DGCA Gas Turbine 1. Introduction

 

Results

Q1. When gases pass through a convergent duct their:

Correct answer is – their velocity increases and their temperature and pressure decrease

Q2. Select the correct order of best propulsive efficiency, from low to high airspeed.

Correct answer is – Turboprop, High bypass ratio turbojet, Low bypass ratio turbojet, Pure turbojet

Q3. The highest pressure in a gas turbine engine occurs:

Correct answer is – between the compressor and the combustion chamber

Q4. In a turbofan engine, the fan speed is controlled by:

Correct answer is – the turbine

Q5. In a High Bypass Ratio engine:

Correct answer is – not all the air goes through the high pressure compressor

Q6. Modular construction:

Correct answer is – enables malfunctioning sections of the engine to be changed without changing the whole engine

Q7. The Bypass Ratio of an engine is the ratio of:

Correct answer is – cold stream air to that flowing through the hot core of the engine

Q8. The Gas Turbine Engine uses the principle of:

Correct answer is – Newton’s Third Law of motion

Q9. The addition of heat in a combustion chamber allows a:

Correct answer is – large expansion at a substantially constant pressure

Q10. In a divergent duct:

Correct answer is – the pressure temperature increases and the velocity decreases

Q11. In a twin spool engine:

Correct answer is – the LP turbine is connected to the LP compressor, the HP turbine is connected to the HP compressor

Q12. A Bypass Ratio of 5:1 means that:

Correct answer is – 5 pounds of air is bypassed for every 1 pound that goes through the hot core of the engine

Q13. Aft of the compressor:

Correct answer is – the velocity of the airflow decreases before the combustion chamber

Q14. The fan in a ducted fan engine, is driven by:

Correct answer is – the rearmost turbine

Q15. In a bypass engine, the bypass air:

Correct answer is – increases the air mass flow and therefore increases the propulsive efficiency

Q16. The majority of the thrust of a:

Correct answer is – turbofan engine comes from the bypass air

Q17. A pure turbojet engine gives:

Correct answer is – a large acceleration to a small mass of air

Q18. During the Brayton cycle, combustion takes place:

Correct answer is – continuously

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