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Internal Combustion Engines
Lecture-11
Ujjwal KSaha, Ph.D.
Department of Mechanical EngineeringIndian Institute of Technology Guwahati
Prepared under
QIP-CD Cell Project
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Carburetion
The process of mixture preparation in an SIengine is called carburetion. This air-fuel mixtureis prepared outside the cylinder in a device
called CARBURETOR.
The carburetor atomizes the fuel and mixeswith air in different proportions for various LOAD
conditions.
Loads
Starting
Idling
Cruising
Accelerating
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Petrol & Diesel Engines
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Functions
It must run the engine smoothly by
supplying a correct mixture strength.
It must atomize, vaporize and mix thefuel homogeneously with air.
It must supply correct amount of air-fuel mixture in correct proportion under
all load conditions and speed of theengine.
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Factors affecting Carburetion
the quality of the fuel supplied
the time available for mixture preparation
the temperature of the incoming air
the engine speed
the design of the carburetor
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Remark
The temperature affects the vaporization offuel. High temperature leads to high rate of
vaporization. This is achieved by heating theinduction manifold in some cases. However,this causes a reduction in the power outputbecause of decrease in mass flow rate.
For high speed engines (3000 rpm), the timeavailable for mixture preparation is very small(0.02 sec).
The design of carburetor, as such, is verycomplicated because the optimum air-fuelratio varies over its operating range.
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Air-Fuel Mixtures
VaryLoad/speed
Chemically Correct (15:1) Rich Mixture (10:1) Lean Mixture (17:1)
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Variation of power output and sfc with A-F ratio in SI engine(Full thro ttle a nd c onsta nt sp eed )
Maximum Output = 12:1 (Best power mixture)
Minimum Fuel Consumption = 16:1(Best economy mixture)
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Various Loads
Idling/Starting: Engine runs without load.Produces power only to overcome frictionbetween the parts. Rich mixture is required tosustain combustion.
Normal Power/Cruising/Medium Load: Engine
runs for most of the period. Therefore, fueleconomy is maintained. Low fuel consumptionfor maximum economy.Requires a lean mixture.
Maximum power/Acceleration: Overtaking avehicle (short period) or climbing up a hill (extraload). Requires a rich mixture.
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Carburetor Performance
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Simple Carburetor
Fuel
Float
Vent
FloatChamber
Throttle
Fuel dischargenozzle
Fuel meteringjet lip, h
Choke
Air
InletValve
Fuelfromsupply
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A float chamber with a float tostore fuel and to adjust its level
A choke valve to control the air supply in
order to provide a rich or a lean mixture
A round cylinder with a venturifor atomization of fuel.
A fuel nozzle to atomize and produce aspray of fuel
A throttle valve to supply varying quantityof the mixture at different load conditions
Components of a Simple Carburetor
Fuel
Float
Vent
FloatChamber
Throttle
Fuel dischargenozzle
Fuel metering
jet lip, h
Choke
Air
InletValve
Fuelfromsupply
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Venturi-type Carburetor
P+1/2 V2 = Constant
Bernoulli Effect:
Valve StemFuel Inlet
Float
Metering Orifice
Throttle Plate
Air/Fuel Mixture To Engine
Choke Plate
Fuel
Nozzle
Inlet Air
Bowl
Atomized Fuel
Venturi
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The fuel supply to the float chamber iscontrolled by the action of the float and the
attached fuel supply valve. During the intake orthe suction stroke of the engine, the pistonmoves from TDC to BDC, and creates a vacuumin the space above it and in the suction
manifold. Due to this fall in pressure, theatmospheric air rushes into the carburetor. Nearthe venturi, velocity increases, pressure
decreases and the fuel comes out in the form ofa jet. The fuel gets mixed with air and goes intothe cylinder.
Operation
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Because of the narrow passage at the venturithroat, the air velocity increases but its pressure falls.This causes a partial vacuum (ca l led carbure to rdepression)at the venturi throat. This carburetordepression causes fuel to come out as jet in theform of a spray. This fuel spray vaporizes and mixeswith the incoming air, and the mixture goes into thecylinder through the throttle valve.
Operation
Fuel
Higher Pressure
Outside Engine
VenturiChoke Throttle
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A simple carburetor as describedsuffers from the fact that it provides therequired air-fuel ratio only at onethrottle position.
At all other throttle positions, themixture is either leaner or richerdepending on whether the throttle is
opened less or more.
Drawback of Simple Carburetor
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Drawback of Simple Carburetor
Throttle opening changes the velocityof air. The opening changes the
pressure differential between the floatchamber and venturi throat, andregulates the fuel flow through thenozzle.
Increased throttle opening gives arich mixture. Opening of throttle usually
increases engine speed. However, asload is also a factor (e.g., climbing anuphill), opening the throttle may notincrease the speed.
