TURBINE TEST Flashcards

1
Q

The primary purpose of an aircraft’s electrical ground is to:
Complete electrical circuit.
Electrically connect the aircraft to the fuel truck in order to prevent sparks from occurring when the truck’s fuel hose first comes in contact with the aircraft’s refueling port.
Dissipate electrical build-ups caused by the airframe interaction with clouds that would otherwise interfere with radio transmissions.
Act as an electrical shock absorber in the event of a lightning strike.
Incorrect

A

Complete electrical circuit.

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2
Q
The principle that fluids are flexible but non-compressible is the basis for which major aircraft system?
  The engine fuel system.
  The hydraulic system.
  The engine lubrication system.
  The pneumatic system.
A

The hydraulic system.

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3
Q

The exhaust section of a turbine engine is designed to:
Impart a low pressure.
Impart a high exit velocity to the exhaust gases.
Impart a low exit velocity.
Reduce pressure and temperature.

A

Impart a high exit velocity to the exhaust gases.

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4
Q

The primary purpose for utilizing boost pumps in the fuel system is to:
Provide a positive fuel flow to the engine driven fuel pump.
Provide fuel transfer between tanks to maintain an optimum C.G. position.
Provide fuel transfer between tanks to prevent a fuel imbalance.
Prevent unporting of fuel on takeoff.

A

Provide a positive fuel flow to the engine driven fuel pump.

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5
Q
The highest heat-to-metal contact in a jet engine is the:
  Compressor section.
  Turbine inlet guide vanes.
  Exhaust section.
  Inlet section.
A

Turbine inlet guide vanes.

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6
Q

If the RPM of an axial-flow compressor remains constant, the angle of attack of the rotor blades can be changed by:
Raising temperature.
Changing the velocity of the airflow.
Changing pressure of the airflow.

A

Changing the velocity of the airflow.

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7
Q
Flight at 0g would most adversely affect what aircraft system?
  Hydraulic
  Electrical
  Fuel
  Engine lubrication
A

Hydraulic

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8
Q

What is an advantage of having generators running in parallel?
The system voltage can be increased.
AC power is more easily converted to DC power.
They can share electrical loads.
Constant speed drives can be taken offline to extend their service lives.

A

They can share electrical loads.

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9
Q

Which are protective functions of an AC generator control unit?
Under voltage, differential fault, and manual paralleling.
Overvoltage, current limiting, and generator overspeed.
Generator underspeed and bus-tie circuit-breaker automatic closing.
Overvoltage, current limiting, and generator underspeed.

A

Overvoltage, current limiting, and generator overspeed.

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10
Q

When the aircraft is shut down after flight, what is the typically used to maintain pressure for the parking break?
The hydraulic accumulator.
The hydraulic fuse.
The hydraulic reservoir.
The in-line variable restrictor orifice.

A

The hydraulic accumulator.

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11
Q

A cool-off period prior to shutdown of a turbine engine is accomplished in order to:
To allow for free rotation.
Allow the turbine wheel to cool before the case contracts around it.
To allow for lubrication coating.

A

Allow the turbine wheel to cool before the case contracts around it.

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12
Q
The purpose of a constant speed drive for an AC generator is to:
  Regulate generator voltage.
  Control field strength.
  Regulate generator current.
  Maintain a uniform frequency.
A

Maintain a uniform frequency.

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13
Q

The non-rotating axial-flow compressor airfoils in an aircraft gas turbine engine, are called
Compressor vanes.
Stator vanes.
Guide Vanes.

A

Stator vanes.

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14
Q

An advantage of a hydraulic powered flight control system over a manual control system is:
Immunity from power failures.
Feedback in controls.
Ease in moving large control surfaces.
Ability to operate outside the flight envelope

A

Ease in moving large control surfaces.

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15
Q

The purpose of a diode is to:
Allow electricity to flow in only one direction.
Act as an electrically operated switch.
Convert AC to DC.
Amplify current.

A

Allow electricity to flow in only one direction.

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16
Q
What increases or decreases the voltage of a generator so it carries its share of the load?
  Current limiter.
  Paralleling circuit.
  Constant speed drive.
  Reverse current cut-out relay.
A

Paralleling circuit.

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17
Q

The stator vanes in an axial-flow compressor:
Convert velocity energy into static pressure energy.
Converts pressure energy into velocity energy.
Convert pressure into higher temperatures.

A

Convert velocity energy into static pressure energy.

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18
Q
Between each row of rotating blades in a turbine engine compressor, there is a row of stationary blades which act to diffuse the air. These stationary blades are called-
  Diffusers.
  Compressors.
  Guide vane sections.
  Stators.
A

Stators.

