chapter 1 introduction - shodhgangashodhganga.inflibnet.ac.in/bitstream/10603/17400/6/06...1 chapter...
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CHAPTER 1
INTRODUCTION
The function of an engine is to produce mechanical movement from
any form of energy. When the fuel is burnt, heat is released. This heat energy
is converted into useful work. Diesel engine is an internal combustion engine
that converts chemical energy that reciprocate piston between top dead centre
and bottom dead centre. The pistons are connected to the engine crank shaft
through connecting rod, which change the reciprocating motion into the rotary
motion needed to propel the vehicle wheels. With both gasoline and diesel
engines, energy is released in a series of small explosions called combustion
as fuel reacts chemically with oxygen from the air. For fuel combustion and
consecutive energy conversion is taken in the combustion chamber. The
different chambers and its function are described in the following headings.
1.1 COMBUSTION CHAMBER
A combustion chamber is the part of an engine in which fuel is
burned. The combustion chamber is recessed in the cylinder head and
commonly contains a single intake valve and a single exhaust valve on the top
roof. Some engines use a dish-in-piston and in this case the combustion
chamber can be considered as partly within the cylinder. The combustion
process is symbolically shown in Figure 1.1. At the end of compression stroke
the fuel is injected into the chamber, air at this condition is in high
temperature and pressure. The heat content of air is used to vaporise the diesel
particle and vapour form of diesel is exploded by the process of oxidisation.
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At the end of working stroke or expansion stroke the combustion process is
ceased and air fuel mixture becomes combustion product. It may contains the
Hydro Carbon(HC), Carbon di Oxide (CO2), Carbon mono Oxide (CO),
Oxides of Nitrogen (NOx), Particulate Matter (PM).
Figure 1.1 Combustion Process
1.2 TYPES OF COMBUSTION CHAMBER
A well-designed engine uses a combustion chamber that is designed
for the intended usage. The following combustion chambers are widely used
in the case of diesel engine.
Open Combustion Chamber
Pre-combustion Chamber
Turbulence Chamber
Spherical Chamber
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1.2.1 Open Combustion Chamber
The open combustion chamber is the simplest form of chamber as
shown in Figure 1.2. It is suitable for only slow-speed, four-stroke cycle
engines, but is widely used in two-stroke cycle diesel engines. In the open
chamber, the fuel is injected directly into the space on top of the cylinder. The
combustion space, formed by the top of the piston and the cylinder head, is
shaped to provide swirling action of the air, as the piston comes up on the
compression stroke. There are no special pockets, cells or passages to aid the
mixing of the fuel and air. This type of chamber requires a higher injection
pressure and a greater degree of fuel atomization than is required by other
combustion chambers to obtain an acceptable level of fuel mixing. To
equalize combustion in the combustion chamber, use a multiple orifice-type
injector tip for effective penetration. This chamber design is very susceptible
to ignition lag.
Figure 1.2 Open Combustion Chamber
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1.2.2 Precombustion Chamber
The pre combustion chamber is an auxiliary chamber at the top of
the cylinder shown in Figure 1.3. It is connected to the main combustion
chamber by a restricted throat or passage. The pre combustion chamber
conditions the fuel for final combustion in the cylinder. A hollowed-out
portion of the piston top causes turbulence in the main combustion chamber,
as the fuel enters from the pre-combustion chamber to aid in mixing with air.
The following steps occur during the pre-combustion process:
During the compression stroke of the engine, air is forced into
the pre-combustion chamber and because the air is
compressed, it is hot. At the beginning of injection, the pre-
combustion chamber contains a definite volume of air.
As the injection begins, combustion begins in the pre-
combustion chamber. The burning of the fuel, combined with
the restricted passage to the main combustion chamber,
creates a tremendous amount of pressure in the combustion
chamber. The pressure and the initial combustion cause a
super-heated fuel charge to enter the main combustion
chamber at a high velocity.
The entering mixture hits the hollowed-out piston top, creating
turbulence in the chamber to ensure complete mixing of the
fuel charge with the air. This mixing ensures uniform and
complete combustion. This chamber design provides
satisfactory performance with low fuel injection pressures and
coarse spray patterns because a large amount of vaporization
occurs in the pre-combustion chamber. This chamber is
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susceptible to ignition lag, making it suitable for high-speed
operations.
Figure 1.3 Pre-combustion Chamber
1.2.3 Turbulence Chamber
The turbulence chamber shown in Figure 1.4 is similar in
appearance to the pre-combustion chamber, but its function is different. There
is very little clearance between the top of the piston and the head, so a high
percentage of the air between the piston and cylinder head is forced into the
turbulence chamber during the compression stroke. The chamber is usually
spherical and the small opening through which the air must pass causes an
increase in air velocity, as it enters the chamber. The turbulence speed of air
in turbulence chamber is about 50 times the crankshaft speed. The fuel
injection is timed to occur when the turbulence in the chamber is greatest.
This ensures a thorough mixing of the fuel and air, causing the greater part of
combustion to take place in the turbulence chamber. The pressure, created by
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the expansion of the burning gases, is the force that drives the piston
downward on the power stroke.
Figure 1.4 Turbulence Chamber
1.2.4 Spherical Chamber
The spherical combustion chamber is designed principally for use in
the multi-fuel diesel engine. The chamber consists of a basic open type
chamber with a spherical shaped relief in the top of the piston head as shown
in Figure 1.5. The chamber works in conjunction with a strategically
positioned injector and an intake port that produces a swirling effect, as it
enters the chamber. Operation of the chamber is as follows:
Figure 1.5 Spherical Chamber
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As the air enters the combustion chamber, the shape of the
intake port introduces a swirling effect to it.
