Powerplant IV FINAL EXAM

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100 Terms

1
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Which section of a gas turbine engine is responsible for driving the fan?


Turbine section


2
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Which type of gas turbine engine is most efficient in the 300 to 400 mph speed range?


Turboprop


3
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What is the purpose of convergent and divergent shaped ducts in supersonic inlets?


To control and drop the air flow to subsonic speeds


4
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What is the role of increasing the forward speed of the aircraft in determining the amount of air passing through a gas turbine engine?


It increases the amount of air passing through the engine


5
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What is the role of increasing the density of the ambient air in determining the amount of air passing through a gas turbine engine?


It increases the amount of air passing through the engine


6
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What is the primary function of the accessory section in a gas turbine engine?


To provide space for mounting accessories


7
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Where is the accessory gear box typically located in a turbofan engine?


On the bottom of the engine


8
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Where is bleed air typically extracted from in a gas turbine engine?


The compressor outlet


9
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What is the purpose of the diffuser in a centrifugal-flow compressor?


To compress air while it continues in its original direction of flow


10
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Where is the combustion section located in relation to the compressor and turbine sections?


 

Directly between the compressor and turbine


11
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What is the purpose of the fuel drainage system in a combustion chamber?


To drain off unburned fuel after engine shutdown


12
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Which type of combustion chamber is typically used on turboshaft and APUs?


Can-type


13
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What is the purpose of the shroud in an annular combustion chamber?


To prevent flame contact with the combustion chamber


14
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What is the purpose of the pre-swirl vanes in a can-annular combustion chamber?


To provide a swirling motion to the fuel spray


15
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What are the advantages of using an annular combustion chamber in modern turbine engines?


Both Answers are correct

Higher efficiency AND Better atomization of fuel

16
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What is the purpose of the gas generator turbine?


To absorb kinetic energy from the exhaust gases


17
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Which type of turbine blade is also referred to as a bucket?


 

Impulse turbine blade


18
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What is the function of the turbine inlet nozzle assembly?


To deflect gases in the direction of turbine rotation


19
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What is the function of the turbine nozzle guide vanes?


To increase the efficiency of the air stream striking the blades


20
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What is the difference between the turbine inlet nozzle assembly and turbine nozzle guide vanes from the previous questions?????


 

Different names for the same component


21
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What material is commonly used for the turbine shaft?


Steel


22
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What is the benefit of using single crystal blades?


Better strength and heat properties


23
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Why would it be necessary to use multiple turbine stages?


To drive heavy rotational loads


24
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What is the purpose of the thermocouple bosses in the outer shell or duct of the exhaust section?


To measure exhaust temperature


25
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What are the principles of convergent and divergent ducts for subsonic gas velocities? 


Convergent increases velocity and decreases pressure, while divergent decreases velocity and increases pressure


26
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What is the recommended method for repairing corrosion pitting on compressor stator vanes?

Blending

27
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What are examples of blade damage in axial-flow and centrifugal-flow engines?

All of the above;

Damage to the outer half of the blade

Nicks and dents in the critical band

Cracks in the leading edges

28
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Why is it important to follow the manufacturer's maintenance and overhaul manuals when performing repairs or inspections on turbine engines?

To ensure proper functioning of the engine

29
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What is the recommended method for cleaning turbine blades during a hot section inspection?

Ultrasonic cleaning

30
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What is the purpose of using a borescope inspection during a hot section inspection?

To check for cracks and warping

31
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What is the importance of following the manufacturer's detailed assembly instructions during engine maintenance?

All of the above;

To extend the engine's service life

To prevent foreign material from entering the engine

To ensure efficient maintenance

32
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Which marking material is recommended for parts directly exposed to the engine's gas path?

All answers are correct;

Felt tip marker and chalk

33
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What method is recommended for inspecting combustion chambers for cracks?

Fluorescent penetrant inspection

34
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Which type of crack is considered the most severe in combustion chambers?

Stress rupture cracks

35
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What is the recommended method for reinstalling turbine blades after inspection?

Numbering the blades and reinstalling them in the same slots

36
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What is the flat rating of a turbine engine?

The guaranteed thrust under specific operating conditions

37
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Why is it important to monitor EGT during takeoff?

To prevent damage to the engine

38
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What is the purpose of the N1 indicator in a turbine engine?

To indicate engine speed

39
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Why is it impractical to measure turbine inlet temperature in most engines?

Because it is too hot

40
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Why are tachometers usually calibrated in percent rpm?

To make it easier to compare different types of engines

41
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What is the purpose of following manufacturer's operating instructions for starting and operating a turbine engine?

To avoid a hot or hung start

42
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What is the appropriate action to take in case of an engine fire during start or ground operation?

Move the fuel lever to the off position and continue cranking or motoring the engine until the fire has been expelled from the engine.

43
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How is the takeoff power for a turboprop engine calculated?

By determining the maximum allowable exhaust gas temperature and torquemeter pressure

44
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What is the purpose of a continuity check in an aircraft EGT circuit?

To eliminate any error caused by one or more inoperative aircraft thermocouples

45
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Why is regular testing and maintenance important for an EGT system?

All answers are correct;

To ensure the accuracy of the EGT indicator

To prevent potential errors in the system

To troubleshoot any issues that may arise

46
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An APU is usually rotated during start by?

