# Influence of Sandwich-Type Constrained Layer Damper Design Parameters on Damping Strength

Authors: Inaki Merideno; Javier Nieto; Nere Gil-Negrete; José Germán Giménez Ortiz; Aitor Landaberea; Jon Iartza
Journal: Shock and Vibration
 (2016)

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## Abstract

This paper presents a theoretical study of the parameters that influence sandwich-type constrained layer damper design. Although there are different ways to reduce the noise generated by a railway wheel, most devices are based on the mechanism of increasing wheel damping. Sandwich-type constrained layer dampers can be designed so their resonance frequencies coincide with the wheel’s resonant vibration frequencies, and thus the damping effect can be concentrated within the frequency ranges of interest. However, the influence of design parameters has not yet been studied. Based on a number of numerical simulations, this paper provides recommendations for the design stages of sandwich-type constrained layer dampers.


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## Body

## 1. Introduction

The environmental requirements for railway operation are becoming more and more demanding. In particular, railway noise has to be taken into account as freight traffic increases and urban trams, metro lines, and high speed lines spread all over the world. Noise reduction at the source is more attractive than the use of noise barriers, but this requires a thorough understanding of the noise source mechanisms as well as methodologies to evaluate the effectiveness of proposed solutions [1].Different sources may contribute to the total noise level, but wheel/rail noise is the most important noise source at middle speed ranges (50–250 km/h), where the vast majority of trains run [2]. At low frequencies the noise is mainly radiated by the sleeper and the rail, whereas at high frequencies (around 1500 Hz), the wheel is the dominant noise source [3]. Thus, the wheel is one of the most critical components of railway noise emission, and the study of its vibroacoustics has attracted the attention of many researchers due to its significant complexity [4].The main wheel/rail noise sources are rolling noise, impact noise, or squeal noise, this last one being the most difficult to mitigate. Wheel squeal is considered to be caused by an instability in wheel vibrations [4–6], so sufficient positive damping, which is only a small fraction of critical damping, can actually stabilize these wheel vibrations and reduce squeal.Different ways of increasing wheel damping have been reported in the literature, the most important ones being resilient wheels [7–10], ring dampers [7, 11–14], CAF dampers [15, 16], and constrained layer dampers (CLD) [17–20], either as a treatment applied on the wheel web [1, 7, 9, 21–25] or as tuned absorbers [1, 7, 26–28].This paper is focused on sandwich-type CLD tuned absorbers, which are frequently employed in metro wheel cases. Sandwich-type CLDs are devices that combine metallic sheets with viscoelastic layers, and they increase the damping of the railway wheel modes. The damping is due to the energy dissipation that occurs through the deformation of the viscoelastic material.A sandwich-type CLD can be designed to reduce both squeal and rolling noise, depending on the treatment configuration. One advantage of the sandwich-type CLD is that it ages well, and it can be removed from a worn wheel and installed on a new one [7]. It can be designed so its resonance frequencies will coincide with wheel resonant vibration frequencies [7, 29], and thus its damping effect can be concentrated within the frequency ranges of interest. The possibilities are endless, and the same problem can often be solved by a number of different solutions.Merideno et al. [30, 31] highlighted the need to develop a specific model that calculates the damping added by sandwich-type CLD to the railway wheel, in order to avoid experimental measurements. They presented a procedure that could be employed in design stages where the damping device is not available. The calculated damping can then be used to simulate the noise generated by a railway wheel [32, 33].This paper makes use of the damping prediction model developed by Merideno et al. [30] to analyse several design parameters of the sandwich-type CLD solution and study their influence on the resulting total damping of the wheel-damper system. The effective noise reduction is not investigated in this paper, since the influence of wheel/rail contact on the radiated noise is out of the scope of this paper. The objective is that the results presented in this paper will be able to serve as a guideline for sandwich-type CLD designs, even for structures other than the railway wheel.


## 2. Objective Function and Design Parameters

According to Merideno et al. [30], the final modal damping ratio (the damping ratio of the wheel with the damping solution) can be calculated as(1)ξequivr=ξr+∑t=1Dϕrt2∑s=1MΥs2mrwr2,(see [30]) where D represents the total number of sandwich-type devices attached to the railway wheel and ∑s=1M{Υs} refers to the sum of the base reaction forces (the imaginary part) appearing in each damper. The theoretical development of this equation can be found in the literature, and so it is not repeated here.In this equation, the termsξr, ϕrt, and mr are specific to the undamped wheel, so if we only aim to study the damping strength of a given sandwich-type CLD in the frequency domain and independently of the railway wheel, these parameters should not be considered. The term ∑s=1M{Υs} refers to all the reaction forces in the damper base nodes, making it directly related to the damping strength that a particular sandwich-type CLD design would have, independent of the railway wheel. The term wr refers to the wheel’s natural frequencies, but when a given sandwich-type CLD is attached to a given railway wheel, wr corresponds to the vibration frequency at which the damper is excited. Therefore, instead of understanding this frequency term as the natural frequency of the railway wheel, it must be understood as the vibration frequency at which the damper is excited. However, when comparing different sandwich-type CLD designs that concentrate their damping strength on different frequency ranges, the reaction forces are normally higher for higher vibrational frequencies. Because of this, we define the concept ofdamping potential as normalizing in terms of frequency the damping strength of a damping solution:(2)∇ξω=∑s=1MΥsωω2,where M is related to the total amount of damper base nodes. This damping potential frequency-dependent value is the objective function in our study, since it defines the potentiality of a sandwich-type CLD to add damping to a given structure in the frequency domain. The frequency at which the sandwich-type CLD has a high damping potential value must then coincide with the frequency at which the designer wants to add damping in the structure to ensure the effectiveness of the sandwich-type CLD.Now that the objective function has been defined, the design parameters under study will be described. The nomenclature that will be used hereafter for the geometric design parameters of a sandwich-type CLD is illustrated in Figure1, which shows a scheme of a four-layer sandwich-type CLD, where mi refers to the thickness of the ith metallic sheet (where 0 corresponds to the base sheet), vi refers to the thickness of the ith viscoelastic layer, and α refers to the angle of the viscoelastic layers. This is a typical design employed in railway wheels for squeal noise. As it is usually an arc-type design, angle α is preferable to referring to the length of the viscoelastic layer.Figure 1
Designing parameters of a sandwich-type CLD.The material of the metallic sheets remains the same (steel in this case) and its influence was not studied because commercial sandwich-type CLDs are made of steel. In addition to this, the thicknesses of the metallic sheets always have values that are whole or half numbers since these are the common commercial thicknesses. The maximum thickness of both the metallic sheets and viscoelastic layers is limited due to the space restrictions of railway wheels. In other applications, bigger sandwich-type CLDs could be appropriate.In this paper, the influence that viscoelastic properties (Section3) and the mi, vi, and α parameters (Section 4) of sandwich-type CLDs have on the damping potential will be studied, and different sandwich-type CLD design simulations will be carried out to examine the effect of varying different design parameters and the assembly (Section 5). Finally, general recommendations for the design stages of sandwich-type CLDs will be presented (Section 6).


