Interview Questions

Top Essential Gas Turbine Instrumentation Interview Questions and Answers

Prepare for gas turbine instrumentation interviews with essential questions and answers on vibration probes, interlocks, Master Trip SOV, and more. This article covers calibration, troubleshooting, and system testing for effective turbine management.

Vibration probes, such as proximity probes or accelerometers, measure the vibration displacement, velocity, or acceleration of rotating equipment like gas turbines. They detect changes in the distance between the probe tip and the rotating shaft or structure. 

Key parameters include vibration amplitude, frequency, and phase, which help assess the condition of bearings, rotors, and other components.

Calibration involves setting the correct gap between the probe and the shaft using a calibration fixture and reference voltage. Installation requires aligning the probe properly and securing it to avoid mechanical looseness. The signal is then verified to ensure it accurately reflects the machine’s vibration.

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Proper gap adjustment between the proximity probe and the shaft is crucial for accurate measurement. An incorrect gap can lead to erroneous readings, affecting data reliability. Correct adjustment ensures the probe operates within its designed linear range, providing accurate and repeatable measurements. 

Dual-voting systems use two independent vibration measurements to prevent false trips and enhance system reliability. Both channels must agree on a high vibration condition before initiating a shutdown, reducing the risk of unnecessary turbine trips due to spurious signals.

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Key interlocks include fuel valve position, rotor speed, lubrication oil pressure, generator breaker status, and exhaust temperature. These interlocks ensure the turbine operates within safe parameters and that critical systems are functioning before allowing startup or during shutdown.

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Testing involves simulating conditions that trigger each interlock and observing the system’s response. This can be achieved using software simulations or physical manipulation of inputs. Verification includes ensuring that the correct actions are taken when interlocks are activated and that they reset appropriately.

Troubleshooting a failed interlock involves checking the sensor or input device for proper operation, verifying wiring and signal integrity, reviewing control system logic for errors, and testing the interlock under controlled conditions to identify and correct the issue.

Gas Turbine Instrumentation Interview Questions and Answers

During the purge cycle, critical interlocks include fuel valve closure, exhaust damper position, and purge air flow rate. These interlocks ensure that residual gases are safely evacuated before ignition, reducing the risk of explosions.

Redundancy can be implemented by using multiple sensors or signals for critical parameters, dual-channel logic systems where two independent systems must agree before taking action, and fail-safe design principles where the system defaults to a safe state in case of a fault.

Troubleshooting involves checking temperature sensors for accuracy and calibration, verifying control system logic, ensuring cooling systems are functioning properly, and inspecting physical components(thermocouples) for signs of overheating or damage.

Common issues include incorrect logic configuration, timing mismatches, and sensor failures. Resolving these involves reviewing and correcting the logic, synchronizing interlock signals, and replacing or recalibrating faulty sensors.

Fail-safe design ensures that, in the event of a system failure, the turbine defaults to a safe state, such as shutting down or preventing startup. This minimizes the risk of accidents or equipment damage by prioritizing safety over continued operation.

Common gas detection systems include infrared sensors, catalytic bead sensors, and electrochemical sensors. These systems detect combustible or toxic gases by measuring changes in absorption, catalytic reaction, or chemical reaction, triggering alarms or shutdowns to prevent hazardous conditions.

Calibration involves exposing the sensor to known concentrations of target gases and adjusting the sensor output to match expected values. Maintenance includes regular calibration, sensor cleaning, and replacing sensors that have reached the end of their operational life.

Troubleshooting involves checking for environmental factors that could trigger the sensor, inspecting the sensor for contamination or damage, reviewing calibration records, and ensuring the control system interprets sensor signals correctly.

During startup, the governor gradually increases fuel flow to ramp up turbine speed smoothly, preventing sudden spikes. During shutdown, it reduces fuel flow to slow down the turbine, ensuring a controlled and safe stop.

Key parameters include turbine speed, load, fuel flow rate, and temperature. The governor continuously monitors these parameters and adjusts fuel supply and turbine speed to maintain stability and performance.

Verification involves checking fuel supply pressure and flow, inspecting burner nozzles for blockages or wear, ensuring igniters and flame detectors are functioning, and performing a test run to observe burner performance and flame stability.

Common issues include poor fuel atomization, uneven flame distribution, burner fouling, and ignition failure. Troubleshooting involves inspecting fuel nozzles, checking fuel quality, verifying air-fuel ratios, and performing maintenance on igniters and flame detectors.

Monitoring is done using sensors that measure the concentration of oxygen and fuel in the combustion process. Control is achieved through automatic systems that adjust fuel and air flow rates to maintain the desired ratio for efficient combustion.

