15.4 Flashcards

1
Q

Compressors are made up of what?

A

Stators and rotors

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2
Q

What pressure do rotors increase?

A

Dynamic pressure

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3
Q

Stator vanes do what?

A

Slow airflow and increase pressure

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4
Q

Which is first in compressor stage out of rotors and stators?

A

Rotors

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5
Q

What are stator vanes also known as?

A

Inlet guide vanes (IGV)

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6
Q

Two types of compressors?

A

Axial flow
Centrifugal flow

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7
Q

What are the main components of a centrifugal compressor?

A

The impeller
The diffuser
The compressor manifold

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8
Q

Centrifugal flow compressors give what pressure ratio?

A

5:1

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9
Q

How many compressor stages are efficient?

A

2

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10
Q

Two impellers mounted back to back are known as what?

A

Double face compressor

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11
Q

What are the benefits of double face compressors?

A

Increase airflow due to two sides
Saves weight

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12
Q

Airflow in axial flow compressor is on what axis?

A

Horizontal axis

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13
Q

As pressure increases, density….

A

Increases

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14
Q

You taper axial flow compressors why?

A

Maintain air velocity

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15
Q

Why are compressors sensitive to airflow change?

A

Because compressors only have one operating condition for a given pressure ratio, rotational speed and airflow

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16
Q

What is the direction of airflow better called?

A

The resultant rotor inlet velocity

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17
Q

The resultant rotor inlet velocity is a result of what?

A

Air inlet velocity and rotor speed

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18
Q

The angle of attack changes when?

A

If rotor speed or inlet velocity changes

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19
Q

Compressor stall causes what for airflow in the compressor?

A

Causes airflow to slowdown, stop or reverse direction

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20
Q

A compressor surge is a very severe what?

A

Compressor stall

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21
Q

How is a compressor surge generated?

A

Rapid decrease of airflow onto blades
Then stall causes a blockage
That then causes low pressure zones

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22
Q

Surge is forward phase affects what?

A

Compressor blades

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23
Q

A surge in the aft stages could cause what to happen?

A

A reverse flow
Could occur from combustion chamber back to engine inlet

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24
Q

What are reasons for stalls and surges?

A

Dents or ice that cause disrupted airflow
Damaged rotor blades could cause disrupted airflow
Dirty compressor blades

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25
How does a fast deceleration cause similar problems on dual to triple spool engines?
The rotor speed of high pressure compressor decreases faster than that of low pressure compressor
26
What is a method to avoid stalls or surges?
Use of dual or triple spools
27
Where are bleed valves found in compressors?
Found in mid and sometimes aft section of compressor
28
Why would you open the bleed valves at slow speeds?
So excessive airflow from forward stages can escape overboard
29
What are the low speed and high speed compressors driven by?
Their respective turbines in latter stages of engine
30
Variable stator vanes in compressor are used to prevent what?
Stall- Along vertical axis
31
The spinner cone is also known as what?
Compressor inlet or nose cone
32
Why do engines have a spinner cone?
-creates smooth aerodynamic fairing at engine inlet -soft tip causes small imbalance to prevent ice build up -heated on some engines
33
What type of attachment is the fan blade attachment?
Dovetailed fitting
34
Two loads on rotor blades?
Air loads Centrifugal loads
35
What is the function of shrouds?
Keeps fan blade from deflection, within safe limits when heavy loads are on them Converts energy of fluttering to friction
36
Why are wide chord fan blades more efficient than conventional blades?
They run with lower speed which reduces noise Flexible Can withstand FOD better than conventional
37
Low pressure compressor is also known as what?
Booster modules
38
Rotor drum of low pressure compressor is attached to what?
Fan disc
39
Between dovetail slots there are rings with sharp edges to create what?
A labyrinth seal
40
What are two methods of making shroud assembly?
Made from plain metal surfaces Or individual segments
41
Shroud assembly segments are made up of what?
Filled with soft, abradable material where knife edges can cut in
42
On modern turbofan engine the fan cause has one or more ring elements, how are they bolted?
They’re bolted together to flanges -Flanges help stiffen the case and prevent deformation
43
Acoustic panels provide what?
Smooth airflow Reduce noise
44
The fan blade containment prevents what?
A fan blade from penetrating the fan case if it breaks during high speed operation
45
What are some things that would affect centrifugal force?
Rotor speed Blade mass Distance of the COG of fan blade from rotational axis
46
Moment weight can be given in what values?
Gram inches CMG ounce inches
47
What is the moment of weight?
The product of blade mass and distance of COG from rotational axis
48
How is moment of weight worked out?
Worked out by special blade scale
49
How is fan number one identified?
Index mark on fan disc or by an offset hole
50
Where are balance weights installed?
On fan disc or in spinner cone
51
A typical high pressure compressor consists of what?
Rotor drum Forward hub Rear hub Rotor blades mounted on a drum
52
What is CDP?
Compressor discharge pressure
53
The compressor discharge pressure (CDP) prevents what?
Prevents the compressor discharge airflow from escaping into the bearing area below the combustion chamber
54
Blades held in by blade retainers prevents what?
Prevents axial movement
55
How are rotor blades secured?
Locking lug
56
The high pressure compressor case is split into what?
Front compressor case Rear compressor case
57
The front compressor case supports what loads?
Structural loads Torsion Bending
58
Variable stator vanes have what at each end?
Trunnion
59
The HP compressor is a source of pressurised air for what?
Pneumatic systems Engine related purposes
60
Bleed air is supplied through what?
Hollow stator vanes
61
Bleed manifolds collect bleed air and do what?
Supply it to consumers
62
What are the fixed axial flow compressor aerofoils in an aircraft gas turbine engine called?
Stators
63
What is the function of the stator vane assembly at the discharge end of a typical axial flow compressor?
To straighten airflow to eliminate turbulence
64
Where does the pressure increase in an axial compressor stage?
In both the rotor and the stator
65
Why do the compressor stators in a gas turbine engine act as diffusers?
To decrease velocity in the gas flow
66
What is known as the design point of a gas turbine engine?
Optimum RPM the engine can operate at
67
Which installed components can prevent compressor stalls?
Bleed valves, multiple spools and variable stator vanes