## 3. Influence of Viscoelastic Properties

The two predominant properties of a viscoelastic material are its stiffness and loss factor (internal damping). Generally, a viscoelastic material with a high damping factor tends to be very stiff, whereas a material with a low damping factor is usually related to low stiffness. Thus, a trade-off between these two properties has to be found when designing a sandwich-type CLD.If the viscoelastic material of a sandwich-type CLD is too stiff, little shear deformation occurs, even though the damping factor is very high, which results in low energy dissipation. The structure and the constraining sheet become rigidly coupled and the material does not deform. On the other hand, if the viscoelastic material is too flexible, both the structure and the constraining sheet nearly become uncoupled. The material undergoes large deformations, but it adds little damping since it offers no resistance, resulting in minimal energy dissipation.When applying a cyclic load to a viscoelastic material, a phase difference between stress and strain known as hysteresis occurs, leading to energy dissipation that results in damping [34]. This hysteresis energy loss can be defined by the loss angle, which relates the in-phase (storage) shear modulus and the out-of-phase (loss) shear modulus [35, 36].In order to determine realistic variabilities in the loss angle and stiffness of viscoelastic materials and study their influence on the damping strength of the sandwich-type CLD under study, two materials that present extreme stiffness and loss angle properties were selected. The first material,Mat1, presents low stiffness and thus a low loss factor; the second material, Mat2, presents high stiffness and therefore a high loss factor.By calculating the geometric mean of these materials’ properties, a reference material was defined over the frequency range under study (100–5000 Hz). Table1 presents the properties of all three materials.Table 1
Material properties of Mat1, Mat2, and reference material.
Average properties
Mat1
Mat2
Reference material
Static shear modulus
5.84
⋅
1
0
4 Pa
3.37
⋅
1
0
5 Pa
1.4
⋅
1
0
5 Pa
Dynamic shear modulus
1
⋅
1
0
5 Pa
2.1
⋅
1
0
6 Pa
4.6
⋅
1
0
5 Pa
Loss angle
1
5
°
3
3
°
2
2
°


### 3.1. Loss Angle of Viscoelastic Material

In a sandwich-type CLD damping is due to the energy dissipation that occurs through the shear deformation of the viscoelastic material. Since the loss angle is a measure of the material’s internal damping behaviour, polymers are normally chosen for these types of dampers because of their high loss angle relative to other viscoelastic materials. However, it is not clear whether having the highest possible loss angle value is beneficial or not.In this section, the influence of the viscoelastic loss angle on the damping potential is analysed. First, a reference four-layer sandwich-type CLD design was modelled with the reference viscoelastic material (see Table2), whose dynamic properties were kept constant over the whole frequency range under study. The sandwich-type CLD modelling methodology described by Merideno et al. [29, 30] was used.Table 2
Geometric parameters of the reference four-layer damper design.
Metallic sheets
Viscoelastic layers
Viscoelastic properties
m
0 = 3 mm
v
1 = 3.5 mm
Density =1000 kg/m3
m
1 = 3.5 mm
v
2 = 3.5 mm
Static shear modulus =1.4⋅105 Pa
m
2 = 3 mm
v
3 = 3.5 mm
Loss angle =22°
m
3 = 2.5 mm
v
4 = 3.5 mm
Poisson modulus = 0.499
m
4 = 2 mm
α
=
10
.
5
°
Dynamic shear modulus =4.6⋅105 PaThen, two variations of the sandwich-type CLD design were built by setting the loss angle of the viscoelastic material to the extreme cases considered in Table1, 15° (low damping model) and 33° (high damping model), leaving the rest of the parameters unchanged (see Table 3). In each damper model, a unity displacement was applied laterally to the damper base and reaction forces were calculated at the base nodes. These reaction forces were divided by the square of their corresponding frequency and the damping potential was calculated in the 100–5000 Hz frequency range.Table 3
Viscoelastic material properties of the reference, low damping, and high damping models.
Average properties
Reference
Low damping
High damping
Static shear modulus
1.4
⋅
1
0
5 Pa
1.4
⋅
1
0
5 Pa
1.4
⋅
1
0
5 Pa
Dynamic shear modulus
4.6
⋅
1
0
5 Pa
4.6
⋅
1
0
5 Pa
4.6
⋅
1
0
5 Pa
Loss angle
2
2
°
1
5
°
3
3
°Figure2 presents the calculated damping potential in the frequency range of interest for the reference,low damping andhigh damping sandwich-type CLD models built. As shown, the natural frequencies of these dampers were insignificantly affected by the loss angle values used in each design. The peak amplitudes of thelow damping model were twice the values of thehigh damping model, whereas the valley amplitudes of thehigh damping model were twice the values of thelow damping model. As a consequence, the peaks and valleys of thelow damping model were more pronounced.Figure 2
Damping potential for viscoelastic materials with different loss angles.Thus, a sandwich-type CLD that has viscoelastic material with a low loss angle must be more accurately designed in order to concentrate its strength to a given frequency than a damper made of a viscoelastic material that has a high loss angle. Special attention should be paid to the variation of the natural frequencies of a railway wheel damped with a sandwich-type CLD solution with pronounced peaks, since it might be detuned. If the wheel’s natural frequency coincided with a valley of the damping potential curve (an example of wheel’s natural frequencies can be found in [33]), the sandwich-type CLD would have a null effect and the wheel would behave like an undamped wheel. We call this phenomenonthe valley effect.In sum, a trade-off has to be found when choosing a viscoelastic material for a sandwich-type CLD design: using a viscoelastic material with a low loss angle will present higher damping strength at a particular frequency, but a viscoelastic material with a high loss angle will be effective even when the wheel wears down and its natural frequencies vary.


### 3.2. Stiffness of Viscoelastic Material

In an analogous manner, the influence that stiffness of the viscoelastic material has on the damping potential, as measured by the static and dynamic shear modulus, is studied using the same reference four-layer sandwich-type CLD design and viscoelastic material (Table2) and building two new models that represent the extreme stiffness conditions identified in Table 1.The viscoelastic materials used are in Table4 and the damping potential curves calculated in the 100–5000 Hz frequency range are shown in Figure 3.Table 4
Viscoelastic material properties of the reference and soft and stiff material models.
Average properties
Reference
Soft material
Stiff material
Static shear modulus
1.4
⋅
1
0
5 Pa
5.84
⋅
1
0
4 Pa
3.37
⋅
1
0
5 Pa
Dynamic shear modulus
4.6
⋅
1
0
5 Pa
1
⋅
1
0
5 Pa
2.1
⋅
1
0
6 Pa
Loss angle
2
2
°
2
2
°
2
2
°Figure 3
Damping potential for viscoelastic materials with different stiffness values.The sandwich-type CLD design with the soft material had its peaks (at least the first three peaks) at lower frequencies than the other designs. Therefore, estimating the optimal stiffness of the viscoelastic material is tied to the optimal location of the damper’s natural frequencies, mainly to the first natural frequency since it determines the initial frequency at which a sandwich-type CLD design starts to add damping to a given railway wheel.In terms of the damping potential peak amplitudes, at the dampers’ first natural frequencies, even though peak differences between the three damping potential curves were not significant, the peak amplitude when the viscoelastic material was soft was higher than for the other models. On the contrary, at the dampers’ second natural frequencies, the peak amplitude when the viscoelastic material was stiff was slightly higher than for the other models. At frequencies above 1500 Hz, it is not possible to reach any conclusions.


