Method for operating a gas turbine below the nominal power thereof
View Patent ↗A method for operating a gas turbine below the nominal power includes: determining a lower power threshold value of the gas turbine which causes the gas turbine to leave a CO-emission-compliant partial load range of the gas turbine; providing a specified threshold value for output gas turbine power, wherein the specified threshold value is less than the nominal power of the gas turbine; and operating the gas turbine at an output gas turbine power above the specified threshold value at a constant exhaust gas temperature, wherein the inlet guide blades of a compressor of the gas turbine are closed further in order to reduce the output gas turbine power. A sufficiently large valve is selected for the specified threshold value so that increases of the primary zone temperature, combustion temperature, and exhaust temperature extend over a CO-emission-compliant partial load range of the gas turbine that is as large as possible.
1. A method for operating a gas turbine during partial load, the gas turbine including a compressor with inlet guide vanes, the method comprising:
choosing a lower power limit value (p 1 ) for an output gas turbine power as a lower limit of a partial load range that corresponds with a carbon monoxide (CO) emissions limit when an exhaust gas temperature is controlled at a constant value,
choosing an upper power limit value (p 2 ) for the output gas turbine power between the lower power limit value (p 1 ) and a rated load of the gas turbine,
operating the gas turbine with the output gas turbine power above the upper power limit value (p 2 ) with the exhaust gas temperature controlled at the constant value, and
lowering the output gas turbine power by decreasing an opening angle of the inlet guide vanes,
wherein, when the output gas turbine power drops below the upper power limit value (p 2 ), raising the exhaust gas temperature of the gas turbine as the output gas turbine power is lowered, up to a maximum exhaust gas temperature, wherein the rise in exhaust gas temperature causes a downward shift in the lower limit of the partial load range resulting in a second lower power limit value (p 1@TAT+ ), thereby extending the partial load range, and
wherein the upper power limit value (p 2 ) is chosen to be closer to the rated load than the lower limit of the partial load range.
2. The method as claimed in claim 1 ,
wherein the upper power limit value (p 2 ) is greater than 70% of the rated load.
3. The method as claimed in claim 1 ,
wherein a last exhaust gas temperature rise up to the maximum exhaust gas temperature takes place before the second lower power limit value (p 1@TAT+ ) is reached.
4. The method as claimed in claim 1 ,
wherein, as the output gas turbine power is lowered, said exhaust gas temperature is raised stepwise or continuously.
5. The method as claimed in claim 4 ,
wherein, in order to raise said exhaust gas temperature, a quantity of combustion air supplied to a combustion chamber of the gas turbine is reduced by further decreasing the opening angle of the inlet guide vanes.
6. The method as claimed in claim 1 ,
wherein said exhaust gas temperature of the gas turbine is regulated, and a set point value for the exhaust gas temperature is raised, when the upper power limit value (p 2 ) is undershot and as the output gas turbine power is further lowered, until a maximum exhaust gas temperature is reached.
7. The method as claimed in claim 1 ,
wherein the upper power limit value (p 2 ) is greater than 80% of the rated load.
8. The method as claimed in claim 1 ,
wherein the upper power limit value (p 2 ) is greater than 90% of the rated load.
9. The method as claimed in claim 1 ,
wherein the upper power limit value (p 2 ) is greater than 95% of the rated load.
10. The method as claimed in claim 1 ,
wherein the upper power limit value (p 2 ) approximately corresponds to the rated load of the gas turbine.
11. The method as claimed in claim 1 ,
wherein the exhaust gas temperature is raised by closing the inlet guide vanes and lowering a compressor mass flow rate.
12. A method for operating a gas turbine during partial load, the gas turbine including a compressor with inlet guide vanes, the method comprising:
choosing a lower power limit value (p 1 ) for an output gas turbine power as a lower limit of a partial load range that corresponds with a carbon monoxide (CO) emissions limit when an exhaust gas temperature is controlled at a constant value,
choosing an upper power limit value (p 2 ) for the output gas turbine power between the lower power limit value (p 1 ) and a rated load of the gas turbine,
operating the gas turbine with the output gas turbine power above the upper power limit value (p 2 ) with the exhaust gas temperature controlled at the constant value, and
lowering the output gas turbine power by decreasing an opening angle of the inlet guide vanes,
wherein, when the output gas turbine power drops below the upper power limit value (p 2 ), raising the exhaust gas temperature of the gas turbine as the output gas turbine power is lowered, up to a maximum exhaust gas temperature, wherein the rise in exhaust gas temperature causes a downward shift in the lower limit of the partial load range resulting in a second lower power limit value (p 1@TAT+ ),
wherein the exhaust gas temperature rises continuously from when the output gas turbine power drops below the upper power limit value (p 2 ) up to the maximum exhaust gas temperature, then levels off so as to not exceed the maximum exhaust gas temperature before reaching the second lower power limit value (p 1@TAT+ ).
13. The method as claimed in claim 12 ,
wherein the exhaust gas temperature begins to fail after reaching the maximum exhaust gas temperature before reaching second lower power limit value (p 1@TAT+ ).