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19
Q

Why are hydraulic reservoirs pressurized?
To assure a positive feed of foam-free fluid to the hydraulic pump at high altitudes.
To provide an alternate source of pressure in case of hydraulic pump failure.
To insure an adequate supply of fluid to the hydraulic pump inlet during negative-G flight.
To provide an alternate source of hydraulic fluid in the event a hydraulic becomes clogged.

A

To assure a positive feed of foam-free fluid to the hydraulic pump at high altitudes.

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20
Q

The purpose of hydraulic accumulator is to:
Filter debris and remove air.
Compensate for potential loss of pressure at high altitudes.
Maintain Fluid pressure and supply fluid under high demand.
Supply hydraulic fluid for normal operations under low demand.

A

Maintain Fluid pressure and supply fluid under high demand.

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21
Q

Your ammeter pointer display a positive indication. What information does this provide to the pilot?
The amount of charging current demanded by the battery.
The battery is fully charged.
More current is being drawn from the battery than is being replaced.
The charging rate of the battery.

A

The charging rate of the battery.

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22
Q

The primary purpose of the fuel-oil heat exchange is to:
Heat the fuel to prevent clogging the transfer lines.
Heat the fuel to prevent ice crystals from clogging fuel filters.
Cool the oil prior to be it being released in to the shafts’ bearing assembly.
Cool the entire oil system oil system in order to keep it within operating limitations.

A

Heat the fuel to prevent ice crystals from clogging fuel filters.

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23
Q

Why do some turbine engines have more than one turbine wheel attached to a single shaft?
To extract more temperature from exhaust gases.
To reduce velocity flow.
To increase pressure.
To extract more power from the exhaust gases than a single wheel can absorb.

A

To extract more power from the exhaust gases than a single wheel can absorb.

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24
Q

Kerosene is used as turbine engine fuel because:
Kerosene has a very high volatility which aids in ignition and lubrication.
Kerosene has more heat energy per gallon and lubricates fuel system components.
Kerosene is not susceptible icing at high altitude.
Kerosene does not contain any water.

A

Kerosene has more heat energy per gallon and lubricates fuel system components.

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25
Q

In an axial-flow compressor, one purpose of the stator vanes at the discharge end of the compressor is to
Increase temperature.
Straighten the airflow and eliminate turbulence.
Reduce temperature.
Increase pressure.

A

Straighten the airflow and eliminate turbulence.

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26
Q

One of the most important characteristics of hydraulic fluid is that it cannot be:
Corrosive.
Harmful while coming into contact with human skin.
Susceptible to vaporization.
Capable of breaking down insulation on electrical wires.

A

Susceptible to vaporization.

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27
Q

A turbine engine hot section is particularly susceptible to which kind of damage?
Cracking/Creep.
Swelling.
Burnout.

A

Cracking/Creep.

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28
Q
Which of the following engine variables is the most critical during turbine engine operation?
  Turbine inlet temperature.
  Turbine velocity.
  Turbine pressure.
  Exhaust velocity.
A

Turbine inlet temperature.

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29
Q
The stators in the turbine section of a gas turbine engine:
  Increases pressure.
  Increase the velocity of the gas flow.
  None of the above.
  Decreases temperature.
A

Increase the velocity of the gas flow.

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30
Q

What would be the indication of an impending constant speed drive failure?
Increased static in headset.
Intermittent “Off” flags in flight instruments.
Large voltage variations.
Large frequency variations.

A

Large frequency variations.

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31
Q

Newton’s First Law of Motion, generally termed the Law of Inertia, states:
Everybody persists in its state of rest, or of motion in a straight line, unless not acted upon by some outside force.
Everybody persists in its state of motion, or of motion in a straight line, unless acted upon by some outside force.
Everybody persists in its state of rest, or of motion in a straight line, unless acted upon by some outside force.

A

Everybody persists in its state of rest, or of motion in a straight line, unless acted upon by some outside force.

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32
Q
How are airplane AC generators rated?
  Volts
  Kilovolt-amps (KVA)
  Amps
  Kilowatts (KW)
A

Kilovolt-amps (KVA)

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33
Q
The purpose of a transformer-rectifier (TR) is to:
  Convert AC generator output to DC.
  Step down DC voltage to a lower value.
  Step down AC voltage to lower value.
  Convert DC generator output to AC.
A

Convert AC generator output to DC.

