Module 15.3 Inlets Flashcards

1
Q

What is used to straighten the airflow and direct it into the first compressor stages?

A

Inlet Guide Vanes (IGV’s)

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2
Q

What is required to avoid compressor stall?

A

Uniform and steady airflow

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3
Q

The air inlet duct is considered part of what?

A

Airframe

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4
Q

What can be said about a divergent duct?

A

Velocity - Decrease
Pressure - Increase
Temperature - Increase

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5
Q

Turboprop and turboshaft engines have what to prevent FOD ingress?

A

Screens

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6
Q

Where can the inlets be in a divided entrance duct aircraft?

A

Wing root or scoop at each side of the fuselage

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7
Q

What is placed in the side scoop inlet to assist in straightening the airflow?

A

Turning vanes

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8
Q

What is a disadvantage of divided entrance ducts W.R.T. Sudden flight movements?

A

Imbalances in Ram air pressure causing a slight power loss

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9
Q

What is the purpose of diffusers?

A

Decrease velocity and increase static pressure

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10
Q

What type of lip do you want at the inlet of a supersonic aircraft?

A

Sharp lip

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11
Q

What aircraft would round lip inlets be used on?

A

Subsonic

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12
Q

What occurs to the inlet area of a variable geometry duct with varying speeds?

A

Inside area changed by a mechanical device

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13
Q

What are the 3 methods of slowing airflow to subsonic levels?

A
  • Vary the area
  • Variable airflow bypass
  • Shockwave in the airstream
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14
Q

What are the disadvantages of compressor inlet screens?

A

Loss in inlet duct pressure and are susceptible to icing

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15
Q

When are inlet screens retracted?

A

After take off or if icing conditions are detected

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16
Q

When would a bell mouth compressor inlet be used?

A

During engine testing in a test cell

17
Q

What are the benefits to the bell mouth compressor inlets during testing?

A
  • Very high aerodynamic efficiency
  • Duct loss is considered 0
18
Q

What is considered the best inlet design for turboprop engines?

A

Ducted arrangement

19
Q

What is used to deflect ice and dust/dirt away from the intake?

A

Deflector doors

20
Q

What is the drawback to two spool engines?

A

Fan and low pressure compressor are connected. Fan has a limited rotational speed which is slower than the optimum compressor rpm. This means that the low pressure compressor is not at its optimum efficiency

21
Q

How does the fan prevent FOD ingestion?

A

Hits the fan and thrown radially outward

22
Q

How is the inlet lip and fan hub/spinner anti-iced?

A

Lip - Warm bleed
Fan hub/spinner - Warm bleed or conical spinner

23
Q

What effects can ice build up cause?

A
  • Engine sucks in ice
  • Disturbed airflow
24
Q

What do turboprops use to anti-ice inlet areas?

25
If only the cowls require anti-ice what may be used?
Electric heat strips
26
When can ice form in inlet areas?
- 5℃ in dry condition - 7℃ in fog/rain conditions
27
What are the types of anti-ice?
- Bleed air - Electric heating
28
What engines is bleed air generally used in?
High-mass airflow
29
Air bled from the HP compressor is used to anti-ice what?
- IGV's - Spinner - Lip
30
What is the purpose of the anti-icing valve?
- Prevent over pressurisation - Limit amount bleed air
31
The engine anti-ice system uses hot air from what?
- Pneumatic system - Directly from the engine
32
When is the manual function of the anti-ice regulator valve used?
Valve or system failure
33
When the engine is controlled by Electronic Engine Control (EEC), what is it linked with?
Anti-ice
34
What is the most common type of engine ice protection system?
Thermal system
35
As aircraft speed increases what happens to the thrust?
Thrust tends to decrease
36
As the aircraft reaches a certain speed, what compensates for the losses in thrust caused by this increase in speed?
Ram recovery
37
What is another name for ram recovery?
Total pressure recovery