turbo 2

turbo 2

23 Qs

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turbo 2

turbo 2

Assessment

Quiz

others

Hard

Created by

Nancy Asistiri

Used 1+ times

FREE Resource

23 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The diffuser section of a jet engine is located between
A. The burner section and the turbine section
B. Station Nº 7 and station Nº8
C. the compressor section and the burner section.

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

When the leading edge of a first-stage turbine blades is found to have stress rupture cracks, which of the fol-lowing should be suspected?
A. Faulty cooling shield
B. Overtemperature condition.
C. Overspeed condition.

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Turbine blades are generally more susceptible to operating damage than blades because of
A. Higher centrifugal loading
B. Exposure to high temperatures
C. High pressure and high velocity gas flow.

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which of the following is the ultimate limiting factor of turbine engine operation?
A. Compressor inlet air temperature
B. Turbine inlet temperature
C. Burner-can pressure

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The recurrent ingestion of dust or other fine airborne particulates into a turbine can result in.
A. Foreign object damage to the compressor section.
B. The need for less frequent abrasive grit cleaning of the engine
C. Erosion damage to the compressor and turbine sections

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Which of the following engine variables is the most critical during turbine engine operation?
A. Compressor inlet air temperature
B. Compressor RPM
C. Turbine inlet temperature

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Reduced blades vibration and improved airflow char-acteristics in gas turbines are brought about by
A. Fir-tree blades attachment
B. Impulse type blades
C. Shrouded turbine rotor blades

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