Piston Engine Fuel Systems Flashcards

1
Q

Characteristics of AVGAS

A

Composition 85Carbon 15Hydrogen. Burn Rate 18-24 M/S
Be able to form a vapour but not to quickly.
Be able to burn quickly but controllably giving a manageable rise in pressure that can be efficiently translated into movement of pistons. Good Anti-knock Capability. Lead is added to control detonation.

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2
Q

What is detonation

A

Extremely rapid spontaneous combustion of part of mixture after burning has begun. Rapid, violent and uneven rise in pressure. Can often be heard as knocking sound in engine. Power output reduces markedly and cylinder temperature rise rapidly. Engine runs rough.

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3
Q

Cause of Detonation

A

High engine temperature
Fuel with poor anti-knock qualities,
Incorrect mixture ratio
Anything that unduly raises the temperature or pressure of mixture before it burns.

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4
Q

What is pre-ignition

A

Uncontrolled Ignition. Ignition of mixture before spark plug fires.
Caused by local hotspots inside cylinder eg small carbon deposits Primary cause is weak mixture..

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5
Q

Pre-ignition and detonation symptoms

A

Loss of power, overheating, rough running

However Pre-Ignition worsens with increased RPM and detonation reduces with RPM.

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6
Q

What is Octane rating.

A

Fuel assigned number to indicate its resistance to detonation. Also known as anti-knock value. Higher number= higher resistance.
Additives are also added which are effective for controlling detonation.

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7
Q

What is mixture ratio

A

Ratio of air to fuel. Ideal 15:1

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8
Q

Rich Mixture and Lean Mixture ratios/characteristics

A

Rich 8:1 Lean 20:1 Lean gives elevated cylinder head temperature and reduced power but reduces fuel consumption.

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9
Q

What is EGT

A

Exhaust Gas Temperature. Affected by ratio of mixture. Often used as a method for adjusting mixture ration in flight. Peak EGT is 15:1

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10
Q

What are the cruise settings

A

Power Cruise. Ratio 12:1. Set by leaning mixture to achieve peak EGT. Then slowly enrich mixture until EGT drops slightly.
Economy Cruise.
17:1 Set by leaning mixture until peak EGT is achieved and then leaning it slightly more until EGT drops slightly.

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11
Q

What are the functions of the Carburettor and fuel injection system

A

Amount of air delivered to engine is controlled by the throttle. Both systems infer the amount of air entering the engine induction system and add sufficient fuel to maintain correct mixture ratio.

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12
Q

What is the basic principle of a carburettor

A

U-tube is formed between fuel chamber an fuel jet in carburettors throat which both have same pressure due to atmospheric air. Carburettor throat has Venturi tube and when engine is running air is drawn in from inlet and accelerates passed Venturi resulting in pressure drop. Fuel is then drawn up u-tube and into air flowing through the flow.

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13
Q

Problems with the basic carburettor system

A

Does not take into account air density.
Ram effect of air would result in leaner mixture with increased airspeed.
Dosent take into account special mixture settings required at very low/high power settings.
Would get a progressively richer mixture as engine speed increases and altitude increases.

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14
Q

What is the Pressure Balance Duct

A

Ensures correct mixture ratio is maintained across a range of air speeds and flight conditions.

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15
Q

How does pressure balance duct work

A

High airspeeds result in intake pressure rising causing drop in fuel flow=weaker mixture.
PBD connects intake and float chamber ensuring pressure remains same.

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16
Q

What is a diffusor

A

Helps maintain a correct fuel mixture ratio over a wide range of engine operations.

17
Q

What is mixture control

A

Air density decreases with altitude. Mass of air passing through throat will reduce with altitude. Result is richer mixture as aircraft climbs. Mixture control valve is fitted.

18
Q

What is slow running jet.

A

At very small throttle openings pressure drop in Venturi is negligible resulting in insufficient flow of fuel from main jet. SRJ is placed at edge of almost closed and designed to provide a rich mixture at idle.

19
Q

What is Power enrichment

A

At high power settings power enrichment systems needed to cool cylinders. At high throttle settings an additional needle jet lifts to allow increased fuel flow.

20
Q

What is the accelerator pump

A

When throttle opens rapidly air flow to engine increases instantaneously. However slight delay before reduced pressure in throat causes more fuel to be added to mixture. When throttle is rammed accelerator pump injects quantity of fuel directly into Venturi.

21
Q

Carburettor icing

A

While throat produces drop in pressure it also produces drop in temperature. Further temperature is caused by fuel evaporating as it emerges from nozzle. At moderate or high levels of humidity ice will form in intake duct or throat restricting amount of air that can enter the engine causing a marked reduction in engine power.
For fixed pitch propellor engine first sign of icing is unexplained drop in RPM.
For variable pitch manifold pressure reduces.

22
Q

Symptoms of Carburettor icing

A

Loss of RPM, reduced performance, Rough running, decreased EGT, Jammed throttle Reduced inlet manifold pressure.

23
Q

What is Carburettor Heating System

A

Hot air drawn from heat exchanger wrapped around exhaust system. 2 advantages as it prevents/removes ice from forming in the throat of carburettor body.
Provides an alternative source of air in event of primary air intake being blocked by ice.

24
Q

What can potentially happen when carburettor heat is switched on

A

Expect a drop in RPM. If carb heat is selected when ice is present, engine may misfire and round roughly as ice is dislodged and ingested by engine.

25
Q

What are disadvantages of heated air

A

Reduces engine power, Use of heated air at high power settings can cause detonation,
As hot air is less dense it will enrich the mixture.

26
Q

What are fuel injection systems.

A

Delivers fuel under pressure to engine. Provide a more reliable fuel delivery, better icing protection and quicker throttle response.

27
Q

How is fuel delivered in a inject system

A

An engine driven pump is required. Supplies fuel at pressure to the injector assembly.