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MCQ Assessment: Gas Turbine Propulsion

Total questions: 60

Worksheet time: 30mins

Name
Class
Date
1.

What cycle does a marine gas turbine operate on?

a)

Otto cycle

b)

Brayton cycle

c)

Diesel cycle

d)

Rankine cycle

2.

Which component mixes fuel with compressed air for ignition?

a)

Combustion chamber

b)

Compressor

c)

Turbine

d)

Reduction gearbox

3.

What is the primary purpose of the lubrication system?

a)

Compress air for combustion

b)

Transmit power to the propeller

c)

Detect fire in the turbine room

d)

Maintain bearing and component temperatures

4.

Which system directs air to the compressor while filtering contaminants?

a)

Fuel system

b)

Air intake and filtration system

c)

Control system

d)

Cooling system

5.

What is the first step in safe turbine startup?

a)

Engage starter

b)

Introduce fuel

c)

Power-up control systems

d)

Purge combustion chamber

6.

What must be checked for proper startup regarding fuel?

a)

Viscosity, purity, and cetane number

b)

Only temperature

7.

Which turbine type extracts energy from combustion gases?

a)

Low-pressure turbine

b)

High-pressure turbine

c)

Both A and B

d)

None of the above

8.

What does EGT stand for?

a)

Engine Gas Temperature

b)

Exhaust Gas Temperature

c)

Electric Generator Test

d)

Engine Gear Transmission

9.

Which safety precaution is mandatory before operating the turbine?

a)

Post warning signs and restrict access

b)

Reduce cooling water flow

c)

Block intake ducts

d)

Disable alarms

10.

Which system ensures sensor calibration and interlock engagement?

a)

Fuel system

b)

Exhaust system

c)

Lubrication system

d)

Control and monitoring system

11.

Why is pre-lubrication performed before turbine startup?

a)

To circulate oil and protect bearings

b)

To ignite the fuel-air mixture

c)

To measure exhaust temperature

d)

To power the reduction gearbox

12.

What is the main purpose of purging the combustion chamber?

a)

Increase fuel pressure

b)

Remove residual fuel vapors

c)

Warm up turbine blades

13.

Why should air intake and exhaust passages be free from obstructions?

a)

To prevent oil leaks

b)

To ensure proper combustion and turbine efficiency

c)

To reduce vibration in the gearbox

d)

To cool the control system

14.

Why must maintenance logs be reviewed before startup?

a)

To determine fuel, lubricating oil and water consumptions

b)

To calibrate sensors automatically and ensure safe operation

c)

To calculate turbine efficiency considering all recorded parameters

d)

To ensure previous issues are resolved and safe operation

15.

What is the reason for gradual fuel introduction during startup?

a)

To prevent overtemperature and hot start

b)

To increase lubrication oil flow

c)

To speed up turbine rotation

d)

To test emergency stop systems

16.

Why are temperature and pressure limits monitored during operation?

a)

To ensure turbine efficiency and prevent damage

b)

To measure ambient air quality

c)

To test exhaust system capacity

d)

To maintain gearbox alignment

17.

How does the reduction gearbox contribute to propulsion?

a)

Generates electricity

b)

Transmits turbine output to the propeller

c)

Increases fuel pressure

d)

Controls exhaust temperature

18.

Why is FOD (Foreign Object Debris) clearance important?

a)

Prevents oil contamination

b)

Prevents compressor and turbine damage

c)

Ensures proper lubrication

d)

Calibrates sensors

19.

Why should emergency shutdown procedures be reviewed with the engineering team?

a)

To increase fuel efficiency

b)

To adjust gearbox alignment after a period of time not in use

c)

To speed up startup sequence

d)

To ensure safe response to abnormal conditions

20.

What is the purpose of the control and monitoring system?

a)

Automates startup and regulates turbine performance

b)

Delivers fuel to combustion chamber

c)

Extracts energy from exhaust gases

d)

Directs cooling water flow

21.

