effect of engine position (full paper)
TRANSCRIPT
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Abstract ² In this paper, a programming of
dynamic system calculation is developed to
determine the body tilt angle in relation to
minimize the shaking forces on the diesel engine¶s
crankshaft. In this study, 1-cylinder diesel engine is
taken as an example. Position, velocity, andacceleration of pins of the engine mechanism
determined by using vector analysis. Masses and
mass moments of inertia of the linkage are used to
generate the forces and moments. Cartesian
coordinate principle is used to form linear
equations. These equations are solved by using
gauss elimination method to obtain the shaking
forces on the crankshaft. Calculation result is
validated by comparing it to the polygon method
and Newton principles. Based on the graphs, the
optimum tilt angle of the engine¶s body had been
obtained at 072.87! F for minimum horizontal
shaking force 07.2! x
R Newton.
Keyword: dynamic system, vector analysis, gauss elimination,
shaking forces, tilt angle.
I. I NTRODUCTION
Recently, researches of diesel engines become more
attractive because of its fuel has similar characteristic with
the environment-friendly fuel resources, such as biodiesel.
In the fact that, biodiesel can be used to replace the
conventional diesel fuel and it is made from the renewable
resources.
Biodiesel is a kind of environment-friendly resources of fuel, clean, grown locally. P alm Oil Methyl Esters (POME)
is one of those. Researchs on this area had been carried out
by researchers such as Agarwal [1], Ramadhas [2], and
Murugesan [3].
This work was supported in part by ANPCYT.* F.N. Balia, PhD student at Mechanical and Manufacturing Engineering
Faculty, UTHM. (corresponding author: e-mail: f n [email protected]).** S. Mahzan, Lecturer at Mech and Manufacturing Eng Faculty, UTHM.***M.I. Ghazali, Professor at Mech and Manufacturing Eng Faculty,
UTHM.***Abas AB Wahab, Professor at Mech and Manufacturing Eng Faculty,
UTHM.
Researches on the vibration analysis on the diesel engines
had been carried out by researchers as follows: Geng, et al
[4], carried out their research on the piston-slap-induced
vibration of 6-cylinder diesel engine. Garlucci, at al [5],
carried out the research on the relation between injection
parameter variation and block vibration of the diesel engine
(FIAT, 2000 cc). Brusa, et al [6], investigated concer ned
with the effect of non-constant moment of inertia of torsional vibration on the crankshaft of 4-cylinder
Lycoming O-360-A3A propeller engine. Guzzomi, et al [7],
conducted the study concer ned with the effect of the piston
friction on the torsional natural frequency of crankshaft of a
single cylinder reciprocating engine.
This research is a preliminary work on the diesel engines
area and its development to the biodiesel engine purpose.
This paper emphasize on the programming of a dynamic
system on the diesel engines. Determining the body tilt
angle in relation to minimize the shaking forces on the
diesel engine¶s crankshaft is very important to reduce the
shaking forces on the body. For illustration, 1-cylinder
diesel engine taken as an example.
II. PROBLEM FORMULATION
In analyzing the shaking forces due to the combustion
process in the chamber on the engine¶s crankshaft can be
describe as follows:
2.1 Kinematic Formulation
The calculation steps of an engine has to be started at the
kinematic formulation, to calculate the position, velocity,
and acceleration of pins and center of mass. Vector analysis
principles are used to calculate those parameters. The
mechanism of engine shown below.
F
Y
X
2
3
4
1
Figure 1, Mechanism of Engine
EFFECT OF BODY TILT ANGLE TO THE SHAK ING FOR CES
ON THE DIESEL ENGINE¶S CRANKSHAFT
*Fuadi Noor Balia,
**Shahruddin bin Mahzan,
***Mohd Imran bin Ghazali, and
***Abas AB Wahab
Proceedings of MUCEET2009
Malaysian Technical Universities Conference on Engineering and Technology
June 20-22, 2009, MS Garden,Kuantan, Pahang, Malaysia
MUCEET2009
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Figure 1, shows a system of the engine mechanism, in
which the body tilt angle is included as a parameter that
can effect to minimize the shaking forces on the engine¶s
crankshaft. Link 1 is cylinder block and jour nal bearing,
link 2 is crankshaft, link 3 is connecting rod, and link 4 is
piston that can move freely on the cylinder (body) axis
direction.
