M15.14 Engine Indication Systems Flashcards

1
Q

Why do we require exhaust gas temperature (EGT) indication?

A

To monitor temps experienced by the turbine engines to prevent thermal damage and indicate when a limit is exceeded

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2
Q

What is the temperature called where the hot gas hits the high pressure turbine?

A

Turbine inlet temperature (TIT)

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3
Q

What is the temperature called where the hot gas hits the high pressure turbine?

A

Turbine inlet temperature (TIT)

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4
Q

Where is the exhaust gas temperature indicator?

A

In the flight deck

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5
Q

What temperature does the EGT show?

A

The average temperatures measured by the individual thermocouples

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6
Q

The EGT indicator is in what type of unit?

A

Hermetically sealed unit

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7
Q

What do the sets of thermocouples do for the TIT?

A

One set is paralleled to transmit signals to the flight deck indicator
The other set provides temperature signals to engine monitoring and control systems

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8
Q

Three groups of engine indications?

A

Performance indications
System indications
Engine trend monitoring

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9
Q

What are system indications?

A

Also called secondary indications
Used to monitor the operation of engine systems such as oil and fuel
Detect malfunctions quickly

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10
Q

What is engine trend monitoring?

A

Uses engine parameters that are automatically recorded by the aircraft condition monitoring system (ACMS)

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11
Q

What two values are used to measure thrust?

A

The rotational speed of the fan (N1)
The engine pressure ratio (EPR)

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12
Q

The engine system indications monitor what systems?

A

Oil quantity
Oil pressure
Oil temperature

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13
Q

What type of warnings would appear on ECAM detected by the engine system indications?

A

When an indication exceeds a limit
When the system detects low pressure
When a filter becomes clogged
When an unlocked thrust reverser is detected

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14
Q

Three types of engine trend monitoring analysis?

A

The thermodynamic analysis
The mechanic- dynamic analysis
The oil consumption analysis

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15
Q

The engine pressure ratio (EPR) indicator gauge compares what?

A

Engine turbine discharge pressure to the pressure of the ram air at the inlet of engine

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16
Q

How is EPR determined?

A

Pressure measurements taken by probe installed in engine inlet and turbine exhaust

17
Q

Two displays on EPR display?

A

Amber or red line that shows maximum available thrust
Blue line that shows the actual throttle position

18
Q

What is FLEX?

A

An Airbus setting for the standard take off thrust setting.
Used to preserve engine wear and prolong engine life

19
Q

Two main types of oil pressure transmitters?

A

The bourdon tube type
The strain gauge type

20
Q

Strain gauges are often used in what type of circuit?

A

Wheatstone bridge circuit

21
Q

If the oil pressure decreases below a limit what does the low oil pressure switch do?

A

The switch closes and a signal is sent to the flight warming computer and a warning message appears on the display unit in the flight deck

22
Q

An oil inlet temperature indicator is used to indicate what?

A

Indicates the temperature of the oil as it enters the oil pressure pump

23
Q

How does the oil temperature sensor work?

A

Designed to respond to changes in temperature and convert them into an electrical signal

24
Q

Does fuel pressure require a warning if it falls outside normal operating range?

25
Q

The fuel flow indicating system provides what two different indications to the flight crew?

A

The actual fuel flow to the engines
The fuel used since the engine was started

26
Q

3 parts of rotor speed indication?

A

The sensor
The data transmission
The indication

27
Q

Two types of sensors to measure rotor speed on engines?

A

Variable reluctance type sensor
Tachometer generator type- located in gearbox

28
Q

What is a tachometer generator?

A

Has a permanent magnet that is driven by the gearbox
Driven at a speed proportional to the n2 rotor speed.

29
Q

Where does the tachometer generator send the 3 phase AC voltage to?

A

FADEC computer

30
Q

Three types of rotor speed indications?

A

Display with clock type scale
Display with moving vertical bar
The classical electromechanical indicator

31
Q

On modern engines, if the engine speed exceeds the n1 redline, what happens?

A

The duration of the overspeed and the speed are recorded and reported to the engine trend monitoring

32
Q

Main parts of engine vibration monitoring system?

A

The indication in the flight deck shows the level of vibration
One or two vibration sensors
Computer collects and filters vibration data for indication and trend monitoring

33
Q

What are the engine vibration sensors?

A

Accelerometers that measure radial acceleration of the rotor system

34
Q

Where are the two engine vibration sensors located on the engine?

A

One in the compressor area, near the N1 shaft
Second sensor is in the turbine area

35
Q

Two types of accelerometers?

A

Electromagnetic accelerometer
Piezoelectric crystal type sensor

36
Q

What is vibration indication on modern aircraft automatically controlled by?

A

The engine vibration monitoring unit

37
Q

A typical electrical torque meter system consists of what?

A

A torque meter assembly, a phase director and an indicator