12. We are now going to look at how the carburettor controls the flow to the engine
THE FLOAT CHAMBER
This is done by the: -
13. SIMPLIFIED PISTON ENGINE FUEL SYSTEM
FLOAT CHAMBER
NEEDLE VALVE AIR VENT
VENTURI
FUEL
FEED
FUEL
NOZZLE
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
FLOAT
FUEL
LEVEL
14. AIR IS SUCKED THROUGH VENTURI BY…..
A PISTON MOVING DOWN ON INDUCTION STROKE
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
MOVING AIR HAS LOWER PRESSURE
FUEL
FLOW
AIR
FLOW
AIR
FLOW
THE LOWER AIR PRESSURE PULLS FUEL THROUGH THE JET
AIR/FUEL
MIXTURE
FLOWS TO
ENGINE
FUEL LEVEL DROPS
15. PULLING AIR INTO FLOAT CHAMBER
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
FUEL LEVEL DROPS
FUEL LEVEL DROPPING LOWERS FLOAT
16. AND ALLOWS FUEL TO ENTER FLOAT CHAMBER FROM PUMP
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
FUEL LEVEL DROPS
FUEL LEVEL RISING FORCES THE NEEDLE VALVE CLOSED
FUEL LEVEL DROPPING LOWERS FLOAT
17. SIMPLIFIED PISTON ENGINE FUEL SYSTEM
FUEL IS PULLED OUT OF THE FLOAT CHAMBER
ONLY WHEN ONE OF THE PISTONS IS ON THE INDUCTION STROKE
FUEL LEVEL RISING FORCES THE NEEDLE VALVE CLOSED
18. We now need to look at controlling the air/fuel mixture flowing into the engine
THE THROTTLE
Controlling the air/fuel mixture means controlling the engine
The carburettor part which controls the flow is….
19. SIMPLIFIED PISTON ENGINE FUEL SYSTEM
LINK TO
THROTTLE
LEVER/PEDAL
THROTTLE
VALVE
VALVE
SPINDLE
VALVE
DISC
20. SIMPLIFIED PISTON ENGINE FUEL SYSTEM
THROTTLE VALVE
THIS WOULD BE A HIGH THROTTLE SETTING OR ‘FULL –POWER’
OPEN THROTTLE ALLOWS VENTURI TO WORK AT MAXIMUM EFFICIENCY
21. LOW THROTTLE SETTING - CALLED ‘IDLE’ OR ‘TICK-OVER’
ALMOST CLOSED THROTTLE MEANS THE VENTURI DOES NOT WORK VERY
WELL
LOW AIR FLOW MEANS VERY LITTLE OR NO FUEL/AIR MIXING IN THE
VENTURI
SO AN ALTERNATIVE AND EFFECTIVE VENTURI NEEDS TO BE FOUND
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
22. T CONTROLS FUEL FLOW
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
LOW THROTTLE SETTING - CALLED ‘IDLE’ OR ‘TICK-OVER’
EDGE GAPS BECOME THE VENTURI FOR THE LOW AIR FLOW
AT IDLE - SLOW RUNNING JET
24. SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
THE AIR FILTER CAN ALSO CAUSE RESTRICTION TO AIR FLOW
THIS WOULD CREATE A PRESSURE
DIFFERENCE BETWEEN:-
HERE AND HERE
AND THEREFORE A SLIGHT VACUUM BEFORE CARB
FLOAT
CHAMBER VENT
25. SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
EQUALISING THE PRESSURE AT LOW SPEED
THEREFORE PREVENTING TOO MUCH FUEL MIXING WITH THE AIR
AND THE FLOAT CHAMBER IS CONNECTED TO THE CARB AIR INTAKE
SO THE VENT TO THE FLOAT CHAMBER IS CLOSED OFF
FLOAT
CHAMBER VENT
27. MORE EFFICIENT MIXING OF AIR AND FUEL
IS ACHIEVED BY FITTING A DIFFUSER TUBE
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
HERE, ABOVE THE MAIN JET
LET’S TAKE A CLOSER LOOK AT THIS AREA
28. IDLE SETTING FUEL
SUPPLIED VIA IDLE JET
OPEN THROTTLE
IDLE JET STOPS WORKING
CRUISE SETTING
HIGH POWER
SETTING
AIR INLET
DIFFUSER TUBE
INCREASED
FLOW OF MIXED
AIR/FUEL
FUEL FEED FROM
FLOAT CHAMBER
MAIN JET
AIR MIXES
WITH FUEL
AIR/FUEL MIXING IN
DIFFUSER TUBE
FUEL LEVEL IN
FLOAT CHAMBER
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
29. AUTOMATIC MIXTURE CONTROL
This is required to take into account that at higher
altitude there is less air, so therefore less fuel is
required.
It is called a pressure bellows or pressure capsule.
This change in fuel flow is controlled by a device that
can sense the change in air pressure.
30. SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
FIXED END
MOVING END
NEEDLE
VALVE
CAPSULE EXPANDS IN LOWER
PRESSURES AND CONTRACTS IN
HIGHER PRESSURES
PRESSURE CAPSULE
31. SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
AT LOW ALTITUDE – HIGHER ATMOSPHERIC PRESSURE
CAPSULE CONTRACTED
HIGH FUEL FLOW
AT HIGH ALTITUDE – LOWER ATMOSPHERIC PRESSURE
CAPSULE EXPANDS
32. SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
SIMPLIFIED PISTON ENGINE FUEL SYSTEM
AT HIGH ALTITUDE – LOWER ATMOSPHERIC PRESSURE
CAPSULE EXPANDS
CLOSING FUEL ORIFICE
E AND REDUCING FUEL FLOW
33. AUTOMATIC MIXTURE CONTROL
This is required to take into account that at higher
altitude there is less air, so therefore less fuel is
required.
It is called a pressure bellows or pressure capsule.
This change in fuel flow is controlled by a device that
can sense the change in air pressure.
34. Battery
Fuel Tank
Pump
Warm Up
Regulator
Fuel
Accumulator
Ignition
Switch
Filter
Primary
Pressure
Valve
Air Sensor
Plate
Mixture Control
Unit (Fuel
Distributor Valve)
Auxiliary Air
Device
Cold Start
Valve
Idle Speed
Adjuster
Fuel
Injector
Throttle
Valve
Engine Temp
Sensor
Safety
Relay
Air
Inlet
High Pressure Fuel
Low Pressure Fuel
Supply Pressure Fuel
Servo Pressure Fuel
Electrical Signal
Legend
PISTON ENGINE – Hydro-Mechanical Fuel Injection System
(from Air
Filter)
35. Air Filter
PISTON ENGINE – Electronic Fuel Injection System
Engine
ECU
Tank
Pump
Cockpit
Gauge
Pressure
Regulator
Injection
Control
Unit
Engine Temp
Engine RPM/TDC
Exhaust Temp
Throttle Position
Forward Speed
Air Temps – Inlet & Ambient
Fuel
Injectors
‘Common Rail’
Throttle