Airframe Fuel Systems Flashcards

(95 cards)

1
Q

What are the two categories of aviation fuels?

A

Aviation Gasoline (AVGAS)
Aviation Turbine Fuel (AVTUR)

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2
Q

Which fuel is used for piston engine aircraft?

A

AVGAS

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3
Q

Which fuel is used for Gas turbine aircraft?

A

AVTUR

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4
Q

Whats calorific value?

A

Amount of heat released when a unit mass of fuel is burned and measured in heat units (KJ)

The higher the calorific value, the more efficient the fuel

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5
Q

Whats volatility?

A

The tendency of a substance to evaporate at normal temperatures.

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6
Q

What kind of volatility is needed in aircraft fuel?

A

Volatile enough to start the engine but not so volatile that fuel is lost from tanks due to vaporisation

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7
Q

Whats specific gravity?

A

Used to define weight or density of a liquid compared to an equal quantity of water

Water has a S.G. of 1.0

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8
Q

Four types of approves fuels?

A

AVTUR
AVTAG
AVCAT
AVGAS

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9
Q

Whats AVTAG?

A

A wide-cut fuel (blend of gasoline and kerosene)

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10
Q

Whats AVCAT?

A

Kerosene type fuel similar to AVTUR but with a higher flashpoint, used by Royal Navy on ships

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11
Q

Whats the fuel anti-icing additive called?

A

Fuel system Ice Inhibitor (FSII)

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12
Q

Two aircraft systems that contain fuel?

A

Airframe Fuel System (Storage)
Engine Fuel System (for ignition)

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13
Q

Design objectives of fuel systems?

A
  • Facilitate rapid and safe fuel replenishment
  • flexibility to provide different ranges & endurance for operational requirements
  • auto or semi-auto control & management of fuel system
  • Tolerance to aircraft manoeuvre or damage
  • secondary uses for fuel
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14
Q

Where is fuel usually stored on aircraft?

A

Wings & centre fuselage

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15
Q

Where are fuel tanks usually on helicopters?

A

Beneath cabin floor or to increase range tanks can be installed in aircraft cabin

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16
Q

Types of fuel tanks?

A

Rigid
Integral
Flexible

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17
Q

Whats the point of a press stud fitting on a bag tank?

A

To attach the bag to the aircraft structure and allow the weight of the bag tank to be carried by the structure of the aircraft

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18
Q

How do self sealing coverings work on a bag tank?

A

When punctured the fuel leaks out and instantly causes a swelling reaction either the rubber which causes swelling and blocks the hole

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19
Q

Why do we need a collector tank?

A

So theres a constant flow of fuel to the engine, regardless of aircraft manoeuvres, collector tank always full

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20
Q

Why do high altitude aircraft need high pressure fuel tanks?

A

Increased altitude decreases boiling temperature of liquids causing an increase in fuel vapours and risk of fire etc.

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21
Q

Whats the purpose of tank pressurisation?

A

To maintain the pressure of the air above the fuel at an appropriate level

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22
Q

How does an air/no fuel valve work?

A

In inverted flight, gravity pushes the float and ball into place to prevent fuel loss

In nose up attitude, the float rises with the fuel and prevents fuel loss

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23
Q

Advantages of pressurising a fuel tank?

A

Transferring fuel between tanks using air pressure

Prevents excessive fuel vapour by increasing boiling point of fuel

Less of a fire risk

Maintains shape of flexible tanks

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24
Q

Disadvantages of pressurising a fuel system?