Figure 2, shows the vector model of engine mechanism
for calculating the position, velocity, and acceleration of
pins and center of mass of the linkages. In this modeling,
vector r2 represent the crankshaft, vector r3 represent the
connecting rod, and vector r4 represent the motion line of
piston. 2U is angle of r2 to x, 2U( is angle of r2 to r4, 3U
is angle of r3 to x, J is angle of r3 to r4, F is angle of r4
to x.
r2
r3
r4
X
Y
F2
3
2
Figure 2, Kinematic Modeling of Engine Mechanism
From figure 2, mathematical model can be gover ned as
a vector equation below,
324r r r ! ««.. (1)
This equation can be derived to obtain the velocity of points along the line vector, such below
33224 xr xr r UU ! ««.. (2)
From this equation can be calculated the connecting
rod angular velocity such below,
2
33
22
3cossin
sincosU
F F
F FU
¹¹ º
¸©©ª
¨
!
x y
y x
r r
r r «« (3)
Equation (2), can be derived to give the equation of
acceleration of points motion along the cylinder axis can bewritten as below,
F
UUUU
cos
....2
3333
2
2222
4
x y x yr r r r
r
! « (4)
Calculation of angular acceleration of linkage 3 can be
derived and the result as below,
D
C B A !3U
««««« (5)
where :
222 .sincos U F F
y xr r
!
2
222 ).cossin( U F F y x
r r B !
2
333 ).cossin( U F F
y x r r C ! )cossin( 33
¡ ¡
x y r r D !
Through equation (1) to equation (5), the position.
velocity (linear and angular) and acceleration (linear and
angular) of pins and center of mass can be obtained.
2.2 Dynamic Formulation
Calculation of shaking forces in any of pins and existing
forces at center of mass of linkage, can be modeled as
figure 3 below [8].
F
Y
X
2
3
4
1
Figure 3, Dynamic Modeling of Engine Mechanism
This model can be solved by using Cartesian coordinate
method (vector analysis for dynamic systems) [9]. Thisengine mechanism can be modeled separately as follows.
2.2.1 Crankshaft Modeling
Ti
m2b.a2b
I2b
p2a
q2a
p2b
¢
2
-¢
3
m2c.a2c
-W2c
I2a 2
2
-W2a
-W2b
m2a.a2a
£
¤
¥
2 2 22, ,
¦ 2
§ igure 4, Modeling of ̈
rankshaft
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Figure 4, shows a physical modeling of Crankshaft. In
this modeling, the crankshaft is separated into two parts,
that are crank and balancer. Center of rotation assumed
located at point A, therefore all of the moments refer to that
point.
The inertia torque22 .U
a I that is generated by rotation
of the crank and located at point A. The inertia torque
22 .Ub I that is generated by rotation of balancer and located
at point B. Reaction torque Ti is in put moment to the shaft
due to the reaction of combustion and inertia loads.
The vector 2
F is the reaction of the crankshaft to the
crank, while vector 3 F is the reaction force of crankpin to
the crank. The massa© 2
is of crank mass and generate the
inertia force of aa
a
22. and centered at point A. The
b© 2is the mass of balancer and generate the inertia force
of bb
a
22. and centered at point B. The mass
c
2is a
half mass of crankpin to the crank, this mass generate a
half of inertia force cc a© 22 . and centered at point C. In
this modeling, the distributed weight of linkage part are
included. W 2 is a half of weight of crankshaft. W 2a is the
weight of crank, W 2b is the weight balancer. W 2c is a half
of the weight of crankpin
2.2.2 Connecting rod Modeling
F3
m3.a3
I3
-F4
q3
p3
3
3
-W3
D
3
, 3 3,
Figure 5, Modeling of Connecting rod
Figure 5 shows a physical modeling of Connecting
rod. Center of rotation assumed to be located at point D.
