Anti-icing And Airflow Control Systems Flashcards

0
Q

On an F108 engine, which manifold is anti-icing air ducted from?

A

Pneumatic

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1
Q

Discharge air used for aircraft engine anti-icing to heat critical areas is taken from which area?

A

Compressor

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2
Q

On an F108-CF-100 engine anti-icing system, what is the purpose of the air injector on the air regulator?

A

Control air temperature and pressure

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3
Q

On an F110-GE-129 engine,the anti-icing system prevents detrimental formation and accumulation of ice on?

A

The front frame struts, forward centerbody, and fan inlet vane flaps

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4
Q

On an F110-GE-129 engine, what is compressor bleed air used for?

A

Inti-icing, costumer bleed, and LPT cooling functions

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5
Q

What does the C-D supersonic inlet use to slow down the airflow?

A

Bernoulli’s law

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6
Q

The compressor bleed system reduces the possibility of compressor stall in a dual-rotor engine by?

A

Reducing the amount of air available to the N2 compressor

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7
Q

Once the cooling airflow has done its job of cooling the turbine section, where does it go?

A

Into the gas stream to exit the engine

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8
Q

On an F108-CF-100 engine, the variable bleed valves bleed air from the?

A

N1 compressor

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9
Q

On an F108-Cf-100 engine, the direction of the variable bleed valve rotation is controlled by the?

A

Fuel gear motor

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10
Q

On an F110-GE-129 engine, which component supplies fuel pressure to operate the IGV actuator?

A

Main fuel control

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11
Q

An F110-GE-129 engine contains how many stages of VSV?

A

Three

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