171 vibrations of a short span, comparison between modelization and measurements performed on a...
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VIBRATIONS OF A SHORT SPAN, COMPARISON BETWEEN MODELIZATION AND MEASUREMENTS PERFORMED ON A
LABORATORY TEST SPAN
S. Guérard (ULg)
J.L. Lilien (ULg)
P. Van Dyke (IREQ)
8th International Symposium on Cable Dynamics (ISCD 2009) September 20-23 2009, Paris
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Introduction
The present work is a sequel to paper 44, ISCD2009
Data collected on IREQ’s cable testbench is used to validate a beam element model of the cable span
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Introduction
(Courtesy of Alcoa 1961)
Example of power line cable damage caused by fatigue
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IntroductionDamage occurs at points where the motion of the conductor is constrained against transverse vibrations.E.g.:suspension clamp, spacer,air warning marker,spacer,damper,…
Need to model the shape of the conductor near those Concentrated masses
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Objectives
• Reproduce mode shapes
• Reproduce the shape of the conductor in the vicinity of span ends
• Take into account conductor’s variable bending stiffness
• Take into account conductor’s self damping characteristics
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Key result with the model
• The impact of tension fluctuations on the model of the 63.5m span is not negligible
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Model description• The finite element code Samcef V13.0 and its non linear module
Mecano has been used• with non linear beam element (T022)• An average bending stiffness value of EI=591.3 N.m² is considered
One of the models used: 331 nodes along the 63.5m span, with mesh refinement near the span extremities
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Shape of eigen modes
ModePosition of
node 1 measure
d [m]
Position of node 1 beam model
[m]
Difference%
Position of node 1 cable model
[m]
Difference %
19 3.65 3.68 3% 3.34 8.5%
40 1.83 1.856 1.5% 1.63 11%
53 1.39 1.40 0.4% 1.22 12.4%
Comparison between measured and computed position of vibration node 1 for the beam and cable models
« Vibration Node 1 »
The position of node 1 is computed with a difference of a few % with the beam model against ~10% for the cable model
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Time Response with a Forced Excitation
• No numerical damping (Newmark’s integration scheme)
• The vibration shaker is modelled by a vertical harmonic force
Hypotheses
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Time Response with a Forced ExcitationResults
• Eigenfrequencies are shifted with the introduction of the shaker
• Even after a frequency adjustment, beats can be seen in the time evolution of antinode
• The phase between excitation and acceleration is not constant
Lissajous’ curve acceleration vs excitation
Time evolution of antinode position
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Time Response with a Forced Excitation
• A frequency content analysis of the tension shows an important component at twice the excitation frequency => an anti-symmetrical mode is excited
Time evolution of tension
Frequency content of tension
• The presence of vibrations generates a continual tension fluctuation which reaches up to 3% of the conductor average tension and 0.5% RTS
Results
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Sensitivity Analysis
Sensitivity to the value of the average bending stiffness
Sensitivity to the value of the excitation force
A bending stiffness change of 10% leads to an amplitude change comprised between 1 to 6%
Changes of 10% in the amplitude of the excitation force leads to an amplitude change of the order of 5%
time time
Pos
ition
of
antin
ode
Pos
ition
of
antin
ode
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Conductor Self-Dampingvv v
v H
Using a visco-elastic model for the beam material:
It appears that the most adequate value of parameter v is comprised between 0.001 and 0.0001
0.E+00
1.E-04
2.E-04
3.E-04
4.E-04
5.E-04
6.E-04
7.E-04
8.E-04
9.E-04
1.E-03
0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2
distance from span end (m)
pk
-pk
dis
pla
ce
me
nt
(m)
v=0.001
v=0.0001 (minimum and maximum values of the "beat")
Measurements
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Reproduction of Observed Phenomena When In-Span Line Equipment is Introduced
For certain frequencies, higher amplitudes were observed on subspan A…
Equipment
Subspan A
Subspan B
… These higher amplitudes on subspan A are met for excitation frequencies equal to a multiple of the fundamental frequency of subspan A (see graph in the next slide)
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Reproduction of Observed Phenomena When In-Span Line Equipment is Introduced
Higher amplitudes on subspan A are met for excitation frequencies which correspond to a multiple of the fundamental frequency of subspan A
0
0.5
1
1.5
2
2.5
3
3.5
4
4.5
5
0 1 2 3 4 5 6
Ratio "excitation frequency/ fundamental frequency of subspan A"
Rat
io "
anti
no
de
amp
litu
de
of
sub
span
A/a
nti
no
de
amp
litu
de
of
sub
span
B"
M=8kg M=5kg M=0kg
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Conclusions
• The model allowed to show that higher amplitudes on the short portion of the span occur when the excitation frequency is a multiple of the short span’s fundamental frequency
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Conclusions
• The shape of a conductor vibrating at its vibration modes in the vicinity of the span end is correctly reproduced
• tension fluctuations cannot be neglectedContinuous change of eigenfrequencies
Difficult to obtain a perfect resonance with the model
Contribution to node vibrations => potential impact on ISWR damping method has to be checked
Interest for experiments on « real» longer spans