15.4 compressor Flashcards

(30 cards)

1
Q

what is the primary function of the compressor

A

to supply a sufficient quantity of air to satisfy the requirements of the combustion chamber

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2
Q

what are the two main components of the compressor

A

compressor rotor
compressor stator

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3
Q

what is mounted in each rotor

A

rotor blades

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4
Q

what component of the compressor is stationary

A

the stator

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5
Q

what component is always the first part of the compressor stage

A

the rotor

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6
Q

what are inlet guide vanes

A

a set of stator vanes in front of a compressor stage

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7
Q

what are the stator vanes in the fan duct usually called

A

outlet guide vanes

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8
Q

what are the two types of compressors being currently used

A

centrifugal flow compressor
axial flow compressor

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9
Q

what does the centrifugal-flow compressor consist of

A

an impeller, a diffuser, and a compressor manifold

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10
Q

how many stage are there in a centrifugal-flow compressor

A

only 2 stages

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11
Q

what is the function of the impeller

A

to pick up and accelerate the air outwardly to the diffuser

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12
Q

where are axial flow compressors normally found

A

on turbofan engines

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13
Q

where are centrifugal flow compressors usually found

A

on turboshaft and turboprop

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14
Q

what does a single-spool axial flow compressor consist of

A

a single drum and multiple stators

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15
Q

in an axial flow compressor how is the total number of stages determined

A

it is based on the desired pressure increase

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16
Q

what are the three parameters that the centrifugal forces depend on

A
  • rotor speed
  • blade mass
  • the distance of the centre of gravity of the blade from the rotational axis
17
Q

where can the blade moment weight usually be seen

A

on the blade root

18
Q

why is the moment weight sometimes crossed out and another number is shown

A

the moment weight has changed because of blending

19
Q

what are the two methods proposed to change a single fan blade

A
  1. replacing the blade with a new that has a moment weight as close as possible to the old one
  2. always change a pair of blades with similar moment weight
20
Q

what do axial floe and centrifugal flow have in common

A

they are very sensitive to change in the airflow which passes through the compressor

21
Q

what is need for smooth airflow into the rotor

A

the correct relationship between the inlet velocity and the rotor speed is required

22
Q

the airflow in the axial compressor is smooth as long as what

A

the angle on the rotor blades and stator vanes is small

23
Q

what is compressor surge

A

a very severe form of compressor stall

24
Q

what are compressor stall and surge caused by

A

problems in engine operations or damaged engine components

25
aircraft engines have three different design methods to prevent compressor stall and surge what are they
1. compressor bleed valves 2. dual or triple spool rotors 3. variable compressor stator vanes
26
when are bleed valves opened
at low engine speeds
27
what is the most effect method of preventing compressor
variable stator vanes
28
what is the advantage of variable stator vanes
an optimum angle of attack on the following rotor blades can be reached for every engine speed
29
each stage of an axial flow compressor has a ratio of about ...
1.3:1
30
what does the compression ratio varies with
RPM