## 3.1. Loss Angle of Viscoelastic Material

In a sandwich-type CLD damping is due to the energy dissipation that occurs through the shear deformation of the viscoelastic material. Since the loss angle is a measure of the material’s internal damping behaviour, polymers are normally chosen for these types of dampers because of their high loss angle relative to other viscoelastic materials. However, it is not clear whether having the highest possible loss angle value is beneficial or not.In this section, the influence of the viscoelastic loss angle on the damping potential is analysed. First, a reference four-layer sandwich-type CLD design was modelled with the reference viscoelastic material (see Table2), whose dynamic properties were kept constant over the whole frequency range under study. The sandwich-type CLD modelling methodology described by Merideno et al. [29, 30] was used.Table 2
Geometric parameters of the reference four-layer damper design.
Metallic sheets
Viscoelastic layers
Viscoelastic properties
m
0 = 3 mm
v
1 = 3.5 mm
Density =1000 kg/m3
m
1 = 3.5 mm
v
2 = 3.5 mm
Static shear modulus =1.4⋅105 Pa
m
2 = 3 mm
v
3 = 3.5 mm
Loss angle =22°
m
3 = 2.5 mm
v
4 = 3.5 mm
Poisson modulus = 0.499
m
4 = 2 mm
α
=
10
.
5
°
Dynamic shear modulus =4.6⋅105 PaThen, two variations of the sandwich-type CLD design were built by setting the loss angle of the viscoelastic material to the extreme cases considered in Table1, 15° (low damping model) and 33° (high damping model), leaving the rest of the parameters unchanged (see Table 3). In each damper model, a unity displacement was applied laterally to the damper base and reaction forces were calculated at the base nodes. These reaction forces were divided by the square of their corresponding frequency and the damping potential was calculated in the 100–5000 Hz frequency range.Table 3
Viscoelastic material properties of the reference, low damping, and high damping models.
Average properties
Reference
Low damping
High damping
Static shear modulus
1.4
⋅
1
0
5 Pa
1.4
⋅
1
0
5 Pa
1.4
⋅
1
0
5 Pa
Dynamic shear modulus
4.6
⋅
1
0
5 Pa
4.6
⋅
1
0
5 Pa
4.6
⋅
1
0
5 Pa
Loss angle
2
2
°
1
5
°
3
3
°Figure2 presents the calculated damping potential in the frequency range of interest for the reference,low damping andhigh damping sandwich-type CLD models built. As shown, the natural frequencies of these dampers were insignificantly affected by the loss angle values used in each design. The peak amplitudes of thelow damping model were twice the values of thehigh damping model, whereas the valley amplitudes of thehigh damping model were twice the values of thelow damping model. As a consequence, the peaks and valleys of thelow damping model were more pronounced.Figure 2
Damping potential for viscoelastic materials with different loss angles.Thus, a sandwich-type CLD that has viscoelastic material with a low loss angle must be more accurately designed in order to concentrate its strength to a given frequency than a damper made of a viscoelastic material that has a high loss angle. Special attention should be paid to the variation of the natural frequencies of a railway wheel damped with a sandwich-type CLD solution with pronounced peaks, since it might be detuned. If the wheel’s natural frequency coincided with a valley of the damping potential curve (an example of wheel’s natural frequencies can be found in [33]), the sandwich-type CLD would have a null effect and the wheel would behave like an undamped wheel. We call this phenomenonthe valley effect.In sum, a trade-off has to be found when choosing a viscoelastic material for a sandwich-type CLD design: using a viscoelastic material with a low loss angle will present higher damping strength at a particular frequency, but a viscoelastic material with a high loss angle will be effective even when the wheel wears down and its natural frequencies vary.


## 3.2. Stiffness of Viscoelastic Material

In an analogous manner, the influence that stiffness of the viscoelastic material has on the damping potential, as measured by the static and dynamic shear modulus, is studied using the same reference four-layer sandwich-type CLD design and viscoelastic material (Table2) and building two new models that represent the extreme stiffness conditions identified in Table 1.The viscoelastic materials used are in Table4 and the damping potential curves calculated in the 100–5000 Hz frequency range are shown in Figure 3.Table 4
Viscoelastic material properties of the reference and soft and stiff material models.
Average properties
Reference
Soft material
Stiff material
Static shear modulus
1.4
⋅
1
0
5 Pa
5.84
⋅
1
0
4 Pa
3.37
⋅
1
0
5 Pa
Dynamic shear modulus
4.6
⋅
1
0
5 Pa
1
⋅
1
0
5 Pa
2.1
⋅
1
0
6 Pa
Loss angle
2
2
°
2
2
°
2
2
°Figure 3
Damping potential for viscoelastic materials with different stiffness values.The sandwich-type CLD design with the soft material had its peaks (at least the first three peaks) at lower frequencies than the other designs. Therefore, estimating the optimal stiffness of the viscoelastic material is tied to the optimal location of the damper’s natural frequencies, mainly to the first natural frequency since it determines the initial frequency at which a sandwich-type CLD design starts to add damping to a given railway wheel.In terms of the damping potential peak amplitudes, at the dampers’ first natural frequencies, even though peak differences between the three damping potential curves were not significant, the peak amplitude when the viscoelastic material was soft was higher than for the other models. On the contrary, at the dampers’ second natural frequencies, the peak amplitude when the viscoelastic material was stiff was slightly higher than for the other models. At frequencies above 1500 Hz, it is not possible to reach any conclusions.


## 4. Influence of Geometric Parameters

A sandwich-type CLD can be designed in order to concentrate its damping strength in a given frequency range by properly defining its geometric parameters: thickness and angle of each viscoelastic layer and thickness of each metallic sheet.In what follows, the effect of varying the thickness and angle of viscoelastic layers is presented. Conclusions about the influence of the thickness of metallic sheets are also presented.


### 4.1. Thickness of the Viscoelastic Layer

This section studies the effect that the thickness of the viscoelastic layers has on the damping potential through studying a monolayer damper.First, a monolayer sandwich-type CLD model denotedM01 was built with the reference viscoelastic material and with the geometry detailed in Table 5. The thickness of the viscoelastic layer was varied from 1.5 mm to 6.5 mm with a step of 0.5 mm, and in each simulation the damping potential was calculated. From each damping potential curve, the peak amplitudes of the first mode were extracted and plotted together (Figure 4) in order to study the influence that varying the thickness of the viscoelastic layers had on the damping potential.Table 5
Geometric parameters of the reference monolayer damper design.
Metallic sheets
Viscoelastic layer
Viscoelastic properties
m
0 = 3 mm m1 = 3.5 mm
v
1 = 1.5–6.5 mm α=10.5°
Density =1000 kg/m3
Static shear modulus =1.4⋅105 Pa
Loss angle =22°
Poisson modulus = 0.499
Dynamic shear modulus =4.6⋅105 PaFigure 4
Damping potential of a monolayer damper for different thickness of the viscoelastic layer.Figure4 shows that the highest damping potential peak amplitudes were calculated for the smallest and the biggest thickness values, that is, when the thickness was set to 1.5 mm and 6.5 mm. Intermediate thickness values led to lower damping potential peak amplitudes.Then, the other two monolayer sandwich-type CLDs,M02 andM03, were modelled in the same way asM01; only in these two models was the thickness of the upper metallic sheet set to 5 mm and 7 mm, respectively. Table 6 shows the geometric parameters for theM01,M02, andM03 sandwich-type CLD designs. Once again, the thickness of the viscoelastic layer in each design was varied from 1.5 mm to 6.5 mm with a step of 0.5 mm.Table 6
Geometric parameters of the three monolayer damper designs.
M01
M02
M03
Metallic sheets
Viscoelastic layers
Metallic sheets
Viscoelastic layers
Metallic sheets
Viscoelastic layers
m
0 = 3 mm
v
1 = 1.5–6.5 mm
m
0 = 3 mm
v
1 = 1.5–6.5 mm
m
0 = 3 mm
v
1 = 1.5–6.5 mm
m
1 = 3.5 mm
α
=
10
.
5
°
m
1 = 5 mm
α
=
10
.
5
°
m
1 = 7 mm
α
=
10
.
5
°Figure5(a) presents the first peak amplitude of the damping potential curve for each design versus the thickness of the viscoelastic layer. The same trend emerged when varying the thickness of the viscoelastic layers in the three sandwich-type CLD designs: the highest damping potential peak amplitudes were calculated for the lowest and the highest thickness values, and for the intermediate thickness value the minimal damping potential peak amplitude was obtained.Figure 5
Analysis of damping potential for different thicknesses of the viscoelastic layer.
(a)
Peak amplitude of damping potential for first mode
(b)
Natural frequency of first mode
(c)
Imaginary part of total reaction forcesFigure5(b) presents the influence of the thickness of the viscoelastic layer on the damper’s first natural frequency. As shown, the first natural frequency decreased continuously when the viscoelastic layer thickness increased.Figure5(c) presents the influence of the thickness of the viscoelastic layer on the sum of all of the reaction forces (the imaginary part) on the base of sandwich-type CLDs. As shown, the curves followed a concave shape: for the highest and the lowest viscoelastic layer thickness values the reaction forces increased, and this behaviour was sharper for the lowest viscoelastic layer thickness.An increase in the viscoelastic layer thickness results in an enlargement of the energy dissipation, since the amount of viscoelastic material is increased. This is the reason for the positive slope of the curve in Figure5(a) when higher viscoelastic thickness values are used. When the viscoelastic layer thickness is small, even though the energy dissipation through the viscoelastic material is low, the movement of the top metallic sheet is fully transmitted to the base sheet, which leads to a significant increase in the resulting reaction forces. This fact explains the negative slope of the curve in Figure 5(a) for the lowest thickness values. Nevertheless, the highest damping potential peak amplitudes were attained for the highest thickness values of the viscoelastic layer.In analysing the peak amplitude of damping potential for a specific thickness of the viscoelastic layer of each damper design in Figure5(a), the highest value was obtained for theM03 design, which had the highest upper metallic sheet thickness. The highest damping potential peak amplitude was attained with theM03 sandwich-type CLD design, which consists of a 6.5 mm thick viscoelastic layer and a 7 mm thick upper metallic sheet, that is, the damper design that had the highest total thickness.In conclusion, the increase in thickness in the viscoelastic layer and in the upper metallic sheet results in higher energy dissipation through the viscoelastic material, and therefore there is an increase in the damping potential. Since geometric and space limitations are common when designing sandwich-type CLD solutions for a given railway wheel, especially tram wheels, whether the upper metallic sheet thickness or the viscoelastic layer thickness is increased will depend on each design situation.Lastly, an increase in the viscoelastic layer thickness leads to a decrease in the first natural frequency, whereas an increase in the upper metallic sheet thickness leads to an increase. The relative increase of each part will be determined by the optimal location of the first natural frequency.


