Purpose of swirl vanes?

Fenwel fire detector system?

Measure temperature rise compared to reference temperature?

MTCS

Installed engine should be represerved at least after?

Convergent Duct purpose?

Turboshaft

Marking procedure for identifying areas to be repaired in both cold and hot section?

Inlet ducting furnish following

Mark the correct statement regarding Turboshaft

Turboprop engine, Gas generator section

Propulsive efficiency

Oil system consist warning light to indicate ?

Control of GTE

Kidde system

MTCS rigging power control

Prevent bearing damage of engine due to clogged jet nozzle?

Purpose of fuel pressurising and damp valve?

Halon 1301 also known as

Anti Ice hot air to inlet duct control by

Component of JE is speed regulated by FCU

Power Augmentation depends upon?

Uninstalled engine stored, humidity should be checked?

APU provide

Primary purpose of fuel metering section of hydroelectrical FCU

Parameter used to measure to determine amount of thrust of
turbojet engine

After all adjustment to engine power control inspect clearance?

APU starter couple to

Fuel low volatility at normal temperature

As temperature of After Burner Increases

MTCS

Highest temperature experienced by

Fuel flow indicator

Thrust and radial load taken by

MTCS Turboprop

Post exit type thrust reverser

Turboshaft ideal for helicopter

Rich blowout occur

Engine oil used in GTE

Convergent-Divergent nozzle advantage because high pressure regulation across engine exhaust

Engine hoist MTCS

Fuel control system sense the

MTCS EPR

FAN thrust produces

Protective envelope while preserving engine partially covered

APU used for

Ring seal

Combustion used

Thrust produced by turbojet in determined by

The rotor shaft provide matching surface for oil seal in earing housing machine surface is called

Kiddie fire detection system

Disadvantage of afterburner

Starter equipped with an output splice shaft having a shear section that permit the shaft to shear if :

Diffuser section

Aircraft having afterburner then which type of exhaust nozzle used

Function of turbine is to convert Kinetic energy into Mechanical energy to

Diethylene glycol solution work as a

Purity issue that is unique related to gas turbine engine

MTCS

Aniticing air is taken from

Mark the most appropriate answer regarding turboprop

Thrust Specific Fuel Consumption

MTCS

a turboshaft engine made up of two-part assemblies the gas generator and

MTICS

Cooling air through larger holes cools the combustion chamber up to

Can type combustion chamber air enters through

Which of the following is not function of centrifugal switch in APU

Uninstalled engine stored humidity checked

Control of GTE

Bellmouth inlet is usually installed in engine undergoing

Blow in door installed within centrifugal compressor admit air during

After Burner is used to increases

Turbine nozzle diagram

Noise suppressor used in GTE supplies the noise up to

FCU Senses many input parameter as power lever, compressor inlet pressure , Engine RPM Burner pressure and

Speed of impulse turbine increased

Engine starting electric circuit

MTCS

Cool down period for APU

Starter used for small turbine engine starting

Better atomization and uniform spray pattern type of fuel nozzle is used

Constant delivery pump plunger type pump consists of

MTCS

Foaming of oil prevented by

Regarding turboprop gearbox

In can type combustion chamber primary air enter

Corrugated noise suppressor suppress the noise

Turboprop 100% propulsive efficiency can be obtained by flying an aircraft at equal to

Advantage of axial flow compressor

Demineralised water compressor wash

Where physical separation of fuel lines from electrical wiring conduit is impractical