If a turbine fails to achieve light-off, which system should be inspected first?

a)

Cooling water system

b)

Lubrication system

c)

Fuel delivery and ignition system

d)

Air intake filter

22.

During startup, exhaust gas temperature rises rapidly. What should the operator do?

a)

Immediately abort start to prevent overtemperature

b)

Introduce more fuel

c)

Ignore until self-sustaining speed

d)

Stop lubrication pumps

23.

A foreign object is detected in the intake duct. What is the correct procedure?

a)

Remove obstruction before starting

b)

Start turbine at low power

c)

Increase air intake speed to dislodge it

d)

Purge fuel system immediately

24.

How should an engineer verify pre-lubrication effectiveness?

a)

Activate control panel alarms

b)

Check exhaust gas temperature

c)

Inspect combustion chamber

d)

Measure oil pressure and flow

25.

A vibration sensor indicates misalignment during startup. What is the best response?

a)

Continue startup cautiously

b)

Shut down turbine and inspect shaft alignment

c)

Increase cooling flow

d)

Adjust fuel flow

26.

How can air quality and temperature affect turbine performance?

a)

Poor quality reduces combustion efficiency

b)

High quality prevents bearing damage

c)

Temperature only affects lubrication

d)

Air quality affects gearbox lubrication

27.

If emergency stop is tested during pre-start, what should be checked?

a)

Fuel valve pressure

b)

Starter disengagement and turbine halt

c)

Bearing oil temperature

d)

Control panel calibration

28.

A fuel filter is partially clogged. How should this be handled?

a)

Clean or replace filter before startup

b)

Increase fuel pressure to compensate

29.

How does aligning the propeller shaft with the gearbox affect operation?

a)

Enhances fuel flow

b)

Increases exhaust temperature

c)

Prevents abnormal vibration and mechanical damage

d)

Adjusts control system sensors

30.

During low-power warm-up, why is monitoring TIT important?

a)

To ensure thermal stability and avoid overheating

b)

To check fuel pressure

c)

To purge the combustion chamber

d)

To calibrate vibration sensors

31.

After startup, EGT is higher than normal while RPM is stable. Which component is likely responsible?

a)

Lubrication oil high viscosity

b)

Dirty air intake filter

c)

Fuel system delivering excess fuel

d)

Insufficient cooling water flow

32.

If oil pressure drops while turbine is running, what could be the root cause?

a)

Foreign object in intake

b)

Misaligned shaft

c)

Excess fuel

d)

Pump malfunction or leak

33.

An engineer observes vibration after light-off. How can the problem be diagnosed?

a)

Verify fuel cetane number to confirm performance

b)

Check for FOD, misalignment, or structural damage

c)

Purge the combustion chamber and check fuel filter

34.

Hot start occurs frequently. Which operational factor is most critical to analyze?

a)

Fuel flow rate and starter acceleration

b)

Oil temperature

c)

Cooling water pressure

d)

Shaft alignment

35.

During inspection, air intake ducts show minor corrosion. What analysis should be performed?

a)

Increase fuel flow to compensate for the corrosion

b)

Ignore because it is a normal wear and tear of the component

c)

Evaluate impact on airflow and turbine efficiency

d)

Reduce RPM during startup and then observe after a period of time

36.

Starter fails to disengage after self-sustaining speed. Which subsystem analysis is needed?

a)

Starter system and interlocks

b)

Lubrication system

c)

Cooling system

d)

Exhaust system

37.

Why analyze previous logbook entries before startup?

a)

Identify recurring issues and preventive measures

b)

Verify exhaust gas temperature

c)

Align propeller shaft

d)

Test fuel system pressure

38.

If control system alarms repeatedly, what analysis should be conducted?

a)

Purge combustion chamber and then operate engine again

b)

Sensor calibration, interlock status, and wiring integrity

c)

Lubricate bearings to eliminate friction that possibly causes the alarms

d)

Replace fuel filter and then restart the system

39.

