Gas Turbine Engine / Parts Of Gas Turbine Engine /Types of Gas Turbine Engine

Gas Turbine Engine :

Parts of gas Turbine Engine:

Intake Section Of Gas Turbine Engine :

Compressor Section:

Combustion Chamber:

Turbine Section:

Exhaust Section:

Gas Turbine Engine:

 

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EASA PART 66 Module-15 Gas Turbine Engine

EASA Part 66 Module 15.1 : Fundamental from soulstalker

EASA Part 66 Module 15.2 : Engine Performance from soulstalker

EASA Part 66 Module 15.3 : Inlet from soulstalker

EASA Part 66 Module 15.4 : Compressors from soulstalker

EASA Part 66 Module 15.5 : Combustion Chamber from soulstalker

EASA Part 66 Module 15.6 : Turbine from soulstalker

EASA Part 66 Module 15.7 : Exhausts from soulstalker

EASA Part 66 Module 15.8 : Bearings and Seals from soulstalker

EASA Part 66 Module 15.9 : Lubrication and Fuel from soulstalker

EASA PART 66 Module 15.10 : Lubrication Systems from soulstalker

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What is Thermocouple ? Construction Of Thermocouple

 Thermocouple:

A kind of thermometer, a thermoelectric device used for measuring temperature, usually at high temperatures Thermocouples are simple and rugged, can be used over a wide range of temperatures        (from -200° C. to 1,600°C.)x

 Video about How thermocouple work 

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M15 Gas Turbine Engine (EASA Module 15 Gas Turbine Engine Part66Prep)

 M15 Gas Turbine Engine

• Total Question =  939
• Powerpoint  Format 
• Each Slide Have 03 Question

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Aircraft Engine Fire Protection System

                           

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M15 Gas Turbine Engine Sub-Module No 17 (Quiz : No 1)

Turboshaft Engines

Quiz

 

1. The turbo shaft engine’s output is measured in ?
   1.   Horsepower
   2.   Thrust
   3.   Shp
2. The primary purpose for turbo shaft engines in aviation is their use as the main power plant for ?
   1.   Turbojet aircraft
   2.   Turbofan aircraft
   3.   Helicopters
3. The drive shaft itself must also carry ?
   1.   Tension loads
   2.   Compression loads
   3.   Torsion loads
4. The power plant is controlled between ground and flight idle by the ?
   1.   Free turbine governor
   2.   Throttle twist grip
   3.   Auto governor
5. The N1 system will speed up and slow down as a function of ?
   1.   N2
   2.   N7
   3.   N4
6. The collective stick, when raised, the angle of attack of all rotor blades ?
   1.   not related to stick
   2.   will decrease
   3.   will increase
7. The _____ allows for small movements between the engines and the transmission ?
   1.   Fexible coupling
   2.   A sprag clutch
   3.   Rigid coupling
8. Helicopter rotors tend to rotate at ?
   1.   3000-4000 rpm
   2.   300-400 rpm
   3.   1600-1700 rpm
9. About___________ of the energy produced by a helicopter turbo shaft engine is used to operate the gas generator ?
   1.   Half
   2.   Two thirds
   3.   One thirds
10. The function of ----- is to reduce the high rpm from the engine to a propeller RPM ?
    1.   Propeller speed governor
    2.   Power lever
    3.   Reduction gear assembly

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M15 Gas Turbine Engine Sub-Module No 16 (Quiz :1)

Turbo Prop Engine

Quiz

 

1. As the aircraft speed increases over 450 mph the propeller will rapidly ------?
   1.   Gain efficiency
   2.   Lose efficiency
   3.   Experience high airflow
2. Turbo-propeller engines, use a propeller to convert ------ into thrust and do not rely on gas exit velocity ?
   1.   Centripetal force
   2.   Compressor power
   3.   Turbine power
3. The governor flyweights spin ---- and ------ to lift the control valve ?
   1.   Faster, outwards
   2.   Slower , inward
   3.   Faster , forward
4. Most reduction gear assemblies use a ------- reduction ?
   1.   Planetary gear
   2.   Spur gear
   3.   Epicyclic reduction gear
5. The function of ----- is to reduce the high rpm from the engine to a propeller rpm ?
   1.   Propeller speed governor
   2.   Power lever
   3.   Reduction gear assembly
6. The power output of a turbo-propeller engine is stated in ?
   1.   Horsepower
   2.   Thrust horsepower (thp)
   3.   Shaft horsepower (shp)
7. The maximum propeller speed for any power lever angle is controlled by the ?
   1.   Propeller speed governor
   2.   Propeller pitch control unit (pcu)
   3.   Fuel supply
8. When it is increased the propeller blade angle increases to absorb the increased engine power output ?
   1.   Engine rpm
   2.   Aircraft speed
   3.   Fuel supply
9. Turbo-propeller control assemblies have a feathering system that feather the propeller when the engine is shut down -----?
   1.   During take off/ landing
   2.   At ground
   3.   In flight
10. Over-speeds cause extreme ------ to the propeller and the engine and can lead to rapid and total failure and in some cases to the loss of the aircraft in flight ?
    1.   Torque
    2.   Stress
    3.   Load

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