14 - Engine Indication System Flashcards

1
Q

Where is the TIT located

A

Directly behind combustion chamber

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2
Q

What is the term for the highest tempreature location

A

Turbine Inlet Tempreature (TIT)

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3
Q

What tempreatures can the TIT reach

A

1400°C

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4
Q

Where is exhaust gas measured

A

Between high and low pressure turbine or directly behind the low pressure turbine

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5
Q

What are exhaust gas tempreature ranges

A

600°C - 900°C

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6
Q

What do the EGT sensors use

A

Thermocouples

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7
Q

What is the tempreature range of the EGT indiactor

A

0°C - 1200°C

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8
Q

What three groups can engine indications be classes

A

Performance/primary - Monitor performance and limits, set thrust in flight phases

System/secondary - Monitor fuel, oil malfunctions

Engine trend - Uses ACMS to identify faults on ground

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9
Q

What two values are useed to determine engine thrust

A

Fan speed (N1) and engine pressure ratio (EPR)

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10
Q

What is shown in engine system indications

A
  • Oil quantity
  • Oil pressure
  • Oil tempreature
  • Engine vibration
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11
Q

What three analysis’ are performed in engine trend monitoring

A
  • Thermodynamic analysis (gas flow pressure and tempreature)
  • Mechanic-dynamic analysis (rotor system)
  • Oil consumption analysis (oil consumption rate)
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12
Q

What is used for EPR measurement

A

Engine turbine discharge pressure and engine ram air inlet

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13
Q

What do the red/amber lines indicate for EPR

A

EPR max

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14
Q

What does the blue circle indicate for EPR

A

Actual throttle position

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15
Q

What are the two main types of oil gauges

A
  • Bourdon type
  • Strain
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16
Q

Briefly explain the Bourdon gauge

A

C or helical shaped with oval cross section, pressure in the tube acts to change to a circular cross section, this distortion moves an indicator

17
Q

What is th