Burner tuning involves adjusting the air-fuel ratio and burner settings to achieve optimal combustion. Proper tuning improves efficiency, reduces emissions, and enhances turbine performance by ensuring complete and efficient fuel combustion.

Critical parameters include flame presence, intensity, and stability. Testing involves using diagnostic tools to simulate flame conditions and verifying that detectors respond accurately to different flame characteristics.

Address issues by checking burner settings, fuel quality, and air supply. Inspect for blockages, leaks, or mechanical faults in the burner system. Perform diagnostic tests to identify the root cause and adjust settings or replace components as needed.

The trip test involves simulating an overspeed condition to verify that the protection system activates correctly. This is done by gradually increasing turbine speed to the trip setpoint, observing the system’s response, and ensuring that the turbine shuts down or takes corrective action as designed.

Verification involves testing the fuel trip interlock by simulating a fault condition, such as a fuel supply issue. The system should respond by shutting off the fuel supply and stopping the turbine. The test ensures that the interlock functions correctly and activates in response to simulated faults.

Testing the ESD system involves simulating emergency conditions such as high vibration, fire, or loss of lubrication. The system’s response is monitored to ensure it shuts down the turbine safely and performs any necessary actions to protect equipment and personnel.

Addressing discrepancies involves analyzing test results, identifying the root cause of the issue, and making necessary adjustments to the interlock system. This may include recalibrating sensors, revising control logic, or replacing faulty components. Follow-up testing ensures that corrective actions have resolved the issue and that the system functions as intended.

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The Master Trip SOV controls the fuel supply to the gas turbine. During normal operations, it regulates fuel flow based on system demands. During a trip or emergency, it rapidly closes to stop fuel flow, ensuring a safe and controlled shutdown of the turbine.

The Master Trip SOV ensures reliable operation by using a solenoid to rapidly and securely close the valve in response to an emergency signal. It is designed to be fail-safe, meaning it will close upon loss of power or signal, ensuring fuel is cut off even in the event of control system failures.

Testing involves simulating a trip condition to ensure the valve closes correctly. This includes activating the emergency signal, observing the valve’s response to ensure it shuts off the fuel supply, and verifying that the valve returns to its normal position when the signal is removed.

The Master Trip SOV is integrated into the control system via electrical signals that trigger its operation during normal and emergency conditions. It is also part of the safety system, receiving trip signals from various sensors and interlocks to ensure it functions correctly in emergency situations.

Verification involves simulating an emergency trip condition and observing the valve’s response. Ensure the valve closes completely, stops the fuel flow, and returns to its normal position when the test is concluded. Check the system’s feedback to confirm the trip was executed correctly.

A scenario could be a high vibration condition or a critical fault detected by the control system. In such cases, the Master Trip SOV would receive a signal to close, shutting off the fuel supply and stopping the turbine to prevent damage or unsafe conditions.

A gas turbine is a thermodynamic machine that operates on the admission-compression-combustion-exhaust cycle. It converts chemical energy in fuel into mechanical energy, typically used for power generation or propulsion.

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A typical gas turbine consists of three main stages: the compressor stage, the combustion stage, and the turbine stage.

The main components of a gas turbine engine are the compressor, the combustion chamber, and the turbine. The compressor draws in and compresses air, the combustion chamber ignites the fuel-air mixture, and the turbine extracts energy from the expanding gases to power the compressor.

The compressor in a gas turbine usually has around 17 stages.

Gas turbines use an axial flow compressor, which compresses air as it flows along the axis of the compressor.

There are typically four bleed valves in the compressor.

Air is extracted through bleed valves at the 11th stage of the compressor.

Air bleeding is required to protect against pulsations during startup.

After the turbine rotor reaches operating speed, the combustion chamber pressure causes the spark plugs to retract, removing their electrodes from the hot flame zone.

Safety measures include thorough personnel training, regular equipment inspections, adherence to industry guidelines, wearing appropriate personal protective equipment, and implementing emergency shutdown procedures to ensure a safe working environment.

Combined cycle power plants integrate gas turbines and steam turbines to maximize energy output. This combination results in higher overall efficiency compared to standalone systems. Additionally, combined cycle plants offer lower environmental impact with reduced emissions.

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Sundareswaran Iyalunaidu

With over 24 years of dedicated experience, I am a seasoned professional specializing in the commissioning, maintenance, and installation of Electrical, Instrumentation and Control systems. My expertise extends across a spectrum of industries, including Power stations, Oil and Gas, Aluminium, Utilities, Steel and Continuous process industries. Tweet me @sundareshinfohe

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