Internal Combustion Engines

Combustion in SI Engine
 Combustion in SI Engine

❑Normal Combustion: When the flame

travels evenly or uniformly across the
combustion chamber.

❑ Abnormal Combustion: When the

combustion gets deviated from the
normal behavior resulting in loss of
performance or damage to the engine.

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❑Combustion is dependent upon the rate of
propagation of flame front (or flame speed).

❑Flame Front: Boundary or front surfa ce of the

flame that separates the burnt charges from
the unburnt one.

❑Flame Speed: The speed at which the flame

front travels.
Flame speed affects the combustion
phenomena, pressure developed
and power produced.

Burning rate of mixture depends on

the flame speed and shape / contour
of combustion chamber. 3
 Factors Affecting Flame Speed (FS)

1. Turbulence: Helps in mixing and accelerates

chemical reaction. A lean mixture can be burnt
without difficulty.

2. Engine Speed:
When engine speed
incre ases, flame
speed incre ases
due to turbulence,
swirl squish, and
tumble.

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 Factors Affecting Flame Speed (FS)

3. Compression Ratio (CR): A higher CR

increases the pressure and temperature of
mixture. This reduces the initial phase of
combustion, and hence less ignition advance is
needed. High p and T of the compressed
mixture speed up the 2nd phase of combustion.
Increased CR reduces the clearance volume,
and hence the density of charge. This further
incre ases the peak pressure and temperature,
reducing the total combustion duration. Thus, an
engine with higher CR have higher flame
speeds.

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 Factors Affecting Flame Speed (FS)

4. Inlet Temp. & Pressure: FS increases with an

increase of inlet temperature and pressure. A
higher values of these form a better
homogeneous mixture, which helps in
increasing the FS.
5. Fuel-Air Ratio: The highest flame speeds
(minimum time for complete combustion) are
obtained with slightly rich mixture (point A).
When the mixture is leaner or richer, flame
speed decreases ( a lean mixture releases less
thermal energy, and hence a lower flame
temperature; while a rich mixture leads to
incomplete combustion, and hence a release of less
thermal energy).
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Effect of mixture strength on burning rate

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 Average flame speed in CC of an SI
engine as a function of air-fuel ratio.

Lean air-fuel mixtures have slower flame speeds

with maximum speed occurring when slightly rich
at an equivalence ratio near 1.2. 8
 Stages of Combustion

a → b : Compression
b → c : Combustion
c → d : Expansion
❑Ideally, entire pressure rise during combustion occurs
at constant volume, i.e., when the piston is at TDC. 9
 Actual p- diagram

I. Ignition lag (A→B): Flame front begins to travel.

II. Spreading of Flame (B→C): Flame spreads
throughout the Combustion Chamber.
III. Afterburning (C→D): C is the point of max. pressure,
a few degrees after TDC. Power stroke begins.
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 Effect of Ignition: Constant Volume Cycle

❖Because of ignition
lag, it is necessary to
ignite the charge in the
cylinder some degrees
before the crankshaft
reaches TDC. The
number of degrees
before TDC at which
ignition occurs is called
Ignition Advance.

❖The optimum angle of advance allows combustion

to cease just after TDC, so that maximum possible
pressure is built at a point just at the beginning of
expansion stroke. This is shown as the normal curve,
indicating smooth engine running.
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 Effect of Over-advanced ignition

❖When the engine

ignition is over-advanced ,
combustion is initiated too
early and the cylinder
pressure begins to rise
rapidly while the piston is
still trying to complete its
compression stroke.

❖This creates excessive cylinder pressures and

may even produce shock waves in the cylinder as
illustrated by the ragged top on curve 2. An over-
advanced engine will run rough, it will tend to
overheat resulting in loss of power.
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 Effect of Retarded Ignition

❖When the engine ignition

is retarded (curve 3),
combustion is initiated late.
In fact, combustion will
continue while the piston is
sweeping out its power
stroke.

❖Maximum pressure will occur late, and will not as

high as that of the normal case. A retarded engine
will produce less power output, and due to the late
burning the engine will run hot, and may cause
damage to the exhaust valves and ports.

