Research Article | Open Access
A New Design of Vibration Absorber for Periodic Excitation
Bothrops mattogrossensis snake is widely distributed throughout eastern South America and is responsible for snakebites in this region. This paper reports the purification and biochemical characterization of three new phospholipases A2 (PLA2s), one of which is presumably an enzymatically active Asp49 and two are very likely enzymatically inactive Lys49 PLA2 homologues. The purification was obtained after two chromatographic steps on ion exchange and reverse phase column. The 2D SDS-PAGE analysis revealed that the proteins have pI values around 10, are each made of a single chain, and have molecular masses near 13 kDa, which was confirmed by MALDI-TOF mass spectrometry. The N-terminal similarity analysis of the sequences showed that the proteins are highly homologous with other Lys49 and Asp49 PLA2s from Bothrops species. The PLA2s isolated were named BmatTX-I (Lys49 PLA2-like), BmatTX-II (Lys49 PLA2-like), and BmatTX-III (Asp49 PLA2). The PLA2s induced cytokine release from mouse neutrophils and showed cytotoxicity towards JURKAT (leukemia T) and SK-BR-3 (breast adenocarcinoma) cell lines and promastigote forms of Leishmania amazonensis. The structural and functional elucidation of snake venoms components may contribute to a better understanding of the mechanism of action of these proteins during envenomation and their potential pharmacological and therapeutic applications.
Dynamic vibration absorber (DVA), also known as tuned mass damper (TMD) , has been proven to be a useful device for mechanical vibration attenuation. A conventional DVA, composed of a spring-mass-damper (SMD), is mostly mounted to a primary structure, as shown in Figure 1(a) , to absorb the vibration of one single (tonal) frequency. The fundamental design of an SMD can be seen from many vibration textbooks and is not addressed here. The more elaborate works on SMD fall into the category of damper design. Brock  derived an optimum Lanchester damper. Ozer and Royston  extended Den Hartog’s method to multi-DOF structure and derived the optimal dampers and mounting locations. They further employed Sherman-Morrison matrix inversion formula to calculate the optimal parameters for a damped multi-DOF absorber system . Ren  introduced the so-called ground-hook DVA as shown in Figure 1(b). Of the same mass ratio and under harmonic excitation, the ground-hook DVA appeared to have better absorption than the traditional one. Wong and Cheung, similarly, concluded that the ground-hook DVA’s vibration suppression is superior to the traditional one particularly when the excitation comes from the ground motion .
In order to enhance the DVA’s absorption ability, numerous papers have been aimed at different research aspects, such as control rules derivation, structure’s properties variation, special material and different DVA’s combination. Details of these researches may be referenced to Sun et al. , where they surveyed the gradual development of the passive, adaptive, and active tuned vibration absorber. Chen and Xu  discussed a DVA comprised of not only mass-spring-viscous damper but feedback control force to suppress broadband vibration and their results showed that the response had been reduced by 90%. Burdisso and Heilmann  developed a hybrid DVA for vibration control as shown in Figure 1(c). The DVA comprised two reaction masses and in between there was a passive/semiactive/active damper. This hybrid DVA has been proven to have better suppression effect than an ordinary SMD, particularly for broadband vibration.
As to multifrequency vibration suppression, Sun et al.  studied the differences in vibration absorption between the conventional DVA, the state-switched absorber (SSA), and dual-DVA (Figure 1(d)). Under the optimization process, their results showed that dual-DVA had very close performance as the SSA and both were, as expected, superior to the conventional DVA in multifrequency vibration suppression. The conclusion for dual-DVA design is as simple as tuning each DVA to a frequency wanted to be absorbed. Hill and Snyder  designed a dual mass absorber to suppress the vibration at multiple frequencies, which consisted of two rods (smooth and threaded) supporting two equal masses (bells) on both sides. This device was able to tune the first six natural frequencies, mixed in bending and torsion modes. The natural frequencies were yet restricted to be tuned in pairs, that is, first and second together, and so on. In 2006, Wang and Cheng  used the impedance technique to design a multifrequency absorber by varying single beam’s several cross-sectional areas such that the beam’s natural frequencies coincided with the designated frequencies. Although a geometrically nonuniform beam could theoretically attain any desired multifrequency, it however required very tedious calculations and complicated shaping in manufacturing.
