15.14 - Engine Indication systems Flashcards Preview

Mod 15: Engines > 15.14 - Engine Indication systems > Flashcards

Flashcards in 15.14 - Engine Indication systems Deck (21)
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1
Q

List the 6 primary engine indications displayed in the cockpit?

A
  • Engine Pressure Ratio
  • Engine Rotational Speeds (N, N2, N3 if applicable)
  • EGT (Exhaust Gas Temperature)
  • Fuel Flow
  • Engine Vibration
  • Engine Torque
2
Q

What is used to measure EGT for the purpose of temp indication?

A

Thermocouples made of chromel and alumel conductor wires.

3
Q

What is “EPR” and what does it measure?

A

Engine Pressure Ratio (EPR) measures engine power. It works on the basis that thrust is proportional to the energy rise when comparing intake pressure and turbine discharge pressure.

EPR = Tubrine Discharge pressure / Intake pressure

4
Q

What sensors are used to measure Engine Speed and briefly describe their principal of operation? (2 sensors)

A

Tachometer Generator – Used for older engines and consists of a three phase AC tachometer generator driven from an accessory gearbox fitted to the relevant spool. A synchronous motor driven indicator displays an analogue reading in the cockpit or frequency as a % of RPM in a ‘digital’ cockpit.

Magnetic Pickup (Phonic Wheel) – A single or double pole magnetic sensor where it’s magnetic field can be intercepted by a part of the rotating assembly such as fan blade tips can be utilised to measure RPM.

5
Q

Monitoring Engine temperature to determine engine performance is known as what kind of monitoring?

A

Condition or secondary monitoring.

6
Q

List the primary Engine instruments (6)

A
  1. Engine Pressure Ratio
  2. Engine Rotational speeds: - N, N2 (and N3 if used)
  3. Exhaust Gas Temperature
  4. Fuel Flow
  5. Engine Vibration
  6. Engine Torque
7
Q

List the secondary Engine instruments? (5)

A
  1. Oil Pressure
  2. Oil Temperature
  3. Oil Quantity
  4. Fuel Temperature
  5. Fuel Pressure
8
Q

What metals are EGT probes made from and what colour are their connections?

A

EGT probes are commonly referred to as ‘‘thermocouples’’

EGT probe consists of a thermocouple of chromel and alumel

Chromel is white

Alumel is green

9
Q

Where is EPR normally measured?

A

Pt2 probe or intake probe exists in fron of the intake ‘‘bullet’’

Pt7 probe or Turbine Discharge probe is located in a manifold just aft of the turbine final stage

Engine Pressure Ratio = Turbine Discharge Pressure / Intake pressure

10
Q

What type of sensor is normally used to measure oil temperature (what metal is used)?

A

The most common type of oil sensor is the Resistance Bulb.

Pure nickel is the metal used

(change in temp. = change in resistance)

is possible to use thermocouple - Iron and constantan

11
Q

On most oil pressure gauges what does the indicated pressure represent?

A

The difference between system vent pressure and main system pressure

12
Q

How are engine oil contents measured? (2 methods)

A

The Reed Switch Transmitter - A reference voltage, supplied by the EICAS computer, is applied across the switches and resistors. At least two or three switches will close at any one time as the height of the float varies with oil level.

The Variable Capacitance Transmitter - same principle as those located in aircraft fuel tanks - dielectric value of oil and air - capacitance

13
Q

How and why is fuel temperature measured?

A

Fuel temperature is measured by a temperature bulb (varying voltage which is read out)

Fuel temperature is measured to warn the operating crew of impending fuel filter blockage resulting from the formation of ice crystals in the fuel

14
Q

How is fuel pump tank pressure normally monitored?

A

a Simpe Pressure Switch is used

15
Q

How is fuel flow normally monitored? (2)

A
  1. The Synchronous Mass Flow Meter
  2. The Motorless Mass Flow Meter
16
Q

What two methods are used to monitor engine speed on N1 and N2?

A

N1 = Magnetic Pickup (Phonic Wheel) — (no convenient location for tachometer generator)

N2 = Tachometer Generator (N3 also included as both are core and have gearboxes)

17
Q

Define EIS, ECAM, EICAS?

A

EIS = Electronic Instrument System

ECAM = Electronic Centralized Aircraft Monitor

EICAS = Engine Indicating and Crew Alerting System

18
Q

What 2 types of devices are used to monitor engine vibration?

A
  1. The Sprung magnet type on older engines
  2. The piezo-electric type
19
Q

What devices are used to monitor engine vibration and where is it located?

is engine vibration primary or secondary instrumentation?

A

Devices to measure engine vibration:

  1. The sprung magnet type on older engines
  2. The piezo-electric type

The two pick-ups are located on the fan case and the other on the turbine case

Primary instrumentation

20
Q

Torque sensing systems are located where?

A

Teeth machined on the front end of both shafts are aligned at zero torque. When a torque load is applied to the inner shaft by driving a propeller, the inner shaft will twist through an angle proportional to the load. The outer shaft, being only connected at the rear, will not
twist as it is not subject to the load. The teeth on the inner shaft move out of alignment with the teeth on the outer shaft.

The electronic sensor can detect the angle of misalignment and convert it to a reading on the Flight Deck indicator.

21
Q

How is the power of an engine expressed?

A

Turboprop = engine RPM

Gas turbine engine = EPR or N1 depending on type of engine used