engine 2

engine 2

13 Qs

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engine 2

engine 2

Assessment

Quiz

Others

Practice Problem

Easy

Created by

Khaled Alzahrani

Used 84+ times

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13 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

20 sec • 1 pt

How are the compressor rotor blades attached to the wheel?

Fir tree and locking strip.

Dovetail and locking strip.

Dovetail and pin.

Fir tree and pin.

2.

MULTIPLE CHOICE QUESTION

20 sec • 1 pt

What is the purpose of the grommets at the aft end of the combustion Liners?

Minimizes air leakage around the thermocouples.

For cooling of the thermocouples.

Support for the thermocouples

Support for the liner

3.

MULTIPLE CHOICE QUESTION

20 sec • 1 pt

How are the turbine rotor blades attached to the wheels?

A dovetail and retainer.

A fir tree and retainer.

A dovetail and pin.

A fir tree and pin.

4.

MULTIPLE CHOICE QUESTION

20 sec • 1 pt

What holds the turbine wheels together?

Turbine tie bolt

Tubine clamp bolts

. Turbine coupling shaft.

Turbine rear bearing support.

5.

MULTIPLE CHOICE QUESTION

20 sec • 1 pt

What is the purpose of the diffuser assembly?

Directs compressor discharge air to the turbine section.

Directs compressor discharge air to the combustion section.

Directs air in to the compressor section.

Directs air into the exhaust section

6.

MULTIPLE CHOICE QUESTION

20 sec • 1 pt

During acceleration what holds the compressor bleed air valves open?

Oil pressure

Fuel pressure

14 th stage air

Compressor pressure

7.

MULTIPLE CHOICE QUESTION

20 sec • 1 pt

How will the engine anti-icing system be affected if aircraft electrical power fails?

(a) The anti-icing valves will close and the system will be off.

(b) The anti-icing valves will open and the system will be on.

It will have no effect on the anti-icing system.

(d) The system will not work.

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