combustor, the plurality of fuel injection valves being capable of injecting fuel into the combustor; and
an ignition device provided in the combustor which is capable of igniting a fuel-air mixture within the combustor, the start up method comprising:
controlling the operation of the plurality of fuel injection valves so that when the gas turbine is started up, fuel injection opening times of the fuel injection valves positioned far from the ignition device are later than fuel injection opening times of the fuel injection valves positioned close to the ignition device, wherein
when a temperature within the combustor becomes equal to or greater than a prescribed determination temperature in a state in which fuel is being injected from the fuel injection valve closest to the ignition device, fuel is injected from the fuel injection valves other than the fuel injection valve closest to the ignition device.
7. The start up method according to claim 6 , wherein when the gas turbine is started up, the fuel injection valves between the fuel injection valve closest to the ignition device and the fuel injection valve farthest from the ignition device are sequentially opened at prescribed intervals from the fuel injection valve closest to the ignition device toward the fuel injection valve farthest from the fuel injection device.
8. A start up method applied to a gas turbine, the as turbine includes:
a combustor in which air compressed by a compressor is supplied, the combustor having a combustion chamber, a shape of the combustion chamber being cylindrical;
a plurality of fuel injection valves aligned in a circumferential direction in the combustor, the plurality of fuel injection valves being capable of injecting fuel into the combustor; and
an ignition device provided in the combustor which is capable of igniting a fuel-air mixture within the combustor, the start up method comprising:
controlling the operation of the plurality of fuel injection valves so that when the gas turbine is started up, fuel injection opening times of the fuel injection valves positioned far from the ignition device are later than fuel injection opening times of the fuel injection valves positioned close to the ignition device, wherein
delay times are set for each fuel injection valve, the delay times depending on a distance from the ignition device, and
when an elapsed time from when fuel from the fuel injection valve closest to the ignition device is injected becomes equal to or greater than a delay time of one of the fuel injection valves, fuel is injected from the fuel injection valve for which that delay time is set.
9. The start up method according to claim 8 , wherein the delay times are times at which a flame generated by fuel injected from the fuel injection valve closest to the ignition device is predicted to reach each fuel injection valve.
10. The start up method according to claim 8 , wherein when the gas turbine is started up, the fuel injection valves between the fuel injection valve closest to the ignition device and the fuel injection valve farthest from the ignition device are sequentially opened at prescribed intervals from the fuel injection valve closest to the ignition device toward the fuel injection valve farthest from the fuel injection device.