a study on the modeling and simulation method of torsional
TRANSCRIPT
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A Study on the Modeling and Simulation Method
of Torsional Vibration Considering Dynamic
Properties of Rubber Parts for Engine Crankshaft
System with Rubber Damper Pulley
Tomoaki Kodama and Yasuhiro Honda Department of Science and Engineering, Kokushikan University, Tokyo, Japan
Email: [email protected] , [email protected]
Abstract— In this paper, we first describe the dynamic
properties of rubber parts of rubber damper pulley that are necessary for the modeling and numerical simulation of
torsional vibration. Secondly, we describe an experiment in
which two crankshaft pulleys with a torsional rubber
damper pulley are fitted to a 6-cylinder, high-speed diesel
engine. Torsional waveforms of the rubber damper inertia ring and the pulley are measured by means of phase-shift
torsiograph equipment. The measured waveforms are
harmonically analyzed and the dynamic properties of the
torsional stiffness and the torsional damping are investigated from an experimental viewpoint. As a results of
comparisons with experimental data, certain dynamic
properties of damper pulleys with a torsional rubber
damper have been clarified. The model used for the
numerical simulation of the torsional vibration is a multi -degree-of-freedom equivalent torsional vibration system.
The tension acting on the damper pulley and the rotational
resistance of the alternator, the cooling water pump, the
valve train system, etc., as well as the frictional resistance of
other accessories, were considered. Moreover, as a numerical simulation method of the torsional vibration, a
transition matrix method is adopted. The validity of this
method has been confirmed from comparison and
examination of measured values of torsional vibration and
simulation values results.
Index Terms— damper pulley, rubber parts, torsional
vibration, modeling, simulation method, dynamic properties,
engine crankshaft system, experiment, numerical simulation
I. INTRODUCTION
The important requirements in the design stage are
that the vibration and noise (NVH) levels of automobile
engines be reduced and that the timbre be improved
further [1]-[4]. Torsional v ibration dampers of high
performance, and crankshaft pulleys with a torsional
rubber damper (hereafter called "damper pulleys"), which
can reduce both torsional and bending vibrations, and
flywheels with a torsional rubber damper have been
widely employed in automobile engines [5]-[8]. When
designers estimate the amplitude of angular displacement
of engine crankshafts with the abovementioned damper
Manuscript received July 1, 2019; revised May 21, 2020.
pulleys in the design process, the following issues are of
concern:
[1] the estimation of dynamic properties (torsional
stiffness and damping of the damper pulley).
These dynamic properties are indeterminable [9],[10].
Therefore, an experimental equation for determin ing the
values has not existed until now and the quantitative
values are inaccurate. Unless these values can be
accurately estimated to a certain degree, it is d ifficult to
achieve high-precision computation. We clarify some of
the complicated dynamic properties of the rubber
vibration isolator by measuring the torsional vib rations of
the engine crankshaft system with a damper pulley. The
model used for the numerical simulation of the torsional
vibration is a multi-degree-of-freedom equivalent
vibration system. The tension acting on the damper pulley
and the rotational resistance of the alternator, the cooling
water pump, the valve train system, etc., as well as the
frictional resistance of other accessories, were considered.
Moreover, as a numerical simulation method of the
torsional vibration, a t ransition matrix method is adopted.
The validity of this method has been confirmed from
comparison and examination of measured values of
torsional vibration and numerical simulation values
results.
II. EXPERIMENTAL EQUIPMENT AND EXPERIMENTAL
METHOD FOR MEASUREMENT OF TORSIONAL
VIBRATION WAVEFORMS
This section concerns the main specifications of the
test engine and damper pulley, as well as the method of
measuring the torsional vibration waveforms. In the
experiment, the engines are operated under fu ll load to
cause steady forced torsional vibration.