A

Added weight

Routing complexity

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25
Whats a pressure reducing valve?
Senses changes in atmospheric pressure and opens/closes to allow air from engine into pressurised tanks to moderate system pressure
26
Whats an outward relief valve?
Spring loaded valve that opens if tank pressure reaches highest system limit to prevent damage
27
Whats an inward relief valve?
Spring loaded valve forced open by atmospheric pressure when it becomes higher than tank pressure to prevent cavitation
28
Whats a vent valve?
To depressurise tanks (during and before refuelling)
29
Whats a Pressure switch for?
Provides electrical signal to cockpit warning indicator of low tank pressure Prevents excessive
30
Whats APU stand for?
Auxiliary power units
31
Whats used to ensure a positive supply of fuel to the engine regardless of aircraft attitude?
Booster pumps (positioned in a sump)
32
What must be carried out after disturbing any NRV in fuel system?
A mandatory flow check
33
What an LP Fuel Cock for?
Separates the airframe fuel system from the engine fuel system (full flow or no flow)
34
Why should you only shut down an engine using an LP Fuel cock in emergencys?
It can damage the engine components and pipe
35
Whats a Fuel cooled oil cooler (FCOC)?
Hot oil is cooled as it flows around a series of small pipes carrying cool fuel. The temperature increase of fuel will prevent any icing.
36
Whats an Air cooled fuel cooler (ACFC)?
Cooling fuel by using ram air similar to car radiator
37
Ejector (jet pump) purpose?
A tube with a decreased cross sectional area creates a drop in pressure to suck the cold fuel into the tube to mix with the hot fuel before returning to storage
38
Methods of transferring fuel between tanks
Air pressure (tank 1 to 2) Electric transfer (tank 2 to 3) Fuel ejectors (tank 3 to 4) Gravity (tank 4 to 5)
39
Whats are the purposes of fuel management and control system?
Maintain CoG by managing transfer Provide indications of various parameters and warnings of malfunctions Give crew various options in movement of fuel and to counter any system malfunctions
40
Whats are the purposes of fuel management and control system?
Maintain CoG by managing transfer Provide indications of various parameters and warnings of malfunctions Give crew various options in movement of fuel and to counter any system malfunctions
41
Automatic control of fuel system?
System design/ layout Electrical components Mechanical components
42
Fuel flow proportioners
Empties different sized tanks at proportional speeds to maintain CoG by using larger and smaller proportioner cell
43
Whats a fuel dump (Jettison) for?
Aircraft max permissible take off weight is higher than landing weight so they dump fuel to drop weight
44
What can the fuel gauging system provide?
Total fuel system counts Contents of individual tanks or group of tanks Amount of fuel being used at any given time
45
Two types of fuel contents transmitters
Float type fuel contents transmitter Capacitance gauging units (inner/outer conductive plates)
46
Why is it important to know Engine fuel flow?
To estimate range and duration of flight, higher than normal flow will indicate a problem with engine performance
47
Fuel flow transmitter purpose?
Measures the flow of fuel after the LP cock, senses volume flow rate and transmits to the cockpit
48
What causes the love fuel level warning light to turn on?
The fuel reaches a predetermined low level in the tank and energises the switch
49
What are 3 types of manual fuel level measurements for ground use?
Dipstick Drip stick Drop stick
50
When checking for contaminants in aviation fuel, how should the fuel appear?
Clear, bright, no detectable free water or significant visible solid matter
51
What should you do if a BFI is suspected of being contaminated?
All aircraft refuelled from suspect source should be placed unserviceable and inspected (Bulk Fuel Installation)
52
What are the principal contamination threats for fuel?
Foreign particles Water (suspended/free) Microbiological organisms Cross contamination
53
Whats the purpose of a water sediment check?
To check for contamination of fuel with water (microbes in fuel cannot grow without water)
54
What does microbes in fuel eventually create with the presence of water?
Scums and sludges (biomass) Surface scum (biofilm)
55
How is a water sediment check carried out?
Sample drained from a valve at bottom of tank Visual check for water/fuel separation (cloudy is a water/fuel emulsion) Water detection capsules detect dissolved water (yellow detection paper, turns blue if too much water)
56
When must a fuel system be tested?
After being disturbed by removal or fitting of any system components Leak checks Fuel flow test
57
What is required in a fuel system check?
Leak check while system is pressurised Fuel flow test to ensure minimum fuel flow rate is being delivered to the engine (tested by an authorised person)
58
Why would a leak be greater during flight?
Due to flexing of the aircraft structure
59
How do you repair a leaky rigid tank?
Removal for specialist repair
60
How are leaky flexible tanks repaired?
Repair by manufacturer (tank replacement usually inevitable)
61
What is the leak rate of a flexible tank affected by?
Cavity drain blockage Tank being plugged by contact with aircraft structure Self sealing layer activation Fuel tank level Aircraft attitude Tank pressurisation
62
How are leaky integral tanks repaired?
