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UNIT IV
Importance of air motion - Swirl, squish and turbulence - Swirl ratio. Fuel air mixing -Stages of combustion - Delay period -Factors affecting delay period, Knock in CI Factors affecting delay period, Knock in CI engines - methods of controlling diesel knock. CI engine combustion chambers -Combustion chamber design objectives -open and divided. Induction swirl, turbulent combustion chambers. - Air cell chamber - M Combustion chamber.
COMBUSTION IN CI ENGINES
1. Ignition delay or Delay Period
2. Uncontrolled combustion
STAGES OF COMBUSTION IN CI ENGINES
3. Rapid or Controlled Combustion
4. After Burning
COMBUSTION IN CI ENGINES1.Ignition delay - fuel is injected directly into the cylinder
towards the end of the compression stroke. The liquid fuel
atomizes into small drops /droplets and penetrates into the
combustion chamber. The fuel vaporizes and mixes with
the high-temperature, high-pressure air.
2.Uncontrolled combustion [Premixed combustion phase
]– combustion of the fuel which has mixed with the air to
within the flammability limits (air at high-temperature and
high-pressure) during the ignition delay period occurs
rapidly in a few crank angles.
3.Rapid or Controlled Combustion [Mixing controlled
combustion phase ] – Burning rate is controlled by the rate
at which mixture becomes available for burning. The
burning rate is controlled primarily by the fuel-air mixing
COMBUSTION IN CI ENGINES
burning rate is controlled primarily by the fuel-air mixing
process.
4.After Burning [Late combustion phase] – heat release
may proceed at a lower rate well into the expansion stroke
(no additional fuel injected during this phase).
Combustion of any unburned liquid fuel and soot is
responsible for this.
Delay period1. Physical Delay
� The period of physical delay is the time between the beginning
of injection and the attainment of chemical reaction conditions.
� During this time, the fuel is atomized, vapourised, mixed with air
and the temperature is raised.and the temperature is raised.
� Physical delay depends on type of fuel.
� High viscuous fuel means high physical delay. It is reduced by
high injection pressures.
2. Chemical Delay
� During this period, preflame reaction start slowly and then
accelerate until the local inflammation or ignition takes place.
� The delay period refers to the sum of physical and chemical
delay.
� In most CI engines, the ignition delay is shorter than the
duration of injection.
� Ignition lag in SI engines is equivalent to the chemical delay in CI
Delay period
� Ignition lag in SI engines is equivalent to the chemical delay in CI
engines.
� The delay period in the CI engines affects the rate of pressure
rise and hence, knocking results.
� It also affects the engine startability.
� The pressure reached during the combustion depends up
on delay period.
� The longer the delay period, the more rapid is the pressure
rise, since more fuel will be present in the cylinder before
the rate of burning comes under control.
Delay period
the rate of burning comes under control.
� Therefore the diesel engine designers aim to keep the delay
period as short as possible.
� But, some delay period is necessary, otherwise the droplets
would not be dispersed in the air for complete combustion.
Factors Affecting the Delay period� Compression ratio
� Engine speed
�Output
�Atomization of fuel�Atomization of fuel
� Injection timing
�Quality of fuel
� Intake temperature & pressure
Variables affecting delay period1. Fuel
� Self ignition temperature
� Cetane number
� Viscosity
2. Injection pressure or size of droplet2. Injection pressure or size of droplet
� Fuel should be injected at the smallest size to obtain
largest surface to volume ratio
�Rate of burning depends upon the rate at which the
products of combustion can be removed from the
surface and replaced by fresh oxygen.
� Smaller droplets will have lesser momentum and hence lesser
relative velocity and once its initial velocity is lost it will travel
in air resulting in partial suffocation by its own products of
combustion.
� As the pressure rise after ignition depends on the area of
Variables affecting delay period
� As the pressure rise after ignition depends on the area of
inflammation, if the droplet size is small, more aggregate area
of inflammation results in greater uncontrolled pressure rise.
� As the size of the droplet depends upon the injection pressure,
lower the rate of pressure rise during the uncontrolled phase
and smoother engine running.
3. Injection advance :
� The delay period increases with increase in injection advance.
This is due to the lower pressure and temperature when the
injection begins.
� If the injection advance is small, the delay period reduces and
Variables affecting delay period
� If the injection advance is small, the delay period reduces and
operation of the engine is smoother, but the power produced
is reduced as large amount of fuel burns during expansion.
