M15.11 Flashcards

(55 cards)

1
Q

What is a rich blow out

A

If the quantity of fuel becomes excessive the limiting temperature of the turbine blades can be exceeded, or a compressor stall could occur

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2
Q

Gas turbine engine fuel control systems are generally divided into three categories:

A
  • Hydromechanical
  • Hydromechanical/electronic
  • Full Authority Digital Engine (or Electronics) Control (FADEC)
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3
Q

The hydromechanical/electronic fuel control is a hybrid of the two types of fuel control but can function solely as a hydromechanical control. In the dual mode, inputs and outputs are electronic, and fuel flow is set by

A

Servo motors

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4
Q

The FADEC-type control gives the electronic controller (computer) what type of control

A

Full control

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5
Q

What 2 sections do fuel controls have

A

Computing and metering

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6
Q

Does a hydro mechanical fuel system have any electronic interface in computing or metering fuel flow

A

A pure hydromechanical fuel control system has no electronic interface assisting in computing or metering the fuel flow. It is generally driven by the gas generator gear train of the engine to sense engine speed

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7
Q

What parameters do hydro mechanical fuel systems sense

A

compressor discharge pressure, burner pressure, exhaust temperature, and inlet air temperature and pressure

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8
Q

How is fuel metering achieved through a hydro mechanical fuel system

A

When the computing section determines the correct amount of fuel flow, the metering section through cams and servo valves delivers the appropriate quantity of fuel to the engine fuel system.

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9
Q

Is a hydro mechanical fuel delivery system as accurate as electric

A

No

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10
Q

Why is the fuel control unit sometimes mounted on the fuel pump

A

The fuel control unit is sometimes mounted on the vane fuel pump assembly. It provides the power lever connection and the fuel shut-off function. The unit provides mechanical overspeed protection for the gas generator spool during normal (automatic mode) engine operation.

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11
Q

What type of filter is fuel supplied through

A

A 200 micron inlet screen

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12
Q

Is the fuel manual mode solenoid valve energised or de energised in the automatic mode

A

The manual mode solenoid valve is energised in the automatic mode.

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13
Q

Fuel sub systems

A
  • Distribution
  • Control
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14
Q

LP fuel pump pressure

A

175psi

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15
Q

HO fuel pump max pressure

A

900psi at max power

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16
Q

Overpressure relief valve pressure

A

1250psi

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17
Q

Types of HP fuel pump

A
  • Gear type
  • Piston type
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18
Q

Most common type of fuel pump in turbofans

A

Gear type

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19
Q

Heat exchangers that can be found in the engine fuel system

A
  • Engine oil cooler
  • Servo fuel heater
  • IDG oil cooler
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20
Q

What prevents fuel leaks in the hot environment of the HPC and combustion case

A

Fuel lines protected by shrouds

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21
Q

Methods to protect the connections of fluid lines against leaks

A
  • Shrouded connections
  • Double sealed connections
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22
Q

Disadvantage of ding,e flow nozzles

A

Only has good atomisation at a small fuel flow range

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23
Q

How do we overcome the disadvantages of single flow nozzles

A
  • Having a primary and secondary set
  • Primary for start and idle
  • Secondary for max
24
Q

How are primary and secondary fuel nozzle usually supplied

A

Independent fuel manifolds

25
What do we use in modern engines in regards to fuel nozzles
Duplex fuel nozzles
26
What prevents residual fuel and carbon build up on duplex fuel nozzles
- Combustion airflow - Shut off valves
27
Can the air spray nozzle be a duplex type
Never
28
Why is the air spray nozzle always simplex
It can provide suffice t fuel at all speeds
29
Operating conditions important fuel metering
- Steady state - Transient
30
Fuel metering demand limits
- Over temp - Over speed - Compressor stall - Flame out
31
N2 speed for most engine idle
50-65%
32
How does the FCU switch minimum idle to approach idle
Air config via air-ground logic or other config switches
33
What is the N2 command signal
Signal from thrust lever to the FCU
34
Types of FCU
- Speed governed - Constant thrust FCU
35
What signals do hydro mechanical FCUs have
Hydraulic, mechanical and pneumatic
36
FCU major sections
- Metering - Power control - Engine protection
37
Where is the PMC (Power Management Computer) usually located
On the fan stator case of the engine
38
PMC function
Calculates required N1 based on throttle lever input
39
Where does the PMC send the control signal
Torque motor on the FCU if the required is different to the actual
40
FADEC
Full Authority Digital Engine Control
41
What is FADEC
Digital computer that has full authority over engine control functions
42
First and second main component of FADEC
1 - Digital computer 2 - FMU
43
Engines with FADEC do not have what component installed
Hydromechanical FCU
44
Typical FADEC systems have what components
ECU FMU Electrical sensor Control of other engine sub systems
45
How many ECU computers are there
2 which are A and B
46
How many sensors are at the T12 sensor
2 one for A and B ECU
47
What concerns pressure signals to electric signals
Pressure transducers
48
Power management calculates the thrust command based on what
- Thrust lever angle - Ambient air temp - Pressure such as T12 and Ps12
49
What does the FMU servo valve control
- VSV - VBV - HP and LP turbine clearance control valves
50
EIU
Engine Interface Unit
51
How many EIUs are there
One for each engine
52
What supplies the ECU with power
PMA
53
Advantage of EIU in a FADEC system
- Saves weight - Reduces risk of wiring faults
54
What is the only signal FADEC needs to operate
Trust Lever Angle
55
Can FADEC operate with out signals from the aircraft
Yes it only uses the additional signals to improve accuracy