Chap - 2 Compressors Flashcards

1
Q

Two basic types of compressor

A

Centrifugal flow
Axial flow

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2
Q

What is the purpose of a compressor

A

To give a pre-determined pressure rise throughout the compressor

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3
Q

Principles of operation of a Centrifugal compressor

A

Pushes air into the centre of the impeller (the eye)
Centrifugal force then cause flow to go along divergent vanes

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4
Q

What is the diffuser section used for

A

Passages form divergent nozzles that convert kinetic energy into pressure energy

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5
Q

How much does the pressure rise in the impeller and in diffuser in compressor

A

50/50

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6
Q

What is done to maintain efficency in compressor

A

Prevent excessive air leakage between impeller and the casing.

Keeping their clearances as small as possible

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7
Q

Adv of Centrifugal compressor

A

Robust cheap to make
Low surge tendancy
Efficency over wide speed range
Withstand icing/FOD
Balancing is relatively easily
Simple to maintain

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8
Q

Dis Centrifugal compressor

A

Low compression ratio
Large frontal area
High impeller speeds
No straight through airflow

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9
Q

What compressor is this

Consists of one or more rotor assemblies that carry blades of aerofoil sections

Casing Incorporate the stator vanes

Multi stage unit. Pressure increase by each stage

A

Axial compressor

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10
Q

In axial compressor what does a stage consist off

A

Set of rotors
Set of stators

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11
Q

What term is this called

To maintain axial air velocity,the shape between the drum and outer Casing forms convergent duct

A

Cascade effect

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12
Q

What do these do

A

Rotor blade increases velocity
Stator blade decreases velocity

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13
Q

What is stagger angle

A

Rotor blades have a slight twist to make sure there is an even amount of work being done across the whole balde

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14
Q

Adv axial flow compressors

A

Higher compression ratio
Straight through airflow
Smaller frontal area
Capacity for further development

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15
Q

Dis for axial flow compressors

A

Complex
Expensive to build
Will not readily accept ram air
Slow to accelerate

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16
Q

Determine stall

A

A breakdown of airflow over one or more stages of the compressor

17
Q

Determine surge

A

The event that occurs when compressor delivery air pressure is less than combustion pressure leading to hot combustion gases flowing backwards through the compressor

18
Q

Identification of stall

A

Audible rumbling
Loss of RPM
High jet pipe temperature
Vibration

19
Q

Identifications of surge

A

Loud bangs accompanied by flames from the intake

Rise in JPT

Lose of RPM

Extensive damage to the engine

20
Q

How is airflow controlled

A

Inlet guide vanes
Variable stator vanes
Twin spool
Compressor discharge valve

21
Q

What do inlet guide vanes achieve

A

Stationary or automatic

Guide the airflow onto the 1st stage rotors at correct AOA

22
Q

What do Variable stator vanes achieve

A

Similar to IGV but operate over more stages

23
Q

What does twin spool achieve

A

LP, HP Spool will run at different speeds

More flexibility

Less prone to stall and surge

24
Q

What do compressor discharge valve achieve

A

It assists engine starting and helps to avoid stall and surge during start, acceleration and deceleration

Compensates for over efficency at low RPMs

25
Q

FOD damage what does it do

A

Aero dynamic change

Deterioration malfunctions and engine failure

26
Q

Blade bending

A

May be repairable by using correct tools
Carried out by authorised person