The Fuel System Flashcards
Fuel Types
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
MOGAS
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
Octane Rating
The resistance of the fuel to detonation
The higher the rating, the more the mixture can be compressed and heated without detonating
Fuel/Air Mixture
Ratio of fuel to air in the cylinder for combustion
Chemically Correct Mixture
The mixture which results in no excess fuel or air present in the cylinder after combustion takes place
Approx ratio = 1:16
Leaning Using an EGT Gauge
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
Detonation
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
Symptoms of Detonation
High CHTs and rough running
Causes of Detonation
Mixture being too hot
- Over-lean mixture (no excess fuel to evaporate and cool the cylinders)
- Time expired or wrong fuel octane rating
- Low airspeed (less air cooling)
- Unnecessarily high power settings
- Excessive manifold pressure with a low RPM
Remedial Action For Detonation
Enrich the mixture
Reduce power settings
Increase airspeed
Pre-Ignition
Uncontrolled ignition of the mixture before the spark plugs fire on the compression stroke
Forms a progressive-burn
A problem in one cylinder
Causes of Pre-Ignition
- Carbon deposits
- Hot spots in the cylinder
- Overheated spark plugs
- High power settings and a lean mixture
Symptoms of Pre-Ignition
Rough running and high CHTs with possible backfiring
Remedial Action For Pre-Ignition
Enrich the mixture
Decrease power
Increase airspeed
Purpose of The Fuel System
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
Types of Fuel Tanks
Aluminium (C-152, C-172, etc): A metal rigid structure
Rubber cells/bladder
The whole wing (big boys): Integral/wet wing design
Fuel Tanks
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
Fuel Tank Vents
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
Rich Mixtures
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
Lean Mixtures
Ratio of fuel to air is reduced
Mixtures leaner than 1:18 will not burn
Mixture Strength
Affects the temperature of combustion and exhaust gases
Mixture Versus Power Output
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
Best Economy Mixture
The point at which TAS begins to reduce faster than the fuel flow
Very close to peak EGT
Best Power Mixture
The mixture that gives the max TAS
Leaning at Altitude
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
Consequences of an Over-Rich Mixture
Reduced power
Rough running
High fuel consumption
Fouling of the spark plugs and lead deposits
Black exhaust smoke is often an indication
Consequences of an Over-Lean Mixture
High CHTs and detonation
Blue exhaust smoke is often an indication
Components of the Fuel System
Fuel Tanks Fuel Tank Vents Fuel Lines Fuel Selector Fuel Strainer (Gascolator) Fuel Pumps Fuel Mixture Control
Fuel System Mixture Control
Mixture control linked to carburettor or fuel injection system
Fuel Drain
Drains in the bottom of the tanks and below the strainers
Allow to check for contaminants
Fuel Selector Valve
Allows the fuel flow from the tanks, or either tank separately, to be turned on and off
Fuel Quantity Gauge
Operated via a float in the fuel tank
Fuel Pump
A mechanical engine-driven pump for normal operation
A backup electric pump for takeoff, landing and engine failure is also available
Fuel Vaporisation
The fuel will expand in the lines and the fuel flow to the engine will be interrupted
Risk of Vaporisation Increased By
- Volatility
- High temperatures
- Low atmospheric pressure
Boost Pump
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