What can be inferred (concluded) if self-sustaining speed is delayed?

a)

Control system functioning imperfectly

b)

Excess lubrication that adds load to the moving components

c)

Due to normal wear and tear of the engine

d)

Possible insufficient air pressure, fuel delivery issues, or starter inefficiency

40.

During startup, compressor surge is observed. Which factors should be analyzed?

a)

Airflow, FOD, and compressor blade condition

b)

Oil flow rate

c)

Fuel temperature only

d)

Cooling system pressure

41.

Design a pre-start checklist that ensures turbine readiness. Which elements must be included?

a)

Perform a basic visual check to verify leaks around the engine

b)

Inspect lubrication systems and cooling water levels after engaging startup

c)

Fuel, lubrication, cooling, control, safety systems, and FOD clearance all confirmed

d)

Test the electrical circuits prior addressing any other operational requirements

42.

How could a startup sequence be modified to prevent hot start in cold environments?

a)

Limit the air intake and skip any temperature monitoring to accelerate ignition

b)

Initiate the sequence without pre-lubrication or system temperature verification

c)

Gradually introduce fuel while pre-warming key components

d)

Override starter interlocks and engage full power immediately

43.

Combining vibration and oil pressure monitoring, what proactive strategy can be implemented?

a)

Continue operation until vibration levels become critical and alarms are triggered

b)

Schedule early shutdown and maintenance interventions before catastrophic component failure

c)

Reduce cooling water flow as a first response to abnormal readings

44.

How can control and monitoring data be synthesized to improve efficiency?

a)

Prioritize monitoring lubricating oil system parameters without reviewing other operational indicators

b)

Monitor exhaust temperature in relation to changes in fuel demand

c)

Adjust fuel flow, RPM, and load application dynamically based on sensor trends and real-time performance data

d)

Bypass erratic sensor readings and rely on manual visual inspections to ensure correct parameter readings

45.

Integrating fire detection and emergency stop systems, what procedure ensures safety?

a)

Ensure that safety signage are posted or clearly marked around the equipment

b)

Conduct isolated extinguisher checks without linking them to shutdown protocols

c)

Inspect ventilation systems regularly to skip alarm and trip circuit verification

d)

Activate alarms, confirm emergency shutdown readiness, and restrict access before and during startup operations

46.

How can previous startup failures be used to design preventive measures?

a)

Analyze the root causes of past incidents and incorporate improved procedures, staff training, and revised protocols

b)

Continue utilizing existing procedures that has always been working, ensuring design perfection

c)

Focus on lubrication checks even without addressing other contributing factors

d)

Monitor exhaust gas temperature and consider system history or performance trends while in normal operation

47.

Synthesize safe startup steps for a ship operating in high ambient temperatures. Which approach is correct?

a)

Bypass lubrication checks and rely on natural convection cooling for faster startup

b)

Introduce fuel quickly to achieve faster turbine acceleration regardless of heat load

c)

Verify fuel, oil, cooling systems, and air quality, and monitor EGT closely to prevent thermal stress

d)

Reduce ventilation rates to maintain pressure in the intake system and to prevent unnecessarily cooling of the system

48.

How can multiple system checks be combined to ensure operational readiness?

a)

Inspect the fuel system pressure after carrying out filter maintenance to ensure no fluctuations will occur during operation

b)

Limit pre-start checks to compressor alignment and ignore emergency subsystems

c)

Observe turbine inlet temperature trends after verifying auxiliary system readiness

d)

Conduct sequential inspections, verify interlocks, test emergency shutdown systems, and log all results for reference

49.

Designing a training scenario for engineers, what elements should it include?

a)

Cover lubrication system procedures and deviate from emergency protocols

b)

Focus on combustion chamber purging and temperature checks before and after startup

c)

Startup sequence, abnormal condition handling, emergency response, and system troubleshooting exercises

d)

Emphasize vibration monitoring data while addressing other diagnostic skills

50.

