npower0073
Electrical
- Jun 24, 2007
- 70
Hi guys. As you know we have a GE 9FA gas turbine with a 324 H2 cooled geenerator with Mark VI control program. I want to ask a question about the DROOP mode. According to documentation Gas Turbine works in DROOP mode while synchronized to the grid.
The speed control changes FSR as it needs to change power (watts) in proportion to the difference between turbine speed and the set point. Thus any change in actual speed (grid frequency) will also cause a proportionate change in unit load. This proportionality is adjustable to the desired regulation or “Droop”.
If the grid tends to be overloaded, grid frequency (or speed) will decrease and cause a FSR increase in proportion to the droop setting. If all units have the same droop, all will share a load increase equally. this is a big advantage.
Another advantage of droop control is that the gain of the system is high. If 4% droop is selected, as it is on our unit, only a 1% change in speed will produce a change in fuel flow equivalent to 25% of rated load. This results in fast system response to transient changes and helps hold system frequency.
Normally 4% droop is selected and the speed set point is calibrated such that 104% set point will generate a speed reference which will produce a FSR resulting in base load at design ambient temperature. On gas turbines having a peak temperature control, 104% set point corresponds to peak load.
On Mark VI logic we read the control constant
Load Rate Droop Conversion Constant G1\TNKR1_CONV is set to 4% (0.04 n/d). Is this the constant that speciies the DROOP 4% governor?
For this 4% dropp governor like ours, a change of 1% in grid frequency will modify the gas turbine output per 25%.
Does may analysis make sense and what are the control constants that specify the DROOP characteristics?
The speed control changes FSR as it needs to change power (watts) in proportion to the difference between turbine speed and the set point. Thus any change in actual speed (grid frequency) will also cause a proportionate change in unit load. This proportionality is adjustable to the desired regulation or “Droop”.
If the grid tends to be overloaded, grid frequency (or speed) will decrease and cause a FSR increase in proportion to the droop setting. If all units have the same droop, all will share a load increase equally. this is a big advantage.
Another advantage of droop control is that the gain of the system is high. If 4% droop is selected, as it is on our unit, only a 1% change in speed will produce a change in fuel flow equivalent to 25% of rated load. This results in fast system response to transient changes and helps hold system frequency.
Normally 4% droop is selected and the speed set point is calibrated such that 104% set point will generate a speed reference which will produce a FSR resulting in base load at design ambient temperature. On gas turbines having a peak temperature control, 104% set point corresponds to peak load.
On Mark VI logic we read the control constant
Load Rate Droop Conversion Constant G1\TNKR1_CONV is set to 4% (0.04 n/d). Is this the constant that speciies the DROOP 4% governor?
For this 4% dropp governor like ours, a change of 1% in grid frequency will modify the gas turbine output per 25%.
Does may analysis make sense and what are the control constants that specify the DROOP characteristics?