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    15

    The compression ignition enginee

    diesel engine

    Topics covered in thischapter

    The four-stroke compression ignition engine (CIE)

    The Diesel cycle and the dual combustion cycle

    The two-stroke CIEDiesel engine construction

    Direct injection engine

    Indirect injection engine

    Turbulence

    Induction stroke turbulence

    Combustion in a compression ignition engine

    Three phases of combustion

    Diesel fuel and products of combustion

    Flash point

    Pour point

    Cloud point

    Products of combustion

    Emissions limits

    Emissions control on CIE

    Particulate trap and selective catalyst reduction

    Exhaust gas recirculation (EGR)

    Rudolf Diesel (1858e1913) is generally accepted as the

    person who first developed an internal combustion engine

    that worked by injecting fuel into compressed air that

    was hot enough to ignite the fuel. His patent used these

    words: Compressing in a cylinder pure air to such an

    extent that the temperature thereby produced is far higher

    than the burning or igniting point of the fuel. The orig-inal diesel engines of the type shown in Fig. 15.1(a)

    were large and heavy, and they operated at slow speed;

    they were used for stationary engines and ships but

    were not considered suitable for use in road vehicles.

    Around the 1920s, developments in fuel injection

    equipment and other technologies led to the develop-

    ment of engines of the type shown in Fig. 15.1(b) that

    were suitable for use in road vehicles e these engines

    work on a cycle of operations that is known as the

    dual combustion cycle. For this reason some authorities

    suggest that the vehicle engines that work on the prin-

    ciple of compression ignition should be called compres-

    sion ignition engines (CIEs). In modern literature the

    terms are used interchangeably.

    The four-stroke compressionignition engine

    The four strokes (Fig. 15.2) are:

    1. The inlet valve is opened and pure air is drawn into

    the cylinder as the piston moves down. This is the

    induction stroke.

    2. Both of the valves are closed and the piston moves up

    the cylinder, compressing the air so that the

    temperature rises above the ignition point of the fuel.

    The high pressure and temperature is achieved by

    a high compression ratio of approximately 20:1. As

    the piston approaches top dead centre (TDC), fuel is

    injected so that ignition has started by the time that

    the piston starts on the next stroke.

    3. Both of the valves are closed and the piston is forced

    down the cylinder by the expanding gas and fuel

    injection continues for a short period. The fuel is shut

    off after a few degrees of crank rotation and the high

    pressure of the gas forces the piston down the

    cylinder on the power stroke.

    4. The exhaust valve is opened and the piston rises in

    the cylinder, expelling the spent gas through the

    exhaust port e at the end of this stroke the engine is

    ready to start the next cycle.

    The Diesel cycle and the dualcombustion cycle

    The difference between the two theoretical cycles can

    be seen in pressureevolume diagrams, which are graphs

    that are used to show how the gas pressure and the

    cylinder volume are related as the piston moves along

    the cylinder.

    2011 Allan Bonnick and Derek Newbold. Published by Elsevier Ltd. All rights reserved

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    The Diesel cycle

    Inthe Dieselcycle the fuel is injectedinto the hot air inthe

    cylinder and the pressureremains constantuntil fuel injec-

    tionceases.Thisis represented bythe linefrom1 to2 inthe

    pressureevolume diagram shown in Fig. 15.3(a). At point

    2 the gas in the cylinder continues to expand, pushing the

    piston along the remainder of the power stroke. Because

    the combustion takes place while the pressure remains

    constant, the Diesel cycle is also known as the constant-

    pressurecycle. This cycle is close to thesequence of eventsthat takes place in very large diesel engines that operate at

    slow speeds of a few hundred revolutions per minute.

    The dual combustion cycle

    In the dual combustion cycle (Fig. 15.3(b)) the fuel

    injection starts at point 1; this causes the pressure to

    rise rapidly, as shown by the vertical line that ends at

    point 2. In this first stage the combustion has taken place

    while the volume in the cylinder remains constant.

    Between points 2 and 3 further injection takes place,

    pushing the piston along the cylinder, while the pressure

    remains constant and the gas expands, pushing the

    piston down the cylinder. At point 3 combustion ceasesand the gas in the cylinder continues to expand, doing

    work on the piston until it reaches the end of the stroke.

