Control of gas turbine for catalyst activation
View Patent ↗A catalytic gas turbine includes a compressor, a catalytic combustor, a turbine, and a flow path conducting a bypass portion of the compressed air around the combustor and turbine. A method of operating the catalytic gas turbine to activate a catalyst in the catalytic combustor includes opening an inlet guide vane upstream of the compressor to a position to produce an increased volume of compressed air. The increased volume exceeds a volume of compressed air needed to support combustion. A bypass portion of the compressed air is extracted and directed around the combustor and turbine. The method may also include extracting a recirculation portion of the compressed air and directing the recirculation portion into the inlet of the compressor.
1. A catalytic gas turbine comprising:
a compressor receiving an inlet air and producing compressed air,
a catalytic combustor receiving a combustion portion of the compressed air and producing a hot combustion gas;
a turbine receiving the combustion gas;
a flow path conducting a bypass portion of the compressed air around the combustor and turbine; and
further comprising a recirculation flow path receiving a recirculation portion of the compressed air and conducting the recirculation portion into the inlet air.
2. The catalytic gas turbine of claim 1 , further comprising a bypass metering valve, responsive to a bypass valve control signal, positioned in the flow path for controlling a flow of the bypass portion.
3. The catalytic gas turbine of claim 2 , further comprising a controller for generating the bypass valve control signal responsive to at least one of the group consisting of an air-to-fuel ratio in the catalytic combustor, a temperature of a catalyst in the combustor, a temperature of the combustion gas, and the speed of rotation of the turbine.
4. The catalytic gas turbine of claim 1 , wherein the compressor comprises stages numbering 1 through N consecutively from a lowest pressure stage to a highest pressure stage, the bypass portion extracted from a stage having a stage number greater than N/2.
5. A catalytic gas turbine comprising:
a compressor receiving inlet air and producing compressed air;
a catalytic combustor receiving a combustion portion of the compressed air and producing a combustion gas;
a turbine receiving the combustion gas and producing an exhaust gas; and
a flow path receiving a recirculation portion of the compressed air and conducting the recirculation portion into the inlet air.
6. The catalytic gas turbine of claim 5 , further comprising a recirculation metering valve, responsive to a recirculation valve control signal, positioned in the flow path for controlling a flow of the recirculation portion.
7. The catalytic gas turbine of claim 6 , further comprising a controller for generating the recirculation valve control signal responsive to at least one of the group consisting of a temperature of the combustion gas, a temperature of the exhaust gas, a temperature of the inlet air, and a temperature of an ambient air.
8. The catalytic gas turbine of claim 6 , wherein the compressor comprises stages numbering 1 through N consecutively from a lowest pressure stage to a highest pressure stage, the recirculation inlet disposed downstream of a stage having a stage number greater than N/2.