A. Main Specifications of Test Engine and Rubber
Damper Pulley
The test engine is a 6-cylinders, in-line, high-speed
diesel engine [5], [6]. Fig. 1 shows the dimensions of the
test damper pulleys. This Table I. also shows the static
stiffness and natural frequency obtained from the static
and free vibrat ion tests, respectively [5], [6]. Types A and
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International Journal of Mechanical Engineering and Robotics Research Vol. 9, No. 7, July 2020
© 2020 Int. J. Mech. Eng. Rob. Resdoi: 10.18178/ijmerr.9.7.1007-1011
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B of the damper pulleys differ in Shore hardness but their
rubber parts have the same shape and dimensions. The
materials are similar-quality rubber (natural rubber and
nitrile rubber).
B. Method of Measuring Torsional Vibration Waveforms.
An eddy current dynamometer was connected via a
universal joint to the flywheel of the engine. The test
damper pu lley was fitted to the end of the crankshaft. The
gears for generating signal pulses were mounted on the
damper inert ia ring and pulley. The electric frequency
signals proportional to engine speed were obtained from
the electromagnetic pickup. The measured signals were
transmitted to the phase-shift torsiograph equipment via
the adapter which numerical calculated the average of
angular velocity (the center frequency). The torsional
vibration waveforms could be obtained from the torsional
angles, which were numerical calculated using the
relationship between the measured and center frequencies.
The measured torsional waveforms of the damper inertia
ring and pulley were harmonically analyzed using the
F.F.T. analyzer. The torsional angular d isplacement was
measured under full load from 800 [r/min] to 3200
[r/min]. The indicator diagrams, data from which were
necessary for the vibration analysis described later, were
measured using the piezotype indicator in the sixth
cylinder from the pulley side.
Figure 1. Dimensions and shape of test torsional vibration rubber damper pulley.
III. NUMERICAL CALCULATION METHOD FOR
DYNAMIC PROPERTIES OF RUBBER PARTS OF
DAMPER PULLEYS
A. Measured Amplitude Curves of Angular Displacement
Fig. 2 shows the measured amplitude curves of
angular displacements at the pulley end of the crankshaft
with the B-type damper pulley. These figures show
merely the main-order amplitude curves of angular
displacements. The large 6-th order resonant point occurs
at 2524 [r/min] and its resonant amplitude is 14.9x10-3
[rad] in the case of installing no damper pulley. Since the
tuning ratio of the B-type damper pulley is not optimum,
the 6-th order amplitude is not greatly reduced.
TABLE I. MAIN SPECIFICATIONS OF TORSIONAL VIBRATION RUBBER
DAMPER PULLEY.
Name of Rubber Damper Pulley Damper Pulley A Damper Pulley B
Measured Natural Frequency of
Rubber Damper Pulley [Hz]
148.0 228.0
Inertia Moment of Damper Inertia
Ring [kgm2]
0.0369 0.0369
Inertia Moment of Damper Pulley
[kgm2]
0.0462 0.0462
Static Torsional Spring Constant [Nm/rad]
2.548×104 3.332×10
4
Material of Rubber Natural Rubber and Nitrile Rubber
Figure 2. Measured Torsional Amplitude Curves of Angular Displacement [with Rubber Damper Pulley: B-Type, Amplitude of
Torsional Angular Displacement Curves at Pulley End].
B. Numerical Calculation of Dynamic Properties Values
from Measured Waveform.
The values of dynamic torsional stiffness and
damping coefficient of damper rubber parts can be
obtained from the harmonically analyzed results of
waveforms measured at the damper inertia ring and the
pulley. The equation of motion at the damper inert ia ring
is
0PULRDPRDPPULRDPRDPRDPRDP
KCI (1)
where tj
O,RDPRDPe and
tj
O,PULPULe
.
