Description
Technical Parameters
Technical Specifications
|
Manufacture |
GE |
|
Model |
IS200AEBMG1A |
| Part Number | IS200AEBMG1AEA |
|
Description |
BOARD |
|
Origin |
USA |
|
Dimension |
15*10*3cm |
|
Weight |
0.2kg |
FUEL CONTROL SYSTEM
The gas turbine fuel control system will change fuel flow to the combustors in response to the fuel stroke reference signal (FSR). FSR actually consists of two separate signals added together, FSR1 being the called–for liquid fuel flow and FSR2 being the called–for gas fuel flow; normally, FSR1 + FSR2 =FSR. Standard fuel systems are designed for operation with liquid fuel and/or gas fuel. This chapter will describe a dual fuel system. It starts with the servo drive system, where the setpoint is compared with the feedback signal and converted to a valve position. It will describe liquid, gas and dual fuel operation and how the FSR from the control systemspreviously described is conditioned and sent as a setpoint to the servo system.
Servo Drive System:
The heart of the fuel system is a three coil electro–hydraulic servovalve (servo) as shown in Figure 13.The servovalve is the interface between the electrical and mechanical systems and controls the direction and rate of motion of a hydraulic actuator based on the input current to the servo.
The servovalve contains three electrically isolated coils on the torque motor. Each coil is connected to one of the three Controllers <RST>. This provides redundancy should one of the Controllers or coils fail. There is a null–bias spring which positions the servo so that the actuator will go to the fail safe position should ALL power and/or control signals be lost.
If the hydraulic actuator is a double–action piston, the control signal positions the servovalve so that it ports high–pressure oil to either side of the hydraulic actuator. If the hydraulic actuator has spring return,hydraulic oil will be ported to one side of the cylinder and the other to drain. A feedback signal provided by a linear variable differential transformer(LVDT, Figure 13) will tell the control whether or not it is in the required position. The LVDT outputs an AC voltage which is proportional to the position of the core of the LVDT. This core in turn is connected to the valve whose position is being controlled; as the valve moves, the feedback voltage changes. The LVDT requires an exciter voltage which is provided by the VSVO card.
Figure 14 shows the major components of the servo positioning loops. The digital (microprocessor signal) to analog conversion is done on the VSVO card; this represents called–for fuel flow. The called–for fuel flow signal is then compared to a feedback representing actual fuel flow. The difference is amplified on the VSVO card and sent through the TSVO card to the servo. This output to the servos is monitored and there will be an alarm on loss of any one of the three signals from <RST>.

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