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Propulsion - Turbine Engine Fundamentals

Total questions: 46

Worksheet time: 45mins

Name
Class
Date
1.

A body will retain at rest or continue it uniform motion in a straight line until acted upon by an external force.

a)

Newton's first law of motion

b)

Newton's second law of motion

c)

Newton's third law of motion

2.

The acceleration of a body is directly proportional to the force applied to it and is inversely proportional to the mass of the body.

a)

Newton's first law of motion

b)

Newton's second law of motion

c)

Newton's third law of motion

3.

Force developed by a gas turbine engine is proportional to?

a)

Mass of air flowing and acceleration given to that mass of air

b)

Weight of air flowing and speed given to that mass of air

c)

Flow of air injected and acceleration of the mass of air

4.

For every action, there is an equal and opposite reaction.

a)

Newton's first law of motion

b)

Newton's second law of motion

c)

Newton's third law of motion

5.

Exhaust gases leaving a turbojet engine producing a reaction force called?

a)

Lift

b)

Drag

c)

Thrust

6.

What is unique to the definition of work?

a)

Does not mention time as being a factor

b)

Does not mention force as being a factor

c)

Does not mention distance as being a factor

7.

One horsepower equals how much through one vertical foot in one minute?

a)

33,000 lbs

b)

550 lbs

c)

3,000 lbs

8.

What is the main difference between speed and velocity?

a)

Speed does not have direction

b)

Velocity does not have direction

c)

Acceleration is only involved in speed

9.

An object in free fall with no drag is how many feet per second?

a)

32.2

b)

1

c)

9.98

10.

A charged capacitor is an example of which type of energy?

a)

Kinetic

b)

Potential

c)

Static

11.

Total kinetic energy of a body or system is equal to?

a)

The sum of the kinetic energies resulting from each type of motion.

b)

One quarter of the mass of the body times the square of its speed.

c)

mph

12.

The velocity and pressure of a fluid going through a compressed area at a constant flow rate will?

a)

V=Increase P=Decrease

b)

V=Decrease P=Increase

c)

V=Increase P=Increase

13.

The air passages between individual blades of a compressor or turbine in a gas turbine engine is the application of?

a)

Bernoulli

b)

Otto

c)

Brayton

14.

What is the four cycles of the otto cycle in order from start to finish?

a)

Intake, compression, combustion, exhaust

b)

Exhaust, combustion, compression, intake

c)

Intake, combustion, compression, exhaust

15.

The constant pressure cycleis also known as?

a)

Otto

b)

Brayton

c)

Bernoulli

16.

The ratio of the turbine discharge pressure to the engine inlet air pressure is called?

a)

Engine pressure ratio

b)

Aircraft pressure ratio

c)

Work pressure ratio

17.

What are EPR readings dependant on?

a)

Pressure altitude and OAT

b)

Temperature and OAT

c)

Altitude and OAT

18.

Two classifications of thrust producing turbine engines are?

a)

Turbojet and Turbofan

b)

Turboprop and Turboshaft

c)

Turbofan and Turboshaft

19.

Two classifications of torque producing trubine engines are?

a)

Turboprop and Turboshaft

b)

Turbojet and Turbofan

c)

Turbofan and Turboshaft

20.

Which type of engine is this?

a)

Turbojet

b)

Turboshaft

c)

Turbofan

21.

Which type of engine is this?

a)

Turbojet

b)

Turbofan

c)

Turboprop

22.

Which type of engine is this?

a)

Turbojet

b)

Turboshaft

c)

Turbofan

23.

Three basic components of a turbojet engine are?

a)

Compressor, combustor and turbine

b)

Compressor, combustor and exhaust

c)

Propeller, compressor and combustion chamber

24.

Why are turbojets less efficient than turbo fans?

a)

Losses from noise and incomplete combustion

b)

Increase air resistance and amount of fuel required to operate

c)

Theory of operation and weight difference

25.

What is the pressure ratio in a turbofan?

a)

2:1

b)

4:1

c)

8:1

26.

In the otto cycle, what is true about the volume during combustion?

a)

Constant

b)

Increase to decrease

c)

Decrease to increase

27.

How many fixed blades are in a turbofan engine?

a)

20 to 40

b)

40 to 80

c)

10 to 20

28.

Why are turbofans used in almost all airliners?

a)

Fuel efficient and cruise speed capability

b)

Increase thrust and and weight reduction

c)

Short field take off and easier maintenance

29.

How is the propulsive efficiency measured in a turbofan?

a)

Fan bypass ratio

b)

Engine pressure ratio

c)

Engine bypass ratio

30.

The ratio of mass airflow which flows through the fan duct, divided by the mass airflow which flows through the core portion of the engine is called?

a)

Fan bypass ratio

b)

Engine pressure ratio

c)

Engine bypass ratio

31.

A high fan bypass ratio is?

a)

4:1

b)

3:1

c)

1:1

32.

The main types of turboprop engines are?

a)

Fixed and free

b)

One spool and two spool

c)

Jet and fan

33.

What type of engines are used to power helicopters and APU fitted to large commercial aircraft?

a)

Turbofan

b)

Turbojet

c)

Turboshaft

34.

Which two parts are considered the "cold section' of an engine?

a)

Air inlet and compressor

b)

Combustors and compressor

c)

Turbines and exhaust

35.

Fixed turbine turboprop engines are directly connect to?

a)

Compressor, gearbox, propeller

b)

Gear box and propeller shaft

c)

Exhaust outlet and compressor

36.

If a turbine is not directly connected to a compressor in a turboprop engine it is said to be?

a)

Free

b)

Fixed

c)

Moving

37.

Which part of an engine recovers as much of the total pressure of the free airstream as possible and provide a uniform supply of air to allow a efficient operation?

a)

Compressor

b)

Air inlet

c)

Exhaust

38.

The total pressure of the free airstream delivered to the compressor is known as what?

a)

Ram recovery

b)

De-pressure recovery

c)

Stam recovery

39.

What is the primary function of a compressor?

a)

Force air into the engine for combustion and provide the air necessary to produce thrust.

b)

Efficiently eliminate any unwanted air entering the engine

c)

Cause a mechanical compression to the engine allowing more airflow into the engine.

40.

How do you measure a compressor's effectiveness?

a)

Compare static pressure of the of the compressor discharge with the static air pressure at the inlet.

b)

Carrying out frequent periodic inspections.

c)

Install gauges/indicators which affectively will demonstrate the data.

41.

What part of the engine is used for cabin pressurization, air conditioning, fuel system de-icing or pneumatic engne starting?

a)

Compressor bleed air

b)

Air inlet

c)

Exhaust air

42.

What parts do a centrifugal flow compressor consist of?

a)

Impeller, diffuser, manifold

b)

Rotor and stator

c)

Gearbox and propeller shaft

43.

What determines the number of stages in axial flow compressors?

a)

Amount of air and total pressure rise required.

b)

Temperature of the air.

c)

The amount of pressure from the bleed air.

44.

Which part of the axial flow compressor slows the speed of the air inlet and increases the pressure?

a)

Rotor

b)

Shroud

c)

Diffuser

45.

Which section in an engine powers both engine accessorises such as generator, hydraulic pumps, fuel pumps and acting as an oil reservoir, sump or reduction gears?

a)

Accessory

b)

Exhaust

c)

Turbine

46.

Which part of an engine supports the engine weight and allow for transfer of stresses?

a)

Mounts

b)

Shafts

c)

Screens