    (a) (b)

    Fig. 15.1 (a) Diesel engine, 1897 (Mirlees). (b) Diesel engine, 2005 (MAN)

    Inlet valve Injector

    First stroke Induction.Inlet valve open pure airdrawn into cylinder as pistonmoves down the stroke.

    Second stroke Compression.Inlet and exhaust valvesclosed. Piston moves up thestroke. Air is compresseduntil it is very hot. Fuelsprayed into cylinder andignites.

    Third stroke Power.Both valves closed. Further fuelinjected. The burning fuel raisesthe pressure in the cylinder andforces the piston down the cylinderon the power stroke.

    Fourth stroke Exhaust.Exhaust valve opens. Pistonraises in the cylinder andexpels the spent gas. Exhaustvalve closes at end of strokeand inlet valve opens readyto start the next cycle.

    Fig. 15.2 The four-stroke compression ignition cycle

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    This theoretical cycle is considered to be close to the

    cycle of events that takes place in the compression igni-

    tion engines used in motor vehicles. Indicator diagrams

    for the Diesel cycle and the dual combustion cycle are

    shown in Fig. 15.3.

    The two-stroke CIEThe two-stroke CIE shown in Fig. 15.4 employs end-to-

    end scavenging, where there is a compressor that feeds

    compressed air to a ring of ports around the circumfer-

    ence of the cylinder and a pair of exhaust valves that

    are operated by a camshaft. The air ports are controlled

    by the piston. When the piston is at bottom dead centre

    the air ports are uncovered and air under pressure enters

    the cylinder. At this stage the cylinder is occupied by the

    exhausted gas from the previous power stroke e the

    entering fresh air is denser and at higher pressure than

    the exhaust and this, coupled with the upward motion

    of the piston, pushes the exhaust gas out through the

    open exhaust valves. As the piston rises further it covers

    the air ports; at this stage the exhaust valves close and the

    compression process begins. Towards the end of the

    compression stage, fuel is injected and combustion takes

    place to drive the piston down the cylinder on the power

    stage of the cycle. At the end of the compression stage the

    air ports are uncovered, the exhaust valves are opened,

    and the process is completed in two strokes of the piston.

    The compressor is similar to a supercharger and it is nor-mally gear driven from the crankshaft.

    Diesel engine construction

    Much of the diesel engine mechanism and structural

    details are similar to those found in petrol engines. The

    principal differences are concerned with the way in

    which combustion takes place and the stronger

    components that are required to cope with the high pres-

    sures that are needed to produce the temperature required

    for combustion. Diesel engines can conveniently be

    divided into two types:

    1. Direct injection engines

    2. Indirect injection engines.

    Fig. 15.4 Principle of the two-stroke CIE

    (a) (b)

    TDC

    1 2

    BDC

    Diesel Cycle

    Power

    Comp

    Pressure

    bar

    1

    2 3

    TDC BDC

    Dual Combustion Cycle

    Power

    Comp

    Pressure

    bar

    Fig. 15.3 Diesel and dual combustion cycles

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    Direct injection engines

    In the direct injection engine shown in Fig. 15.5 the fuel

    is sprayed directly into the cylinder. The circular space

    in the piston crown forms part of the combustion

    chamber; it is designed to produce turbulence when

    air is forced in towards the end of the compression

    stroke. This type of turbulence is known as squish

    turbulence because it is produced by the squashingof air as the piston forces the air down into the piston

    cavity. The injector is normally of the multi-hole type

    and operates at a pressure of approximately 180 bar e

    the compression ratio of the direct injection engine is

    of the order of 16:1, which is somewhat lower than

    that used in indirect injection engines.

    Indirect injection engines

    In the indirect engine (Fig. 15.6) the fuel is sprayed

    into a small pre-combustion chamber that is placed in

    the cylinder head above the piston. As the piston

    approaches TDC, air is forced into the pre-combustionchamber, which is designed to produce the swirling

    action necessary for good combustion.

    The combustion that starts in the pre-chamber rapidly

    heats the air and the burning fuel, and air is forced into

    the space at the top of the piston, where it mixes with the

    main body of air to complete the combustion process.

    The injection pressure in the indirect injection engine

    is of the order of 120 bar e compression ratios between

    22:1 and 28:1 are normal in these engines.