In real world, most of the mechanical systems are subjected to periodic rather than simple harmonic excitation. Mathematically, periodic excitation is composed of a series of infinite harmonics in integer multiples of base frequency. Nevertheless, only are the first few components significant in mechanical vibration. In general cases, the first three harmonics contain about 90% of the overall excitation. To suppress periodic excitation, one may employ the multifrequency DVA technique  and tune three DVA’s frequencies to the first three harmonics. The consequence, yet, will be significant mass loading to the main system. The mass loading effect may be reduced by lowering the DVA’s mass ratio but the cost would be the absorber highly sensitive to excitation frequency variation. The present investigation is hence motivated by the necessity of developing a simple, passive PVA of relatively low mass ratio for periodic excitation. The derived dual-beam PVA (Figure 2) in this paper will prove itself to meet the goal and to provide significant applicability for vibration engineers.
2. Frequency Equation of PVA
Figure 2 schematically shows the designed PVA mounted on a primary system to resist periodic excitation.anddenote the primary system’s mass and stiffness, respectively. The PVA is composed of two cantilever beams (dual-beam) with an intermediate spring of constant. The intermediate spring is connected at the position of . For simplicity, though not necessary, the two beams’ length is assumed to be the same. , , , and , , stand for the beam’s density, cross-sectional area, Young’s modulus, and area moment of inertia, respectively.
Utilizing the structure combination technique and the receptance method [14, 15], this PVA can be divided into two parts, as shown in Figure 3, and the corresponding frequency equation is where is the receptance of the first cantilever beam and can be expressed  as Similarly, stands for the receptance of the second cantilever beam plus spring, where is a cantilever beam’s mode shape. is the beam’s natural frequency. and , respectively, are the mode numbers of two beams. Note that the cantilever beam is assumed to be of Bernoulli-Euler’s model and (or , ) denotes the PVA’s natural frequency to be solved.
The design criterion is to make the PVA’s first few natural frequencies be in integer multiples of the base frequency of periodic excitation; that is, , . Substituting (2) and (3) into (1), and it is obtained that where is the normalized spring location and is the PVA’s natural frequency.
For simplicity, a dimensionless parameter, denoting the known ratios of a cantilever beam’s natural frequency to its first natural frequency, is introduced. Equation (4) is then rewritten as We further define two design variables, and , denoting the ratios of the first and the second cantilever beam’s fundamental natural frequency to the base frequency of excitation. Equation (5) becomes
Utilizing the orthogonal property of beam’s mode shapes and one normalized equation, , (6) is simplified to be Subsequently, further reduction yields where denotes another design variable, the mass ratio of the two beams. The normalized spring constant is the last design variable, where is the first mode wave number of single cantilever beams; that is, . Equation (8) presents the PVA’s frequency equation in a dimensionless form. Mathematically, we have derived the design problem as an explicit function of five design variables (,,,, and ); that is, . It implies that the maximum number of PVA’s frequencies could be tuned up to five; that is, PVA’s first five natural frequencies might be determined via appropriate selection of the five design variables. It is yet unnecessary and nonrealistic to tune so many frequencies since the first three harmonics usually contain more than 90% of the excitation. To tune higher harmonics more closely it will sacrifice the accuracy of lower ones, which are yet the most important. In the following examples, we will tune the PVA only up to the first three natural frequencies; that is,.
