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CHAPTER 2
Thermodynamics of IC Engines
2.1 Introduction
 The cycle experienced in the cylinder of an internal combustion engine is
very complex.
 First, air (CI engine) or air mixed with fuel (SI engine) is ingested and
mixed with the slight amount of exhaust residual remaining from the
previous cycle.
 This mixture is then compressed and combusted, changing the composition
to exhaust products consisting largely of CO2, H20, and N2 with many other
lesser components.
Con…………
 Then, after an expansion process, the exhaust valve is opened and this gas
mixture is expelled to the surroundings.
 Thus, it is an open cycle with changing composition, a difficult system to
analyze.
 To make the analysis of the engine cycle much more manageable, the real
cycle is approximated with an ideal air-standard cycle.
Con…………
The Three Thermodynamic Analysis of IC Engines are
I. Ideal Gas Cycle (Air Standard Cycle)
 Idealized processes
 Idealize working Fluid
II. Fuel-Air Cycle
 Idealized Processes
 Accurate Working Fluid Model
III. Actual Engine Cycle
 Accurate Models of Processes
 Accurate Working Fluid Model
Con…......
 The operating cycle of an IC engine can be broken down into a sequence
of separate processes
Intake, Compression, Expansion and Exhaust.
 The accurate analysis of IC engine processes is very complicated, to
understand it well, it is advantageous to analyze the performance of an
Idealized closed cycle.
2.2 Air Standard Cycles
Air-Standard cycle differs from the actual by the following
1. The gas mixture in the cylinder is treated as air for the entire cycle, and
property values of air are used in the analysis.
2. The real open cycle is changed into a closed cycle by assuming that the
gases being exhausted are fed back into the intake system.
3. The combustion process is replaced with a heat addition term Qin of
equal energy value
Con………
4. Actual engine processes are approximated with ideal processes
a. The almost-constant-pressure intake and exhaust strokes are assumed to be
constant pressure.
b. Compression strokes and expansion strokes are approximated by isentropic
processes
c. The combustion process is idealized by a constant-volume process (SI cycle),
a constant-pressure process (CI cycle), or a combination of both (CI Dual
cycle).
d. Exhaust blow down is approximated by a constant-volume process.
e. All processes are considered reversible
Con………
 In air-standard cycles, air is considered an ideal gas such that the following
ideal gas relationships can be used:
Isentropic Process
 Isentropic process is a special case of an adiabatic process in which there
is no transfer of heat or matter.
 For an ideal gas k is constant.
 Using the equation of state for an ideal gas
Air Properties
 For thermodynamic analysis the specific heats of air can be treated as functions of
temperature, which they are, or they can be treated as constants, which simplifies
calculations at a slight loss of accuracy.
Because of the high temperatures and large temperature range experienced during
an engine cycle, the specific heats and ratio of specific heats k do vary by a fair
amount.
 At the low-temperature end of a cycle during intake and start of compression, a
value of k = 1.4 is correct. However, at the end of combustion the temperature has
risen such that k = 1.3 would be more accurate.
2.2.1 Otto Cycle
 The Otto cycle is one of the most common thermodynamic cycles found in
automobile engines and describes the functioning of a typical Spark
Ignition Engine.
 A typical gasoline automotive engine operates at around 25% to 30% of
thermal efficiency.
Con………..
Intake Stroke
 Starts with the piston at TDC
 Constant pressure process at the inlet
pressure of one atmosphere.
 In real engine process 0-1 will be slightly less
than atmospheric due to pressure losses in the
inlet air flow.
 The temperature of the air during the inlet
stroke is increased as the air passes through
the hot intake manifold.
Con………..
Compression Stroke
 It is an isentropic compression from BDC to TDC
(process 1-2)
(Isentropic process is a special case of an adiabatic process in which there is no
transfer of heat or matter.)
 In real engine, the beginning of the stroke is affected by
the intake valve not being fully closed until slightly
after BDC.
 The end of compression is affected by the firing of the
sparkplug before TDC.
 In addition to increase in pressure there is also increase
in temperature due to compressive heating
Con………..
Combustion Process
 It is a constant-volume heat input process 2-3 at
TDC while the piston is at rest at the top dead
center.
 In real engines combustion starts slightly bTDC,
reaches its maximum speed near TDC, is
terminated a little aTDC.