� The optimum angle of injection advance depends upon many
factors, but generally it varies between 12° to 20° before TDC.
This causes the peak pressure to occur 10° to 15° after TDC.
4. Compression ratio
� Increase in compression ratio reduces delay period as it
rises both temperature and density.
1200
1400
Variables affecting delay period
0
200
400
600
800
1000
1200
0 5 10 15 20 25
Te
mp
era
ture
(K
)
Compression Ratio
Max Air Temperature
Min Auto ignition Temp
5. Intake temperature
� Increasing the intake temperature results in increase in the
compressed air temperature, which reduces delay period.
� Increasing the inlet temperature reduces density of air
entering the cylinder, hence volumetric efficiency and power
Variables affecting delay period
entering the cylinder, hence volumetric efficiency and power
output.
6. Jacket water temperature
� Increase in jacket water temperature increases compressed
air temperature and hence delay period is reduced.
7. Fuel temperature
� Increase in fuel temperature reduces both physical and
chemical delay period.
2
57 Cetane Fuel
9. Speed
8. Intake pressure and supercharging
� Increase in intake pressure or supercharging reduces the
auto ignition temperature and hence reduces delay period.
Variables affecting delay period
0.5
1
1.5
500 700 900 1100 1300 1500 1700 1900 2100
Ign
itio
n D
ela
y (
ms)
Engine Speed (RPM)
57 Cetane Fuel
10. Air fuel ratio
With increase in air-fuel ratio (lean mixture), the combustion
temperatures are less and cylinder wall temperatures are
lowered and hence delay period increases. The rate of pressure
rise is unaffected but the maximum pressure is reduced.
Variables affecting delay period
rise is unaffected but the maximum pressure is reduced.
11. Engine size
The engine size has little effect on the delay period in
milliseconds. As large engines operate at low rpm, the delay
period in terms of crank angle is smaller and hence less fuel
enters the cylinder during delay period.
12. Type of combustion chamber.
Pre combustion chambers give shorter delay period compared to
open type of combustion chamber.
Sl no Increase in Variable Effect on Delay
Period
Reason
1 Cetane No of Fuel Reduces Reduces SI Temperature
2 Injection Pressure Reduces Greater S/V ratio, hence less
physical delay
Factors affecting delay period in CI Engines
physical delay
3 Injection timing
Advance
Reduces Pressures and temperature
lower when injection begins
4 Compression Ratio Reduces Increases air temperature
and pressure
5 Intake Temperature Reduces Increases air temperature
6 Jacket Water
Temperature
Reduces Increases wall temperature,
hence air temperature
Sl no Increase in Variable Effect on Delay
Period
Reason
7 Fuel Temperature Reduces Better vaporation and
increases chemical reaction
8 Intake Pressure
(Supercharging)
Reduces Increases in density, reach
auto ignition temperature fast
9 Speed Reduces in time, Less loss of heat.9 Speed Reduces in time,
increases in crank
angle
Less loss of heat.
10 Load (Fuel-Air
Ratio)
Decreases Operating temperature
increases
11 Engine Size Little effect on time
but crank angle
decreases
Low RPM
12 Type of Combustion
Chamber
Lower for pre-
combustion
chamber
Due to compactness of
chamber.
Diesel Knock� If the delay period is long, a large amount of fuel
will be injected and accumulated in the chamber.
�The auto ignition of this large amount of fuel cause
high rate of pressure rise and high maximum high rate of pressure rise and high maximum
pressure which causes knocking in a diesel engine
�A long delay period not only increases the amount
of fuel injected by the moment of ignition, it also
improves the homogeneity of the fuel-air mixture
and its chemical preparedness for explosion type of
self ignition
Difference between SI and CI knock1. In SI engines, detonation occurs near the end of
combustion, whereas in the CI engine, detonation occurs near the beginning of combustion
Difference between SI and CI knock2. The detonation of SI engine is of a homogeneous
charge causing very high rate of pressure rise and
very high maximum pressure. In the CI engine, the
fuel and air are imperfectly mixed and hence the fuel and air are imperfectly mixed and hence the
rate of pressure rise is normally lower than that in
the detonating part of the charge in the SI engine.