3. Simulations and Experimental Verification
From (8), it is seen that there is room to set two out of five design variables as known values. Prior to doing that, it is helpful to realize the intercorrelation between all design variables. We first set the mass ratio (), once at a time, at a specific value and look into the correlations between and the other three parameters (, , and ). The curves are drawn in Figure 4. It is seen that all parameters vary with in a nonlinear trend. From the shown curves, it is obvious that and are more sensitive to . curves are rather flat relative to variations. , yet, shows much larger sensitivity (curves farther apart) to μ’s change than and do. These correlations shown in Figure 4 provide us with a reference to determine the design variables, although not in an optimal sense. For example, one may first select appropriate and (most sensitive); then, from its corresponding one can continue for suitable and . The above-mentioned process is just one of many possibilities. Two examples solved by the above process are illustrated and the calculations are given in Table 1.
|Spring constant: KN/m; connecting location: mm.|
|Spring constant: KN/m; Connecting location: mm.|
A simple experiment is then set up to verify if the obtained PVA (Table 1) has integer multiples of the base frequency as we desired. Figure 5 shows the setup of experimental apparatus. The displacement and corresponding FRFs of the PVA are picked up and transferred by an ONO SOKKI Laser Vibrometer (LV-1710). Figure 6 shows the FRFs of two specimens and it is seen that the first three natural frequencies are very close to integer multiples of the base frequency, one 70 Hz and one 35 Hz. The PVAs’ first resonance frequencies coincided precisely with the base frequency but the second and the third showed some errors (3.80% at most). The first three modes of specimen A are sketched in Figure 7 and it is seen that the first beam deforms more significantly than the second one for its larger flexibility (Table 1).
Now, implement the PVA onto the main system and analytically calculate the vibration reduction of the main system due to periodic excitation. The data of the main system are chosen as follows: Kg, kN/m, and = 17.6 Hz. Unit square wave loading is first discussed. Note that in the following simulations, the excitation frequency is set at 120 Hz throughout the paper unless compared to experiments, in which the excitation is set at 55 Hz. Figure 8 shows three simulated response amplitudes of the primary system for (i) with no absorber, (ii) with a single DVA tuned at , and (iii) with the designed PVA. To have a fair comparison, DVA’s mass is equal to PVA’s. Figure 8(a) compares the responses of (i) and (iii) and the absorption effects of PVA are very significant. The reason we did not superimpose (ii) in Figure 8(a) is because under the same scale it is difficult to see the differences between (ii) and (iii). Instead, Figure 8(b) enlarges the responses of (ii) and (iii) and the differences between them reflect the contribution of higher harmonics. Note that the response amplitudes shown in the above figures, afterwards as well, are all in a dimensionless form by normalizing them with respect to the static displacement; that is, ,. Simulations for unit saw-tooth wave loading at the same frequency are illustrated in Figure 9 and similar results are obtained. From Figures 8(b) and 9(b), one may notice that the higher harmonics of saw-tooth and square-wave have different frequencies even though they are of the same base frequency. This can be explained after Fourier series expansion of the square-wave and saw-tooth functions, Since we used odd functions in both cases, the second harmonic () of the square wave is zero by itself but not in the saw-tooth case and the third harmonics for both cases are of the same magnitude. That explains why Figure 8(b) showed the 3rd harmonic and Figure 9(b) showed the 2nd in the curves of (ii). Table 2 compares the absorption effects of all the simulated cases. In a square-wave case, a DVA is good enough to reduce the system response amplitude by 28.8 dB but just 16.8 dB in the case of saw-tooth because the square-wave originally contains no second harmonic. The PVA yet reduces the system responses by 38.3 dB and 28.2 dB, respectively, for the square-wave and the saw-tooth, contrast to the DVA, 9.5 dB, and 11.4 dB more.
Experiments follow to verify the above simulations. Figure 10(a) shows the photo and Figure 10(b) shows the schematic diagram of apparatus setup. Figure 11 is the experimental time responses of the system with and without PVA under saw-tooth excitation of frequency 55 Hz. It is observed that the main system’s vibration is drastically reduced by PVA. Figure 12 compares the experimental data of Figure 11 and the simulation results. Note that at the first glance there seems a huge discrepancy between experiment and simulation but thorough inspection will reveal that the major difference comes from the nonzero DC term in the experimental data. If one shifts the DC bias, the maximum amplitudes of the simulation and the experiment are, respectively, 0.001 and 0.0015. Table 3 illustrates the data and the difference is about 3.5 dB. This difference seems not to be negligible but in contrast to the overall effect of 19.4 dB, this discrepancy is acceptable. This discrepancy can be attributed to the following causes. First, the PVA did not perfectly match the higher harmonics (3.8% error) and secondly all the analyses were based on undamped situation. Though no intended damper was added in the primary system or PVA, there exists damping in the real world. A small amount of damping would shift the best absorption frequency and reduces the attenuation effects.