The following Eq. (2) can be obtained by rearranging the
expression of Eq. (1) by substituting the above-mentioned
relational expression into Eq. (1) and rearranging;
RDPRDPRDP
RDPRDPRDPRDPRDP
RDPcosMM
cosMMIK
212
2
,
RDPRDPRDP
RDPRDPRDPRDP
RDPcosMM
sinMIC
212
2
(2)
In Eq. (2), the values of amplitude ratio RDPM and
phase angle RDP can be obtained by analyzing
harmonically the waveforms measured at the damper
inertia ring and the pulley, where the values of RDPI ,
RDP are known. Therefore, the values of dynamic
torsional stiffness RDPK and damping coefficient RDP
C
can be determined from Eq. (2). The dynamic properties
of the vibration isolator rubber depend generally on [1]
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temperature, [2] frequency, and [3] average strain and
strain amplitude effects on the basis of same shape and
material. To reveal the effect of one factor among the
above-mentioned factors on the dynamic properties, it is
necessary to keep the values of the other factors constant
in the experiment. In our experiments, the surface
temperature of the rubber part was kept at 313 [K], but
the other factors could not be controlled due to the
vibration properties of the crankshaft. In full
consideration of these conditions of the other factors,
strain rate RDP
, which is the product of strain
amplitude and angular frequency, is defined by the
following equation.
RDP
RDPRDPlRe
RDPb
(3)
3
1
3
2
4
1
4
2
4
3
,RDP,RDP
,RDP,RDP
RDPrr
rr
(4)
Eq. (4) is obtained for the unifo rm, hollow, circular
cross section under the condition that the torsional
moment (in such a case that the shearing stress in the
representative radius RDP
is uniformly distributed over
the entire cross section) is equal to that (in the case that
shearing stress distribution x,RDPRDPRDP
CGRDP
caused by the simple shearing deformat ion in the
circumferential direction.
IV. NUMERICAL SIMULATION METHOD OF RESULTANT
TORSIONAL VIBRATION WAVEFORM
A. Derivation of General Expressions.
From what we have just discussed, vibration
calculations will be made by replacing the crankshaft
system with such equivalent vibration systems as shown
in Fig. 3. The equation of motion for the m th mass
can be expressed as follows.
tFKK
CCCJ
mmmmmmm
mm
'
mmm
'
mmmmm
111
111
(5)
Considering equations of motion for all masses ( n :
number of masses) from Eq . (5), they can be expressed in
matrix as follows.
FKCJ (6)
In this method, numerical calcu lations are made,
taking into consideration the constant coefficients in Eq.
(6). Therefore, it has the advantage that the time required
for making numerical calcu lations can be so much
reduced. Eq. (6) can be rewritten
FJKJCJ 111 (7)
If Eq. (7) is successively differentiated with respect to
time, taking the constant coefficient into consideration,
the n th derived function 2n of can be
written as follows.
21
2111
n
nnn
FJ
KJCJ (8)
Now if the angular displacements at the time t and
t are replaced by k
and 1k
respectively and the
angular velocit ies by k
and 1k
, 1k
and 1k
are
expand into a Taylor series, considering up to the i th
derived function, they can be expressed by Eq. (9).
i
k
i
i
k
i
kkkkk
!i!i
!!!
1
1
3
32
1
1
321
ik
i
kkkkk
!i
!!!
1
3211
4
3
3
2
1
(9)
Where in kt is the step size. If Eq. (8) is
repeatedly applied to Eq. (9), the second and higher
derivatives on the right hand side of these equations may
be written in terms of the angular displacements k
and
velocity k
.
k,i
i
k,i
i
k.k,
k,k,ki
i
i
i
ki
i
i
i
k
W!i
W!i
W!
W!
W!
WY!i
Y!i
Y!
Y!
Y!
YX!i
X
!iX
!X
!X
!X
1
1
3
3
2
2
101
1
3
3
2
2
101
1
3
3
2
2
101
132
11
321
1321
k,i
i
k,k,k,
ki
i
ki
i
k
W!i
W!
W!
W
Y!i
Y!
Y!
Y
X!i
X!
X!