 Peak cycle pressure and temperature is reached at
point 3 due to energy added to the air within the
cylinder.
Con………..
Power (Expansion) Stroke
 The gas expands adiabatically from state 3 to
state 4 as the piston moves from top dead
center to bottom dead center.
 The power stroke of the real engine cycle is
approximated with an isentropic process in the
Otto cycle.
 Values of both the temperature and pressure
within the cylinder decrease as volume
increases from TDC to BDC.
Con………..
Exhaust Blowdown
 Exhaust valve is opened near the end of the power
stroke
 A large amount of exhaust gas is expelled from the
cylinder, reducing the pressure to that of the exhaust
manifold
 The exhaust valve is opened bBDC to allow for the
finite time of blowdown to occur.
 The Otto cycle replaces the exhaust blowdown open-
system process of the real cycle with a constant–
volume pressure reduction, closed-system process.
Con………..
Exhaust Stroke
 Occurs as the piston travels from BDC to
TDC.
 Process 5-6 is the exhaust stroke that occurs
at a constant pressure of one atmosphere
due to the open exhaust valve.
Con………
Point 0 to 1 - Constant Pressure Intake
Point 1 to 2 - Isentropic Compression
Point 2 to 3 - Constant Volume Heat Input
Point 3 to 4 - Isentropic Expansion
Point 4 to 1 - Blow Down
Point 1 to 0 - Exhaust
Otto Cycle
Closing Thoughts on Otto Cycle
 The Otto-cycle efficiency serves as an upper limit to the efficiency of
SI engines.
 In practice this efficiency is never achieved.
 This theoretical analysis is flawed in that it ignores friction and heat
transfer.
2.2.2 Diesel Cycle
 Fuel is injected into the combustion chamber very late in the compression
stroke.
 Due to ignition delay and the finite time required to inject the fuel,
combustion lasted into the expansion stroke
 This keeps the pressure at peak levels well past TDC.
 Combustion process is approximated as constant-pressure heat input in an
air standard cycle
con………
Point 0 to 1 - Constant Pressure Intake
Point 1 to 2 - Isentropic Compression
Point 2 to 3 - Constant Pressure Heat Input
Point 3 to 4 - Isentropic Expansion
Point 4 to 1 - Blow Down
Point 1 to 0 - Exhaust
Diesel Cycle
Cut of ratio
Cut of Ratio (β): The change in volume that occurs during combustion, given
as a ratio.
Con………….
Thermal efficiency of Diesel Cycle
Note: the term in the square bracket is always larger than unity so for the same
compression ratio the Diesel cycle has a lower thermal efficiency than the Otto
cycle
2.2.3 Dual Cycle
 Fuel is injected earlier in the compression stroke, around 20 deg bTDC
 Some of the combustion occurs almost at constant volume at TDC similar
to Otto Cycle
 The fuel is being injected at TDC, and combustion of this fuel keeps the
pressure high into the expansion stroke.
 The heat input process of combustion is approximated by a dual process of
constant volume followed by constant pressure.
Con…………
Comparison of Otto, Diesel, and Dual Cycles
 For the same inlet conditions, the same
compression ratios and same heat removal:
Con………
 For the same inlet conditions, the same
peak pressure and same heat removal :
2.3 Fuel-Air Cycle
 The theoretical cycle based on the actual properties of the cylinder contents
is called the fuel air cycle.
 The fuel air cycle take the following into consideration:
1. The actual composition of the cylinder contents.
2. The variation in the specific heat of the gases in the cylinder.
3. The dissociation effect.
Con………..
4. Compression & expansion processes are frictionless
5. No chemical changes in either fuel or air prior to combustion.
6. Combustion takes place instantaneously at top dead center.
7. All processes are adiabatic.
8. The fuel is mixed well with air.
Composition of Cylinder Gases
 The composition of the working fluid, which changes during the engine
operating cycle, is indicated in the following table:
Variable Specific Heats
 All gases except mono-atomic gases, show an increase in specific heat with
temperature. The increase in specific heat does not follow any particular law.
 However between the temperature range 300 K – 1500 K the specific heat curve
is nearly a straight line.
 Above 1500 K the specific heat increases is much more rapid and may be
expressed in the form
Con……….
