An experimental determination of joint connection type influence to damping in frame towers.
Prodanovic, Novak ; Isic, Safet ; Voloder, Avdo 等
1. INTRODUCTION
Damping is material or system property that is characterized by
energy dissipation in a vibration. Analysis of mechanical vibrations
without damping is a mathematical fiction, which takes place in the
introductory considerations in the theory of vibrations (Beards, 1996).
Any realistic analysis of system vibrations requires consideration of
the damping effect. However, the damping is the effect that is still
less researched and which modeling is the difficult. Practically,
experimental determination of a damping is the most used method (Fanti
et al., 2006), (Dolecek et al., 2008). In many constructions exploited
to a dynamical load it is also desirable to have possibility of damping
increasing. This is very important in the case of towers, exploited to a
wind load, which may cause effect of galloping vibrations. In this paper
is presented experimental determination of damping factor and its
dependence on considered type joint in the case of tower construction
model.
2. PRELIMINARY VIBRATION MODE ANALYSIS
In order to produce the simplest vibration form of the tower model,
its vibration modes are determined. Vibration modes are extracted from
the finite element equation
[M]{[??]}+[K]{D} = 0 (1)
where [M] is mass matrix, [K] is stiffness matrix and {D} is
displacement vector of the tower. It should be noted that mass and
stiffness matrix could be calculated from geometry and material
properties of the tower. First bending and torsional modes are shown in
the Fig. 1.
[FIGURE 1 OMITTED]
These vibration modes are used as the template for tower initial
deformation in order to produce vibration for damping measurement.
Initial deformation in the form of selected vibration modes is possible
to obtain by simple force acting on the top of the tower. Axerting of
two forces in the same direction produce the bending mode and two forces
of the opposite direction produce the torsional mode.
3. EXPERIMENT SETUP
Experimental setup for damping research is presented in the Fig. 2.
The model of the tower is mounted on the heavy concrete foundation.
"L" shaped members of the tower are connected by using joints
with screws and rivets. For all used joint types, tower is excited to
vibrate in the form of bending and torsional eigenmodes, shown in the
Fig. 1. Acceleration of produced vibrations are measured in the two
perpendicular directions by two acceleration sensors KD 37V (Metra Mess
Technick--Germany) mounted on the tower (Fig. 3). Measuring signal is
recorded on the computer by using CATMAN software (Hottinger Baldwin
Messtechnik--Germany).
[FIGURE 2 OMITTED]
[FIGURE 3 OMITTED]
The recorded accelerograms of vibrations are shown in the Fig. 4.
It could be seen that resulting vibration have the form of free damped
vibration, which amplitude exponentially decrease.
[FIGURE 4 OMITTED]
For statistical analysis of the results, for all joint type and
form of vibration ten repetition of the measurement are made.
4. DAMPING FACTOR CALCULATION
In the case of damped vibrations, amplitude decreases exponentially
as shown in the Fig. 5, and amplitude decreasing could be expressed as
x(t)[[varies][e.sup.-ct] (2)
where x is amplitude of vibration, c is damping factor and t is
time.
[FIGURE 5 OMITTED]
In order to calculate damping factor from recorded accelerograms,
maximum values of accelerations are extracted and interpolated by
exponential function of the form Aexp(-ct), from which damping factor c
is determined. Obtained results for all performed measurement by using
screwed and riveted joints and vibration in the form of bending (B) and
torsional (T) eigenmode are given in the Table 1.
5. RESULTS ANALYSIS
Statistical analysis of experimental results is presented in the
Fig. 6. It could be seen that damping factor is less about 30% in the
case of riveted joints. Statistical analysis of the results obtained
from different vibration modes for one joint type show that there is no
significant difference between them.
[FIGURE 6 OMITTED]
6. CONCLUSION
Influence of used joint type to the damping in frame towers is
analysed experimentally. Experimental results of damping factor in the
case of joints with screws and rivets are presented. Presented results
of experimental damping factor determination show that screw joints
produce about 30% higher damping factor than joints with rivets. The
reason for it is in the fact that screws enable better tightening of
members in the joints what produces higher stiffness of the used tower.
7. REFERENCES
Beards, C.F. (1996). Structural Vibration--Analysis and Damping,
Arnold, ISBN 0-340-64580-6, London
Dolecek V., Isic S. & Voloder A. (2008). An Experimental
Damping Determination In Beam Bifurcation Process, Proceedings of 19th
International DAAAM Symposium "Intelligent Manufacturing &
Automation: Focus on Next Generation of Intelligent Systems and
Solutions", Trnava, Slovakia, 22-25th October 2008, Katalinic, B.
(Ed.), pp 205-206, ISBN 978-3-901509-68-1, Published by DAAAM
International, Vienna
Fanti, G., Basso, R. & Montauti, V. (2006).Damping
Measurement of Bending Vibration in Alpine Skis: An Improvement of
Standard ISO 6267, Applied Mechanics and Materials, Vols. 5-6, 2006, pp
199-206, ISSN 1662-7482
Geradin, M. & Rixon, D. (1998). Mechanical Vibrations, Second
Edition, John Willey & Sons, ISBN 047197546X, New York
Isic, S., Dolecek, V. & Karabegovic, I. (2007). The Simulation
and Vizualization of Plane Truss Eigenvibration, Proceedings of 18th
International DAAAM Symposium "Intelligent Manufacturing &
Automation: Focus on Creativity, Responsibility and Ethics of
Engineers", Katalinic, B. (Ed.), Zadar, 24-27th October, 2007, pp
347-348, ISBN 3-901509-58-5, Published by DAAAM International, Vienna
Virgin, L.N. (2000). Introduction to Experimental Nonlinear
Dynamics: A Case Study in Mechanical Vibration, Cambridge University
Press, ISBN 0-521-66286-9
Tab. 1. Experimental values of damping factor c
Screw joints
T 0.0232 0.0234 0.02883 0.02693 0.02960
0.03265 0.03407 0.03072 0.02904 0.02632
B 0.02323 0.03231 0.02936 0.02870 0.02960
0.03079 0.02724 0.03916 0.03417 0.02531
Riveted joints
T 0,03039 0,01059 0,01851 0,02439 0,02232
0,02313 0,02211 0,02057 0,02136 0,01895
B 0,02139 0,01023 0,02558 0,02345 0,02407
0,01229 0,01600 0,01730 0,01964 0,02043