    TurbulenceTurbulence is required to ensure that all droplets of fuel

    are surrounded by sufficient air to provide the oxygen

    that is required for efficient combustion. There are

    basically two methods of creating turbulence:

    1. Turbulence created on the induction stroke

    2. Turbulence created on the compression stroke.

    Induction stroke turbulence

    Figure 15.7(a) shows the arrangement of the inductionports on a modern diesel engine. The tangential port is

    designed to set up a rotary motion in the air as it passes

    through the port into the cylinder on the induction

    stroke, as indicated in Fig. 15.7(b).

    Circularcombustionchamber inthe pistoncrown

    Coolentjacket

    Squish

    Air swirl

    Piston

    InjectorCylinder head

    Direct injection

    Fig. 15.5 A direct injection engine

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    Special shape inthe piston crowninduces swirl asburning mixtureleaves the pre-combustion chamber

    Cylinderblock

    Piston

    Port

    Indirect injection

    Pre-combustionchamber

    Injector

    Fig. 15.6 An indirect injection system

    1. Exhaust port2. Exhaust valve3. Fuel injector4. Inlet swirl port5. Inlet valve6. Tangential inlet port7. Heater plug

    3

    4

    5

    6

    7

    (a) (b)

    2

    1

    Fig. 15.7 A tangential inlet port

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    Combustion in a compressionignition engine

    The power output of a compression ignition engine is

    determined by the amount of fuel that is injected e

    for low power output such as engine idling a very small

    amount of fuel is injected, while for high power output

    a large amount of fuel is required. The amount of fuelinjected is determined by the length of time for which

    the fuel is injected and this is controlled by the design

    of the fuel injection system, which is covered in a later

    section. For the time being I wish to concentrate on the

    process of combustion.

    Three phases of combustion

    Sir Harry Ricardo, the founder of the Ricardo research

    laboratories at Shoreham in Sussex, first put forward

    the idea that combustion in a compression ignition engine

    takes place in three separate phases. The graph in

    Fig. 15.8 shows how pressure, temperature, and heatrelease from combustion changes from the point at which

    injection of fuel starts. Images (a)e(d) are photographs of

    the cylinder contents from the start of injection at about

    258 before TDC, through to full combustion, which

    continues some way down the power stroke. The three

    phases of combustion shown in Fig. 15.8 are:

    1. The first phase, from (a) to (b). This is known as the

    delay period. In this period the fuel is sprayed into the

    dense high-pressure and high-temperature air, and

    a small period of time elapses during which the tiny

    particles of fuel are being evaporated. The resultantfuel vapour must then be brought into contact with

    oxygen so that combustion can start. The length of the

    delay period depends on several factors, such as:

    The ignition quality of the fuel (cetane rating).

    The relative velocity between the fuel and the air

    in the cylinder (turbulence).

    The fineness of the atomization of the fuel.

    The airefuel ratio.

    The temperature and pressure of the air in the

    cylinder.

    The presence of residual exhaust gas from the

    previous cycle.

    2. The second phase, from (b) to (c). This is the periodwhen combustion spreads rapidly through the

    combustion space, leading to a rapid rise in pressure.

    The rate at which pressure rises in this phase governs

    a. Start of injection

    b. Combustion begins

    c. Peak rate of heat release

    Crank angle (degrees)

    -30 -20 -10

    a

    b

    d

    c

    Maximum gas pressureapprox. 55 bar

    Max gas temperatureapprox. 1850K

    10TDC 20 30 40 50 60

    d. Combustion by turbulentdiffusion

    Fig. 15.8 Compression ignition engine combustion (Lucas CAV)

    The compression ignition engine e diesel engine 173

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    the extent of combustion knock, which is a feature of

    compression ignition engines and is known as diesel

    knock.

    3. The third phase, from (c) to (d), is the period when

    combustion is fully operational and the flame spreads

    to encompass all of the fuel. In this phase the

    pressure continues to rise at a more gradual rate until

    injection ceases a few degrees later. After this the

    expansive working effect of the gas drives the pistondown the remainder of the power stroke.

    Diesel fuel and products ofcombustion

    Diesel fuel

    Diesel fuel has a calorific value of approximately

    45 MJ/kg and a specific gravity of about 0.8 g/cm3.

    The ignition quality of diesel fuel is denoted by the

    cetane number; a figure of 50 indicates good ignition

    properties. Among other properties of diesel fuel thataffect normal operation are flash point, pour point,

    and cloud point or cold filter plugging point.