3. In CI engine, fuel is injected into the cylinder only at the end of the compression stroke - there is no pre-ignition as in the case of a SI engine
4. In SI engine, it is relatively easy to distinguish between knocking and non-knocking operation
Difference between SI and CI knock
4. In SI engine, it is relatively easy to distinguish between knocking and non-knocking operation as the human ear can easily find the distinction. In the case of CI engine, the normal ignition itself is by auto-ignition and most CI engines have sufficiently high rate of pressure rise per degree of crank angle to cause audible noise.
Factors reducing knock in SI and CI engines
S. No Factors SI Engine CI Engine
1 SI Temperature of Fuel High Low
2 Delay period of fuel Long Short
3 Compression Ratio Low High
4 Inlet Temperature Low High
5 Inlet Pressure Low High
6 Combustion Chamber wall
Temperature
Low High
7 Speed High Low
8 Cylinder Size Small Large
Methods of controlling diesel knocka) Design and operating factors for reducing delay
period
The delay period can be reduced by reducing the degree of turbulence as it will reduce heat loss. degree of turbulence as it will reduce heat loss. However, it will increase the combustion period.
b) High rate of pressure rise and high maximum pressure in the second stage if large amount of fuel collects during the delay period.
It can be reduced by arranging the injector so that only a small amount of fuel is injected at first.
c) The delay angle is reduced (cetane number is
increased) by adding chemical dopes.
� The two chemical dopes added are ethyl nitrate
and amyl nitrate in concentrations of 8.8gm/litre
and 7.7gm/litre respectively
Methods of controlling diesel knock
and 7.7gm/litre respectively
� The chemical dopes increase the cetane number
and accelerate the pre-flame reactions and
reduce the flash point.
� NOx emissions will be a problem.
COMBUSTION CHAMBER
�It is the space within the cylinder when the piston
is at the top dead centre.
�It is formed by the top of the piston and a cavity�It is formed by the top of the piston and a cavity
in the cylinder head.
�Since the air-fuel mixture burns in this space, its
design and shape greatly affect the power, fuel
efficiency and emissions of the engine.
Factors to be considered while designing a
diesel engine combustion chamber• High thermal efficiency
• Fuel requirement – ability to use less expensive fuel; multi fuel capability
• Ease of starting• Ease of starting
• Variable speed operation
• Smoothness of operation, without knock
• Low exhaust emissions
• Simple nozzle design
• High volumetric efficiency
• High brake mean effective pressure
Classification of CI Engine combustion Chambers
CI Engine Combustion Chambers
Open Chamber Divided Chamber
OrOr
Turbulent Chamber
Swirl Chamber Pre-Combustion Chamber Air Cell Chamber
Combustion Induced Swirl
Induction Swirl
Compression Swirl
CI Engine combustion chambers
Air motion - Proper mixing of fuel in a short timeThree parameters are used to characterize large-
scale in-cylinder fluid motion: swirl, squish, and
tumble.
Swirl is the rotational flow about the cylinder axis.Swirl is the rotational flow about the cylinder axis.
Swirl is used to:
Rapidly mix fuel and air in direct injection engines
The swirl is generated during air induction into the
cylinder by either:
i) tangentially directing the flow into the cylinder,
or
ii) pre-swirling the incoming flow by the use of
helical ports.
Induction Swirl and Open Combustion Chambers
Induction Swirl can be achieved by
�Careful formation of the air intake passages
�Making or shrouding the intake valve
Squish
• Induction swirl is augmented by secondary air
movement called squish
• Squish is the radial inward movement of air
towards the combustion recess by squeezing it towards the combustion recess by squeezing it
out from between the piston and cylinder
head as they approach each other at the end
of the stroke.
Important point to be noted
• With a weak swirl, single hole nozzle cannot
provide desired air-fuel mixing.
• Hence, always multi hole nozzle (4 to 8 @ 1.2
to 1.5mm) is preferred for open combustion to 1.5mm) is preferred for open combustion
chambers
Direct and indirect injection systems
Direct Injection (DI) System. In this system, fuel is injected
directly into a combustion chamber formed in the cylinder itself,i.e. between a suitably shaped non-stationary piston crown and afixed cylinder head in which is mounted the fuel injector with itssingle or multiple spray orifices or nozzles.
Quiescent combustion system. Application-Four-stroke and two-
stroke engines mostly above 150 mm bore
Direct injection combustion systems
The wide flat chambers are associated with high pressure injectionsystems and the deeper bowls are used with high swirl, lowinjection pressure systems. Direct injection engines dependprimarily on the kinetic energy of the fuel spray to mix the air andfuel. This dependence increases the importance of the fuelinjection system for optimizing the combustion system in DIengines. Increased air swirl can enhance the fuel-air mixing andextend the smoke limiting fuel-air ratio, but it increases NOx at thesame time.
