15.12 Air Systems Flashcards

(22 cards)

1
Q

What is the ideal air/fuel ratio?

A

15:1

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2
Q

What is the acceptable range of engine temperature?

A

800-1150 degrees

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3
Q

What is the function of secondary air?

A

Cools combustion chamber liners

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4
Q

What does zone 1 consist of?

A

Area around fan case containing accessory case and EEC

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5
Q

How is zone 2 cooled?

A

By fan air

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6
Q

What does zone 3 consist of?

A

Area around the HP compressor to turbine cases

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7
Q

What are the 3 zones in an engine divided by fireproof bulkheads?

A

Fan case compartment, intermediate compressor case, core engine compartment

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8
Q

How is the engine exterior and engine nacelle cooled?

A

Fan air

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9
Q

Where is anti ice used?

A

Engine inlet cowls

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10
Q

How is anti ice controlled?

A

Automatically by switch in flight deck

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11
Q

What % of air is used as primary airflow?

A

20-30%

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12
Q

What % of air is used as secondary airflow?

A

70-80%

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13
Q

How is the life expectancy of NGVs and turbine blades increased?

A

Cooled by compressor air

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14
Q

How do cooling systems benefit turbine NGVs and blades?

A

Allow them to operate 300-400 degrees above their limits

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15
Q

How is accessory cooling air provided?

A

From intakes in the fans cowling or from specific compressor stage

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16
Q

How is the compressor rotor cavity cooled?

A

From IP compressor air

17
Q

What is the temperature of the rear compressor stages?

A

350-400 degrees

18
Q

How does pressurised air affect engine bearing chambers?

A

Provides additional sealing

19
Q

What is used for the sealing of engine bearing components?

A

LP compressor bleed air

20
Q

Where does the air entering bearing compartments vent?

A

Through N1 rotor shaft

21
Q

Why is air often bled from the highest pressure stage?

A

Because pressure and temperature are at their max

22
Q

What is a bowed rotor?

A

Where the engine can bend due to different expansions of upper and lower zones after engine shutdown