The inertia torque33U I is generated due to the
rotation of connecting rod. The mass3m is the connecting
rod mass and generate the inertia force 33.am and centered
at point D. The vector F 3 is the reaction force of crankpin
to the connecting rod, while the force of F 4 is reaction of
piston pin to the connecting rod. The weight W 3 is
connecting rod weight and centered at point D.
2.2.3 Piston Modeling
m4.a4
F14
Fc
z
F4
F
-W4
E
4
1
Figure 6, Modeling of Piston
The vector 4
F is the reaction force of connecting rod to
the pin of piston. The mass4m is the sum of piston¶s pin
and piston mass itself and generated the inertia force
44.am and located at point E. The weight W 4 is the sum
of pin and piston weight. The vector 14
F is reaction force
of cylinder to the piston and located at the length of vector
z from the center of mass, and the vector c F is a force as a
result of the combustion process in the cylinder to the
piston.
2.3 Mathematical Equations
Mathematical modeling can be developed by using
vector analysis (Cartesian coordinate) method for engine
mechanism.
2.3.1 Equation for Crankshaft
Crankshaft mechanism is modeled by assumed that the
center of rotation located on point A and mass of each of
crank part located at the center of each part.
Equation of the forces equilibrium vector of the
Crankshaft,
ccbbaaamamam F F
22222232... ! «.. (6)
Equation of moment equilibrium vector of the Crankshaft,
J I H G F E
T x F p x F q iaa
! 3222
««. (7)
where:
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bbaba xmq p E
2222.)( !
bab xW q p F 222 )( !
22 xW qG a!
ca xW p H 22!
ccaa xm p I
222.!
222 )( Uba I I J !
Equation (6) can be developed to give the force equations
in x and y direction, it mean give two rows of equation.
Equation (7) give the moment equations to the center of
rotation, after developing it using vector analysis, this
equation give a row of moment equation.
From equation (6) and (7) can result three rows of linear
equation to form matrix.
2.3.2 Equation for Connecting rod
Equation of the forces equilibrium vector of Connecting
rod,
33343 . W am F F ! «««««.. (8)
Equation of the moment equilibrium vector of Connecting
rod,
334333.U I x F p x F q ! «««««.. (9)
Equation (8) is developed to give two rows of the force
equations in x and y direction, and equation (9) give a row
of moment equation.
From equation (8) and (9) can result three rows of linear
equation to form matrix.
2.3.3 Equation for Piston
Equation of forces equilibrium of piston,
c F am F F ! 44144 . ««««« (10)
Equation of moments equilibrium,
014 ! z x F «««... «.. (11)
Equation (10) can be developed into two rows of the
force equation, in x and y direction, while equation (11)
can be developed to be a row of moment equation in x and
y.
These equations give three rows of linear equation to
form matrix.
2.3.4 Matrix Formation
The equation (6) to equation (11) that have nine of
linear equations and can be solved simultaneously by
matrix formation,
? A _ a _ab x A ! «««««. (12)
where, ? A A is a coefficient of symmetric matrix (9x9
matrix element), _ a x are the forces and torque parameter to
be solved (9x1 matrix element), while _ ab are the effective
inertia forces and moment (9x1 matrix element) due to the
moment and forces of inertia.
The forces and torque in matrix _ a x can be solved by
using Gauss-Jordan Elimination principle for solving
Simultaneously Linear Equation [10].
III. METHOD OF SOLUTION
This programming is divided in two category
calculation. Firstly, kinematic step and secondly, dynamic
system formulation. Compiler Visual C++ is used for
programming language [11].
Briefly, figure 7, shows a flow chart of programming.
Figure 7, Flow Chart of Programming
On the kinematic step, calculation of position, velocity,and acceleration of pins and center of mass of each link
were carried out. Vector of position was written as
equation (1). In this development vector 2
r and
3r considered as the length of crank and connecting rod, the
values are constant. Vector 4r considered as the length of
position between piston and the main bearing, this is an
unconstant variable. Equation (2) gives the linear velocity
of piston motion along the cylinder axis. Rotation of the
crank gives the angular velocity and acceleration of the
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connecting rod,3U and
3U , it can be seen in equation (3)
and (5). For this purpose, the main bearing is fixed, and
body tilt angle is included as a parameter to ad just the
position of axis of piston to x (same as engine¶s body tilt
angle axis). Through this development, the effect of body
tilt angle F can be seen from the equation (3) to equation
(5). Equation (4) shows the linear acceleration of piston
motion along the cylinder axis.
