Carburation Flashcards
(41 cards)
Gasoline will not burn unless it is first vaporised and then mixed with ______ which is normally obtained from the ______.
oxygen; air
The workable limits of fuel-air ratio for reliable ignition by spark are from as rich as 1:______ to as lean as 1:______.
1:9; 1:18
The ‘chemically correct’ or stoichiometric mixture is very close to 1:______. In theory, at this mixture strength, complete combustion of both the ______ and ______ will occur. In a richer mixture some ______ will be left over after combustion. In a leaner mixture, some ______ will be left over.
1:15; fuel; oxygen; fuel; oxygen
In practice, it has been found that maximum power output is achieved with a relatively rich mixture strength of about 1:______, and best economy with a relatively weak mixture around 1:______.
1:12; 1:16
Aircraft carburettors are typically set up to operate with a rich mixture at (idling / cruise / high) power settings, and with a lean mixture at (idling / cruise / high) power.
rich for idling and high power; lean for cruise
In normal operation, fuel will flow from the float chamber through the main jet of the carburettor because the air pressure above the fuel in the float chamber is (at ambient / higher than ambient) pressure while the venturi air pressure affecting the jet is at (ambient / lower than ambient) pressure.
pistions fit closely within the cylinders. Three or more grooves are machined around the piston near the top into which are set the steel pistion rings. The function of the upper rings is to prevent combustion gases from escaping between the pistion and cylinder walls. The lower piston ring is usually desinged to prevent lubricating oil from entering and being burnt in the combustion space. The piston is what compresses the fuel air mixure.
Atomisation and diffusion of the fuel leaving the main jet (improves / prevents) vaporisation and even mixing with the air.
improves
The density (and inertia) of the fuel is (higher / lower) than that of the air. Hence, an accelerating system is required to provide extra (fuel / air) to maintain the mixture strength when the throttle is opened.
higher; fuel
A separate idling system is required because, at low rpm:
A. The main jet provides too much fuel.
B. With little difference in air pressure between the float chamber and venturi, the flow of fuel from the main jet drops to zero or becomes unreliable.
B. With little difference in air pressure between the float chamber and venturi, the flow of fuel from the main jet drops to zero or becomes unreliable.
Idling fuel is drawn from an outlet (a jet) situated (near the gap between the butterfly valve and carburettor wall / in the middle of the venturi).
near the gap between the butterfly valve and carburettor wall
The phasing out of the idling system and phasing in of the main fuel metering system takes place typically between ______ rpm and ______ rpm.
1000; 1400
A power enrichment system is needed at high rpm and manifold pressure to avoid ______ and ______.
overheating; detonation
A mixture control system is needed because, as an aircraft climbs, the carburettor will meter (less / the same weight of) fuel into a decreasing weight of air, making the mixture (too rich / too lean).
the same weight of; too rich
The idle cut-off part of the mixture control system operates by ______ the fuel supply at the carburettor.
cutting off
The two main disadvantages of the float-type carburettor are that fuel flow can be interrupted by manoeuvres and ______ and susceptibility to ______.
turbulance; icing
The pressure injection carburettor (has / does not have) a float chamber. A ______ is still used to measure the amount of air entering the engine and a fuel pressure regulator unit varies the amount of ______ in the mixture.
does not have; venturi; fuel
The main jet (or discharge nozzle) of the pressure-injection carburettor is (ahead of / on the engine side of) the throttle butterfly. This makes it (less / more) susceptible to carburettor icing than the float-type carburettor.
on the engine side of; less
Other advantages are that it (will / will not) operate when inverted, has (more / less) accurate fuel metering, has better ______ and mixing and there is (less / a greater) chance of vapour lock.
will; more; atomisation; less
Fuel injection systems (have / do not have) a carburettor. The fuel is injected into the intake air as a high-pressure spray near the inlet valve or ______ impeller or, on some large engines, directly into the ______ chamber. The amount of air (and therefore of the mixture) is controlled in the normal way through ______ butterfly valve.
do not have; supercharger; combustion; throttle
In a continuous flow system, the fuel is injected ______ into the intake manifold air at the inlet port of each cylinder. In a direct injection system, the fuel is injected directly into the cylinder, only during the ______ stroke.
continuously; induction
Which of the following are true?
The advantages of fuel injection systems are:
A. Freedom from refrigeration ice.
B. More accurate delivery of the mixture to Individual cylinders.
C. Improved control of the mixture and therefore increased engine efficiency.
D. Better throttle response.
E. Less susceptibility to vapour lock and fuel contamination.
A, B, C and D are true.
E is not true - fuel injection systems are more susceptible.
The mixture control is almost always placed in ______ ______ for takeoff.
full rich
As the aircraft is climbed with the mixture in FULL RICH, the excess fuel in the mixture assists in ______ the engine and helps to prevent ______.
cooling; detonation
To lean the mixture manually for the cruise, you should move the mixture control toward the lean position until the rpm begin to ______ and the engine shows signs of running a little ______. Then move the control back toward rich to regain best ______ and the engine runs ______. Finally, move the mixture control to a slightly ______ position.
drop; roughly; rpm; smootly; richer
