M15.14 Engine Indicstiing Systems Flashcards

1
Q

Types of engine indication

A
  • Performance indication
  • System indications
  • Engine trend monitoring
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2
Q

Methods of indirectly measuring thrust

A
  • N1 speed (fan)
  • EPR
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3
Q

What records the engine trend monitoring

A

ACMS

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4
Q

What three analyses are completed by engine trend monitoring

A
  • Thermodynamic analysis
  • Mechanic-dynamic analysis
  • Oil consumption analyses
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5
Q

What does thermodynamic analysis check

A
  • Pressure and temp along gas flow path
  • Feedback from VSVs and VBVs
  • Active clearance control
  • Fuel flow
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6
Q

What does the mechanical-dynamic analysis check

A

Mainly for failure in the rotor system (imbalances and bearing failures

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7
Q

Main parts of rotor speed indication

A
  • Sensor
  • Data transmission
  • Indication
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8
Q

N1 is what

A

LP

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9
Q

N2 is what

A

HP

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10
Q

How are engine rotor speeds expressed

A

As a percentage of the 100%design speed

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11
Q

Types of sensors that measure rotor speed

A
  • Variable reluctance type sensor
  • Tachometer generator type
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12
Q

Where is a tachometer generator type sensor usually located

A

In the gearbox

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13
Q

What converts a synchronous motor into a indication

A

Eddy current clutch

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14
Q

What sensor is normally used to measure N1 speeds

A

Variable reluctance speed sensor

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15
Q

Where is the variable reluctance speed sensor normally located

A

Positioned directly in line with the phonic wheel on the compressor shaft

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16
Q

Types of rotor speed indication

A
  • Display clock
  • Moving vertical bar
  • Electromechanical indicator
17
Q

What happens if the actual N1 speed exceeds the limit

A

Indications turn red along with audible warning via CWS

Can a,so be recorded in modern aircraft

18
Q

What happens after the N1 speed decreases below the allowed limit

A

Exceedence pointer records how much into overspeed it reached

19
Q

When the N1 indication is used to set the engine power what values appear on the indications

A
  • N1 limit
  • N1 CMD
  • Reference N1
20
Q

Where does EPR measure the pressure

A

Fan inlet and turbine outlet

21
Q

What calculates EPR in modern aircraft

A

FADEC

22
Q

With systems with FADEC what measures the pressure

A

Electronic pressure transducers

23
Q

Where is the highest temperature in the engine

A

Turbine inlet temp or TIT

24
Q

How is torque measured in turbo props

A

Hydraulic or electric torque meter

25
Q

How are thermocouples used to measure EGT connected

A

Parallel

26
Q

How is engine vibration indicated

A

Level of vibration (units 0 to about 6)

27
Q

How many vibration sensors on each engine and their locations

A

One in the compressor area (Near N1 rotor)
Second in the turbine area (Turbine frame)

28
Q

Types of accelerometers used in engines

A
  • Electromagnetic
  • Piezoelectric crystal
29
Q

What is the BB vibration signal

A

Unfiltered vibration signal from the aft sensor

30
Q

What basic law is used to measure fuel flow

A

F=MA (Newtons second law)

31
Q

How many magnets are in a modern fuel flow transmitter

A
  1. (2 on the drum and 2 on the impeller)
32
Q

Types of oil quantity transmitter

A
  • Capacitance type
  • Reed switch
33
Q

Types of oil pressure sensor

A
  • Bourdon tube
  • Strain gauge
34
Q

Types of oil temp indication

A
  • Thermocouple
  • Thermistor
35
Q

What is used to measure internal wear of lubricated engine components

A

SOAP (Spectrometric Oil Analysis Program)