### 4.2. Angle of the Viscoelastic Layer

In this section, the influence that varying the viscoelastic layer’sα-value has on the damping potential is analysed through a monolayer damper approach.A monolayer sandwich-type CLD denotedL01 was built with the reference viscoelastic material and with the geometry detailed in Table 7. In this case, the thickness of the viscoelastic layer was fixed to 1.5 mm and its angle was varied from 2° to 14.5°, which in the sandwich-type CLD design under study corresponded to the noncantilevered state of the upper metallic sheet. For angles smaller than this, the upper metallic sheet was partially cantilevered. For an α-value of 10.5°, this damper design coincided with the previousM01 design.Table 7
Geometric parameters of the reference monolayer damper design.
Metallic sheets
Viscoelastic layers
Viscoelastic properties
m
0 = 3 mm m1 = 3.5 mm
v
1 = 1.5 mm α=2°–14.5°
Density =1000 kg/m3
Static shear modulus =1.4⋅105 Pa
Loss angle =22°
Poisson modulus = 0.499
Dynamic shear modulus =4.6⋅105 PaAs in the previous section, theα-value was varied, and for each simulation, the peak amplitude of damping potential (Figure 6(a)) and the first natural frequency (Figure 6(b)) were plotted. In this sandwich-type CLD design, an increase in the α-value corresponded to a decrease in the damping potential peak amplitude and an increase in the first natural frequency.Figure 6
Influence of the angle of the viscoelastic layer on a monolayer damper.
(a)
Peak amplitude of damping potential
(b)
First natural frequencyThen, another two monolayer sandwich-type CLDs,L02 andL03, were modelled identically toL01 except for the thickness of the viscoelastic layer, which was set to 4 mm and 6.5 mm, respectively. Table 8 gathers the geometric parameters of the sandwich-type CLD designs forL01,L02, andL03. Once again, the α-value was varied from 2° to 14.5°.Table 8
Geometric parameters of the three mono-layer damper designs.
L01
L02
L03
Metallic sheets
Viscoelastic layers
Metallic sheets
Viscoelastic layers
Metallic sheets
Viscoelastic layers
m
0 = 3 mm
v
1 = 1.5 mm
m
0 = 3 mm
v
1 = 4 mm
m
0 = 3 mm
v
1 = 6.5 mm
m
1 = 3.5 mm
α
=
2
°
–
14
.
5
°
m
1 = 3.5 mm
α
=
2
°
–
14
.
5
°
m
1 = 3.5 mm
α
=
2
°
–
14
.
5
°Figure7 shows that the damping potential peak amplitude decreased when the α-value increased, whereas the first natural frequency increased in each sandwich-type CLD design. In addition to this, the increase in the first natural frequency was more significant for theL01 design, that is, for the sandwich-type CLD with the thinnest viscoelastic layer. Furthermore, for α-values equal to 2°, the three sandwich-type CLD designs had approximately the same first natural frequency, which corresponded to the natural frequency of the metallic structure. As α-values increased, the increase in the first natural frequency for theL03 damper design was lower than for the other designs. For the maximal α-value, the first natural frequency of theL01 design is twice as high as theL03 design. Therefore, the angle of the viscoelastic layer, the α value, can be used to adjust the damping strength to the frequency range of interest.Figure 7
Influence of the angle of the viscoelastic layer on theL01,L02, andL03 monolayer damper designs.
(a)
Peak amplitude of damping potential
(b)
First natural frequencyHowever, theα-values adopted in commercial sandwich-type CLDs are usually high, which is not in line with what would be expected from the results in Figure 7(a). In order to clarify this disagreement, two variations of theL03 design were modelled: one with a viscoelastic layer of 3° angle and the other with 11° angle. Figure 8 shows that the peak of damping potential was higher for the 3° angle than for the 11°-angle, meaning that a higher damping strength would be attained with lower α-values. However, Figure 8 shows that the peak of damping potential was more pronounced for the 3° angle than for the 11° angle. Therefore, a sandwich-type CLD with a viscoelastic layer with a low α-value has to concentrate its damping strength more precisely to a given wheel eigenfrequency. For this reason, a flatter damping potential curve is preferred so as to overcome a railway wheel’s frequency variations due to the wheel wearing down as well as the valley effect.Figure 8
Damping potential for two particular sandwich-type CLD designs.