Validation of kinematic calculations had been carriedout by comparing it to the hand calculation of polygon
method (see attachment-1 and attachment-2).
On the dynamics step, calculation of forces and
moments started of physical modeling of the crank and
balancer, connecting rod, and piston. Figure 3 shows the
physical dynamics modeling of engine mechanism.
Concept of Cartesian coordinate is used in accordance with
the vector analysis of forces and moments.
Crankshaft model, as showed at figure 4, can be derived
mathematically in accordance with d¶Alembert principle of
equilibrium. Equation (6) shows the vector for force
equilibrium, while equation (7) for moment equilibrium.
Connecting rod, as showed at figure 5, can be derived intothe forces and moments (equation (8) and (9)). Piston is
considered as the body motion along the cylinder axis.
Friction is neglected in this situation, because of the
complexity of calculation.
Matrix formation is used to collect the ninth of
equations had been developed from equation (6) to equation
(11). For detail explanation, see section 2.3 (Mathematical
Equations) for every step of modeling.
The data that are used for this solution is taken from
the size of diesel engine mechanism. Piston bore size d =
82.5 mm, stroke L = 92.5 mm, connecting rod length = 15
mm. Length of crank r a = 47 mm, balancer length r b = 78
mm. The inter nal pressure force data delivered to the
equation (10) depend on the crank angle of combustion [12].
Simultaneously linear equations in a matrix form can be
solved by using Gauss Elimination procedure, by inserting
pivot point algorithm. This solution gives the result of
parameters that are considered as the reaction forces of the
pins.
Validation of dynamics system had been carried out by
comparing it to the static equilibrium, by eliminating the
dynamic parameters, such the effective forces and moments
of inertia (see attachment-3 and attachment-4).
Validation for mass of piston carried out by getting its
weight. For connecting rod, the mass, centroid and mass
moment of inertia by calculation and getting its weight andcompare it, the parts are modeled as a volume combination
of the separately blocks. For crankshaft, calculation of
mass, centroid and mass moment of inertia carried out by
modeling its volume as the combination of many blocks
(same procedure with connecting rod).
IV. R ESULT AND DISCUSSION
Tilt Rx Ry
75
85
90
100
-12000
-10000
-8000
-6000
-4000
-2000
0
2000
4000
Force
Tilt Angle
Body Tilt Angle
75 80 85 87.72 90 95 100
Figure 8, Graphic of Tilt Angle to Shaking Force
Programming of this engine mechanism gives a
comparatively result, even for accuracy of calculation and
in accordance with the engine¶s body tilt angle, see figure8.
This angle result gives the minimum shaking force in
horizontal direction, Rx = 2.07 Newton, while for vertical
direction, R y = -11957.05 Newton. For diesel engine has
pressure 3,5 MPa, so inter nal pressure force F c = 18709.70
Newton, at 100 of crank angle. Rotation of engine is
constant, n = 4500 rpm. This condition is very important
consideration for the human body comfort characteristic.
The human body characteristic can stand for up and down
shaking motion, but for horizontal shake must be avoided
for a long period. The optimum tilt angle of engine¶s body
obtained072.87! F .
Validation of kinematic calculation, a good result was
reached. Calculation for n = 2000 rpm ( 4.209![
rad/sec),00! F , gives angular velocity for Connecting
rod 98.613 ![ rad/sec for calculation and 0.623 ![
rad/sec for polygon method. Angular acceleration
41.99363 !E rad/sec2 for calculation and 99403 !E
rad/sec2 for polygon method. Piston acceleration of
polygon method 9290!a ft/sec2 , for calculation
54.111435!a in/sec2 = 9286.3 ft/sec2 (see
attachment-1 and attachment-2).