Though the simulation has shown PVA’s excellent vibration absorbability, to meet engineering applications, the PVA has to be adjustable to slight excitation frequency variation without reconstructing PVA. Reviewing all of the design variables, and , the spring’s stiffness and position appear to be the two easiest ones for adjustment without reassembling the structure. Figure 13 illustrates how the PVA’s first three resonance frequencies vary with (a) the spring stiffness and (b) the spring location. The ordinates are the dimensionless frequency variations; that is, ,. As anticipated, both the spring stiffness and location change PVA’s resonance frequencies monotonically, that is, changing and , will shift all the first three frequencies in the same direction but of different sensitivity. For instance, the first frequency () is the most sensitive to but the third one () is the most sensitive to . Since all the sensitivities are not in proportion, it is unable to tune , and simultaneously retain the first three natural frequencies in exact integer multiples as wanted. The objective is to reduce the response to a maximum amount; therefore, the first harmonic should be adjusted to the least error. Figure 14 shows some of the solutions to reducing the mismatch effect. Figure 14(a) compares the system responses of perfect match, 1% frequency mismatch without any adjustment and with single adjustment. It is seen that the system’s vibration level increased by mismatch and was obviously attenuated by simply tuning the spring stiffness constant (3.78% increase). Figure 14(b) compares the differences of tuning one and two variables. With simultaneous adjustment of and , the response amplitude is further reduced. From the above illustration we are confident that the designed PVA offers satisfactory periodic vibration absorbability and can be tuned to correspond to slightly external frequency variations.
Our calculations revealed, not shown in this paper, that the adjustment yielded poor results for the 3rd harmonic as the mismatch exceeded 3%. It is yet still assured that the first frequency can always be adjusted to meet the base frequency even for larger excitation frequency variation and the PVA still performs better than a single DVA. This can be verified by comparing the response amplitudes. From Table 2, the amplitude with a DVA is 0.026 and the maximum amplitude in Figure 14(b) is around 0.02, less than DVA’s. Figure 15 shows the FRF of the combined primary-PVA system. The dash lines denote the PVA’s resonance frequencies and they become antiresonance frequencies of the combined system.
In this paper, a periodic vibration absorber (PVA) of dual-beam type is for the first time ever designed, analytically discussed, and experimentally verified. The PVA consists of two cantilever beams interconnected with an intermediate discrete spring. When the spring is appropriately chosen and located, the PVA can very effectively attenuate any periodic excitation. The frequency equation of the designed PVA was theoretically derived from the receptance method and subsequently arranged in a general, dimensionless form in terms of five design variables. Enforcing the PVA’s resonance frequencies in integer multiples and solving the frequency equation, the PVA’s parameters were determined according to the excitation base frequency. This paper demonstrated examples of setting the PVA’s first three resonance frequencies in integer multiples of the base frequency and the results appeared to be accurate by experimental verification.
The responses of the primary system with/without the designed PVA were calculated in simulations. As expected, the results showed PVA’s excellent absorption effect to periodic excitation. Experiments followed to verify the theoretical calculations and satisfactory agreement has been obtained. From the shown examples, PVA could improve the response amplitude 9.5~11.4 dB more, compared to a single DVA. The error of PVA’s absorption between simulation and experiment was about 3.5 dB that might be attributed to the design variables’ variations and the ignored damping existed in structures. The ability of adjusting spring’s stiffness and location to compensate the mismatch of excitation frequency was studied as well. The results showed that PVA could be well tuned if mismatch was less than 3% and the tuned PVA still performed better than a single DVA. The derived PVA in this paper is useful for the audience in vibration engineering and is believed to provide an efficient and effective tool for suppressing periodic vibration of structures.