    Flash point

    The flash point of a fuel is the lowest temperature at

    which sufficient vapour is given off to cause temporary

    burning when a flame is introduced near the surface. A

    figure of 1258F (528C) minimum is quoted in some

    specifications.

    Pour point

    The pour point of a fuel is the temperature at which thefuel begins to thicken and congeal and can no longer be

    poured from a container; a pour point of 2188C is

    considered suitable for some conditions.

    Cloud point

    The cloud point, which is sometimes known as the cold

    filter plugging point (CFPP), is the temperature at which

    the fuel begins to have a cloudy appearance and will no

    longer flow freely through a filtering medium. The cloud

    point is normally a few 8C higher than the pour point.

    Note

    These figures for diesel fuel are approximate and are

    presented here as a guide only. Readers who require

    more detailed information are advised to contact

    their fuel supplier.

    Products of combustion

    Exhaust gases are the products of combustion and under

    ideal circumstances they would comprise carbon

    dioxide, steam (water), and nitrogen. However, owing

    to the large range of operating conditions that engines

    experience, exhaust gas contains several other gases

    and substances, such as:

    COe carbon monoxide due to excess fuel and

    incomplete combustion.

    NOxe oxides of nitrogen arising from extremely

    high combustion temperature.

    HC e hydrocarbons arising largely from incomplete

    combustion. PMe particulate material. The bulk of PM is soot,

    which is incompletely burnt carbon. Other

    particulates arise from lubricating oil on cylinder

    walls and metallic substances from engine wear.

    SO2 e sulphur dioxide. Some diesel fuels contain

    small amounts of sulphur, which combines with

    oxygen during combustion to form SO2. This in turn

    can combine with water to form sulphurous acid.

    CO2e carbon dioxide is not treated as a harmful

    emission but it is considered to be a major contributor

    to the greenhouse effect and efforts are constantly

    being made to reduce the amount that is produced. In

    the UK the quantity of CO2that a vehicle produces ina standard test appears in the specification, and

    vehicle taxation (road tax) is less for small CO2emitters than it is for large ones.

    Emissions limits

    In the UK the emissions limits are set by the European

    Union. The limits are the subject of constant review e

    those shown in Table 15.1 are for the standards known

    as Euro 4. The figures apply to vehicles as they leave

    the manufacturer; once in service the standards set by

    the UK Department for Transport apply and it is their

    figures that are used in the annual tests that are knownas the MOT.

    At the time of writing the test is conducted by passing

    the exhaust gas through an approved apparatus such as

    the Hartridge smoke meter, which measures the opacity

    of the exhaust gas. Figure 15.9 shows how the opacity of

    the exaust gas relates to the Hartridge and the Bosch

    scales.

    Emissions control on the CIE

    The airefuel ratio in compression ignition engines

    varies from very weak (probably 50:1) to slightly rich(12:1), and combustion temperatures are high. The

    three-way catalyst used with petrol engines is not suit-

    able for use with compression ignition engines because

    Table 15.1 Emissions limits (g/km)

    CO HC HC 1 NOx

    NOx

    PM

    Petrol 1.0 0.10 e 0.08 e

    Diesel 0.50 e 0.30 0.25 0.025

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    it requires the airefuel ratio to be held near to 15:1 and

    alternative methods of dealing with harmful emissions

    are used. The two systems that are used on heavy vehi-

    cles are:

    1. Selective catalyst reduction (SCR) and a particulate

    matter (PM) filter.

    2. Exhaust gas recirculation (EGR).

    Particulate trap and selectivecatalyst reduction

    The three-way catalyst used on petrol engines requires

    an airefuel ratio of about 15:1. Diesel engines operate

    on mixture strengths that may be as low as 40:1, which

    means that an alternative system is used to reduce NOx.

    On light vehicles there is a tendency to rely on exhaust

    gas recirculation to limit NOxand an oxidation catalyst

    to control HC; in addition, a particulate filter may be

    used to deal with soot and other particulates. This

    system is shown in outline in Fig. 15.10.