For dynamics calculation, validation had been carried
out with a good result. The effective force and momentmust be eliminated (set to zero) to get static balance. For r 2
= 10 cm, r 3 = 20 cm,0
230!U gives the result for
manual calculation, for F c = 2500 N, obtained F 14y = 645.5
N, F 2 x = 2500 N, F 2y = -645.5 N, T i = -18090.19 N.cm. The
result of computer calculation, for F c = 2500 N, obtained
F 14y = 645.5 N, F 2 x = 2500 N, F 2y = -645.5 N, T i = -
18090.17 N.cm (see attachment-3 and attachment-4).
Validation for calculating the connecting rod mass and
centroid can be explained, total mass m = 0.79 kg,
045.0! y m, 00314.0! zz I kg-m2. By getting weight
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procedure, it is obtained that mass m = 0.75 kg,
049.0! y m. By this validation procedure, it can be
assumed that the calculation value of crankshaft can be
accepted. For crank: mass ma = 0.5867 kg, centroid
0272445.0! y m, mass moment of inertia I zz =
0.000494 kg-m2 (one crank). For balancer: mass mb =
0.8829 kg, centroid 03988.0! y m, mass moment of
inertia I zz = 0.001028 kg-m2.
V. CONCLUSION
For revolution n = 4500 rpm, and maximum inter nal
pressure force F c = 18709.70 N, at crank angle of 100, it is
obtained the minimum horizontal shaking force of Rx =
2.07 N, and the vertical force Ry = -11957.05 N. By this
calculation, the optimum body tilt angle can be ad justed to
be072.87! F .
This programming has reached a good accuracy for
calculating dynamic system of engine mechanism.
VI. R EFERENCES
[1] A.K. Agarwal, Biofuel (alcohols and biodiesel)
applications as fuel for inter nal combustion engines,
Progress in Energy and Combustion Science 33
(2007) 233-271.
[2] A.S. Ramadhas, S. Jayara j, and C. Muraleedharan,
Use of vegetable oil as IC engine fuel: A review,
Renewable Energy 29 (2004) 727-742.
[3] A. Murugesan., A. Umarani, R. Subramanian., and
N. Nedunchezhian, Bio-diesel as an alter native fuel
for diesel engines, Renewable and Sustainable
Energy Reviews (2007).[4] Z. Geng, and J. Chen, Investigation into piston-slap-
induced vibration for engine condition simulation
and monitoring, Jour nal of Sound and Vibration
282(2005) 735-751.
[5] A.P. Garlucci, F.F. Chiara, and D. Laforgia, Analysis
of the relation between injection parameter variation
and block vibration of an inter nal combustion diesel
engine, Jour nal of Sound and Vibration, 295 (2006)
141-164.
[6] E. Brusa, Torsional Vibration of Crankshaft: Effects
of Non-Constant Moments of Inertia, Jour nal of
Sound and Vibration, 205(1997) 135-150
[7] A.L. Guzzomi, The effect of piston friction on the
torsional natural frequency of a reciprocating engine,
Jour nal of Mechanical Systems and Signal
Processing (2007) 2833-2837.
[8] A.R. Holowenko, Dynamics of Machinery, John Wiley
& Sons, 1955, pp. 184-237.
[9] F.P. Beer, and E.R. Johnston. Jr, Vector Mechanics
for Engineers, Dynamics, Sixth Edition, McGraw-
Hill, 1997, pp. 885-895.
[10] W.H. Press, Numerical Recipes in C++, The Art of
Scientific Computing, Second Edition, Cambridge
University Press, 2002, pp. 39-51.
[11] I. Horton, Beginning Visual C++ 6, Wrox Press,
1998
[12] J.B. Heywood, Inter nal Combustion Engine
Fundamentals, Mc Graw Hill, 1988, pp. 491-561.
ACKNOWLEDGMENT
Thanks to ANPCYT for supporting this event. Special
thanks to UTHM that has collaborated with UMP, UTeM,and UniMAP.
Unforgettable special thanks to my colleagues, Muhaimin
Ismoen and Dr. Waluyo A.S, who have given much support
and the efforts for this research development.