|:||Cross-sectional area of th beam|
|:||Young’s modulus of th beam|
|:||Area moment of inertia of th beam|
|:||Stiffness of an intermediate spring|
|:||Normalized spring constant|
|:||Stiffness of the primary system|
|:||Length of beam|
|:||Mass of the primary system|
|:||Normalized spring location,|
|:||Receptance of the first cantilever beam|
|:||Ratios of cantilever beam’s th natural frequency to its first natural frequency|
|:||Receptance of the second cantilever beam plus spring|
|:||First mode coefficient of a single cantilever beam|
|PVA’s natural frequency|
|:||th natural frequency of th beam|
|:||Fundamental frequency of the periodic excitation|
|:||Ratios of the th beam’s first natural frequency to the fundamental frequency of the excitation|
|:||Density of th beam|
|:||Mass ratio of the two beams|
|:||th mode of a cantilever beam.|
Conflict of Interests
The authors declare that there is no conflict of interests regarding the publication of this paper.
The authors are grateful to the National Science Council for its support of this research under the Grant no. NSC 98-2811-E-011-001.
- J. Ormondroyd and J. P. den Hartog, “Theory of the dynamic vibration absorber,” Transactions of the ASME, vol. 50, pp. 9–22, 1928.
- J. P. den Hartog, Mechanical Vibration, McGraw-Hill, New York, NY, USA, 1934.
- J. E. Brock, “A note on the damped vibration absorber,” Journal of Applied Mechanics, vol. 68, p. A-284, 1946.
- M. B. Ozer and T. J. Royston, “Extending den Hartog's vibration absorber technique to multi-degree-of-freedom systems,” ASME Journal of Vibration and Acoustics, vol. 127, no. 4, pp. 341–350, 2005.
- M. B. Ozer and T. J. Royston, “Application of Sherman-Morrison matrix inversion formula to damped vibration absorbers attached to multi-degree of freedom systems,” Journal of Sound and Vibration, vol. 283, no. 3–5, pp. 1235–1249, 2005.
- M. Z. Ren, “A variant design of the dynamic vibration absorber,” Journal of Sound and Vibration, vol. 245, no. 4, pp. 762–770, 2001.
- W. O. Wong and Y. L. Cheung, “Optimal design of a damped dynamic vibration absorber for vibration control of structure excited by ground motion,” Engineering Structures, vol. 30, no. 1, pp. 282–286, 2008.
- J. Q. Sun, M. R. Jolly, and M. A. Norris, “Passive, adaptive and active tuned vibration absorbers—a survey,” ASME Journal of Mechanical Design, vol. 117, pp. 234–242, 1995.
- D. Chen and H. Xu, “Dynamic analysis of delayed damper system in engineering structures,” Journal of Sound and Vibration, vol. 250, no. 4, pp. 609–616, 2002.
- R. A. Burdisso and J. D. Heilmann, “A new dual-reaction mass dynamic vibration absorber actuator for active vibration control,” Journal of Sound and Vibration, vol. 214, no. 5, pp. 817–831, 1998.
- H. L. Sun, P. Q. Zhang, H. B. Chen, K. Zhang, and X. L. Gong, “Application of dynamic vibration absorbers in structural vibration control under multi-frequency harmonic excitations,” Applied Acoustics, vol. 69, no. 12, pp. 1361–1367, 2008.
- S. G. Hill and S. D. Snyder, “Design of an adaptive vibration absorber to reduce electrical transformer structural vibration,” ASME Journal of Vibration and Acoustics, vol. 124, no. 4, pp. 606–611, 2002.
- P. W. Wang and C. C. Cheng, “Design of vibration absorbers for structures subject to multiple-tonal excitations,” ASME Journal of Vibration and Acoustics, vol. 128, no. 1, pp. 106–114, 2006.
- R. E. D. Bishop and D. C. Johnson, The Mechanics of Vibration, Cambridge University Press, Cambridge, UK, 1960.
- K. A. Lin and S. C. Huang, “Modeling and vibration analysis of spinning hard disk and head assembly,” Journal of System Design and Dynamics, vol. 2, pp. 528–539, 2008.
Copyright © 2014 Shyh-Chin Huang and Kao-An Lin. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.