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Calculation of Air-Fuel Ratio
Let the tip ofthe fuel nozzlebe at a height z
from fuel levelin the floatchamber.
i.e., we need tocalculate
mA a
F mf
=
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2 1 2 1
1 2 2( )
2
q w h h c c = +
Applying SFEE between A-A (point 1) and B-B
(point 2) and considering unit mass of airflow
For adiabatic flow,
10, 0, 0q w and c= = We have,
2 1 2
2 1 2
2( )
2 ( )
c h h
c C T T p
= =
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1
211
11 1
1 2
2 2
2
2 2 1
A Cma
vk
kA pm C Ta p
pkRT p
p p
gives =
=
Finally, we have12
2 2
1 1
2 1( ) 2
1
kk kA p p p
m Ca theoretical p p pR T
+
=
( ) ( )m C ma actual d a theoreticalt
=
argwhere C coefficient of disch e of venturi throatdt =
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To find mass flow rate of fuel
1 2 2
2
2
p p C
zg = + +
Assuming fuel to be incompressible, we havefrom Bernoullis theorem
1 2
2
2
f
f f
Cp p
gz = +
1 2
2ff
p p
C gz
=
fbeing the density of fuel, Cfis the fuel velocity
at the nozzle exit and z is the nozzle lip.
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Thus, we have velocity of fuel at the nozzle exit
argwhere C coefficient of disch e of fuel nozzled
f
=
1 2
( )
( ) 2 ( )
ff
f
f f
f f f
m A Ctheoretical
m A p p gztheoretical
=
=
( ) ( )f f
m C mactual d theoreticalf
=
1 22f
f
p pC gz
=
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A simple carburetor is capable to supply acorrect air-fuel mixture to the engine only at aparticular load and speed. In order to meet the
engine demand at various operating conditions,the following additional systems are added to thesimple carburetor.
idling system
auxiliary port system
power enrichment by economizer system accelerating pump system
choke
Complete Carburetor
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During startingor idling, engineruns without load
and the throttlevalve remains inclosed position.
Engine producespower only toovercome frictionbetween the parts,and a rich mixtureis to be fed to theengine to sustain
combustion.
Idling system
Idling jet
Air bleed
Adjustingscrew
Float chamber
Mainjet
Air
Throttle
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The idling system as
shown consists of an idlingfuel passage and an idlingport. When the throttle ispartially closed, adepression past the throttleallows the fuel to go intothe intake through the idle
tube. The depression alsodraws air through the idleair bleed and mixes with
fuel. The fuel flow dependson the location of the idlenozzle and the adjustment
of the idle screw.
Idling system contd.
Idling jet
Air bleed
Adjusting
screw
Float chamber
Mainjet
Air
Throttle
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During normal power orcruising operation, where theengine runs for most of theperiod, the fuel economy hasto be maintained. Thus, it is
necessary to have lower fuelconsumption for maximumeconomy. One sucharrangement used is the
auxiliary port carburetor asshown, where opening ofbutterfly valve allowsadditional air to be admitted,and at the same timedepression at the venturithroat gets reduced, thereby
decreasing the fuel flow rate.
Auxiliary port system
Butterflyvalve
Throttle
Main jet
Air
Air +Fuel
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During sudden
acceleration of anengine (e.g., overtakinga vehicle), an extraamount of fuel is
momentarily required tosupply a rich mixture.This is obtained by anaccelerating pumpsystem. It consists of aspring-loaded plunger,and the necessary
linkage mechanism.
Accelerating pump system
Pump
Open
Plunger
Floatchamber
Accelerating pump system
The rapid opening of the throttle moves theplunger into the cylinder, and an additional
amount of fuel is forced into the venturi.
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During cold starting period, at low crankingspeed and before the engine gets warmed up,
a rich mixture has to be supplied, simplybecause a large fraction of the fuel remains inliquid state in the cylinder, and only the vaporfraction forms the combustible mixture with air.The most common method of obtaining this richmixture is to use a choke valve between theentry to the carburetor and the venturi throat.
Remark
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Up-draught (updraft) carburetor Down-draught (downdraft) carburetor
Cross-draught or horizontal carburetor
Types of Carburetor
based on direction of flow
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A single barrel carburetor has one outletconnected to the intake manifold of engine.
Multi-barrel Carburetor
A multi-barrel barrel carburetor is one with twooutlets connected to two intake manifolds ofengine. Such unit is basically one with twocarburetors.
As such, a multi-barrel barrel carburetor hastwo numbers of idling, power and acceleratingsystems, two chokes, two throttles but withalternate cylinders in the firing order. As forexample, in a six cylinder engine, one barrelsupplies mixture to cylinders 1, 3 and 2; while
the other barrel supplies to 5, 6 and 4.
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Automobile carburetors are calibrated atsea-level conditions
Aircraft Carburetors
Lower altitudes (than sea-level): Lean mixture
Higher altitudes (than sea-level): Rich mixture
(emits hydrocarbon, CO)
At higher altitudes, density decreases andhence, the mass flow rate gets reduced.