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34
Q

The primary reason for using crossfeed fuel system is to:
Allow fuel to be used for ballast when needed.
Be able to purge any fuel tank.
Help maintain aircraft center of gravity.
Jettison fuel during emergencies.

A

Help maintain aircraft center of gravity.

35
Q
What is the primary factor which controls the pressure ratio of an axial-flow compressor?
  Combustion Temperature.
  EGT.
  Airspeed.
  Number of stages in compressor.
A

Number of stages in compressor.

36
Q

Anti-icing of jet engine air inlets is commonly accomplished by-
Engine bleed air ducted through the critical areas.
Compressor air ducted within the engine.
Static air ducted through critical areas.

A

Engine bleed air ducted through the critical areas.

37
Q

A major advantage of ni-cad batteries over lead-acid batteries is that ni-cad batteries:
Are less expensive.
Do not need to be deep-cycled for optimal performance.
Are not subject to thermal runaway.
Put out sustained voltage over a longer period of time.

A

Put out sustained voltage over a longer period of time.

38
Q
What electrical device is used to convert Alternating Current to Direct Current?
  Battery relay.
  Static inverter.
  Rectifier.
  Capacitor.
A

Rectifier.

39
Q
What electrical device is used to convert Direct Current from a battery to Alternating Current?
  Capacitor
  Batter relay.
  Static inverter.
  Rectifier.
A

Static inverter.

40
Q

Which is not typical cause of compressor stalls?
Unstable airflow at the engine inlet.
Fuel starvation.
Low airspeed/high thrust power settings.
Mechanical malfunctions.

A

Fuel starvation.

41
Q

In a dual axial-flow compressor, the first stage turbine drives
N(1) Compressor.
N(2) compressor.
Low pressure compressor.

A

N(2) compressor.

42
Q
Mixing aviation gasoline with jet fuel will affect a turbine power plant by forming on the:
  Turbine blades.
  Compressor blades.
  Inlet guide vanes.
  Fan blades.
A

Turbine blades.

43
Q
The purpose of a transformer is to:
  Convert DC power to AC power.
  Step AC system voltage down.
  Convert DC power output to AC.
  Convert AC generator output to DC.
A

Step AC system voltage down.

44
Q

A gas turbine engine comprises which three main sections?
Turbine, compressor, and combustion.
Compressor, Inlet, and exhaust.
Compressor, exhaust, and combustion.

A

Turbine, compressor, and combustion.

45
Q
What device maintains a generator’s frequency?
  Reductions gears.
  Voltage regulator.
  Transformer rectifier.
  Constant speed drive.
A

Constant speed drive.

46
Q

The compression ratio of an axial-flow compressor is a function of the
Combustion.
Number of compressor stages.
Velocity.

A

Number of compressor stages.

47
Q

The air passing through the combustion chamber of a turbine engine is:
Used only for combustion.
Used only for thrust production.
Used to support combustion and to cool the engine.

A

Used to support combustion and to cool the engine.

48
Q

What is the proper starting sequence for a turbojet engine?
Air, Fuel, Ignition.
AIr, ignition, fuel.
Fuel, Ignition, Air.

A

AIr, ignition, fuel.

49
Q

EPR is the:
Inlet pressure divided by the outlet.
Engine outlet pressure divided by the inlet pressure.
Engine pressure ratio divided by the velocity.

A

Engine outlet pressure divided by the inlet pressure.

50
Q
At what stage in a turbine engine are gas pressures the greatest?
  Compressor inlet.
  Compressor outlet.
  Exhaust.
  Combustion chamber.
A

Compressor outlet.

51
Q
What is the primary advantage of an axial-flow compressor over a centrifugal compressor?
  Greater pressure ratio.
  Lower compression.
  Greater Velocity.
  Greater temperature range.
A

Greater pressure ratio.

52
Q

What is the major function of the turbine assembly in a turbojet engine?
To diffuse air pressure.
To increase temperature in combustion section.
To increase airflow velocity.
Supplies the power to turn the compressor.

A

Supplies the power to turn the compressor.

53
Q

What’s the hottest section of a turbine engine?

A

What’s the hottest section of a turbine engine?

•The turbine section. Its also the same section where the TIT information is coming from.
LETS TAKE IT FROM THE HOTTEST

54
Q

Which section has the greatest pressure?

A

•Compressor section.

55
Q

What does EPR measure?

A

Know the difference. The answer is the outlet pressure divided by the inlet pressure. NOT THE OTHER WAY AROUND!!!

56
Q

Which section experiences the highest velocity?

A

The exhaust

57
Q

What does the turbine section provide?

