15.16 Flashcards

1
Q

turboprop best for operating at what speed

A

483-725kmh / 300-450mph

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2
Q

What height is turboprop good for

A

6000m / 20000ft +

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3
Q

In cruising what makes turboprop better then turbo jet

A

Propulsion efficiency is constant in turboprop whereas it increases in turbojet as airspeed increases

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4
Q

How much power can turboprop extract

A

95%

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5
Q

What’s the core engine known as in turboprop

A

Gas generator or producer

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

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6
Q

What connection is there in a free power turbine and gas generator

A

No mechanical connection only a gas flow connection

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7
Q

Advantages of free power turbine

A

Vibration not directly transmitted to the gas generator

Easier to start , especially in cold weather

Propeller held at low rpm during taxing

Can use a propeller brake to stop propeller movement during aircraft loading when shutdown not desired

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8
Q

How are gear-direct coupled turbines different to free power

A

Extra discs that are mechanically connected to compressor and reduction gearbox

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9
Q

Why does the propeller pitch and fuel flow need to be coordinated

A

So if fuel flow changes then propeller pitch must change to maintain a constant speed

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10
Q

What’s the function of the reduction gear assembly

A

Reduce high rpm from the engine to a propeller rpm

Needs to be maintained without exceeding the maximum propeller tip speed (SoS)

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11
Q

When would you use an epicyclic gear

A

Larger high torque reductions

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12
Q

2 types of reduction gears

A

Parallel spur and epicyclic

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13
Q

Advantage and disadvantage of straight cut parallel spur gear

A

Easy to cut and have lowest frictional losses

Very noisey

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14
Q

Helical cut parallel spur gear advantage and disadvantage

A

Quieter

Less efficient in transmission of power

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15
Q

What gear wheel does a epicyclic reduction gear use

A

Planet gears

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16
Q

How is epicyclic reduction gear ratio calculated

A

Dividing number of driven teeth by number is of driving teeth

17
Q

What direction does the propeller shaft drive in rotating annulus

A

Opposite direction of rotation to the power turbine shaft

18
Q

What direction does the propeller shaft drive in a fixed annulus

A

Same direction of rotation as the power turbine shaft

19
Q

What speed does the propeller rotate in fixed annulus

A

At a speed dependent on the reduction gear ratio

20
Q

What does the fadec system control

A

Engine and propeller

21
Q

What shape is the spinner

A

Cone-shaped configuration that mounts on the propeller and encloses he some and barrel to reduce drag

22
Q

What does the feathering system do

A

Feathers propeller when engine is shut down and unfeather if engine needs to be started

23
Q

On multi-engine aircraft where is the lever for number one engine

A

On the left

24
Q

What uses a single thrust lever

A

Gear couple engine

25
Q

What lever does a turbo propeller engine use

A

Dual lever if it has a free turbine

26
Q

What does the thrust lever do

A

Schedule fuel flow from idle - takeoff

Blade angle from 20 to -20 degrees (BETA / ground operating range)

27
Q

What does the control lock do

A

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

28
Q

What does the propeller lever do

A

Selects the required rpm by applying or releasing pressure on the governor control spring

29
Q

What does overspeed cause

A

Extreme stress to the propeller and engine and can lead to rapid and total failure

30
Q

How low can reduction gearing be

A

Low as 1:22

One revolution = 22 engine rotations

31
Q

What is the feathering angle

A

90 degrees to the plane of rotation

Blade chord is in line with the airflow

32
Q

What does the automatic drag limiting system do

A

Feathers the propeller if the oil supply fails to avoid it from windmilling

33
Q

When does a propeller overspeed governor activate

A

Propeller speed exceeds 105% governor dumps oil pressure to increase blade angle

34
Q

What’s the governor a safety device for

A

Operate if normal propeller governor and fuel control overspeed governor fail to contain the engine speed

35
Q

What happens in turbine shaft failure

A

Mechanical system in place to immediately shut off the engine-metered fuel supply in event of turbine shaft failure