 Since the difference between Cp & Cv is constant, the value of k decreases
with increase in temperature
 Thus, if the variation of specific heats is taken in to account during the
compression stroke, the final temperature and pressure would be lower
compared to the value obtained at constant specific heat.
Loss Due to Variable Specific Heats
 The magnitude of drop of temperature at the end of compression is
proportional to the drop in values of ratio of specific heats.
Dissociation
The effect of dissociation
 Dissociation is the disintegration of combustion products, at high
temperature above 1600K.
 Dissociation is the reverse process to combustion
 Dissociation is the heat absorption (endothermic process)
 Combustion is heat liberation (Exothermic process)
 In IC engine, mainly dissociation of CO2 and little dissociation of H20
Con…………
Con……….
 There is no dissociation in the burnt gases of a lean fuel-air mixture. This
mainly due to the fact that the temperature produced is too low for this
phenomenon to occur.
 The maximum dissociation occurs in the burnt gases of the chemically
correct fuel-air mixture when the temperature are expected to be high but
decreases with the leaner and richer mixtures.
The Effect of Dissociation
 On Exhaust Gas Temperature, the
Figure shows the reduction in the
temperature of the exhaust gas mixtures
due to dissociation w.r.t air fuel ratio.
The Effect of Dissociation
On the p-v diagram of Otto Cycle
 Because of lower maximum
temperature due to dissociation. The
maximum pressure is also reduced
and state after combustion will be
replaced by 3’ instead of 3.
2.4 The Actual Cycle
 The actual cycle experienced by internal combustion engines is an open
cycle with changing composition, actual cycle efficiency is much lower
than the air standard efficiency due to various losses occurring in the actual
engine.
Con………
These losses are as follows:
1. Losses due to variation of specific
heats with temperature
2. Losses due to dissociation.
3. Time losses, effect of spark timing
4. Incomplete combustion loss.
5. Direct heat loss.
6. Exhaust blow down loss.
7. Pumping losses.
8. Friction losses.
9. Effect of throttle opening
Con………
‘Actual’Cycle Processes of SI Engines
‘Actual’Cycle Processes of CI Engines
THANK YOU!!

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Chapter 2 .pptxvbbhdsssfghjnbxssscbnnxaasvn

  • 2. 2.1 Introduction  The cycle experienced in the cylinder of an internal combustion engine is very complex.  First, air (CI engine) or air mixed with fuel (SI engine) is ingested and mixed with the slight amount of exhaust residual remaining from the previous cycle.  This mixture is then compressed and combusted, changing the composition to exhaust products consisting largely of CO2, H20, and N2 with many other lesser components.
  • 3. Con…………  Then, after an expansion process, the exhaust valve is opened and this gas mixture is expelled to the surroundings.  Thus, it is an open cycle with changing composition, a difficult system to analyze.  To make the analysis of the engine cycle much more manageable, the real cycle is approximated with an ideal air-standard cycle.
  • 4. Con………… The Three Thermodynamic Analysis of IC Engines are I. Ideal Gas Cycle (Air Standard Cycle)  Idealized processes  Idealize working Fluid II. Fuel-Air Cycle  Idealized Processes  Accurate Working Fluid Model III. Actual Engine Cycle  Accurate Models of Processes  Accurate Working Fluid Model
  • 5. Con…......  The operating cycle of an IC engine can be broken down into a sequence of separate processes Intake, Compression, Expansion and Exhaust.  The accurate analysis of IC engine processes is very complicated, to understand it well, it is advantageous to analyze the performance of an Idealized closed cycle.
