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Compressor Chapter 3

Authored by Dimitrios Chua

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University

Used 4+ times

Compressor Chapter 3
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10 questions

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1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

"A stage" of an axial-flow compressor consists of _____________ and ___________

Impeller and Stator

Stator and Rotor

Impeller and Rotor

Guide vane and stator

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

As air flows through the axial flow compressor rotor blades, its _______________.

pressure and absolute velocity decreases

pressure and absolute velocity increases

pressure decreases and absolute velocity increases

pressure increases and absolute velocity decreases

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the purpose of the diffuser section just before the combustion chamber in a turbine engine?

To convert pressure to velocity.

To increase pressure and reduce velocity.

To reduce pressure and increase velocity.

To speed up the air flow in the combustor section.

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

At what point in an axial flow turbojet engine will the highest gas pressures occur?      

At the compressor outlet.  

At the turbine entrance.

At combustor inlet

At the turbine exist.

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The purpose of the variable inlet guide vanes is to  prevent ______________ .

FOD entering the compressor

engine flame out at high speed

compressor from overspeed

compressor from stalling

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

A twin-spool turbojet engine has a compression ratio of 36. if the low pressure compressor has a pressure ratio of 4, calculate the high pressure compressor pressure ratio?

1/9

9

40

144

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which of the following is TRUE about the axial flow compressor?

It has low peak efficiencies.

It is easy to manufacture and low cost.

It required low starting power.

It is susceptible to foreign object damage.

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