The Fuel System Flashcards

1
Q

Fuel Types

A

AVGAS 100/130: Aviation gasoline, coloured green, normally used in aircraft piston engines
AVGAS 100LL (low lead): A suitable alternative to AVGAS, coloured blue
MOGAS: Coloured red, and unsuitable for use in aircraft
AVTUR: Jet fuel, clear or straw-coloured, will damage an aircraft piston engine

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2
Q

MOGAS

A

In an aircraft engine it will cause a lower power output and an increased risk of detonation
More volatile and will vaporise more readily
Will boil at about 15,000ft compared to AVGAS at 30,000ft

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3
Q

Octane Rating

A

The resistance of the fuel to detonation

The higher the rating, the more the mixture can be compressed and heated without detonating

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4
Q

Fuel/Air Mixture

A

Ratio of fuel to air in the cylinder for combustion

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5
Q

Chemically Correct Mixture

A

The mixture which results in no excess fuel or air present in the cylinder after combustion takes place
Approx ratio = 1:16

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6
Q

Leaning Using an EGT Gauge

A

Each marking on the gauge = 25 degrees F starting at 1000 degrees F
Pull mixture out until the needle on the EGT gauge wont rise any more (max EGT) and then enrich by 2 markings

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7
Q

Detonation

A

An explosive and instantaneous combustion of the mixture in the cylinder
Can severely damage the piston, valves, spark plugs and cause engine failure
Usually occurs in all cylinders

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8
Q

Symptoms of Detonation

A

High CHTs and rough running

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9
Q

Causes of Detonation

A

Mixture being too hot

  1. Over-lean mixture (no excess fuel to evaporate and cool the cylinders)
  2. Time expired or wrong fuel octane rating
  3. Low airspeed (less air cooling)
  4. Unnecessarily high power settings
  5. Excessive manifold pressure with a low RPM
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10
Q

Remedial Action For Detonation

A

Enrich the mixture
Reduce power settings
Increase airspeed

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11
Q

Pre-Ignition

A

Uncontrolled ignition of the mixture before the spark plugs fire on the compression stroke
Forms a progressive-burn
A problem in one cylinder

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12
Q

Causes of Pre-Ignition

A
  1. Carbon deposits
  2. Hot spots in the cylinder
  3. Overheated spark plugs
  4. High power settings and a lean mixture
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13
Q

Symptoms of Pre-Ignition

A

Rough running and high CHTs with possible backfiring

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14
Q

Remedial Action For Pre-Ignition

A

Enrich the mixture
Decrease power
Increase airspeed

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15
Q

Purpose of The Fuel System

A

Store fuel
Provide fuel to the engine via the carburettor
Provide flow of fuel continuously and in correct amounts
A means to monitor the fuel load and usage during flight

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16
Q

Types of Fuel Tanks

A

Aluminium (C-152, C-172, etc): A metal rigid structure
Rubber cells/bladder
The whole wing (big boys): Integral/wet wing design

17
Q

Fuel Tanks

A

Store fuel for the flight
Different aircraft have different numbers of tanks
Have a sump with a drain point
May contain baffles to prevent movement of the fuel within the tank during flight

18
Q

Fuel Tank Vents

A

Provides positive pressure at all times
Allows atmospheric pressure to be retained as altitude increases
Ensures that fuel will always be capable of being drawn from the tank to the engine
Used as an overflow drain should pressure become too high at any stage
Should be clear of obsructions

19
Q

Rich Mixtures

A

When the ratio of fuel to air is increased
Mixtures richer than 1:8 wont burn (flooding)
Burns cooler as the un-burnt fuel evaporates and cools the cylinders

20
Q

Lean Mixtures

A

Ratio of fuel to air is reduced

Mixtures leaner than 1:18 will not burn

21
Q

Mixture Strength

A

Affects the temperature of combustion and exhaust gases

22
Q

Mixture Versus Power Output

A

As mixture is leaned the power output will increase (increasing TAS in level flight)
Leaning past the best power mixture will reduce the TAS and the fuel flow

23
Q

Best Economy Mixture

A

The point at which TAS begins to reduce faster than the fuel flow
Very close to peak EGT

24
Q

Best Power Mixture

A

The mixture that gives the max TAS

25
Q

Leaning at Altitude

A

As altitude increases, pressure reduces and the weight of the air entering the carburettor reduces
If the fuel flow is not adjusted, the mixture will become too rich

26
Q

Consequences of an Over-Rich Mixture

A

Reduced power
Rough running
High fuel consumption
Fouling of the spark plugs and lead deposits
Black exhaust smoke is often an indication

27
Q

Consequences of an Over-Lean Mixture

A

High CHTs and detonation

Blue exhaust smoke is often an indication

28
Q

Components of the Fuel System

A
Fuel Tanks
Fuel Tank Vents
Fuel Lines
Fuel Selector
Fuel Strainer (Gascolator)
Fuel Pumps
Fuel Mixture Control
29
Q

Fuel System Mixture Control

A

Mixture control linked to carburettor or fuel injection system

30
Q

Fuel Drain

A

Drains in the bottom of the tanks and below the strainers

Allow to check for contaminants

31
Q

Fuel Selector Valve

A

Allows the fuel flow from the tanks, or either tank separately, to be turned on and off

32
Q

Fuel Quantity Gauge

A

Operated via a float in the fuel tank

33
Q

Fuel Pump

A

A mechanical engine-driven pump for normal operation

A backup electric pump for takeoff, landing and engine failure is also available

34
Q

Fuel Vaporisation

A

The fuel will expand in the lines and the fuel flow to the engine will be interrupted

35
Q

Risk of Vaporisation Increased By

A
  1. Volatility
  2. High temperatures
  3. Low atmospheric pressure
36
Q

Boost Pump

A

Helps to prevent vapour locks
Acts as a:
- Primer to purge the fuel lines of vapour prior to start
- Substitute in case the engine-driven pump fails