X
121
121
121
1
3
2
21
1
3
2
21
1
3
2
211
(10)
Where,
KJE,CJD
FJWEWDW
FJWEWDW
FJWEWDW
W
XEYDYXEXDX
YEYDYXEXDX
YEYDYXEXDX
WIYX
YIX
i
kk,ik,ik,i
kk,k,k,
kk,k,k,
k,
iiiiii
k,
11
21
21
1
123
1
012
0
2121
123123
012012
111
00
0
00
0
(11)
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Therefore, in this section, the equations will be
derived, considering up to the fourth derived function. If
the angular displacement 1k
and velocity 1k
at the
time t are expanded into the Taylor series,
considering up to the fourth derived function, they can be
expressed by Eq. (12) instead of Eqs. (10) and (11).
kkkkkkFDFCFBAA
11112111
kkkkkkFDFCFBAA
22222211
(12)
Eq. (13) can be rearranged.
k
kk
kk
FD
D
FC
CF
B
B
AA
AA
2
1
2
1
2
1
2221
1211
1
(13)
Where ij
A , i
B , i
C , and i
D 2121 ,j,,i
which constitute the transition matrix. are part ial matrices
of nn . The part ial matrices ij
A , i
B , i
C , and i
D
can be defined by the step size which satisfies the
condition for not diverging during the process of repeated
numerical simulat ions, that is the stabilizing condition,
and also satisfies the condition for obtaining the correct
solution and by the various factors constituting the
equivalent vibration systems shown in Fig. 3. The
excitation torque k
F and the time differentials k
F and
kF in Eq. (13). The angular d isplacement
1k and
velocity 1k
at the time t can be numerical
calculated by giv ing in itial values of k
and k
. This
numerical calcu lation can be repeated continuously. Since
no steady waveform was obtained for the first two or
three periods, the subsequent periods were adopted as the
final results. Since the values of the excit ing torques in
Eq. (13) are equals to zero in the case of free v ibrations,
only the first term need to be considered.
V. ANALYTICAL INVESTIGATION OF TORSIONAL
VIBRATION PROPERTIES OF ENGINE
CRANKSHAFT WITH DAMPER PULLEY
A. Input Data Necessary for Numerical Simulation of
Torsional Vibration Waveforms
Fig. 3 shows the equivalent torsional v ibration system
of a crankshaft with a rubber damper pulley rep laced
according to the analytical method described in section
(Measured Amplitude Curves of Angular Displacement).
The rubber part of the damper pulley is replaced with a
Voight model. Since the simulation program can yield the
torsional vibration waveform for a given engine speed,
the value of the strain rate is numerical simulation using
the measured dominant-order amplitude of angular
displacement at a given engine speed. Then, the values of
the dynamic torsional stiffness RDP
K and damping
coefficient RDP
C of the rubber part can be obtained by
referring to Eqs. (2) to (4), respectively. These obtained
values of RDP
K and RDP
C are used as the input data for
the numerical simulation. Since the curve-fitted curves in
Eqs. (3) and (4) are representative of all the experimental
data, the obtained values of RDP
K and RDP
C can be
regarded as the mean values.
Figure 3. Multi-degree of freedom of equivalent torsional vibration system of an engine crankshaft system with a rubber damper pulley [numerical simulation model].
PUL
RDP
IPUL
IRDP
KRDP
CRDP
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B. Numerical Simulation Results and Considerations.
Fig. 4 shows the main-order amplitude curves of the
angular displacements at the damper pulley end obtained
by analyzing harmonically the numerical simulat ion
torsional vibration waveforms of the crankshaft with the
rubber damper pulley. The numerical simulat ion
amplitude curves in th is figure correspond to the
measured amplitude curves of the angular displacements
in Fig. 2. As compared with the experimental results,
these numerical simulation results contain slight error,
but this degree of error is allowable in practice.
VI. SUMMARY
Accurate estimation of the dynamic p roperties of the
rubber part of the damper pulley are proble ms in the
numerical simulation of torsional vibration of a
crankshaft with a rubber damper pulley. The results of
investigation of these properties from experimental and
analytical viewpoints are as follows:
[1] We expressed the absolute torsional stiffness and
damping of the rubber part of the damper pulley as a
function of the strain rate under the conditions of the
same kind rubber material, constant temperature and
invariable shape factor.
[2] The valid ity of this method has been confirmed
from comparison and examination of measured values of
torsional vibration and simulation results.
