Module 15.16 Turboprop Engines Flashcards

1
Q

What speed range are turboprop engines most efficient at?

A

483 to 725 km/h (300 to 450 mph).

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2
Q

At what height are turbo prop engines most efficient at?

A

6000 metres (20 000 ft)

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3
Q

What percentage of the total power produced to the components can the engine extract?

A

95%

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4
Q

What is the core engine commonly known as?

A

The gas generator/producer.

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5
Q

What does the gas generator do?

A

Produces high-velocity gases that provide the energy to drive the power turbine.

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6
Q

What is a gas coupled/free-power turbine engine?

A

An engine with no mechanical connection between the gas generator and the free-power turbine.

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7
Q

What are the advantages of gas-coupled/free-power turbine engines?

A

Vibration is not directly transmitted to the gas generator.

Engine is easier to start due to only needing to drive the gas generator.

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8
Q

How does a gear/direct coupled turbine engine differ from a free-turbine one?

A

The addition of extra turbine discs which remain mechanically connected to the compressor and reduction gearbox.

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9
Q

As the propeller is driven directly by the engine, what is needed?

A

An integrated propeller control system.

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10
Q

What adjusts the propeller pitch for the power requirements of the engine.

A

The propeller control system.

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11
Q

Why must propeller pitch and fuel flow be coordinated?

A

To maintain a constant speed condition.

If fuel flow changes, then the propeller pitch must change.

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12
Q

What does the reduction gear assembly do?

A

Reduces high rpm from the engine to a propeller rpm that can be maintained.

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13
Q

What type of gear is used for small reductions?

A

Spur gears

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14
Q

What type of gear is used for high torque reductions?

A

Epicyclic gears

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15
Q

What are the larger shafts supported by?

A

Ball bearings

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16
Q

What do the ball bearings supporting the larger shafts do?

A

Absorb and transmit all loads imposed on them to the casing.

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17
Q

What are the two main types of reduction gears?

A

Parallel spur gear

Epicyclic

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18
Q

What are the two types of spur gear?

A

Straight-cut or helical

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19
Q

What is the disadvantage to straight-cut spur gears?

A

Very noisy

20
Q

What is the advantage to helical-cut spur gears?

A

More gradual onset of torque making it quiet.

21
Q

What is a fixed annulus and rotating annulus epicyclic gear?

A

Fixed - ring (outer) gear does not move.

Rotating - ring (outer) gear moves.

22
Q

What must the propellor do to its blades if oil supply to the propeller fails?

A

It must feather them.

23
Q

What happens if the torque indication system senses negative torque?

A

A signal is sent to the auto-feather system.

24
Q

What happens if propeller speed exceeds 105%?

A

A separate governor will dump oil pressure to the return. This will cause the blade angle to increase until the overspeed condition ceases.

25
Q

What is the governor?

A

A safety device designed to operate if the normal propeller governor and the fuel control overspeed governor fail to contain the engine speed.

26
Q

What do modern turboprop engines now utilise to control the engine and propeller?

A

Dual Full Authority Digital Engine Control (FADEC) system

27
Q

What is the spinner assembly?

A

A cone-shaped configuration that mounts on the propeller and encloses the dome and barrel.

28
Q

What does the feathering system do?

A

Feathers the propeller when the engine is shut down in flight.

29
Q

Can the propeller be unfeathered during flight?

30
Q

What type of turboprop engine will use a single thrust lever?

A

Gear-coupled engines.

31
Q

What does the single thrust lever control?

A

Fuel flow and propeller rpm.

32
Q

What happens if a single lever control system is moved forward?

A

Increase in fuel flow and propeller rpm.

33
Q

What does the Propeller Control Unit (PCU) do?

A

Controls the maximum rpm of the engine.

34
Q

What happens when propeller rpm rises to a predetermined level?

A

The fuel control unit will take over and control the rise in rpm.

35
Q

What type of turboprop engine will use a dual thrust lever?

A

Free-turbine engines.

36
Q

What do the separate levers in a dual-lever system do?

A

One for power (fuel flow) and the other for propeller control (rpm).

37
Q

What happens when the fuel lever goes from idle to reverse?

A

It changes fuel input and the blade angle.

38
Q

What angle do the propeller blades go to when the thrust lever is in reverse?

A

From +20° to -20°.

39
Q

When the propeller blades go from +20° to -20°, what is this called?

A

‘BETA’ or “ground operating range”.

40
Q

What happens when the thrust lever is moved into ‘Beta Range’?

A

A control unit changes the propeller blade angle. It’s fined below the ‘flight fine’ pitch into ‘ground fine’.

41
Q

What controls the degree of the propeller fining off into reverse?

A

Position of the thrust control lever in the Beta range.

42
Q

What is the propeller lever connected to?

A

The Propeller Control Unit (PCU).

43
Q

What does the propeller lever do?

A

Selects the required rpm.

44
Q

What does the control lock do?

A

Ensures the aircraft control surfaces do not flutter excessively on the ground with the engines running.

45
Q

Is the viscosity of the turboprop oil higher or lower in comparison to oil used for turbojet engines?

Why?

A

It’s higher due to having heavier loads imposed on the gears.

46
Q

What is done in the event of a turbine shaft failure?

A

The fuel supply is immediately shut off.

47
Q

Which type of gearbox will cause the propeller to turn in the opposite direction to the engine?

A

Epecyclic reduction gearbox with a rotating annulus?