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Aircraft Technic
#1. On an axial flow, dual compressor turbofan engine, the fan turns the same speed as the
#2. A turbo jet engine gives
#3. As subsonic air flows through a convergent nozzle, the velocity
#4. Bleed valves are normally spring loaded to the
#5. ............reduces the temperature and the thermal expansion around the HP and LP turbine
#6. VBV's (Variable Bleed Valves) are
#7. Ignition Exciters input and output voltages are
#8. Operating sequence of components at engine start
#9. Engine Pressure Ratio
#10. If fire handle is released, LP fuel valve .........
You can also look Gas Turbine Engine Quiz 1, Gas Turbine Engine Quiz 2, Gas Turbine Engine Quiz 3
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Denpends on who engines the questions are base, ignitors 24v in 4400v at ignitors on RR
Ref Question on Bleed Valves –> Bleed valves on most aircraft are fail safe closed, engine anti valves are normally fail safe open
Ref Question on ignition –> Input voltage depends on a/c system. 115V AC or 28V AC on modern jets
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