## 4.1. Thickness of the Viscoelastic Layer

This section studies the effect that the thickness of the viscoelastic layers has on the damping potential through studying a monolayer damper.First, a monolayer sandwich-type CLD model denotedM01 was built with the reference viscoelastic material and with the geometry detailed in Table 5. The thickness of the viscoelastic layer was varied from 1.5 mm to 6.5 mm with a step of 0.5 mm, and in each simulation the damping potential was calculated. From each damping potential curve, the peak amplitudes of the first mode were extracted and plotted together (Figure 4) in order to study the influence that varying the thickness of the viscoelastic layers had on the damping potential.Table 5
Geometric parameters of the reference monolayer damper design.
Metallic sheets
Viscoelastic layer
Viscoelastic properties
m
0 = 3 mm m1 = 3.5 mm
v
1 = 1.5–6.5 mm α=10.5°
Density =1000 kg/m3
Static shear modulus =1.4⋅105 Pa
Loss angle =22°
Poisson modulus = 0.499
Dynamic shear modulus =4.6⋅105 PaFigure 4
Damping potential of a monolayer damper for different thickness of the viscoelastic layer.Figure4 shows that the highest damping potential peak amplitudes were calculated for the smallest and the biggest thickness values, that is, when the thickness was set to 1.5 mm and 6.5 mm. Intermediate thickness values led to lower damping potential peak amplitudes.Then, the other two monolayer sandwich-type CLDs,M02 andM03, were modelled in the same way asM01; only in these two models was the thickness of the upper metallic sheet set to 5 mm and 7 mm, respectively. Table 6 shows the geometric parameters for theM01,M02, andM03 sandwich-type CLD designs. Once again, the thickness of the viscoelastic layer in each design was varied from 1.5 mm to 6.5 mm with a step of 0.5 mm.Table 6
Geometric parameters of the three monolayer damper designs.
M01
M02
M03
Metallic sheets
Viscoelastic layers
Metallic sheets
Viscoelastic layers
Metallic sheets
Viscoelastic layers
m
0 = 3 mm
v
1 = 1.5–6.5 mm
m
0 = 3 mm
v
1 = 1.5–6.5 mm
m
0 = 3 mm
v
1 = 1.5–6.5 mm
m
1 = 3.5 mm
α
=
10
.
5
°
m
1 = 5 mm
α
=
10
.
5
°
m
1 = 7 mm
α
=
10
.
5
°Figure5(a) presents the first peak amplitude of the damping potential curve for each design versus the thickness of the viscoelastic layer. The same trend emerged when varying the thickness of the viscoelastic layers in the three sandwich-type CLD designs: the highest damping potential peak amplitudes were calculated for the lowest and the highest thickness values, and for the intermediate thickness value the minimal damping potential peak amplitude was obtained.Figure 5
Analysis of damping potential for different thicknesses of the viscoelastic layer.
(a)
Peak amplitude of damping potential for first mode
(b)
Natural frequency of first mode
(c)
Imaginary part of total reaction forcesFigure5(b) presents the influence of the thickness of the viscoelastic layer on the damper’s first natural frequency. As shown, the first natural frequency decreased continuously when the viscoelastic layer thickness increased.Figure5(c) presents the influence of the thickness of the viscoelastic layer on the sum of all of the reaction forces (the imaginary part) on the base of sandwich-type CLDs. As shown, the curves followed a concave shape: for the highest and the lowest viscoelastic layer thickness values the reaction forces increased, and this behaviour was sharper for the lowest viscoelastic layer thickness.An increase in the viscoelastic layer thickness results in an enlargement of the energy dissipation, since the amount of viscoelastic material is increased. This is the reason for the positive slope of the curve in Figure5(a) when higher viscoelastic thickness values are used. When the viscoelastic layer thickness is small, even though the energy dissipation through the viscoelastic material is low, the movement of the top metallic sheet is fully transmitted to the base sheet, which leads to a significant increase in the resulting reaction forces. This fact explains the negative slope of the curve in Figure 5(a) for the lowest thickness values. Nevertheless, the highest damping potential peak amplitudes were attained for the highest thickness values of the viscoelastic layer.In analysing the peak amplitude of damping potential for a specific thickness of the viscoelastic layer of each damper design in Figure5(a), the highest value was obtained for theM03 design, which had the highest upper metallic sheet thickness. The highest damping potential peak amplitude was attained with theM03 sandwich-type CLD design, which consists of a 6.5 mm thick viscoelastic layer and a 7 mm thick upper metallic sheet, that is, the damper design that had the highest total thickness.In conclusion, the increase in thickness in the viscoelastic layer and in the upper metallic sheet results in higher energy dissipation through the viscoelastic material, and therefore there is an increase in the damping potential. Since geometric and space limitations are common when designing sandwich-type CLD solutions for a given railway wheel, especially tram wheels, whether the upper metallic sheet thickness or the viscoelastic layer thickness is increased will depend on each design situation.Lastly, an increase in the viscoelastic layer thickness leads to a decrease in the first natural frequency, whereas an increase in the upper metallic sheet thickness leads to an increase. The relative increase of each part will be determined by the optimal location of the first natural frequency.


## 4.2. Angle of the Viscoelastic Layer

In this section, the influence that varying the viscoelastic layer’sα-value has on the damping potential is analysed through a monolayer damper approach.A monolayer sandwich-type CLD denotedL01 was built with the reference viscoelastic material and with the geometry detailed in Table 7. In this case, the thickness of the viscoelastic layer was fixed to 1.5 mm and its angle was varied from 2° to 14.5°, which in the sandwich-type CLD design under study corresponded to the noncantilevered state of the upper metallic sheet. For angles smaller than this, the upper metallic sheet was partially cantilevered. For an α-value of 10.5°, this damper design coincided with the previousM01 design.Table 7
Geometric parameters of the reference monolayer damper design.
Metallic sheets
Viscoelastic layers
Viscoelastic properties
m
0 = 3 mm m1 = 3.5 mm
v
1 = 1.5 mm α=2°–14.5°
Density =1000 kg/m3
Static shear modulus =1.4⋅105 Pa
Loss angle =22°
Poisson modulus = 0.499
Dynamic shear modulus =4.6⋅105 PaAs in the previous section, theα-value was varied, and for each simulation, the peak amplitude of damping potential (Figure 6(a)) and the first natural frequency (Figure 6(b)) were plotted. In this sandwich-type CLD design, an increase in the α-value corresponded to a decrease in the damping potential peak amplitude and an increase in the first natural frequency.Figure 6
Influence of the angle of the viscoelastic layer on a monolayer damper.
(a)
Peak amplitude of damping potential
(b)
First natural frequencyThen, another two monolayer sandwich-type CLDs,L02 andL03, were modelled identically toL01 except for the thickness of the viscoelastic layer, which was set to 4 mm and 6.5 mm, respectively. Table 8 gathers the geometric parameters of the sandwich-type CLD designs forL01,L02, andL03. Once again, the α-value was varied from 2° to 14.5°.Table 8
Geometric parameters of the three mono-layer damper designs.
L01
L02
L03
Metallic sheets
Viscoelastic layers
Metallic sheets
Viscoelastic layers
Metallic sheets
Viscoelastic layers
m
0 = 3 mm
v
1 = 1.5 mm
m
0 = 3 mm
v
1 = 4 mm
m
0 = 3 mm
v
1 = 6.5 mm
m
1 = 3.5 mm
α
=
2
°
–
14
.
5
°
m
1 = 3.5 mm
α
=
2
°
–
14
.
5
°
m
1 = 3.5 mm
α
=
2
°
–
14
.
5
°Figure7 shows that the damping potential peak amplitude decreased when the α-value increased, whereas the first natural frequency increased in each sandwich-type CLD design. In addition to this, the increase in the first natural frequency was more significant for theL01 design, that is, for the sandwich-type CLD with the thinnest viscoelastic layer. Furthermore, for α-values equal to 2°, the three sandwich-type CLD designs had approximately the same first natural frequency, which corresponded to the natural frequency of the metallic structure. As α-values increased, the increase in the first natural frequency for theL03 damper design was lower than for the other designs. For the maximal α-value, the first natural frequency of theL01 design is twice as high as theL03 design. Therefore, the angle of the viscoelastic layer, the α value, can be used to adjust the damping strength to the frequency range of interest.Figure 7
Influence of the angle of the viscoelastic layer on theL01,L02, andL03 monolayer damper designs.
(a)
Peak amplitude of damping potential
(b)
First natural frequencyHowever, theα-values adopted in commercial sandwich-type CLDs are usually high, which is not in line with what would be expected from the results in Figure 7(a). In order to clarify this disagreement, two variations of theL03 design were modelled: one with a viscoelastic layer of 3° angle and the other with 11° angle. Figure 8 shows that the peak of damping potential was higher for the 3° angle than for the 11°-angle, meaning that a higher damping strength would be attained with lower α-values. However, Figure 8 shows that the peak of damping potential was more pronounced for the 3° angle than for the 11° angle. Therefore, a sandwich-type CLD with a viscoelastic layer with a low α-value has to concentrate its damping strength more precisely to a given wheel eigenfrequency. For this reason, a flatter damping potential curve is preferred so as to overcome a railway wheel’s frequency variations due to the wheel wearing down as well as the valley effect.Figure 8
Damping potential for two particular sandwich-type CLD designs.


## 5. Damper Design

The influence of several design parameters of sandwich-type CLDs has been studied in the previous sections. In this section, the influence of the relative thicknesses of the different parts of a multilayer sandwich-type CLD and the order in which they are assembled is studied. For this purpose, two-layer sandwich-type CLDs are analysed in Sections5.1, 5.2, and 5.3, and four-layer sandwich-type CLDs are analysed in Section 5.4.