During the compression stroke, the swirling motion of the air
continues as the temperature in the chamber increases.
As the fuel is injected, most of the fuel is deposited on the
head of the piston and the remainder mixes with the air in the
spherical combustion chamber.
As combustion begins, the main portion of the fuel is swept
off the piston head by the high-velocity swirl that was created
by the intake and the compression strokes. As the fuel is swept
off of the head, it burns through the power stroke, maintaining
even combustion and eliminating detonation.
1.3 ENGINE VIBRATION
A basic correlation amongst the in-cylinder combustion pressure,
indicting power expression and surface vibration of diesel engine is shown in
Figure 1.6 (Roa and Gupta, 1999). Actually it expresses a mutually dependent
connection amongst the in-cylinder working process, relative transmission
relationship of the mechanical systems and the dynamic performance of the
engine. Obviously, the in-cylinder working process dominates the dynamic
performance of the engine and results in the largest and most significant
impact excitation in it. At the same time, the widespread mechanical and fluid
impacts inside the engine form its high-frequency excitations. A fluid impact
is produced by knocking of gas pressure wave on the cylinder wall. It is
necessary to make an in-depth discussion to them and their influences to the
engine vibration response.
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Figure 1.6 Basic IC engine vibration correlations
1.3.1 The Unstable Combustion Excitation (I)
The in-cylinder high-pressure gas oscillation inside a diesel engine
can be theoretically described as a standing-wave equation in polar
coordinates as follows (Roa and Gupta, 1999):
+ (1.1)
Where is the specific heat constant ratio.
Taking the cylinder as a rigid constraint to the inner-cylinder gas
oscillation, the boundary condition around the cylinder diameter D can be
supposed as:
(1.2)
Generalized solution as
( ) = ( ) (1.3)
Where is the phase lag angle
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Equation (1.1) can be rewritten as:
+ + (1.4)
The frequency composition of the in-cylinder gas oscillation can be
expressed as (Roa and Gupta 1999)
= , ( , … , ) (1.5)
In a theoretical sense, Equation(1.5) expresses a definite description
on the in-cylinder gas oscillation. Firstly, m kinds of solution of the n order
Bessel Equation (1.4) explain the existence of unsteady in-cylinder gas
oscillation with m kinds of frequency composition; it may be single or
complex. Secondly, it is shown that the actual oscillating waveform and
frequency composition are mainly influenced by the structural and/or working
conditions of the engine, such as the geometrical parameters of the cylinder,
the in-cylinder oil and gas pressure and their mixing and combustion status
etc. This explains that the in-cylinder gas pressure with an unstable frequency
composition is a major cause of the abnormal working performance and non-
stationary dynamic process of the engine, and it is also directly related to the
structural and working conditions of the engine.
1.3.2 The Modulated High-Frequency Excitations
In Figure 1.5 segments II and III depict high frequency impulses
modulated by the relative transmission relationship of the sub-mechanical
systems in the engine. These high frequency impulses can be classified into
two groups:
1. Fluid impact induced vibration.
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2. Mechanical impact induced vibration.
1.3.2.1 Fluid Impact Induced Vibration
Fluid impacts are important sources of the high-frequency vibration
and noise inside the engine (Roa and Gupta, 1999). The fluid impact induced
high-frequency vibration in the reciprocating engine has a permanent
frequency composition which does not vary with changes of the engine
operating condition. If the speed is increased, it wouldn’t increase the
temperature and thermodynamic properties. Examples of this are the impacts
caused by combustion, cavitations, and pre-ignition.
1.3.2.2 Mechanical Impact Induced Vibration
The widely existing transient impacts caused by the in-engine
mechanical systems tend to be periodic at the operating condition when they
cause high-frequency resonant responses of the impacting mechanical parts.
Examples of this are the impacts caused by the inlet, outlet valves, piston and
others component failures. The high-frequency resonant response possesses
permanent frequency compositions and successively transforms itself as one
part of the engine vibration. In summary, the transient response caused by the
in-engine mechanical and fluid impacts possesses permanent frequency
compositions. At the same time, the unstable inner-cylinder working process
and relative transmission relationship of the in-engine mechanical systems
irregularly modulate them. In consequence, the practically measured vibration
signal on the engine casing reveals itself as a series of impulses modulated
along the time history.
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Typically, the main sources of excitation that are likely to be
observable from the vibration signal are associated with the following
mechanisms (Liu et al., 2008):
1. Rocking and twisting of the engine block on its supports, due
to the action of inertial forces
2. Impacts due to clearances at links, those at the crankshaft
bearings
3. Piston slap being extremely noisy
4. Closures and openings of valves
5. High-pressure injection of fuel in diesel engines
6. Rapid rising of gas pressure in the cylinders during the
combustion, especially in diesel engines where it has been
compared with a hammer blow.
The impulse responses on a typical engine structure usually last for
a few milliseconds for an engine running at 1500 rpm. This means angular
duration greater than 100 so that within the intervals where impacts occur
close together the vibration signatures will inevitably overlap. This is
typically what happens in the vicinity of the top dead centre, where injection,
piston, combustion and valve impacts occur within few degrees.