  • 6. 2.2 Air Standard Cycles Air-Standard cycle differs from the actual by the following 1. The gas mixture in the cylinder is treated as air for the entire cycle, and property values of air are used in the analysis. 2. The real open cycle is changed into a closed cycle by assuming that the gases being exhausted are fed back into the intake system. 3. The combustion process is replaced with a heat addition term Qin of equal energy value
  • 7. Con……… 4. Actual engine processes are approximated with ideal processes a. The almost-constant-pressure intake and exhaust strokes are assumed to be constant pressure. b. Compression strokes and expansion strokes are approximated by isentropic processes c. The combustion process is idealized by a constant-volume process (SI cycle), a constant-pressure process (CI cycle), or a combination of both (CI Dual cycle). d. Exhaust blow down is approximated by a constant-volume process. e. All processes are considered reversible
  • 8. Con………  In air-standard cycles, air is considered an ideal gas such that the following ideal gas relationships can be used:
  • 9. Isentropic Process  Isentropic process is a special case of an adiabatic process in which there is no transfer of heat or matter.  For an ideal gas k is constant.  Using the equation of state for an ideal gas
  • 10. Air Properties  For thermodynamic analysis the specific heats of air can be treated as functions of temperature, which they are, or they can be treated as constants, which simplifies calculations at a slight loss of accuracy. Because of the high temperatures and large temperature range experienced during an engine cycle, the specific heats and ratio of specific heats k do vary by a fair amount.  At the low-temperature end of a cycle during intake and start of compression, a value of k = 1.4 is correct. However, at the end of combustion the temperature has risen such that k = 1.3 would be more accurate.
  • 11. 2.2.1 Otto Cycle  The Otto cycle is one of the most common thermodynamic cycles found in automobile engines and describes the functioning of a typical Spark Ignition Engine.  A typical gasoline automotive engine operates at around 25% to 30% of thermal efficiency.
  • 12. Con……….. Intake Stroke  Starts with the piston at TDC  Constant pressure process at the inlet pressure of one atmosphere.  In real engine process 0-1 will be slightly less than atmospheric due to pressure losses in the inlet air flow.  The temperature of the air during the inlet stroke is increased as the air passes through the hot intake manifold.
  • 13. Con……….. Compression Stroke  It is an isentropic compression from BDC to TDC (process 1-2) (Isentropic process is a special case of an adiabatic process in which there is no transfer of heat or matter.)  In real engine, the beginning of the stroke is affected by the intake valve not being fully closed until slightly after BDC.  The end of compression is affected by the firing of the sparkplug before TDC.  In addition to increase in pressure there is also increase in temperature due to compressive heating
  • 14. Con……….. Combustion Process  It is a constant-volume heat input process 2-3 at TDC while the piston is at rest at the top dead center.  In real engines combustion starts slightly bTDC, reaches its maximum speed near TDC, is terminated a little aTDC.  Peak cycle pressure and temperature is reached at point 3 due to energy added to the air within the cylinder.
  • 15. Con……….. Power (Expansion) Stroke  The gas expands adiabatically from state 3 to state 4 as the piston moves from top dead center to bottom dead center.  The power stroke of the real engine cycle is approximated with an isentropic process in the Otto cycle.  Values of both the temperature and pressure within the cylinder decrease as volume increases from TDC to BDC.
  • 16. Con……….. Exhaust Blowdown  Exhaust valve is opened near the end of the power stroke  A large amount of exhaust gas is expelled from the cylinder, reducing the pressure to that of the exhaust manifold  The exhaust valve is opened bBDC to allow for the finite time of blowdown to occur.  The Otto cycle replaces the exhaust blowdown open- system process of the real cycle with a constant– volume pressure reduction, closed-system process.
  • 17. Con……….. Exhaust Stroke  Occurs as the piston travels from BDC to TDC.  Process 5-6 is the exhaust stroke that occurs at a constant pressure of one atmosphere due to the open exhaust valve.
  • 18. Con……… Point 0 to 1 - Constant Pressure Intake Point 1 to 2 - Isentropic Compression Point 2 to 3 - Constant Volume Heat Input Point 3 to 4 - Isentropic Expansion Point 4 to 1 - Blow Down Point 1 to 0 - Exhaust Otto Cycle
  • 19. Closing Thoughts on Otto Cycle  The Otto-cycle efficiency serves as an upper limit to the efficiency of SI engines.  In practice this efficiency is never achieved.  This theoretical analysis is flawed in that it ignores friction and heat transfer.
  • 20. 2.2.2 Diesel Cycle  Fuel is injected into the combustion chamber very late in the compression stroke.  Due to ignition delay and the finite time required to inject the fuel, combustion lasted into the expansion stroke  This keeps the pressure at peak levels well past TDC.  Combustion process is approximated as constant-pressure heat input in an air standard cycle
  • 21. con……… Point 0 to 1 - Constant Pressure Intake Point 1 to 2 - Isentropic Compression Point 2 to 3 - Constant Pressure Heat Input Point 3 to 4 - Isentropic Expansion Point 4 to 1 - Blow Down Point 1 to 0 - Exhaust Diesel Cycle
  • 22. Cut of ratio Cut of Ratio (β): The change in volume that occurs during combustion, given as a ratio.
