Lecture 25 Flashcards

1
Q

How is turbine engine ignition different from piston engine ignition?

A

Turbine engines use an untimed continuous combustion process
High-energy sparks only during engine start
Igniters are also not prone to carbon fouling due to the high-energy spark blasting off any deposits

Piston engines have timed magnetos
Low-energy spark every other revolution of the crankshaft
Ignition in pistons is constant while ignition in turbine engines only happens at start-up

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2
Q

How is heat energy in turbine engine fuel different from piston engine fuel?

A

Turbine engine fuel has less heat energy in it and requires a much hotter spark for ignition than piston engine fuel

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3
Q

When is ignition needed in a turbine engine?*

Why?

A

Only needed during the start sequence

Pressurized flammable gas, don’t have to keep lighting the fuel

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4
Q

What are the parts of a turbine engine ignition system?*

What combination makes up a typical turbine engine ignition system?

A

Excitor box
Lead
Igniter

2 Ignition Exciters
2 High-Tension Leads
2 Igniters

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5
Q

Turbine engine ignition systems have a _____ rate of current and a _____ voltage to produce a _____.

A

high

high

spark

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6
Q

Why is it beneficial to have an extremely short spark time?

A

Ignition systems can be small and light

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7
Q

When is the ignition system turned on?

A

Takeoff
Landing
Flight into turbulent conditions
Turbine engine flameout

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8
Q

Cooling-down period for the ignition system is called a _____.

A

duty cycle

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9
Q

What are the two types of duty systems?

A

Intermittent
Continuous

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10
Q

When are intermittent-duty systems used?

What is the operating time limit? How much cool down must follow the first operation and second operation?

A

Main ignition

2 minutes of operation
3 minutes of cool down
2 minutes of operation
20 minutes of cool down

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11
Q

Where does a continuous-duty system provide energy?

Do they have a operating time limit?

A

One igniter

No operating time limit

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12
Q

What is the purpose of igniters?

A

Ignite the fuel-air mixture

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13
Q

What are the two types of igniters?

A

Spark
Glow plug

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14
Q

What is the main goal of turbine engine start systems?*

A

Get air flowing through the combustor so we can mix it with fuel and burn it

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15
Q

Describe air starters*

A

Used in large engines
Light weight with good amount of torque produced
Requires large volumes of low pressure compressed air
APU, GPU, and cross-flow of compressor bleed air

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16
Q

Describe electrical starters

A

Used in small engines
Series-wound electric starters
Connected to the engine through a ratcheting starter jaw similar to reciprocating engines
Starter jaw engages a mating jaw on the engine starter drive

17
Q

Describe a starter generator

A

Used for smaller engines on business jets
A combination of starter and generator
Once engine is running is automatically switches off

18
Q

Describe an air impingement starter

A

Low-pressure air is ducted through the turbine blades
Once engine reaches self-sustaining speed, check-valve closes the air path

19
Q

Describe auxiliary power units (APU)*

A

Self-contained gas-turbine-powered unit in the tail
Provides electric power, compressed air when main engines are not running