How can a synthesis of cooling and lubrication system data improve turbine lifespan?

a)

Do not ignore sensor data and rely entirely on manual operational adjustments

b)

Monitor RPM exclusively while analyzing thermal balance or lubrication performance

c)

Optimize oil and water flow rates to maintain safe component temperatures and minimize wear

d)

Focus on exhaust gas behavior even without correlating it to component heat transfer

51.

A turbine is started without purging the combustion chamber. What is the risk assessment?

a)

Minor efficiency reduction that might slightly affect output but not safety-critical operations

b)

No operational risk provided ignition occurs promptly

c)

Only affects lubrication system and bearing wear

d)

High risk of fire or explosion due to unburned fuel accumulation

52.

Which action best demonstrates adherence to safe startup protocols?

a)

Bypassing interlocks to shorten startup duration and achieve faster readiness

b)

Verifying all interlocks, safety devices, and emergency shutdown systems before initiating startup

c)

Relying on operator experience to override automatic safety checks

d)

Ignoring auxiliary system readiness to expedite main system startup

53.

How would you evaluate the effectiveness of a new turbine control system?

a)

Compare startup performance, alarm responsiveness, and sensor accuracy against established benchmarks

b)

Carry out sensor calibration to ensure that the RPM stays within limits

c)

Measure fuel flow during a single startup attempt and then use it to compute future consumption

d)

Check exhaust temperature trends and ensure that other diagnostics are unnecessary

54.

If vibration persists after alignment, what is the safest course of action?

a)

Operate at reduced power until the next maintenance period to minimize downtime

b)

Increase fuel flow to stabilize turbine speed and reduce vibration amplitude

c)

Shut down the system and conduct a thorough mechanical inspection before resuming operation

d)

Delay analysis until the next scheduled voyage since the system is still running

55.

How should abnormal EGT readings during startup be judged?

a)

Abort the startup immediately and troubleshoot to prevent severe damage

b)

As acceptable variation as long as turbine load is within rated capacity

c)

Reduce oil pressure and cooling water flow to stabilize internal conditions

d)

Ignore and continue startup since the readings may normalize after ignition

56.

When evaluating turbine readiness, which factor is most critical?

a)

Only shaft alignment and gearbox torque transmission efficiency

b)

Only lubrication pressure and oil temperature within normal range

c)

All safety, fuel, lubrication, cooling, and control systems are operational and verified

d)

Only exhaust system backpressure and gas discharge measurements

57.

Assessing the risk of starting a turbine in high ambient temperature with borderline oil pressure involves:

a)

Recognizing a high risk of equipment damage due to inadequate lubrication.

b)

Assuming normal operation as long as the turbine starts.

c)

Ignoring oil pressure if temperature is within limits.

d)

Expecting improved oil pressure as the turbine warms up.

58.

Which practice reflects the best evaluation of safety compliance during operation?

a)

Continuous monitoring and immediate corrective action in response to abnormal conditions

b)

Bypassing interlocks for convenience if no alarms are triggered

c)

Skipping alarm checks to save time during startup procedures

d)

Operating without control system data as long as mechanical systems appear functional

59.

A turbine repeatedly experiences hot starts. What evaluation action is most appropriate?

a)

Increase cooling water flow during startup to prevent combustion instability

b)

Ignore the condition and continue since the turbine still achieves ignition

c)

Review fuel control settings, starter operation, and operator procedures to identify root causes

d)

Only adjust lubrication pressure and oil filter flow rate

60.

Which decision ensures operational safety when a foreign object is detected in the intake duct?

a)

Purge the combustion chamber only before attempting ignition

b)

Start the turbine carefully at low power to prevent intake surge

c)

Proceed without checking to avoid delaying operational schedule

d)

Stop immediately and remove the object before initiating startup