Turbine Engine Starting; Ignition; and Shutdown Flashcards

1
Q

What is the function of a turbine engine starting system?

A

To uniformly accelerate the engine from rest to a rpm at which the gas flow through the turbine section provides sufficient torque to drive the compressor at idle rpm.

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2
Q

What is the most common type of starter used on large modern turbofan engines?

A

An air turbine starter.

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3
Q

What are the sources of bleed air to the air turbine starter?

A

An APU, another engine or from a ground compressed air source.

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4
Q

When/how is an air turbine starter disengaged?

A

Automatically by a starter clutch at a pre-determined rpm.

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5
Q

Why is a uniform rate of acceleration required during engine start?

A

To uniformly accelerate the engine from rest to a rpm at which the gas flow through the turbine section provides sufficient torque to drive the compressor at idle rpm, thereby avoiding a hung start.

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6
Q

What is the most positive indication of light-up (light-off) during a turbine engine’s start cycle?

A

The most positive indication of light-up (light-off) during a turbine engine’s start cycle is an increase in the turbine temperature, however it is measured and displayed - EGT, ITT etc.

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7
Q

What is “self-sustaining” rpm?

A

The rpm at which the starter has cut-out and the turbine is able to accelerate on its own.

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8
Q

What actions should be taken if the turbine or exhaust gas temperature is rising rapidly to exceed or nearly exceed the specified limits?

A

If a hot start is experienced, the fuel flow to engine should be shut off immediately and the engine should be dry motored to reduce the turbine or exhaust gas temperature.

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9
Q

What is a hot start?

A

A hot start is a start or attempted start where the turbine or exhaust gas temperature is rising rapidly to exceed, or nearly exceed the specified limits.

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10
Q

What are the potential causes of a hot start?

A
  1. Excessive fuel flow/excessive fuel to air ratio.
  2. A starter that is slow to accelerate the compressor /turbine spool.
  3. A starter that cuts out too early.
  4. Low battery voltage.
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11
Q

What actions are usually recommended in the event of a hot start?

A

Shut off the fuel supply and continue to dry motor the engine.

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12
Q

What is the main indication of a hung start?

A

Very slow or no increase in rpm.

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13
Q

What actions are usually recommended in the event of a hung start?

A

Shut off the fuel supply, discontinue the start cycle and continue to dry motor the engine.

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14
Q

What are the indications of a compressor stall during start?

A

The indications of a compressor stall during start are the same as for any compressor stall, i.e. a popping or banging noise, fluctuating rpm indications and rapidly increasing turbine or exhaust gas temperature.

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15
Q

What actions are usually recommended in the event that an engine stalls during start?

A

Shut off the fuel supply and continue to dry motor the engine.

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16
Q

What are the indications of a wet start?

A

Torching out of the exhaust section.

17
Q

What actions are usually recommended in the event of a wet start?

A

Shut off the fuel supply and continue to dry motor the engine.

18
Q

What are the normal indications of an engine power loss/flame-out in a turboprop in the cruise? 4

A

Torque, rpm, temperature and fuel flow decrease.

19
Q

What are the potential causes of a turbine engine flame-out? 6

A
  1. Fuel exhaustion.
  2. Compressor stall.
  3. Flight at extremely high altitude.
  4. Severe turbulence.
  5. Severe icing.
  6. High speed manoeuvres.
20
Q

What is the purpose of the high energy component of the ignition system?

A

For in-flight relight/starting.

21
Q

What is the purpose of the low energy component of the ignition system?

A

For continuous energising of the igniter system.

22
Q

What output is usually available from the ignition system when continuous is selected?

A

Low output of 3 to 6 joules.

23
Q

Why are most aircraft (helicopters and agricultural a/c) left running during short stops?

A

Because the stop/start cycles are where most damage/wear is done to turbine engines.