Categorisation and subsequent repair is carried out in accordance with the AMM
63
Whats preparation draining?
Fuel system drained, pockets of duel removed by mopping with fluff free absorbent material
64
Whats venting?
Clearing the explosive fumes from a fuel tank using an induced warm airflow to blow the vapours out through open panels.
65
Whats to be considered for inspection lamps inside or near a fuel tank?
An explosion proof light needs to be used
66
How can personnel protect themselves from solvents and fuels?
Avoid breathing fumes given off by fuels and solvents Protect the skin by wearing approved protective clothing and barrier cream
67
What PPE is needed in a Fuel tank?
Rubber overalls, rubber boots, rubber gloves, special head gear, Respirator
68
What conditions must be met before an operator enters a fuel tank?
Medically examined Remote intake breathing apparatus Intake free end of respirator upwind of fuel tank Correct PPE worn and lifeline attached Correct Fire extinguishers ready for use Second person as observer outside the tank Time in the tank controlled to adhere to guidelines
69
Two methods of ground refuelling?
Open line refuelling (gravity) Pressure refuelling
70
What method of ground refuel is used on smaller aircraft?
Open line refuel (low pressure) Used on motor vehicles
71
Whats the purpose of pressure refuelling?
To uplift large volumes rapidly, cleanly and with minimal risk of spillage
72
Why is the pressure for defuelling lower than refuelling?
To avoid damage to aircraft structure, suction pressure is lower at defuel
73
What is a risk of open line defuel?
The walls of a flexible tank being sucked into nozzle
74
Three methods of ground defuel
Pressure defuel Open line defuel Drain defuel
75
Whats minimum PPE to be worn for general fuelling operations?
Safety boots Coveralls Gloves Goggles or visor
76
What should you do in event of fuel spillage during refuelling?
Stop refuelling until cleaned up
77
When are liquid oxygen (LOX) systems not to be replenished?
During fuelling operations
78
Bonding requirements during fuelling operations
Ensure aircraft and bowser are earthed
79
What is needed for refuelling to take place in a hangar?
- Authorised - Adequate ventilation - High- volume firefighting vehicle in attendance - suitable towing equipment incase anything goes wrong - fuel bowser located outside - clearly defined escape route
80
Classifications for Ice
Trace - not hazardous unless its been accumulating for up to a period of 1 hour Light - built up icing that can be readily removed by ice protection equipment used periodically Moderate - hazardous, builds up quickly, removed by constant use of ice protection equipment used Severe - most hazardous, should not fly in these considerations, ice protection equipment may fail/malfunction
81
What are critical areas of an aircraft in relation to icing?
Aerofoil surfaces Engine intakes and internal surfaces Rotor blades and propellers Windscreens/canopies Pitot probes and static vents Control surfaces Weapons and weapon carriers
82
Hazards of Ice on aircraft
Increase in stall speed Increased landing speed and distance Hampers true instrument readings Adverse effects on radios Severe/ destructive vibrations Chunks breaking off can cause damage structurally or in engine intakes
83
Effects of Ice formation on helicopters
Rotor blade imbalance due to uneven ice build up on the blades (more towards tip) Shedding of Ice of one blade and not the others can cause severe vibrations Additionally: Ice can build up rapidly on blades in freezing fog conditions Hovering can cause a large build up of pack ice over wet snow or slushy surfaces Caution by ground crew due to ice shed from rotors, engine risk also
84
How should protective covers be used to protect aircraft from snow/ice? And what are they called?
Approved aircraft covers Need to be a tight perfect fit Not to be fitted when aircraft is wet due to adhesion when it freezes Not to be fitted over snow/ice due to adhesion when thawed and refrozen De-icing fluid can be applied before cover to prevent this
85
Two types of principle of operation? (Ice protection systems)
Aftive Passive
86
How do active ice protection systems work?
Increase temperature of local areas of aircraft to above freezing Further categorised as: Anti-icing De-icing
87
Whats passive ice protection?
Harness momentum of airstream ti separate out precipitation and divert it away
88
Advantage if de-icing over anti-icing?
Lighter and use less energy
89
Where would you need to use anti-icing instead of de-icing?
Engine air intake
90
How does momentum separation device work?
A dam will force the airflow to change direction, causing the water particles with a higher mass to divert away from the engine intake
91
Types of ice protection system
Engine air intake - active and passive systems used Thermal hot air - leading edges heated with hot air from engine Thermal electrical - electrically heated leading edges Mechanical (pneumatic) - inflatable/ deflatable tubes that break the ice off
92
Windscreen ice protection
Overheat sensors sandwiched in the glass laminations of the screen. Heated window using thin film of gold on the glass.
93
Rain protection windscreen
Windscreen wipers
94
When must windscreen wipers be used?
Worn to limits Damaged Contaminated
95
General rules of windscreen wiper maintenance?
Rubber blades replaced when necessary Lubricated Check for clearance between blades and screen Check for correct tension in wiper arms