CONFLICT OF INTEREST
The authors declare no conflict of interest
AUTHOR CONTRIBUTIONS
Tomoaki Kodama analyzed the experimental and
measured data, concuted the research, wrote the paper.
Yasuhiro Honda wrote the paper. All authors had
approved the final version.
REFERENCES
[1] T. Kodama, Y. Honda, K. Wakabayashi, S. Iwamoto, “A
calculation method for torsional vibration of a crankshafting system with a conventional rubber damper by considering rubber form, SAE 1996 International Congress and Exposition , SAE Technical Paper Series No. 960060, 1996, pp. 103-121.
[2] Y. Honda, K. Wakabayashi, T. Kodama, S. Hama, S. Iwamoto, “An experimental study on dynamic properties of rubber test specimens for design of shear-type torsional vibration dampers,“ in Proc. the Ninth International Pacific Conference on
Automotive Engineering, vol. 2, no. 971400 (Abstract Code:
00088), 1997, p. 217-222.
[3] Y. Honda, K. Wakabayashi, T. Kodama, H. Okamura, “An experimental study of dynamic properties of rubber specimens for a crankshaft torsional vibration of automobiles,” in Proc.
ASME 1999 International Design Engineering Technical
Conference and The Computers and Information in Engineering Conference, 17th Biennial Conference on Mechanical Vibration and Noise Symposium on Dynamics and Vibration of Machine Systems, Session VIB-00037: Dynamics and Vibration of
Machine System 02, DETC99/VIB-08125, 1999, pp. 1-14. [4] Y. Honda, T. Kodama, K. Wakabayashi, “Relationships between
rubber shapes and dynamic properties of some torsional vibration rubber dampers for diesel engines,“ in Proc. the 15th Pacific
Automotive Engineering Conference – APAC15, No.0320, 2009, pp. 1-8.
[5] T. Kodama, Y. Honda, “A study on the modeling consideration dynamic properties of vibration damper rubber parts,” in Proc.
2018_The 7th International Conference on Engineering and Innovative Materials ICEMI 2018, EM028, 2018, pp. 01-07.
[6] T. Kodama, Y. Honda, “A study on the modeling consideration dynamic properties of vibration damper rubber parts,” 2nd
International Conference on Robotics and Mechatronics, IOP Conference Series: Materials Science and Engineering 517, 012003, 2019, pp. 1-7.
[7] A. S. Mendes, P. S. Meirelles, “Application of the hardware-in-the-loop technique to an elastomeric torsional vibration damper,” SAE International Journal of Engines-V122-3, 2013, pp. 1-11.
[8] K. Yoon, I. Oh, J. I. Ahn, S. Y. Kim, Y. C. Chung, “A study for
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[9] A. K. Yadav, M. Birari, V. Bijwe, D. Billade, “Critique of Torsional Vibration Damper (TVD) design for powertrain NVH,” Symposium on International Automotive Technology 2017 , SAE Technical Paper 2017-26-0217, 2017, pp. 1-5.
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Copyright © 2020 by the authors. This is an open access article distributed under the Creative Commons Attribution License (CC BY-NC-ND 4.0), which permits use, distribution and reproduction in any
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Tomoaki Kodama
h as a Ph.D. degree in
engineering, with the Course of Mechanical En gineer in g, Dep artment of Scien ce an d En gin eer in g, Sch o o l o f Sc ien ce an d Engineering, Kokushikan University, T okyo,
Japan.
His research interests are NVH of int ern al com bust ion en gines ( in cludin g automotive and
marine engines), engineering
education, experiments in mechanical engineering, and mechanical
design.
He can be reached by e-mail at
Yasuhiro Honda
has a Ph.D. degree, with the
Course of Mechanical Engineering, Department of Science and Engineering, School of Science and Engineering, Kokushikan University,
Tokyo,
Japan.
His research interests are NVH of internal combustion engines, engineering education, vehicle kinematics,
mechanics, and automotive design.
He can be reached by e-mail
at
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International Journal of Mechanical Engineering and Robotics Research Vol. 9, No. 7, July 2020
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