Chapter 3: Compressor Flashcards

1
Q

compressor qualities

A

1) compressor pressure ratio
2) mass flow rate
3) rotational speed
4) adiabatic efficiency (no heat loss/gain)

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2
Q

components of centrifugal flow compressor

A

1) impeller (rotor)
2) diffuser (convert kinetic to pressure energy)
3) compressor manifold (transfer air to next stage)

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3
Q

what is the centrifugal compressor efficiency?

A

80% with compressor ratio of 4/5 to 1

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4
Q

advantages of centrifugal flow compressor

A

1) higher stage pressure ratio
2) simplicity & ruggedness of building
3) less drop in performance from dust on blades
4) shorter length for same pressure ratio
5) wider range of stable operation

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5
Q

disadvantages of centrifugal flow compressor

A

1) larger frontal area
2) more than 2 stages not practical due to energy loss between stages

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6
Q

types of centrifugal compressor to increase flow rate

A

double entry impeller

double entry centrifugal compressor

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7
Q

disadvantages of double entry impeller

A

1) implication of design to get air to rear impeller
2) volume of air not uniform from both inlet duct due to flow of air

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8
Q

disadvantages of double entry centrifugal compressor

A

1) energy lost in air (slows down to make turns from 1 impeller to another)
2) more weight & power needed to drive compressor

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9
Q

what is the compression ratio achieved with 2 centrifugal stages?

A

14/1

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10
Q

what happens if tip clearance for centrifugal compressor is too small?

A

vibration of engine (rubbing of impeller and stationary vanes)

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11
Q

what happens if tip clearance for centrifugal compressor is too large?

A

efficiency of compressor affected (some airflow will rotate with impeller without entering diffuser)

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12
Q

what does 1 stage of axial compressor consist of?

A

1 row of rotor & 1 row of stator

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13
Q

what is the compressor ratio for axial flow compressor?

A

1.2 per stage

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14
Q

what does an axial compressor consist of?

A

1) inlet guide vane (directs airflow to 1st rotor)
2) rotor
3) stator (stationary vanes)

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15
Q

how to count the number of stages in axial flow compressor when theres 7 rows?

A

IGV 1st row

1st rotor 1st stator
2nd rotor 2nd stator
3rd rotor 3rd stator

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16
Q

advantages of axial flow compressor

A

1) small frontal area
2) flow direction discharge suitable for multi staging
3) higher efficiency at high pressure ratio

17
Q

disadvantages of axial flow compressor

A

1) complex mechanical design
2) higher possibility of surge
3) more prone to FOD

18
Q

what does the rotor do in axial compressor?

A

impart motion to air (v increase), p increase due to divergent shape

19
Q

what does the stator do in axial compressor?

A

transform part of velocity into pressure (divergent)

flow is straightened &directed to next stage at correct angle

20
Q

solutions for perfect tip clearance for axial compressor

A

1) apply soft coat in edge tips on rotor blades (form own clearance)

2) coat inner layer surface with soft material (material worn away by blades without damaging it)

21
Q

advantages of multi spool engine

A

1) higher compressor ratios
2) quick acceleration (less intertia of spools during starting)
3) low weight (less number of stages and smaller spool)
4) better control of stall characteristics

22
Q

disadvantage of multi spool engine

A

bearings being the weakest link

23
Q

what is compressor stall?

A

localised condition where one or few stages are affected by airflow disruption

24
Q

what is compressor surge?

A

entire compressor suffers complete airflow disruption

25
Q

signs of compressor stall/surge?

A

1) loss of power
2) vibration
3) rpm fluctuation
4) increase in EGT & noise

26
Q

factors that lead to compressor stall/surge?

A

1) high power operation at low speed
2) abrupt change in altitude
3) air turbulence
4) deficiency air volume
5) rapid throttle movement

air quality & fuel quantity

27
Q

mechanical malfunctions leading to compressor stall/surge

A

1) variable stator vane
2) fuel control unit
3) FOD
4) variable exhaust nozzle

28
Q

effects of compressor stall/surge

A

1) increase in gas temp.
2) severe vibration (damage bearings)
3) violent noise
4) smoke/flame from exhaust
5) power drop

29
Q

solution fo compressor surge/stall

A

1) place variable stator vane infront
2) add air bleed valve (relief pressure)
3) split spool
4) variable exhaust nozzle (input must be same as output air)

30
Q

what compressor assembly does a turboshaft engine use?

A

axial centrifugal compressor

31
Q

methods of fan blade attachment

A

1) dovetail
2) solid
3) fir tree

32
Q

types of fan blades

A

1) narrow
2) wide-chord

33
Q

which type of fan blade needs mid span support and why?

A

narrow fan blade, prevent aerodynamic instability and bending

34
Q

what is shingling?

A

overlapping of mid span shrouds

35
Q

disadvantage of mid span support on narrow blades

A

block some airflow & cause shingling

36
Q

advantages of wide chord fan blade

A

1) fewer FOD ingestion
2) increase aerodynamic efficiency
3) lower noise level
4) decrease opportunity for surge

37
Q

material of fan blade

A

sandwich titanium honeycomb & titanium panels