DGCA Gas Turbine 11. Ignition Systems

 

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Q1. The low energy ignition system would be used:

Correct answer is – during take-off from wet runways.

Q2. Precautionary use of igniters may be necessary during:

Correct answer is – flight through heavy tropical rainstorm.

Q3. A high energy ignition system works on the principle of:

Correct answer is – obtaining energy from the discharge of a capacitor.

Q4. A gas turbine engine which has both high and low energy ignition systems uses the high energy system for (i), and the low energy system for (ii):

Correct answer is – high altitude relighting / take-off from contaminated runways

Q5. In a High Energy Igniter Unit, the discharge resistors:

Correct answer is – allow the capacitor to discharge when the unit is switched off.

Q6. In a High Energy Igniter Unit, the choke:

Correct answer is – prolongs the discharge to the plug.

Q7. The rate of discharge of a High Energy Ignition Unit is:

Correct answer is – 60-100 times per minute.

Q8. The power supply for the spark in the combustion chamber is:

Correct answer is – high volts high current

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