  • 23. Con…………. Thermal efficiency of Diesel Cycle Note: the term in the square bracket is always larger than unity so for the same compression ratio the Diesel cycle has a lower thermal efficiency than the Otto cycle
  • 24. 2.2.3 Dual Cycle  Fuel is injected earlier in the compression stroke, around 20 deg bTDC  Some of the combustion occurs almost at constant volume at TDC similar to Otto Cycle  The fuel is being injected at TDC, and combustion of this fuel keeps the pressure high into the expansion stroke.  The heat input process of combustion is approximated by a dual process of constant volume followed by constant pressure.
  • 26. Comparison of Otto, Diesel, and Dual Cycles  For the same inlet conditions, the same compression ratios and same heat removal:
  • 27. Con………  For the same inlet conditions, the same peak pressure and same heat removal :
  • 28. 2.3 Fuel-Air Cycle  The theoretical cycle based on the actual properties of the cylinder contents is called the fuel air cycle.  The fuel air cycle take the following into consideration: 1. The actual composition of the cylinder contents. 2. The variation in the specific heat of the gases in the cylinder. 3. The dissociation effect.
  • 29. Con……….. 4. Compression & expansion processes are frictionless 5. No chemical changes in either fuel or air prior to combustion. 6. Combustion takes place instantaneously at top dead center. 7. All processes are adiabatic. 8. The fuel is mixed well with air.
  • 30. Composition of Cylinder Gases  The composition of the working fluid, which changes during the engine operating cycle, is indicated in the following table:
  • 31. Variable Specific Heats  All gases except mono-atomic gases, show an increase in specific heat with temperature. The increase in specific heat does not follow any particular law.  However between the temperature range 300 K – 1500 K the specific heat curve is nearly a straight line.  Above 1500 K the specific heat increases is much more rapid and may be expressed in the form
  • 32. Con……….  Since the difference between Cp & Cv is constant, the value of k decreases with increase in temperature  Thus, if the variation of specific heats is taken in to account during the compression stroke, the final temperature and pressure would be lower compared to the value obtained at constant specific heat.
  • 33. Loss Due to Variable Specific Heats  The magnitude of drop of temperature at the end of compression is proportional to the drop in values of ratio of specific heats.
  • 34. Dissociation The effect of dissociation  Dissociation is the disintegration of combustion products, at high temperature above 1600K.  Dissociation is the reverse process to combustion  Dissociation is the heat absorption (endothermic process)  Combustion is heat liberation (Exothermic process)  In IC engine, mainly dissociation of CO2 and little dissociation of H20
  • 36. Con……….  There is no dissociation in the burnt gases of a lean fuel-air mixture. This mainly due to the fact that the temperature produced is too low for this phenomenon to occur.  The maximum dissociation occurs in the burnt gases of the chemically correct fuel-air mixture when the temperature are expected to be high but decreases with the leaner and richer mixtures.
  • 37. The Effect of Dissociation  On Exhaust Gas Temperature, the Figure shows the reduction in the temperature of the exhaust gas mixtures due to dissociation w.r.t air fuel ratio.
  • 38. The Effect of Dissociation On the p-v diagram of Otto Cycle  Because of lower maximum temperature due to dissociation. The maximum pressure is also reduced and state after combustion will be replaced by 3’ instead of 3.
  • 39. 2.4 The Actual Cycle  The actual cycle experienced by internal combustion engines is an open cycle with changing composition, actual cycle efficiency is much lower than the air standard efficiency due to various losses occurring in the actual engine.
  • 40. Con……… These losses are as follows: 1. Losses due to variation of specific heats with temperature 2. Losses due to dissociation. 3. Time losses, effect of spark timing 4. Incomplete combustion loss. 5. Direct heat loss. 6. Exhaust blow down loss. 7. Pumping losses. 8. Friction losses. 9. Effect of throttle opening
  • 41. Con……… ‘Actual’Cycle Processes of SI Engines ‘Actual’Cycle Processes of CI Engines