Direct Injection
High swirl system
Application to all truck and bus engines, but increasingly to the high speed
passenger car engine
Indirect InjectionIndirect Injection (IDI) Systems as used in IDI engines in which
fuel is injected into a prechamber which communicates with thecylinder through a narrow passage. The rapid transfer of air from themain cylinder into the prechamber towards top dead centre (TDC) ofthe firing stroke promotes a very high degree of air motion in theprechamber which is particularly conducive to rapid fuel-air mixing.
Prechamber system-compression swirl. Application traditionally to high speed passenger car engines but now increasingly replaced by direct
injection engine
Classification of indirect combustion
chambers
Swirl chamber� It consists of a spherical chamber located in the
cylinder head and separated from the engine cylinderby a tangential throat. About 30 to 50% of the airenters the swirl chamber during the compressionstroke of the engine, producing a swirl.enters the swirl chamber during the compressionstroke of the engine, producing a swirl.
� After combustion, the products return through thesame throat to the main cylinder at much highervelocity. So more heat loss to walls of the passagetakes place. This type of chamber finds application inengines in which fuel control and engine stability aremore important than fuel economy.
Pre-combustion chamber� This chamber is located at the cylinder head and is
connected to the engine cylinder by small holes. Itoccupies 40% of the total cylinder volume. During thecompression stroke, air from the main cylinder entersthe precombustion chamber. At this moment, fuel is
Classification of indirect combustion
chambers
the precombustion chamber. At this moment, fuel isinjected into the precombustion chamber andcombustion begins. Pressure increases and the fueldroplets are forced through the small holes into themain cylinder, resulting in a very good mix of the fueland air. The bulk of the combustion actually takes placein the main cylinder. This type of combustion chamberhas multi-fuel capability because the temperature ofthe prechamber vaporizes the fuel before the maincombustion event occurs
• Air cell chamber• The air cell is a small cylindrical chamber with a hole in one
end. It is mounted more or less coaxially with the injector,on opposite sides, axis being parallel to the piston crown,with the injector firing across a small cavity which is opento the cylinder into the hole in the end of the air cell. Theair cell is mounted so as to minimise thermal contact with
Classification of indirect combustion
chambers
air cell is mounted so as to minimise thermal contact withthe mass of the head. A pintle injector with a narrow spraypattern is used. At TDC the majority of the charge mass iscontained in the cavity and air cell.
• Air cell injection is considered as a sort of half way stagebetween fully indirect and fully direct injection, gainingsome of the efficiency advantages of direct injection whileretaining the simplicity and ease of indirect injection
Advantages of Induction swirl
1. High excess air allows low average combustion
temperature. Low turbulence and low heat losses permits
ηthermal to approach ideal cycle efficiency
2. Intensity of swirl is low – heat losses to chamber wall is less
– easy cold starting
3. Swirl is obtained during suction stroke – no additional work
for creating swirl. Hence better ηbrake thermal and fuel economy.for creating swirl. Hence better ηbrake thermal and fuel economy.
4. When used in low speed engines, poor quality fuel can be
used as injection spreads for a long duration of time.
5. When used in high speed engines, high cetane fuel
produces good thermal efficiency with better swirl results
in better economy.
6. Very simple in construction
1. As the swirl is of low intensity, multi hole nozzles with high
injection pressure is required – problems like clogging, low
injection quantity etc
2. Use of shrouded valves lowers ηVol. Injector has to be located at
the centre of the CC, restricting the size of the valve in multi valve
Disadvantages of Induction swirl
the centre of the CC, restricting the size of the valve in multi valve
engines
3. Mixing of fuel and air and fuel is not easy at low speeds and high
loads
4. Weak swirl necessitates excess air ie low air utilisation, hence low
mean effective pressure
5. Swirl is not proportional to engine speed, hence efficiency is not
maintained over a wide speed range in a variable speed engine.
1. Due to strong swirl, single orifice injector with low injection pressure can be used. Pintle type nozzle with self cleaning capacity can be used
2. Due to strong swirl, better utilization of air. Hence higher mean effective pressure.
3. As the injector is located inside the swirl chamber, valves of
Advantages of Compression swirl
3. As the injector is located inside the swirl chamber, valves of larger diameter can be conveniently located, hence better volumetric efficiency.
