VIBRATIONS OF A SHORT SPAN, COMPARISON BETWEEN MODELIZATION AND MEASUREMENTS PERFORMED ON A LABORATORY TEST SPAN - PowerPoint PPT Presentation

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VIBRATIONS OF A SHORT SPAN, COMPARISON BETWEEN MODELIZATION AND MEASUREMENTS PERFORMED ON A LABORATORY TEST SPAN

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vibrations of a short span, comparison between modelization and measurements performed on a laboratory test span s. gu rard (ulg) j.l. lilien (ulg) – PowerPoint PPT presentation

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Title: VIBRATIONS OF A SHORT SPAN, COMPARISON BETWEEN MODELIZATION AND MEASUREMENTS PERFORMED ON A LABORATORY TEST SPAN


1
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
2
Introduction
  • The present work is a sequel to paper 44, ISCD2009

Data collected on IREQs cable testbench is used
to validate a beam element model of the cable span
3
Introduction
Example of power line cable damage caused by
fatigue

(Courtesy of Alcoa 1961)
4
Introduction
  • Damage 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
5
Objectives
  • Reproduce mode shapes
  • Reproduce the shape of the conductor in the
    vicinity of span ends
  • Take into account conductors variable bending
    stiffness
  • Take into account conductors self damping
    characteristics

6
Key result with the model
  • The impact of tension fluctuations on the model
    of the 63.5m span is not negligible

7
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
    EI591.3 N.m² is considered

One of the models used 331 nodes along the 63.5m
span, with mesh refinement near the span
extremities
8
Shape of eigen modes
Comparison between measured and computed position
of vibration node 1 for the beam and cable models
Mode Position of node 1 measured 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
The position of node 1 is computed with a
difference of a few with the beam model against
10 for the cable model
 Vibration Node 1 
9
Time Response with a Forced Excitation
Hypotheses
  • No numerical damping (Newmarks integration
    scheme)
  • The vibration shaker is modelled by a vertical
    harmonic force

10
Time Response with a Forced Excitation
Results
  • 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

Time evolution of antinode position
Lissajous curve acceleration vs excitation
11
Time Response with a Forced Excitation
Time evolution of tension
Results
  • The presence of vibrations generates a continual
    tension fluctuation which reaches up to 3 of the
    conductor average tension and 0.5 RTS

Frequency content of tension
  • A frequency content analysis of the tension shows
    an important component at twice the excitation
    frequency gt an anti-symmetrical mode is excited

12
Sensitivity Analysis
Sensitivity to the value of the average bending
stiffness
Sensitivity to the value of the excitation force
Position of antinode
Position of antinode
time
time
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
13
Conductor Self-Damping
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
14
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)
15
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
16
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
    spans fundamental frequency

17
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 neglected

Continuous change of eigenfrequencies Difficult
to obtain a perfect resonance with the
model Contribution to node vibrations gt
potential impact on ISWR damping method has to be
checked Interest for experiments on  real
longer spans
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