Experimental research of dynamic damping of lateral vibrations of a rigid cantilever beam
S. Polukoshko^{1} , O. Kononova^{2} , I. Schukin^{3} , R. Smirnova^{4}
^{1}Ventspils University College, Engineering Research Institute “VSRC”, Inzenieru str. 101, Ventspils, LV3601, Latvia
^{2}Riga Technical University, Institute of Mechanics, Ezermalas str. 6, Riga, LV1006, Latvia
^{3, 4}Daugavpils Branch of Riga Technical University, Smilshu str. 90, LV5410, Daugavpils, Latvia
Journal of Vibroengineering, Vol. 15, Issue 1, 2013, p. 265270.
Received 22 October 2012; accepted 4 March 2013; published 31 March 2013
This work considers passive dynamic absorber (without additional energy source) of the simplest type: a noncontrolled spring with one degree of freedom. Object of vibration suppression is transversal vibrations of rigid cantilever beam. The inertial element is connected to the vibration protection object by means of elastic metal element  nonlinear conical coil spring. Experiments were performed on the universal vibration system TM 150.
Keywords: vibration attenuation, transversal vibration, single mass spring absorber, rigid beam, nonlinear spring.
1. Introduction
The problem of constructions and mechanisms vibration suppression appeared a long time ago and becomes more complicated because of transition to high speed, frequency and loading. A large number of solutions of this problem has been proposed [2, 3, 4, 7]. Nevertheless it remains of high interest these days [1, 6, 8, 11, 12]. There are two basic methods of vibroprotection: isolation and absorption. With a history of almost a century, dynamic vibration absorber has proven to be a useful vibrationsuppression device, widely used in hundreds of applications [7, 9, 10].
In accordance with principle of action, the absorbers can be inertial (mass) and impact. They are realized as spring, pendulum or roller. Vibrationcontrol system may be active, passive or semiactive depending on the amount of external power required for performing its function.
In this work the passive inertial single mass dynamic absorber of a spring type is examined. Basic system constitutes a rigid beam with one hinge joint supported with elastic spring, absorber are added to the rigid beam by means of conical helical spring. Conical spring has large inflexibility to the shear forces acting in the plane of coils of the spring in comparison with the cylindrical spring. Transversal vibrations of beam cause the lateral and bending vibrations of cylindrical springs connecting the additional mass. Conical spring was selected because of its ability to resist to the shear forces. A beam is exposed to power excitation by means of electric motor with unbalanced mass. Frequency can be changed within 050 Hz. In this research the effectiveness of absorber under constant sinusoidal excitation is studied. Forced vibrations of beams without absorbers and with absorbers were investigated.
The objective of this work is to develop the mathematical model of beam with a dynamic absorber on a nonlinear spring and to confirm its validity by experiments, executed on the laboratory equipment of TM150  equipment for engineering education (Gunt, Hamburg).
2. Experimental setup
The trainer laboratory equipment TM150 covers a wide range of topics in mechanical vibration technology. The schematic layout of the experimental laboratory setting for vibration testing is shown in Fig. 1. It is mounted on a sturdy, lowvibration aluminum sectional frame which is installed on a laboratory trolley with braked wheels. Elements may be quickly fastened to the frame. Forced vibration is generated with an electrical motordriven imbalance exciter. The exciter frequency can be set precisely on a control unit with a digital display.
Rigid beam dimensions: L×W×H = 730×25×12 mm, mass $m=$ 1.68 kg, beam has holes through 50 mm where different device may be fastened. Supporting tension – compression springs with stiffness $k=$ 3000 N/m is fastened at the distance $a=$ 0.30 m.
Fig. 1. Scheme of experimental setup: 1 – study frame, 2 – rigid bar, 3 – bearing, 4 – suspension cylindrical spring, 5 – height adjustable spring retainer, 6 – electrical imbalance exciter, 7 – conical spring, 8 – additional mass, 9 – sensor devices
Mass of the electroexciter is $m=$ 0.772 kg, electric motor has unbalanced mass ${m}_{u}=$ 100 g with eccentricity $\epsilon =$ 10 mm, rotation frequency of engine p ranges from 0 to 50 Hz. During experiments frequency of engine was varied from 0 to 5 Hz. Periodic excitation force is:
$F\left(t\right)={m}_{u}{p}^{2}\epsilon \mathrm{s}\mathrm{i}\mathrm{n}pt={F}_{u}\mathrm{s}\mathrm{i}\mathrm{n}pt$.
For precise amplitude measurements the contact device – dynamic sensor, based on principle of measuring of the electric field strength between a metallic beam and sensor, is used. Distance $e$ is about 15 mm, distance $d$ is changeable (in experiments it was 5.0 and 7.5 mm).
Measuring element reading are displayed on the computer monitor.
At the distance of $b=$ 0.65 m from the axis of rotation the additional mass of 0.3 kg and 0.5 kg are joined to the beam. For comparing the results the additional mass is joined without spring and with conical helical spring.
3. Conical spring properties
The conical spring is not standard equipment. It was custombuilt and tested in order to examine vibration dampening. A conical helical spring was fabricated from a highstrength steel wire of 1 mm diameter with the middle diameter of small coil of 13 mm, the middle diameter of large coil of 26 mm, 60 mm high with the permanent angle of slope of coil. Number of coils is 9. Testing of spring was executed to study its behavior under loading, test results are presented in Table 1. Analytical expression for conical spring stiffness characteristic, derived based on the test results is:
Table 1. Experimental results of conical helical spring stretching and compression
Spring stretching


