15.04 Compressors Flashcards

1
Q

What are the two ways to compress air in an engine?

A
  • Decrease the volume of a cylinder using a piston.

- Make use of Bernoulli’s principle to get compressed air.

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2
Q

What two main parts make up the compressor?

A

Stators and rotors.

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3
Q

How are the rotor blades used?

A

They rotate around the axis and suck in the air to energise the airflow.

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4
Q

How are the stator vanes used?

A

They guide and slow the airflow to increase the pressure.

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5
Q

What is another name for a combination of the stator and rotor ?

A

Compressor stage.

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6
Q

What do the compressor inlet and outlet cases provide?

A

support for the compressor rotor bearings, and they improve and straighten the airflow.

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7
Q

What are the two types of compressor?

A

Axial flow and centrifugal.

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8
Q

Main components of a centrifugal compressor ?

A
  • the impeller
  • the diffuser
  • the compressor manifold.
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9
Q

Where are you most likely to find a centrifugal compressor?

A

Small gas turbine engines (APUs)

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10
Q

What is the compressor ratio of a centrifugal compressor ?

A

5:1

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11
Q

What is a double entry type impeller?

A

Two impellers mounted back to back, also known as double face compressor, to increase airflow and save weight by having a smaller engine frontal area.

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12
Q

What is the pressure ratio of each stage of an axial flow compressor?

A

1.3:1

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13
Q

in an axial flow compressor, why are many stages needed?

A

The pressure increase at each stage is very small.

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14
Q

What are the advantages of an axial flow compressor?

A
  • More efficient at optimum speeds.
  • Less aerodynamic drag.
  • Addition of many stages creates the ability to reach very high pressures.
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15
Q

What are the advantages of a centrifugal flow compressor?

A
  • Less power needed for engine start.
  • less weight.
  • simpler and less expensive.
  • high pressure increase at each stage.
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16
Q

What is definition of the design point?

A

The single optimum operating pressure, rotational speed and airflow.

17
Q

What is the resultant rotor inlet velocity?

A

The correct relationship between rotor speed and inlet velocity, generating smooth airflow.

18
Q

What angle of attack on the rotor blades creates smooth airflow?

A

A small one.

19
Q

What can cause the angle of attack of rotor blades to change?

A

A change in inlet velocity or rotor speed.

20
Q

What causes a compressor stall?

A

Turbulent vortexes causing flow separation on many of the rotor blade aerofoils.