A

•Rotation to the compressor and accessory section drive

58
Q

Turbine engine are best at____ rpm and ____ airspeed

A

high

high

59
Q

What is the purpose of a diffuser?

A

•The divergent duct shape converts most of the air’s velocity into static pressure.

60
Q
  1. What are the two basic sections of a turbine engine?
A
  1. What are the two basic sections of a turbine engine?

The hot section and the cold section.

61
Q
  1. What are the two basic types of compressors that are used in aircraft turbine engines?
A

Axial-flow and centrifugal.

62
Q
  1. What is the purpose of the stators in an axial-flow compressor?
A

The stators convert some velocity energy into pressure energy and change the direction of the air so it is proper for the next stage of rotors.

63
Q
  1. What are three types of combustors used on aircraft turbine engines?
A
  1. Can-type
  2. annular-type and
  3. can-annular-type.
64
Q
  1. How many igniters are there normally in an aircraft turbine engine?
A

Two.

65
Q
  1. What is the main purpose of the turbine nozzle in an aircraft turbine engine?
A

The turbine nozzle directs the hot gases as they leave the combustors so they will turn the turbine wheel with maximum efficiency.

66
Q
  1. What is meant by a free-turbine turboshaft engine?
A

A turboshaft engine that has a turbine wheel or stage of turbine wheels that is not used to drive the compressor of the gas generator section of the engine. This free turbine drives the propeller in a turboprop engine or the transmission and rotor of a helicopter.

67
Q
  1. Why do some axial-flow turbine engines have more than one set of turbines and compressors?
A

A two-spool turbine engine has a low-pressure and a high-pressure compressor each driven by its own turbine. The two independent systems operate at the speed at which they are most efficient.

68
Q
  1. What kind of bearings are used to support the rotor shaft of an aircraft turbine engine?
A

Anti-friction bearings such as ball bearings or roller bearings.

69
Q
  1. What is meant by a turbofan engine?
A

An axial-flow turbine engine in which the first stage of compressor blades are lengthened so they can force air around the outside of the gas generator portion of the engine.

70
Q
  1. Where can you find the limits of repair allowed for the compressor blades of an aircraft turbine engine?
A

In the FAA-approved service manual issued by the manufacturer of the engine.

71
Q
  1. Why is it important that a turbojet engine be allowed to cool before it is shut down after it has been operated at a high power setting?
A

If the engine is shut down while it is hot there is a possibility that the shroud will contract around the turbine wheel and seize the rotor.

72
Q
  1. What is meant by a hung start in a turbine engine?
A

A start in which ignition occurs but the engine does not accelerate to a self-sustaining speed.

73
Q
  1. What is meant by a hot start in a turbine engine?
A

A start in which ignition occurs but the internal temperatures go high enough that they can damage the engine.

74
Q
  1. What is meant by creep of the turbine blades?
A

A condition of permanent elongation of the turbine blades. Creep is caused by the high temperatures and the high centrifugal loading imposed on the blades.

75
Q
  1. How is the compressor of a turbine engine cleaned?
A

An emulsion-type cleaner is sprayed through the engine while it is being motored by the starter or operated at a low speed. The wash is followed by a clean water rinse.

76
Q
  1. Where is water injected into a turbine engine for cooling purposes?
A

Into the compressor inlet and into the engine diffuser case.

77
Q
  1. At what point in a turbine engine is the temperature the highest?
A

At the inlet to the high-pressure turbine.

78
Q
  1. What is the function of the interconnect tubes between the cans of a turbine engine that uses can-type combustors?
A

These tubes allow the flame to travel from the cans that contain the igniters to all of the other cans when the engine is being started.

79
Q
  1. What are two types of thrust reversers that are used on turbojet engines?
A

The mechanical blockage-type and the aerodynamic blockage-type.

80
Q
  1. What is meant by trimming a turbojet engine?
A

Adjusting the fuel control to get the correct idling and maximum-thrust RPM

81
Q

Of the listed items which one is not typically found in an accessory drive?

A

?

82
Q

Which is not found within an accessory drive component?

A

?

83
Q

Which turbine section powers the accessory drive?

A

HIGH PRESSURE TURBINE

84
Q

What is the the purpose of an accessory drive?

A

The accessory drive is a gearbox that forms part of a gas turbine engine.Although not part of the engine’s core, it drives the accessories, fuel pumps etc., that are otherwise essential for the operation of the engine or the aircraft on which it is mounted. Accessory drives on large engines handle between 400–500 hp It provides space for the mounting of accessories necessary for operation and control of the engine.