### 5.1. Two-Layer Sandwich-Type CLD: Influence of Metallic Sheets

The influence that the metallic sheets’ thickness has on two-layer sandwich-type CLDs of identical viscoelastic layers (v1=v2 in Figure 9) was studied by modelling and building different metallic sheets and viscoelastic layer configurations using the reference viscoelastic material detailed in Table 1.Figure 9
Scheme of a two-layer damper.Table9 gathers the two-layer sandwich-type CLD designs that were modelled and simulated and the results. The thicknesses of the middle and upper metallic sheets were varied (the thickness of the base metallic sheet was fixed at m0=3 mm) and the viscoelastic layer thickness was adjusted in order to always set the first natural frequency to approximately 400 Hz.Table 9
Simulated two-layer sandwich-type CLD designing geometric parameters and simulation results.m0 = 3 mm.
Design
Designing geometric parameters
Results
m
1 (mm)
m
2 (mm)
v
12 (mm)
w
1 (Hz)
Damp. pot.a
1
1
1
4
400.12
18
2
1.5
1
4.5
394.56
22
3
2
1
4.5
405.41
24
4
2.5
1
5
389.83
26
5
3
1
5
396.62
28
6
3.5
1
5
403.34
29
7
1
1.5
5
391.42
27
8
1
2
5
408.8
34
9
1
2.5
5.5
401.15
44
10
1
3
6
402.52
56
11
1
3.5
6.5
407.79
55
12
1
4
7
408.39
38
13
1.5
1.5
5
401.18
32
14
2
1.5
5
407.88
36
15
2.5
1.5
5.5
390.49
42
16
3
1.5
5.5
400.27
48
17
3.5
1.5
6
392.66
54
18
1.5
2
5.5
390.91
41
19
1.5
2.5
5.5
407.778
55
20
1.5
3
6.5
396.96
82
21
1.5
3.5
7.5
402.07
97
22
2
2
5.5
395.57
48
23
2.5
2
5.5
402.45
55
24
3
2
6
392.36
67
25
3.5
2
6
405.29
73
26
2
2.5
6
391.9
67
27
2
3
6.5
401.74
98
28
2
3.5
7.5
409.4
127
29
2.5
2.5
6
398.81
78
30
3
2.5
6
408.92
90
31
3.5
2.5
6.5
406.84
105
32
2.5
3
6.5
408.82
116
33
2.5
3.5
8.5
403.29
172
34
3
3
7.5
400.09
167
35
3.5
3
8
405.96
193
36
3
3.5
11
397.23
288
37
3.5
3.5
15
406.28
782
aDamp. pot. refers to the peak amplitude of the damping potential curve.The following design considerations can be highlighted:(i)
When the thickness of either of the two metallic sheets was increased, the first natural frequency of the damper increased. As a consequence, the viscoelastic layer thickness had to be increased to counteract this effect. This resulted in an increase in the damping potential, which can be seen, for example, by comparing designs 1 to 6.(ii)
The damping potential was higher if the upper metallic sheet was thicker than the middle metallic sheet, in comparison with its analogue inverse design: designs 2 and 7, designs 3 and 8, designs 4 and 9, designs 5 and 10, and designs 6 and 11.(iii)
In order to keep the first natural frequency constant, the viscoelastic layer thickness had to be increased more when the thickness of the upper metallic sheet was increased than when the thickness of the middle metallic sheet was increased (see the abovementioned inverse designs).(iv)
If the thickness of the upper metallic sheet was much greater than the thickness of the middle metallic sheet, the first modal shape transformed from a mode in which both metallic sheets deformed together (see Figure10(a)) to a mode in which only the middle metallic sheet deformed (see Figure 10(b)). When this happened, the damping potential dropped dramatically, as seen in designs 11 and 12.Figure 10
Different modal shapes.
(a)
Mode in which both metallic sheets deform together
(b)
Mode in which only the middle metallic sheet deforms


### 5.2. Two-Layer Sandwich-Type CLD: Influence of Viscoelastic Layers

Once the influence of metallic sheet’ thickness had been studied, the influence of the relative thicknesses of the viscoelastic layers was analysed through two-layer sandwich-type CLDs composed of viscoelastic layers of different thicknesses (see Figure9). Table 10 presents the two-layer sandwich-type CLD designs modelled and simulated. The thickness of the base metallic sheet was fixed at m0=3 mm. Once again, these sandwich-type CLDs were designed to have their first natural frequency at around 400 Hz by adjusting the thickness of the upper viscoelastic layer.Table 10
Simulated two-layer sandwich-type CLD designing geometric parameters and simulation results.m0 = 3 mm.
Design
Designing geometric parameters
Results
m
1 (mm)
m
2 (mm)
v
1 (mm)
v
2 (mm)
w
1 (Hz)
Pot. damp.
1
3
1.5
5.5
5.5
400.27
48
2
3
1.5
7
2
398.8
68
3
3
1.5
6
4.5
403.07
57
4
3
1.5
5
6
400.58
40
5
3
1.5
4
7
391.213
27
6
3
1.5
3
7
402.2
21
7
1.5
3
6.5
6.5
396.96
82
8
1.5
3
7
2.5
397.5
70
9
1.5
3
6
7
402.93
83
10
1.5
3
5
9
402.46
88
11
1.5
3
4
10
398.24
81
12
1.5
3
3
10
401.48
72
13
1.5
3
2
10.5
395.23
70The following designing considerations can be highlighted:(i)
When the thickness of the upper metallic sheet was greater than the thickness of the middle metallic sheet, a higher damping potential was obtained if the thickness of the upper viscoelastic layer was also higher than the thickness of the middle viscoelastic layer. This tendency can be seen by comparing designs 7 and 10.(ii)
When the thickness of the middle metallic sheet was greater than the thickness of the upper metallic sheet, a higher damping potential was calculated if the thickness of the middle viscoelastic layer was also higher than the thickness of the upper viscoelastic layer. This tendency can be seen by comparing designs 1 and 2.(iii)
A higher damping potential was achieved when the thicknesses of the upper metallic sheet and upper viscoelastic layer were greater than the thicknesses of the middle metallic sheet and the middle viscoelastic layer. In order to keep the first natural frequency constant, the total thickness had to be higher than the analogue inverse design, which can be observed by comparing designs 2 and 10.In conclusion, if the total thickness of the sandwich-type CLD is not limited, in order to obtain the highest possible damping potential, the upper metallic sheet should be thicker than the middle metallic sheet and the upper viscoelastic layer should be thicker than the middle viscoelastic layer. The difference between both thicknesses should not exceed a given value, beyond which modal shapes change to a mode in which only the middle metallic sheet deforms and the damping potential drops.


### 5.3. Comparison of Representative Two-Layer Sandwich-Type CLD Designs

Four two-layer sandwich-type CLD models that represented the previous designs were analysed (see Table11). These designs had metallic sheets that were 3 mm thick and a 1.5 mm thick, but the order in which the metallic sheets were assembled changed for each design. All the designs had a 3 mm thick base metallic sheet. DesignsN01 andN02 consisted of viscoelastic layers of different thicknesses whereas designsN03 andN04 consisted of equal viscoelastic layers.Table 11
Simulated two-layer sandwich-type CLD designs.
Design
m
0 (mm)
m
1 (mm)
m
2 (mm)
v
1 (mm)
v
2 (mm)
N01
3
3
1.5
7
2
N02
3
1.5
3
5
9
N03
3
3
1.5
5.5
5.5
N04
3
1.5
3
6.5
6.5Figure11 presents the damping potential in the frequency domain for each design. As shown, the highest peak amplitude for the first natural frequency corresponded to theN02 design, followed byN04,N01, andN03; the converse is true for the highest peak amplitude of the second natural frequency, which corresponded to theN03 design followed byN01,N04, andN02. It seemed that, for a given amount of viscoelastic material used in a two-layer sandwich-type CLD, thetotal damping potential was distributed around the damper modes, depending on the sandwich-type CLD design.Figure 11
Damping potential for four damper designs.


