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TEST 10 – Gas Turbines and Jet Engines

Total questions: 26

Worksheet time: 13mins

Name
Class
Date
1.

Which cycle modification lowers compressor work?

a)

Intercooling

b)

Regeneration

c)

Reheating

d)

Afterburning

2.

Which turbine stage extracts energy to drive the compressor?

a)

Power turbine

b)

Gas generator turbine

c)

Free turbine

d)

Diffuser

3.

What is the role of a combustor liner?

a)

To cool turbine blades

b)

To provide stable flame and protect outer casing

c)

To increase turbine work

d)

To filter air

4.

Which method improves part-load operation in advanced gas turbines?

a)

Variable stator vanes

b)

Water injection only

c)

Increased inlet temperature

d)

Short exhaust stack

5.

Which factor increases specific power output of gas turbines?

a)

High turbine inlet temperature

b)

High exhaust pressure

c)

Low pressure ratio

d)

High lube oil flow

6.

Which efficiency is used to evaluate compressor stage performance?

a)

Isothermal efficiency

b)

Isentropic efficiency

c)

Volumetric efficiency

d)

Mechanical efficiency

7.

What is the function of turbine shrouds?

a)

To reduce tip leakage and improve efficiency

b)

To cool turbine blades

c)

To increase exhaust velocity

d)

To lower emissions

8.

What is the usual firing order in multiple combustor gas turbines?

a)

Sequential

b)

Random

c)

Simultaneous

d)

Cyclic

9.

Which property of fuel is most important for gas turbines?

a)

Cetane number

b)

High calorific value and clean burning

c)

High viscosity

d)

Low octane number

10.

What is the primary pollutant formed at high turbine inlet temperatures?

a)

CO

b)

HC

c)

NOx

d)

SO2

11.

Which system removes unburnt fuel during shutdown?

a)

Drain valves

b)

Diffuser

c)

Compressor bleed

d)

Lube oil separator

12.

Which loss dominates at part-load in gas turbines?

a)

Mechanical losses

b)

Heat transfer losses

c)

Combustion inefficiency and throttling

d)

Radiation losses

13.

Which gas turbine cycle uses a closed loop with helium as working fluid?

a)

Nuclear gas turbine cycle

b)

Air standard Brayton

c)

Diesel cycle

d)

Otto cycle

14.

What is the usual power factor of gas turbine generators?

a)

0.5

b)

0.7

c)

0.8–0.9

d)

1.0

15.

Which system maintains constant generator frequency?

a)

Voltage regulator

b)

Speed governor

c)

Cooling water pump

d)

Exhaust diffuser

16.

What is the unit of heat rate in gas turbines?

a)

kWh/kg

b)

kJ/kWh

c)

kg/kWh

d)

W/m^2

17.

Which factor influences turbine blade creep life most?

a)

Fuel flow

b)

Temperature and stress

c)

Vibration only

d)

Emissions

18.

Which technique reduces NOx without water injection?

a)

Dry low-NOx combustor

b)

Steam cooling

c)

Regeneration

d)

Reheating

19.

What is the advantage of combined cycle gas turbine plants?

a)

Low exhaust temperature

b)

High efficiency by recovering exhaust heat in a steam cycle

c)

Lower capital cost than simple cycle

d)

No cooling required

20.

Which number defines ratio of actual cycle efficiency to ideal cycle efficiency?

a)

Performance factor

b)

Efficiency ratio

c)

Work ratio

d)

Utilization factor

21.

Which part of the gas turbine plant experiences highest temperature?

a)

Compressor inlet

b)

Combustor exit (turbine inlet)

c)

Diffuser

d)

Exhaust stack

22.

Which type of turbine is used in aircraft jet engines?

a)

Radial flow

b)

Axial flow

c)

Reaction turbine

d)

Pelton turbine

23.

Which modification increases both power output and efficiency?

a)

Combined cycle operation

b)

Regeneration alone

c)

Intercooling alone

d)

Afterburning

24.

What is the unit of specific thrust in jet gas turbines?

a)

N·s/kg

b)

kJ/kg

c)

kW/kg

d)

J/mol

25.

Which factor reduces part-load performance in simple gas turbines?

a)

Reduced pressure ratio

b)

High regeneration

c)

Variable geometry

d)

High efficiency combustor

26.

Which part converts kinetic energy of jets to thrust in jet engines?

a)

Nozzle

b)

Compressor

c)

Combustor

d)

Intercooler