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 Knocking

Flame travels from A→D and compresses the end

charge BB´D and raises its temperature.
Temperature also increases due to heat transfer
from the flame front. Now, if the final temperature
is less than the auto-ignition temperature, Normal
Combustion occurs and charge BB´D is
consumed by the flame itself.
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 Knocking

Now, if the final temperature is greater than and

equal to the auto-ignition temperature, the
charge BB´D auto-ignites (knocking). A second
flame front develops and moves in opposite
direction, where the collision occurs between the
flames. This causes severe pressure pulsation,
and leads to engine damage /failure.
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 Engine Damage From Severe Knock
Damage to the engine is caused by a combination
of high temperature and high pressure.

Piston Piston crown

Cylinder head gasket Aluminum cylinder head

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 Effect of Variables on Knock – Density Factors
❑Density Factors: Factors that reduce the
density of the charge also reduce the knocking
tendency by providing lower energy release.
1.Compression ratio (CR): When CR ratio
increases, p and T increase and an overall
incre ase in density of charge raises the
knocking tendency.
2.Mass of inducted charge: A reduction in
the mass of inducted charge (by throttling or
by reducing the amount of supercharging)
reduces both temperature and density at
the time of ignition. This decreases the
knocking tendency.
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 Effect of Variables on Knock – Density Factors

3.Inlet temperature of mixture: An incre ase in

the inlet temperature of mixture makes the
compression temperature higher. This incre ases
the knocking tendency. Further, volumetric
efficiency is lowered. Hence, a lower inlet
temperature is always preferred. However, it
should not be too low to cause starting and
vaporization problems.

4.Retarding spark timing: Having a spark closer

to TDC, peak pressures are reached down the
on the power stroke, and are of lower
magnitudes. This might reduce the knocking
tendency, however, it will affect the brake
torque and power output.
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 Effect of Variables on Knock – Time Factors
❑Time Factors: Increasing the flame speed or
the ignition lag will tend to reduce the tendency
to knock.
1.Turbulence: Increase of turbulence
increases the flame speed and reduces the
time available for the end charge to reach
auto-ignition condition. This reduces the
knocking tendency.
2.Engine size: Flame requires more time to
travel in Combustion Chamber of larger
engines. Hence, a larger engines will have
more tendency to knock.

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 Effect of Variables on Knock – Time Factors

3.Engine speed: An incre ase in engine speed

incre ases the turbulence of the mixture
considerably resulting in incre ased flame
speed. Hence, knocking tendency reduces at
higher engine speeds.

4.Spark plug locations: To minimize the flame

travel distance, spark plug is located centrally.
For larger engines, two or more spark plugs are
located to achieve this.

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Effect of Variables on Knock – Composition Factors
❑Composition Factors: These includes ratio of air-
fuel mixture, and the properties of fuel
employed in the engine.
1.Fuel-air ratio: The flame speeds are
affected by fuel-air ratio. Also, the flame
temperature and reaction time are different
for different fuel-air ratios.

2.Octane value: In general, paraffin series

of hydrocarbon have the maximum and
aromatic series the minimum tendency to
knock.

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 Combustion Chamber - Definition

• The combustion chamber consists of

an upper and lower half.

– Upper half- Made up of cylinder

head and cylinder wall.

– Lower half- Made up of piston

head (Crown) and piston rings.

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 Design Considerations

• Minimal flame travel

• The exhaust valve and spark plug
should be close together
• Sufficient turbulence
• A fast combustion, low variability
• High volumetric efficiency at WOT
• Minimum heat loss to combustion
walls
• Low fuel octane requirement

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 Chamber Shapes
• A basic shapes
– Wedge - Hemispherical
– Crescent - Bowl in Piston

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 Chamber Shapes
• Wedge
– Asymmetric design
– Valves at an angle
and off center

• Hemispherical (Hemi)
– Symmetric design
– Valves placed on
a arc shaped head
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 Chamber Shapes
• Bowl-in-Piston
– Symmetric design
– Valves are placed
perpendicular to head

• Crescent (Pent-Roof)
– The valves are placed
at an angle on flat
surfaces of the head
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 Fast Combustion
• Effect of spark plug location

Side plug w/o swirl

Side plug with

normal swirl

Side plug with

high swirl

Central plug w/o

swirl

Two plugs w/o swirl

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Fast Combustion in Relation to Shape