### 5.4. Four-Layer Sandwich-Type CLD Approach

In order to prove thedamping potential distribution hypothesis, four-layer damper designs were modelled (see Table 12) using the viscoelastic reference material (Table 1).Table 12
Simulated four-layer sandwich-type CLD designs.
Design
m
0
m
1
m
2
m
3
m
4
v
1
v
2
v
3
v
4
F01
3
3.5
3
2.5
2
3.5
3.5
3.5
3.5
F02
3
2
2.5
3
3.5
3.5
3.5
3.5
3.5
F03
3
3.5
3
2.5
2
5
4
3
2
F04
3
2
2.5
3
3.5
2
3
4
5TheF01 design had four viscoelastic layers of the same thickness, and metallic sheets were assembled from the thickest to the thinnest, from bottom to top. TheF02 design was identical toF01 except the metallic sheets were assembled in the inverse order. TheF03 design had the same metallic structure as theF01 design, but the thicknesses of its viscoelastic layers were varied in consonance with the thicknesses of the metallic sheets. Finally, theF04 design had the same metallic structure as theF02 design, but its viscoelastic layers were also varied in consonance with the metallic sheets. All the designs had equal total thickness, since the total thicknesses of both the metallic sheets and the viscoelastic layers were kept constant. In this way, the same amount of viscoelastic material and the same metallic sheets were used for all sandwich-type CLD designs.Figure12 shows the damping potential in the frequency domain for the four-layer sandwich-type CLD designs. The area enclosed by each curve was calculated and it was approximately the same for the four configurations. This fact is in line with the damping potential distribution theory, which says that, for a given amount of metal and viscoelastic material, the total amount of damping potential is distributed around the damper natural modes depending on the chosen damper design.Figure 12
Damping potential for four multilayer damper designs.


## 5.1. Two-Layer Sandwich-Type CLD: Influence of Metallic Sheets

The influence that the metallic sheets’ thickness has on two-layer sandwich-type CLDs of identical viscoelastic layers (v1=v2 in Figure 9) was studied by modelling and building different metallic sheets and viscoelastic layer configurations using the reference viscoelastic material detailed in Table 1.Figure 9
Scheme of a two-layer damper.Table9 gathers the two-layer sandwich-type CLD designs that were modelled and simulated and the results. The thicknesses of the middle and upper metallic sheets were varied (the thickness of the base metallic sheet was fixed at m0=3 mm) and the viscoelastic layer thickness was adjusted in order to always set the first natural frequency to approximately 400 Hz.Table 9
Simulated two-layer sandwich-type CLD designing geometric parameters and simulation results.m0 = 3 mm.
Design
Designing geometric parameters
Results
m
1 (mm)
m
2 (mm)
v
12 (mm)
w
1 (Hz)
Damp. pot.a
1
1
1
4
400.12
18
2
1.5
1
4.5
394.56
22
3
2
1
4.5
405.41
24
4
2.5
1
5
389.83
26
5
3
1
5
396.62
28
6
3.5
1
5
403.34
29
7
1
1.5
5
391.42
27
8
1
2
5
408.8
34
9
1
2.5
5.5
401.15
44
10
1
3
6
402.52
56
11
1
3.5
6.5
407.79
55
12
1
4
7
408.39
38
13
1.5
1.5
5
401.18
32
14
2
1.5
5
407.88
36
15
2.5
1.5
5.5
390.49
42
16
3
1.5
5.5
400.27
48
17
3.5
1.5
6
392.66
54
18
1.5
2
5.5
390.91
41
19
1.5
2.5
5.5
407.778
55
20
1.5
3
6.5
396.96
82
21
1.5
3.5
7.5
402.07
97
22
2
2
5.5
395.57
48
23
2.5
2
5.5
402.45
55
24
3
2
6
392.36
67
25
3.5
2
6
405.29
73
26
2
2.5
6
391.9
67
27
2
3
6.5
401.74
98
28
2
3.5
7.5
409.4
127
29
2.5
2.5
6
398.81
78
30
3
2.5
6
408.92
90
31
3.5
2.5
6.5
406.84
105
32
2.5
3
6.5
408.82
116
33
2.5
3.5
8.5
403.29
172
34
3
3
7.5
400.09
167
35
3.5
3
8
405.96
193
36
3
3.5
11
397.23
288
37
3.5
3.5
15
406.28
782
aDamp. pot. refers to the peak amplitude of the damping potential curve.The following design considerations can be highlighted:(i)
When the thickness of either of the two metallic sheets was increased, the first natural frequency of the damper increased. As a consequence, the viscoelastic layer thickness had to be increased to counteract this effect. This resulted in an increase in the damping potential, which can be seen, for example, by comparing designs 1 to 6.(ii)
The damping potential was higher if the upper metallic sheet was thicker than the middle metallic sheet, in comparison with its analogue inverse design: designs 2 and 7, designs 3 and 8, designs 4 and 9, designs 5 and 10, and designs 6 and 11.(iii)
In order to keep the first natural frequency constant, the viscoelastic layer thickness had to be increased more when the thickness of the upper metallic sheet was increased than when the thickness of the middle metallic sheet was increased (see the abovementioned inverse designs).(iv)
If the thickness of the upper metallic sheet was much greater than the thickness of the middle metallic sheet, the first modal shape transformed from a mode in which both metallic sheets deformed together (see Figure10(a)) to a mode in which only the middle metallic sheet deformed (see Figure 10(b)). When this happened, the damping potential dropped dramatically, as seen in designs 11 and 12.Figure 10
Different modal shapes.
(a)
Mode in which both metallic sheets deform together
(b)
Mode in which only the middle metallic sheet deforms


## 5.2. Two-Layer Sandwich-Type CLD: Influence of Viscoelastic Layers

Once the influence of metallic sheet’ thickness had been studied, the influence of the relative thicknesses of the viscoelastic layers was analysed through two-layer sandwich-type CLDs composed of viscoelastic layers of different thicknesses (see Figure9). Table 10 presents the two-layer sandwich-type CLD designs modelled and simulated. The thickness of the base metallic sheet was fixed at m0=3 mm. Once again, these sandwich-type CLDs were designed to have their first natural frequency at around 400 Hz by adjusting the thickness of the upper viscoelastic layer.Table 10
Simulated two-layer sandwich-type CLD designing geometric parameters and simulation results.m0 = 3 mm.
Design
Designing geometric parameters
Results
m
1 (mm)
m
2 (mm)
v
1 (mm)
v
2 (mm)
w
1 (Hz)
Pot. damp.
1
3
1.5
5.5
5.5
400.27
48
2
3
1.5
7
2
398.8
68
3
3
1.5
6
4.5
403.07
57
4
3
1.5
5
6
400.58
40
5
3
1.5
4
7
391.213
27
6
3
1.5
3
7
402.2
21
7
1.5
3
6.5
6.5
396.96
82
8
1.5
3
7
2.5
397.5
70
9
1.5
3
6
7
402.93
83
10
1.5
3
5
9
402.46
88
11
1.5
3
4
10
398.24
81
12
1.5
3
3
10
401.48
72
13
1.5
3
2
10.5
395.23
70The following designing considerations can be highlighted:(i)
When the thickness of the upper metallic sheet was greater than the thickness of the middle metallic sheet, a higher damping potential was obtained if the thickness of the upper viscoelastic layer was also higher than the thickness of the middle viscoelastic layer. This tendency can be seen by comparing designs 7 and 10.(ii)
When the thickness of the middle metallic sheet was greater than the thickness of the upper metallic sheet, a higher damping potential was calculated if the thickness of the middle viscoelastic layer was also higher than the thickness of the upper viscoelastic layer. This tendency can be seen by comparing designs 1 and 2.(iii)
A higher damping potential was achieved when the thicknesses of the upper metallic sheet and upper viscoelastic layer were greater than the thicknesses of the middle metallic sheet and the middle viscoelastic layer. In order to keep the first natural frequency constant, the total thickness had to be higher than the analogue inverse design, which can be observed by comparing designs 2 and 10.In conclusion, if the total thickness of the sandwich-type CLD is not limited, in order to obtain the highest possible damping potential, the upper metallic sheet should be thicker than the middle metallic sheet and the upper viscoelastic layer should be thicker than the middle viscoelastic layer. The difference between both thicknesses should not exceed a given value, beyond which modal shapes change to a mode in which only the middle metallic sheet deforms and the damping potential drops.