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Enrichment(due to variation of air density)
If /0 = 0.84,
0
0
0
0
0
1
1
1
E
p RTERT p
p TE pT
+ =
+ =
+ =
11 1.091
0.84
0.091 9.1 %
E
E
+ = =
= =
Enrichment of mixture over the calibrated ratio
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Altitude Compensation Device
Admit more air and less fuel into the
induction manifold.
METHODS
As density decreases, the mass flow rate also
decreases and hence the Power gets reduced.
Reduction of pressure in float chamber Auxiliary air valve/air port
Supercharger
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Summary
2. Most carbureted (as opposed to fuelinjected) engines have a single carburetor,though some, primarily higher performance
engines, can have multiple carburetors. Mostautomotive carburetors are either downdra f t (flow of air is downwards) or side-draf t(flow ofair is sideways). In the United States, downdraftcarburetors were almost ubiquitous, partlybecause a downdraft unit is ideal for Vengines. In Europe, side-draft carburetors are
much more common in performanceapplications. Small propeller-driven flatairplane engines have the carburetor belowthe engine (updraft).
References
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1.1. Crouse WH,Crouse WH, andandAnglin DLAnglin DL, (1985),Automotive Engines,Tata McGraw Hill.
2.2. Eastop TD,Eastop TD, andand McConkey A,McConkey A, (1993), Applied Thermodynamics for Engg.Technologists, Addison Wisley.
3.3. Fergusan CR,Fergusan CR, andand Kirkpatrick ATKirkpatrick AT,, (2001), Internal Combustion Engines, JohnWiley & Sons.
4.4. Ganesan VGanesan V,, (2003), Internal Combustion Engines,Tata McGraw Hill.
5.5. Gill PW, Smith JH,Gill PW, Smith JH, andandZiurys EJZiurys EJ,, (1959), Fundamentals of I. C. Engines, Oxfordand IBH Pub Ltd.
6.6. Heisler H,Heisler H, (1999), Vehicle and Engine Technology,Arnold Publishers.
7.7. Heywood JB,Heywood JB, (1989), Internal Combustion Engine Fundamentals, McGraw Hill.
8.8. Heywood JB,Heywood JB, andandSher E,Sher E, (1999), The Two-Stroke Cycle Engine,Taylor & Francis.
9.9. Joel R,Joel R, (1996),(1996), Basic Engineering Thermodynamics,Addison-Wesley.
10.10. Mathur ML, and Sharma RP,Mathur ML, and Sharma RP, (1994), A Course in Internal Combustion Engines,Dhanpat Rai & Sons, New Delhi.
11.11. Pulkrabek WW,Pulkrabek WW, (1997),Engineering Fundamentals of the I. C. Engine, Prentice Hall.
12.12. Rogers GFC,Rogers GFC, andand Mayhew YRMayhew YR, (1992), Engineering Thermodynamics, AddisonWisley.
13.13. Srinivasan S,Srinivasan S, (2001),Automotive Engines,Tata McGraw Hill.
14.14. Stone R,Stone R, (1992), Internal Combustion Engines,The Macmillan Press Limited, London.
15.15. Taylor CF,Taylor CF, (1985), The Internal-Combustion Engine in Theory and Practice,Vol.1 & 2,
The MIT Press, Cambridge, Massachusetts.
References
Web Resources
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1. http://www.mne.psu.edu/simpson/courses
2. http://me.queensu.ca/courses3. http://www.eng.fsu.edu4. http://www.personal.utulsa.edu5. http://www.glenroseffa.org/6. http://www.howstuffworks.com7. http://www.me.psu.edu8. http://www.uic.edu/classes/me/ me429/lecture-air-cyc-web%5B1%5D.ppt9. http://www.osti.gov/fcvt/HETE2004/Stable.pdf10. http://www.rmi.org/sitepages/pid457.php11. http://www.tpub.com/content/engine/14081/css12. http://webpages.csus.edu
13. http://www.nebo.edu/misc/learning_resources/ ppt/6-1214. http://netlogo.modelingcomplexity.org/Small_engines.ppt15. http://www.ku.edu/~kunrotc/academics/180/Lesson%2008%20Diesel.ppt16. http://navsci.berkeley.edu/NS10/PPT/17. http://www.career-center.org/ secondary/powerpoint/sge-parts.ppt
18. http://mcdetflw.tecom.usmc.mil19. http://ferl.becta.org.uk/display.cfm20. http://www.eng.fsu.edu/ME_senior_design/2002/folder14/ccd/Combustion21. http://www.me.udel.edu22. http://online.physics.uiuc.edu/courses/phys14023. http://widget.ecn.purdue.edu/~yanchen/ME200/ME200-8.ppt -
Web Resources