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Comparison of Burn Angles

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 Heat Transfer

• Want minimum heat transfer to

combustion chamber walls
• Open and hemispherical have
least heat transfer
• Bowl-in-piston has high heat
transfer

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 Low Octane

• Octane Requirement related to knock

• Close chambers (bowl-in-piston) have
higher knock at high compression
ratios than Open chambers
(hemispheric al and pent-roof)

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 Octane Rating
• Research Octane Number (RON)
• Motor Octane Number (MON)
• Octane is one factor in the combustion
process that another group will speak about
• Straight chain C-H bonds such as heptane
have weaker C-H bonds than branched
chained C-H bonds in branch chained HC
such as iso-octane
• Straight bonds are easier to break

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 Knock

• Surface ignition
– Caused by mixture igniting as a result of
contact with a hot surface, such as an
exhaust valve
• Self-Ignition
– Occurs when temperature and pressure
of unburned gas are high enough to
cause spontaneous ignition

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 Conclusion

• Optimum chamber
– Central spark plug location
– Minimum heat transfer
– Low octane requirement
– High turbulence

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 References
1. Crouse WH, and Anglin DL, (1985), Automotive Engines, Tata McGraw Hill.
2. Eastop TD, and McConkey A, (1993), Applied Thermodynamics for
Engg. Technologists, Addison Wisley.
3. Fergusan CR, and Kirkpatrick AT, (2001), Internal Combustion Engines, John
Wiley & Sons.
4. Ganesan V, (2003), Internal Combustion Engines, Tata McGraw Hill.
5. Gill PW, Smith JH, and Ziurys EJ, (1959), Fundamentals of I. C. Engines, Oxford
and IBH Pub Ltd.
6. Heisler H, (1999), Vehicle and Engine Technology, Arnold Publishers.
7. Heywood JB, (1989), Internal Combustion Engine Fundamentals, McGraw Hill.
8. Heywood JB, and Sher E, (1999), The Two-Stroke Cycle Engine, Taylor & Francis.
9. Joel R, (1996), Basic Engineering Thermodynamics, Addison-Wesley.
10. Mathur ML, and Sharma RP, (1994), A Course in Internal Combustion Engines,
Dhanpat Rai & Sons, New Delhi.
11. Pulkrabek WW, (1997), Engineering Fundamentals of the I. C. Engine, Prentice Hall.
12. Rogers GFC, and Mayhew YR, (1992), EngineeringThermodynamics, Addison
Wisley.
13. Srinivasan S, (2001), Automotive Engines, Tata McGraw Hill.
14. Stone R, (1992), Internal Combustion Engines, The Macmillan Press Limited, London.
15. Taylor CF, (1985), The Internal-CombustionEnginein TheoryandPractice,Vol.1 & 2,
The MIT Press, Cambridge, Massachusetts.
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 Web Resources
1. http://www.mne.psu.edu/simpson/courses
2. http://me.queensu.ca/courses
3. http://www.eng.fsu.edu
4. http://www.personal.utulsa.edu
5. http://www.glenroseffa.org/
6. http://www.howstuffworks.com
7. http://www.me.psu.edu
8. http://www.uic.edu/classes/me/ me429/lecture-air-cyc-web%5B1%5D.ppt
9. http://www.osti.gov/fcvt/HETE2004/Stable.pdf
10. http://www.rmi.org/sitepages/pid457.php
11. http://www.tpub.com/content/engine/14081/css
12. http://webpages.csus.edu
13. http://www.nebo.edu/misc/learning_resources/ ppt/6-12
14. http://netlogo.modelingcomplexity.org/Small_engines.ppt
15. http://www.ku.edu/~kunrotc/academics/180/Lesson%2008%20Diesel.ppt
16. http://navsci.berkeley.edu/NS10/PPT/
17. http://www.career-center.org/ secondary/powerpoint/sge-parts.ppt
18. http://mcdetflw.tecom.usmc.mil
19. http://ferl.becta.org.uk/display.cfm
20. http://www.eng.fsu.edu/ME_senior_design/2002/folder14/ccd/Combustion
21. http://www.me.udel.edu
22. http://online.physics.uiuc.edu/courses/phys140
23. http://widget.ecn.purdue.edu/~yanchen/ME200/ME200-8.ppt -

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