## 5.3. Comparison of Representative Two-Layer Sandwich-Type CLD Designs

Four two-layer sandwich-type CLD models that represented the previous designs were analysed (see Table11). These designs had metallic sheets that were 3 mm thick and a 1.5 mm thick, but the order in which the metallic sheets were assembled changed for each design. All the designs had a 3 mm thick base metallic sheet. DesignsN01 andN02 consisted of viscoelastic layers of different thicknesses whereas designsN03 andN04 consisted of equal viscoelastic layers.Table 11
Simulated two-layer sandwich-type CLD designs.
Design
m
0 (mm)
m
1 (mm)
m
2 (mm)
v
1 (mm)
v
2 (mm)
N01
3
3
1.5
7
2
N02
3
1.5
3
5
9
N03
3
3
1.5
5.5
5.5
N04
3
1.5
3
6.5
6.5Figure11 presents the damping potential in the frequency domain for each design. As shown, the highest peak amplitude for the first natural frequency corresponded to theN02 design, followed byN04,N01, andN03; the converse is true for the highest peak amplitude of the second natural frequency, which corresponded to theN03 design followed byN01,N04, andN02. It seemed that, for a given amount of viscoelastic material used in a two-layer sandwich-type CLD, thetotal damping potential was distributed around the damper modes, depending on the sandwich-type CLD design.Figure 11
Damping potential for four damper designs.


## 5.4. Four-Layer Sandwich-Type CLD Approach

In order to prove thedamping potential distribution hypothesis, four-layer damper designs were modelled (see Table 12) using the viscoelastic reference material (Table 1).Table 12
Simulated four-layer sandwich-type CLD designs.
Design
m
0
m
1
m
2
m
3
m
4
v
1
v
2
v
3
v
4
F01
3
3.5
3
2.5
2
3.5
3.5
3.5
3.5
F02
3
2
2.5
3
3.5
3.5
3.5
3.5
3.5
F03
3
3.5
3
2.5
2
5
4
3
2
F04
3
2
2.5
3
3.5
2
3
4
5TheF01 design had four viscoelastic layers of the same thickness, and metallic sheets were assembled from the thickest to the thinnest, from bottom to top. TheF02 design was identical toF01 except the metallic sheets were assembled in the inverse order. TheF03 design had the same metallic structure as theF01 design, but the thicknesses of its viscoelastic layers were varied in consonance with the thicknesses of the metallic sheets. Finally, theF04 design had the same metallic structure as theF02 design, but its viscoelastic layers were also varied in consonance with the metallic sheets. All the designs had equal total thickness, since the total thicknesses of both the metallic sheets and the viscoelastic layers were kept constant. In this way, the same amount of viscoelastic material and the same metallic sheets were used for all sandwich-type CLD designs.Figure12 shows the damping potential in the frequency domain for the four-layer sandwich-type CLD designs. The area enclosed by each curve was calculated and it was approximately the same for the four configurations. This fact is in line with the damping potential distribution theory, which says that, for a given amount of metal and viscoelastic material, the total amount of damping potential is distributed around the damper natural modes depending on the chosen damper design.Figure 12
Damping potential for four multilayer damper designs.


## 6. General Recommendations for Designing Sandwich-Type CLD Solutions

The design of a given sandwich-type CLD solution depends on its aim. On one hand, a sandwich-type CLD solution designed for a broadband noise problem has to cover a wide frequency range with a relatively flat damping potential curve and avoid the valley effect as much as possible. This can be the case of undamped railway wheels, which normally present a huge number of vibrating modes in the 100–5000 Hz frequency range. In this case, multilayer designs and viscoelastic materials with relatively high loss angles are preferred, and different sandwich-type CLD designs can be combined in such a way that one design can counteract the potential valley effect of another, and vice versa.For example, Figure13 shows the damping potential of two different four-layer sandwich-type CLD designs. It can be seen that both curves are relatively flat (they have a high number of natural modes in the 100–5000 Hz frequency range) and thatdamper B has its first peak just wheredamper A has a valley. In this way,damper B would counteract the valley effect ofdamper A if the noise generating railway wheel mode coincided with this frequency range. These two sandwich-type CLDs can be attached to any type of railway wheel that has its first natural frequency above 380 Hz, which is the first natural frequency ofdamper A and therefore the first peak in the damping potential curve shown in Figure 13. In addition to this, even when the railway wheel wears down, these sandwich-type CLDs would significantly increase the wheel damping.Figure 13
Damping potential of two dampers designed for broadband noise.On the other hand, when the noise problem under study is punctual, meaning in a specific narrow frequency range, a sandwich-type CLD solution that concentrates its damping strength specifically to this frequency range is desirable. In this case, a viscoelastic material with a lower loss factor is recommended, as it would have higher peak amplitudes in the damping potential curve. However, a lower loss factor would make these peaks be more pronounced and thus the sandwich-type CLD would have to concentrate its damping strength more accurately in order to avoid the valley effect, which would be more likely to happen. In this second case, a monolayer or two-layer sandwich-type CLD approach is recommended, as it would have fewer natural modes and therefore fewer peaks in the damping potential curve, resulting in higher damping strength in the peaks that do appear. If this small number of peaks was matched to the railway wheel eigenfrequencies prone to generating noise, a significant damping increase would be achieved for these modes, resulting in a considerable reduction of the total noise level.For example, Figure14 shows the damping potential of a damper designed for a particular purpose. In comparison to the previously mentioneddamper A anddamper B, this design consists of fewer peaks in the 100–5000 Hz frequency range, and therefore fewer modes. In this way, the total amount of damping potential is concentrated in these specific frequencies, which have to be tuned to the railway wheel modes to be damped.Figure 14
Damping potential of a damper designed for a particular purpose.In addition to this, it has been demonstrated that normally the first natural frequency of a sandwich-type CLD has the highest damping strength. If the railway wheel mode to be damped was at a high frequency, in order to match the damper’s first eigenfrequency with wheel mode’s frequency, a stiff viscoelastic material would be desirable, since it would locate the natural modes of the sandwich-type CLD at higher frequencies, allowing the matching of the sandwich-type CLD’s first natural frequency with the natural frequency of the railway wheel that is to be damped.


## 7. Conclusions

Given that the noise generated by a railway wheel is inversely related to the damping of its modes, the higher the damping is, the lower the emitted noise will be. Among the different ways of increasing wheel damping, this paper focused on sandwich-type CLDs.For structural or acoustic simulations of damped railway wheels, the damping added by a given sandwich-type CLD solution has to be known. According to the literature, these damping values can be theoretically predicted. They depend on both the sandwich-type CLD design and the railway wheel. However, a damping solution that is not effective for a given railway wheel might be very effective for another one, and the literature does not give any guidelines or recommendations for optimally evaluating sandwich-type CLD solutions without taking the railway wheel into account. This paper intends to fill this gap: it presents the influence that several sandwich-type CLD design parameters have on damping strength, which yields the most appropriate design of a sandwich-type CLD for a given railway wheel.The concept ofdamping potential has been defined to represent the damping strength of a given sandwich-type CLD design. Using this concept and the procedure presented here, sandwich-type CLD designs have been simulated in order to study the influence of the properties of the viscoelastic material, the geometric parameter design of the metallic sheets, and viscoelastic layers, as well as the order in which different components of the sandwich-type CLD are assembled. It has been shown that the sandwich-type CLD solution presents wide design capabilities for increasing wheel damping under noise problems of diverse characteristics. A collection of design recommendations has been provided throughout the paper.In sum, this procedure serves to qualitatively compare different sandwich-type CLD solutions, facilitate design stage decisions, and significantly reduce cost and time. For a given problem for a specific railway wheel, the proper geometry, material, and damping configuration can be chosen in order to achieve the most appropriate solution in an efficient way.



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*Source: 7846369-2016-02-28.xml*