An electric starter

47
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Fuel is normally supplied to an APU from

The airplanes main fuel supply

48
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Frequently, an aircraft auxiliary power unit (APU) generator

Is identical to the engine-driven generators

49
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Usually, the most load placed on an APU occurs when

The bleed air valve is opened

50
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Fuel scheduling during APU start and under varying pneumatic bleed and electrical loads is maintained by

Automatically by the APU fuel control system

51
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The function of an APU plenum is to

Stabilize the pressure before of the air before it enters the compressor

52
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Standard sea level pressure is:

29.92 in. Hg

53
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When in operation the speed of an APU

Remains at or near rated speed regardless of the load condition

54
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An APU uses aircraft fuel, supplied under pressure by

Electric boost pump

55
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An APU can provide redundancy to aircraft systems by

Providing a back up electrical and pneumatic source

56
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Where is the highest temperature in a turbine engine with respect to the metal parts?

Turbine inlet nozzle vanes

57
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What is the name given to the thermodynamic cycle of a APU gas turbine engine uses to produce electrical or pneumatic power?

Continuous combustion cycle

58
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T or F:
Compressor inlet screens are used on Turboprops and APUs to prevent all FOD from entering the intake of the engine

False

59
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T or F:
APUs are installed in the aircraft and are used to supply electrical power, air hydraulic pressure, and fuel to the aircraft engines when the main engines are not running.

False

60
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T or F:
APU’s are small gas turbine engines or reciprocating-engine that power a generator, hydraulic pump, and air pump.

True

61
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An APU can be operated:


Both A and B;
While the aircraft is in flight and While the aircraft is on the ground

62
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T or F:
An APU is usually manually controlled

False

63
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T or F:

An APU can only be operated while on the ground?

False

64
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An APU is usually rotated during start by:

An electrical starter

65
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Most APU’s have automatic controls for starting, stopping and maintaining operation within safe limits because:

They provide the correct sequencing of the start cycle

66
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Where is the highest gas pressure in a turbojet engine?

At the outlet of the compressor section

67
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The pressure of subsonic air as it flows through a convergent duct :

Decreases Pressure

68
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Name the four basic types of Combustion Sections used in aircraft turbine engines?

Can type, Reverse-flow type, Annular type and Can-annular type

69
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The exhaust section of a turbine engine is designed to

Impart a high exit velocity to the exhaust gases

70
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Using Standard Day Conditions, What is the standard sea level temperature?

59 degrees F

71
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Using Standard Day Conditions, What is the standard sea level pressure?

29.92 in. Hg

72
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What are the two types of compressors used in turbine engines?

Axial and centrifugal flow

73
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Where is the highest temperature in a turbine engine with respect to the metal parts?


Turbine inlet nozzle vanes


74
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What are the three types of turbine blades?

Impulse, reaction and impulse-reaction

75
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What is the name given to the thermodynamic cycle of a gas turbine engine to produce thrust?

Brayton cycle

76
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What is the effect of a blocked inlet screen on a turbine engine?


Decreased engine performance


77
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What is the function of a variable geometry inlet in a turbine engine?


 

To adjust the shape of the inlet for different flight conditions


78
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In which type of engine are inlet screens generally not used?


 

Turbofan engines with steel or titanium compressor blades


79
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What is the purpose of a compressor inlet screen?


 

To prevent FOD ingestion


80
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What is the main objective of a bellmouth inlet?


 

To obtain high aerodynamic efficiency


81
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What is the purpose of the inlet cowl on a turbofan engine?


 

To provide an airflow path into the engine


82
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What is the function of deflector doors in engine inlets?


 

To deflect ice and dirt away from the intake


83
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What is the primary source of thrust in a high-bypass engine?


 

The secondary airstream


84
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What is the function of the fan hub or spinner in a high-bypass engine?


 

To provide warm bleed air for anti-icing


85
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What is the function of the abraidable rub strip in a high-bypass engine?


 

To allow the fan blades to rub during flightpath changes


86
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What is the purpose of a cabin heater exhaust shroud?


 

To induce airflow through the exhaust ejectors


87
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What is the purpose of an exhaust system on a reciprocating engine?


 

To dispose of exhaust gases with safety


88
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Which type of exhaust system is typically used on modern aircraft?


 

Collector system


89
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What material is the exhaust collector ring typically made of?


 

Corrosion-resistant steel


90
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What is the purpose of the augmentor vane actuator on a radial engine?


 

To control vane positions


91
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What are the primary inspection areas of three types of exhaust systems?


 

Exhaust gas leakage, external surfaces, and internal baffles


92
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What is the importance of regular inspections for exhaust systems?


 

To prevent carbon monoxide hazards


93
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What is the best approach for inspecting an inaccessible component of an exhaust system?


 

Remove the component and check for leaks


94
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What are the potential consequences of using galvanized or zinc-plated tools on an exhaust system?


 

Cracks and eventual failure


95
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What is the purpose of a converging nozzle in a turboprop engine?


 

To increase the velocity of the exhaust gases


96
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What is the purpose of an insulating blanket on an exhaust nozzle assembly?


 

To shield the surrounding area from high heat


97
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What is the purpose of the convergent component of the exhaust nozzle?


 

To increase gas velocity


98
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What is the purpose of the exhaust nozzle in an aircraft engine?


 

To provide increased thrust


99
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What is the term used to describe the pressure difference between the inside of the nozzle and the ambient air?


 

Pressure thrust


100
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What is the purpose of locking the thrust reverser system in the stowed position?


 

To prevent deployment during maintenance