Force $F$, N

5.0

6.0

9.0

10.0

11.00

14.

15.0

16.0

19.0

20.0

Deformation x, mm

14.0

17.0

26.0

28.5

31.0

39.0

42.0

45.0

54.0

57.0

Spring compression


Force $F$, N

5.0

6.0

9.0

10.0

11.0

14.0

15.0

16.0

19.0

20.0

Deformation x, mm

14.0

16.0

24.0

25.0

27.0

33.0

35.0

37.0

40.0

41.0

Plots of spring force dependence on its deflection, based on experimental data and in accordance with analytical expression (1), are shown in Fig. 2.
Fig. 2. Plots of spring force dependence on its deflection: experimental data, analytical dependence
The dependence between spring force and deflection is linear in the tension zone and partially in compression zone and nonlinear in compression zone.
4. Analytical model of beam. Equations of motion
Fig. 3 provides the scheme of beam and analytical model with the imposed forces. Parameters of vibration system are given in Table 2, were $J$ – the moment of inertia of system in relation to the axis of bearing, $\omega $ – natural circular frequency of the system and $f$ – natural frequency: $\omega =\sqrt{\frac{{a}^{2}k}{J}}$, $f=\frac{\omega}{2\pi}$.
Inertia moment $J$ for rigid beam, beam with exciter and beam with exciter and additional mass, respectively: ${J}_{0}=\frac{{m}_{b}{L}^{2}}{3}$, $J={J}_{0}+{m}_{el}{c}^{2}$, $J={J}_{0}+{m}_{el}{c}^{2}+m{b}^{2}$.
Fig. 3. a) Scheme of the beam vibration, b) analytical model of rigid beam
a)
b)
Table 2. Parameters of vibration system
System description

