Combustor and gas turbine
A combustor includes: a nozzle main body having a shaft body and a swirl vane; a first fuel flow path configured to supply fuel to a first fuel injection hole defined in the nozzle main body; a second fuel flow path configured to supply fuel to a second fuel injection hole defined in the nozzle main body on a radial outer side of the first fuel injection hole; a first regulating valve provided in the first fuel flow path and configured to regulate a flow rate of the fuel in the first fuel flow path; a temperature sensor-configured to detect a temperature on a downstream side of the swirl vane; and a control device configured to control the first regulating valve so that the flow rate of the fuel in the first fuel flow path is lowered when the temperature detected by the temperature sensor satisfies a predetermined condition.
1. A combustor comprising:
a nozzle main body including a shaft body extending along an axis and a swirl vane configured to swirl a fluid flowing toward a downstream side in an axial direction around the axis;
a first fuel flow path configured to supply fuel to a first fuel injection hole, wherein the first fuel injection hole is defined in the nozzle main body;
a second fuel flow path configured to supply fuel to a second fuel injection hole defined in the nozzle main body, wherein the second fuel injection hole is radially outward of the first fuel injection hole;
a first regulating valve provided in the first fuel flow path and configured to regulate a flow rate of the fuel flowing through the first fuel flow path;
a second regulating valve provided in the second fuel flow path and configured to regulate a flow rate of the fuel flowing through the second fuel flow path;
a temperature sensor disposed at a distal end of the shaft body and located on the shaft body downstream of the swirl vane, wherein the temperature sensor is configured to detect a temperature; and
a control device connected to the temperature sensor and configured to control the first regulating valve and the second regulating valve so that the flow rate of the fuel flowing through the first fuel flow path is lowered and the flow rate of the fuel flowing through the second fuel flow path is maintained or increased when the temperature detected by the temperature sensor satisfies a predetermined condition.
2. The combustor according to claim 1 , wherein the control device is configured to control the first regulating valve so that the flow rate of the fuel flowing through the first fuel flow path is lowered when the temperature detected by the temperature sensor has risen from a steady-state value by more than a predetermined temperature.
3. A gas turbine comprising:
the combustor according to claim 1 ;
a compressor configured to compress air to supply compressed air to the combustor; and
a turbine configured to be driven by a combustion gas formed by combustion of fuel in the combustor.