    There is some debate in the heavy vehicle field about

    the most suitable system for exhaust gas after treatment,

    and some large vehicles are equipped with an alternative

    system of the type shown in Fig. 15.11.

    The exhaust gas is first passed through the oxidation

    catalyst and particulate filter. The high concentration of

    oxygen in the fueleair mixture and the relatively high

    temperature allow the oxidation catalyst to convert HC

    and COinto CO2and H2O. The gas then enters the partic-

    ulate filter, where the soot and other materials are filtered

    out. Any PM that is deposited in the filter can be removedlater by active regeneration, which is combustion with

    oxygen at approximately 6008C; this is achieved by

    a temporary increase in the amount of fuel injected.

    The regeneration process is performed by the engine

    management system at intervals dictated by operating

    conditions. After passing through the oxidation catalyst

    and particulate filter, a solution of pure water and urea

    is injected into the exhaust stream, where it reacts with

    the catalyst to reduce the NOx to water vapour and

    nitrogen. In Europe the solution of pure water and urea

    is called AdBlue and is carried in a small tank that is

    about 20% of the capacity of the main fuel tank, and it

    is normally placed next to it, as shown in Fig. 15.12.

    CAT

    Oxidising catalystParticulate filter

    Pressure differentialsensor

    Oxygen sensor

    P.F.

    Fig. 15.10 Light diesel exhaust engine emission control

    N0x oxides of nitrogen

    Urea injectionNitrogenH2O Water vapourPlus normal exhaust gas

    Hc hydrocarbons unburnt fuel

    PM soot etc.

    Plus normal exhaustgas

    1. Particular filter2. Oxidation catalyst

    3. Selective reduction catalyst

    1 2 3

    Fig. 15.11 A heavy diesel engine selective catalyst reduction system

    Light absorption coefficient [m-1]

    Hartridge smoke units [HSU]

    Bosch number [BN]

    0.1

    10

    1.0

    1.5

    2.0

    2.5

    3.0

    3.5

    4.0

    4.5

    5.0

    5.5

    6.0

    6.5

    20

    30

    40

    50

    60

    70

    80

    90

    0.2

    0.3

    0.4

    0.5

    0.6

    0.7

    0.8

    0.9

    1.0

    1.1

    1.2

    1.3

    1.4

    1.5

    1.6

    1.7

    1.8

    1.9

    2.0

    2.2

    2.4

    2.6

    2.8

    3.0

    3.5

    4.0

    5.0

    6.0

    7.0

    8.0

    7.0

    7.5

    Fig. 15.9 Smoke meter scales

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    Exhaust gas recirculation (EGR)

    Oxides of nitrogen (NOx) are formed when combustion

    temperatures are high, as they are in compression igni-

    tion engines. Exhaust gas contains considerable

    amounts of CO2 and H2O and small amounts added to

    the incoming air charge reduce the combustion temper-ature and the production of NOx. An electrically oper-

    ated EGR valve of the type shown in Fig. 15.3 that

    operates under the control of the engine management

    computer is placed between the exhaust and air intake

    systems. The engine computer is programmed to recir-

    culate exhaust gas when operating conditions are suit-

    able e in most cases a quantity of exhaust gas

    equivalent to about 15% of the air intake is recirculated

    when the engine is running between idling speed and

    full load.

    Self-assessment questions1. Why are diesel engines sometimes referred to as

    compression ignition engines?2. How is ignition of the fuel achieved in a diesel

    engine?

    3. How does the compression ratio of a diesel

    compare with that of a petrol engine?

    4. How does exhaust gas recirculation help to reduce

    NOxemissions?

    5. What is meant by the term particulate matter?

    6. How does the airefuel ratio of a diesel engine vary

    across the engine speed and power range?

    7. Give an approximate value of the airefuel ratio for

    a diesel engine at idling speed.

    8. What effect on cold weather starting will low

    compression pressure have on a diesel engine?9. Why doesnt a three-way catalyst work on diesel

    exhaust?

    10. Describe the procedure for conducting the MOT

    exhaust gas test on a light vehicle equipped with

    a turbocharged engine.

    11. What is the approximate maximum temperature

    reached in a diesel engine?

    Fig. 15.13 Exhaust gas recirculation

    Fig. 15.12 The AdBlue tank

    176 A Practical Approach to Motor Vehicle Engineering and Maintenance