$J$, m^{4}

$\omega $, s^{1}

$f$, Hz

Beam without exciter

0.298

30.079

4.787

Beam with exciter

0.677

19.975

3.179

Beam with exciter and mass 0.3 kg on $b=$ 0.65 m

0.803

18.332

2.918

Beam with exciter and mass 0.5 kg on $b=$ 0.65 m

0.888

17.438

2.775

Natural circular frequency of mass on spring in linear zone and natural frequency:
$f=\frac{1}{2\pi}\sqrt{\frac{{k}_{1}}{{m}_{1}}}$, where ${k}_{1}=$ 350 N/m;
for $m=$ 0.3 kg, $f=$ 5.436 Hz; for $m=$ 0.5 kg, $f=$ 4.211 Hz.
Motion of beam with the electroexciter and added mass, taking into account the forces of viscous resistance:
$J\ddot{\varphi}={a}^{2}k\varphi \mu \dot{\varphi}+{F}_{u}c\mathrm{s}\mathrm{i}\mathrm{n}pt\text{,}$
$\ddot{\varphi}+2n\dot{\varphi}+{\omega}^{2}\varphi ={f}_{u}c\mathrm{s}\mathrm{i}\mathrm{n}pt\text{,}$
where: ${\omega}^{2}=\frac{{a}^{2}k}{J}$, $2n=\frac{\mu}{J}$, ${f}_{u}=\frac{{F}_{u}}{J}=\frac{{m}_{u}{p}^{2}\epsilon}{J}$.
The solution of Eq. (2) – steadystate vibration under action of harmonic exciting force [5]:
Comparing the experimental and theoretical amplitudes for given frequency it is possible to estimate the value of coefficient of viscous resistance $\mu $.
Motion of beam with an electroexciter and added mass with conical spring:
$\left\{\begin{array}{l}({J}_{0}+{m}_{el}{c}^{2})\ddot{\varphi}={a}^{2}k\varphi +{F}_{2}b\mu \dot{\varphi}+{F}_{u}c\mathrm{s}\mathrm{i}\mathrm{n}pt,\\ {F}_{2}=\left\begin{array}{c}{k}_{1}(yb\varphi ),if(yb\varphi )>0.01,\\ {k}_{1}(yb\varphi )+{k}_{2}{(}^{b}{k}_{3}{(}^{y},\text{i}\text{f}(yb\kappa )\le 0.01,\end{array}\right.\\ m\ddot{y}={F}_{2},\end{array}\right.$
where conical spring stiffness coefficients ${k}_{1}$, ${k}_{2}$, ${k}_{3}$ are taken in accordance with Eq. (1).
This system has two degrees of freedom and its position is determined by two coordinates: rotation angle $\phi $ of beam round a point $O$ and vertical displacement of mass $y$; $y$  axis is assumed directed upward considering that mass moves vertically. Other forces imposed on the additional mass and beam may be neglected because of small rotation angle.
5. Numerical solutions and experimental results
System (4) and, for comparison, Eq. (2) were solved numerically using Euler’s method with the help of МathCad program for every recorded frequency of excitation force. The examples of the plots of rotation angle dependence on time are given below in Fig. 4 for the beam with additional mass 0.30 kg on conical spring: a) for subresonance value of excitation force frequency, b) for resonance value.
Fig. 4. Plots of dependence of beam rotation angle (degrees) on time: $\mu =$ 0.5, $m=$ 0.3 kg
a)$f=$ 2.612 Hz
b)$f=$ 2.870 Hz
On the basis of received data amplitudefrequency response curve were determined for experimental data and for theoretical calculations. Figs. 56 provide amplitudefrequency characteristic for beam with additional mass without spring and with conical spring. Here the maximal amplitude are measured and put on the plot. The amplitude of steadystate vibrations was also measured.
Fig. 5. Amplitudefrequency responses for the beam with additional mass $m=$ 0.30 kg: theoretical with $\mu =$ 0.5; experimental
a) Mass without spring
b) Mass with conical spring
Fig. 6. Amplitudefrequency responses for the beam with additional mass $m=$ 0.50 kg: theoretical with $\mu =$ 0.5; experimental
a) Mass without spring
b) Mass with conical spring
As calculations indicate, the spring behaves mainly in a linear fashion. Nonlinearity manifests at a large compression in the vicinity of resonance. Viscous resistance is not constant and varies with frequency.
6. Conclusions
This paper reported on the experimental study of dynamic vibration absorber for suppression of rigid beam transversal vibrations. Inertial dynamic vibrations absorber was realized as a mass added to the vibrating object by means of a conical coil spring. Such device reduces oscillations in the vicinity of resonance. A conical coil spring is used because of its ability to resist to the shear forces. Cylindrical coil spring was also tested, which gave a small suppression effect because of arising of bending and lateral vibrations of mass on spring. The mathematical model of inertia dynamic vibration absorber with a nonlinear conical spring was provided. Results of theoretical calculations are in good agreement with experimental findings, thereby confirming the validity of the applied mathematical model.
In future it is necessary to refine the mathematical model by taking into account more carefully joint friction losses and viscous resistance in springs.
Acknowledgements
This work has been supported by the ERDF’s grant, within the project “SATTEH”, No. 2010/0189/2DP/2.1.1.2.0/10/APIA/VIAA/019, being implemented in Engineering Research Institute “Ventspils International Radio Astronomy Centre” of Ventspils University College (VIRAC).
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