4. Swirl is proportional to speed, hence more suitable for variable speed engines.
5. Transfer of air from the main chamber to swirl chamber heats air, hence delay period can be reduced.
6. Engine operation is smooth because, the initial shock of peak pressure is absorbed by the swirl chamber.
1. The work done during compression and expansion are
considerable. Hence ηmech is lower. ηIThermal is also lower due
to low excess air. 5 to 8% excess fuel consumption.
2. Due to the high intensity of swirl, heat losses to the CC walls is
high. S/V ratio is also high as the CC is not compact.
Disadvantages of Compression swirl
high. S/V ratio is also high as the CC is not compact.
3. Cold starting is a very serious problem – glow plug is a must.
4. More heat is lost in the exhaust gases
5. Cylinder construction is more expensive
Comparison of induced and compression swirl
Induction Swirl Compression Swirl
Advantages Disadvantages
1. Indicated thermal efficiency
high due to high excess air
and low turbulence
2. Easier cold starting due to
1. Less excess air, low indicated
thermal efficiency. 5 to 8%
more fuel consumption.
Decreased exhaust valve life2. Easier cold starting due to
low intensity of swirl
3. No additional work required
for producing swirl
4. High mechanical and brake
thermal efficiency
5. Low quality of fuel can be
used when used for low
speed engines
Decreased exhaust valve life
2. Cold starting trouble due to
high heat loss due to strong
swirl, greater S/V ratio.
3. Work loss during
compression results in lower
mechanical efficiency
4. Cylinder complicated and
more expensive.
Induction Swirl Compression Swirl
Disadvantages Advantages
1. Weak swirl, multi orifice nozzle, high
injection pressure, clogging of holes.
High maintenance
2. Idling and high load complications due
to fuel mixing problems.
3. Shrouded valves, smaller valves,
1. Single hole injector can be used, less
maintenance
2. Large valves, higher volumetric
efficiency
3. Greater air utilisation due to strong
swirl
Comparison of induced and compression swirl
3. Shrouded valves, smaller valves,
restriction in inlet passage reduces
volumetric efficiency
4. Weak swirl, low air utilization, low
mean effective pressure
5. Swirl not proportional to speed.
Efficiency is not maintained in a
variable speed engine
swirl
4. Swirl proportional to speed, suitable
for variable speed operation
5. Smooth engine operation
• Dr. Meurer of MAN (Germany) in 1954 developed the
“M-Process” engine
• This engine was very silent, hence he named it as
“whisper” engine
M Combustion Chamber
“whisper” engine
• This belongs to the open combustion chamber category.
• Fuel spray impinges and spreads over the surface of the
spherical cavity in the piston.
M Combustion Chamber1.Fuel injected tangentially from a multi hole nozzle on the surface of
the chamber in the direction of the swirl.
2.Injected fuel spreads on the piston surface and forms a film of about 0.15mm thick.
3.As the film evaporates due to the heat of the piston, it starts burning. burning.
4.Combustion of the fuel is initiated by auto ignition of a small portion of fuel which is air borne.
5.The quantity of air borne fuel is controlled by selecting a proper distance between the nozzle tip and the combustion chamber wall.
6.The heat of the piston has to be within a temperature range to achieve fuel evaporation without causing thermal decomposition and carburizing of the fuel.
7. The fuel vapour rise from the hot surface and mix with the
swirling air in successive layers and combustion takes place in a
near homogeneous air-fuel mixture at the desired rate.
8. The rate of heat release is almost equal to the rate of evaporation
of fuel
M Combustion Chamber cond..
of fuel
9. Even though, the engine works on diesel cycle, its combustion
characteristics is almost like Otto cycle.
10. As thermal decomposition is prevented, soot formation is very
less.
Advantages of M Combustion Chamber
• Low rate of pressure rise
• Low smoke level
• Ability to operate on a wide range of liquid fuels
• Very less combustion noise• Very less combustion noise
Disadvantages of M Combustion Chamber
• Cold starting problem
• White smoke, diesel odour and high HC
emission when the engine is cold
• Low volumetric efficiency
CONCLUSION
• Both IDI and DI engines require small
clearances between the piston and the
cylinder head. This clearance restricts the
timing of exhaust valve closing and intaketiming of exhaust valve closing and intake
valve opening unless valve cutouts are
provided in the piston. These cutouts increase
piston cost and adversely affect the in-cylinder
flow field.