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Master's Degree Thesis ISRN: BTH-AMT-EX--2012/D-23--SE Supervisors: Sharon Kao-Walter, BTH Huang Yayu, Kunming University of Science and Technology Department of Mechanical Engineering Blekinge Institute of Technology Karlskrona, Sweden 2012 Said Daoud Xie Guowei Liu Xiaoming Equivalent Dynamics Model of Ballasted Track Bed

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Page 1: Equivalent Dynamics Model of Ballasted Track Bed829493/FULLTEXT01.pdf · sleepers, and fasteners) and less care has been devoted on su bstructure of the track (ballast, sub-ballast,

Master's Degree Thesis

ISRN: BTH-AMT-EX--2012/D-23--SE

Supervisors: Sharon Kao-Walter, BTH Huang Yayu, Kunming University of Science and Technology

Department of Mechanical Engineering

Blekinge Institute of Technology

Karlskrona, Sweden

2012

Said Daoud

Xie Guowei

Liu Xiaoming

Equivalent Dynamics Model of Ballasted Track Bed

Page 2: Equivalent Dynamics Model of Ballasted Track Bed829493/FULLTEXT01.pdf · sleepers, and fasteners) and less care has been devoted on su bstructure of the track (ballast, sub-ballast,
Page 3: Equivalent Dynamics Model of Ballasted Track Bed829493/FULLTEXT01.pdf · sleepers, and fasteners) and less care has been devoted on su bstructure of the track (ballast, sub-ballast,

Equivalent Dynamics Model of

Ballasted Track Bed

Said Daoud

Xie Guowei

Liu Xiaoming

Department of Mechanical Engineering

Blekinge Institute of Technology

Karlskrona, Sweden

2012

Thesis submitted for completion of Master of Science in Mechanical Engineering with emphasis on Structural Mechanics at the Department of Mechanical Engineering, Blekinge Institute of Technology, Karlskrona, Sweden.

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Abstract:

Increase of track maintenance costs and change of track geometry are due to the vibration of ballasted railway. The aim of this thesis work is to model train-track system as a multiply degree of freedom systems by Lump Parameter Method. In this model, there are two system which both are modeling as series of mass, dampers and stiffness with the irregularity of rail as exciting signal. The two subsystems are coupled by Nonlinear Hertz contact theory, and then the dynamic system is simulated in Matlab by Newmark Beta method and Runge-Kutta method to obtain the dynamic situation of the system. In addition, the ballast parameters are described in details, and the rail is treated as Euler beam. Moreover, estimate the impact of the other factors as rail, ballast, sleeper, the vehicle speed and the irregularity level of vibration system.

The model is validated by comparing with the experiment result done by predecessor. Fundamental fracture analysis of track is also completed, discussed in static analysis, as a start of further work such as dynamical one.

Keywords:

ABAQUS, Ballast, modeling, simulation, train-track, fracture mechanics

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Acknowledgements

This work was carried out at the Department of Mechanical Engineering, Blekinge Institute of Technology, Karlskrona, Sweden, under the supervision of Dr. Sharon Kao-Walter and Dr. Huang Yayu.

The work is a part of a research project, which is carried for (China railway large maintenance machinery CO., LTD), and the Department of Mechanical Engineering, Kunming University of Science and Technology.

We wish to express our sincere appreciation to Dr. Sharon Kao-Walter and Dr. Huang Yayu and also Ansel Berghuvud for their guidance and professional engagement throughout the work. We would like to thank our families and friends. This work would not have been complete without their love and support

Karlskrona, Oct 2012

Said Daoud

XieGuowei

Liu Xiaoming

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Contents

Acknowledgements 3

Contents 4

1 Notation 7

2 Introduction 9

2.1 Literature Review 11 2.2 Aim and Scope 12

3 Ballasted Railway Model 13

3.1 Background 13 3.2 Track and its Components 14

3.2.1 Rails 14 3.2.2 Rail pads 16 3.2.3 Fastening System 16 3.2.4 Sleepers 17 3.2.5 Ballast 19 3.2.6 Sub ballast 20

3.3 Shear Stiffness and Shear Damping 22 3.4 Main Forces act on Ballast 23

3.4.1 Vertical and Squeezing Forces 23 3.4.2 Lateral and Longitudinal Forces 24

3.5 Maintenance Tamping 26 3.6 Main Factors Effecting Modelling of Ballast 26

3.6.1 Vertical Loads Transmission 26 3.6.2 Train’s Speed 27 3.6.3 Drainage 28 3.6.4 Vibration of Running Train 28 3.6.5 Stability 29 3.6.6 Resistance 29

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3.7 Stresses acts on Ballast Bed 29 3.8 Specifications of Ballast 30 3.9 Friction Coefficient of Wheel-rail 31

4 Theoretical Modelling 32

4.1 Introduction 32 4.2 Simplifications 33 4.3 Single Degree of Freedom 35

4.3.1 Introduction 35 4.3.2 Differential Equation 35

4.4 Euler’-beam theory and Timoshenko-beam theory 36 4.5 Modeling of Train-Track System 37

4.5.1 Introduction 37 4.5.2 Modeling of Vehicle 38 4.5.2.1 Differential Equation 38

4.6 Modeling of Track 46 4.6.1 Modeling of Rail 46 4.6.1.1 Differential Equation 46 4.6.2 Modeling of Sleeper 51 4.6.2.1 Differential Equation 38 4.6.3 Modeling of Ballast 53 4.6.3.1Analysis of Ballast Vibration 53 4.6.3.1.1 Non-Overlapping Case 53 4.6.3.1.2Overlapping Case 53

4.7 Wheel/Rail Bonding Force 61 4.8 Track Irregularities 63

4.8.1 Introduction 63 4.8.2 Differential Equation and Analysis of Track Irregularities 63 4.8.3 Comparison between Experiment and Simulation Data 69 4.8.4 Conclusion and Result 70

5 Simulation Part in ABAQUS 71

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5.1 Overview 71 5.2 Fundamental Fracture Analysis of Track 71

5.2.1 Problem description 71 5.2.2 Background 722 5.2.3 Rationale from Fracture Mechanics 72 5.2.4 Fracture Analysis Model in ABAQUS 74 5.2.5 Comparison of Crack Analysis Results 75 5.2.5.1 Rresults of Rectangle Beam 75

5.2.5.2 Results od different Models in ABAQUS 78 5.2.6 Elementary Ensemble Model 78 5.2.7 Objective Evaluation of Comparison 79

7 Conclusion and Future Work 80

7.1 Conclusion 80 7.2 Future Work 81

8. References 82

Appendix 84

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1Notation

a Stress Distribution Angle Degree

C Damping

E Young’s modulus

F Force

G Dynamic force

g Acceleration of gravity

h Thickness

I Gross Sectional Area

J Mass moment of inertia

Sleeper width

Half-length of Car

Support length of half sleeper

Sleeper spacing

Half-length of bogie

m Mass

N Number of Segments

P Load Force

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p Density

q Distributed Load

Angular Acceleration

Angular Velocity

Angular Deformation

Position

Indices

b Ballast

f Subgrade

p Rail Pad

n step Number of steps

s Sleeper

w Wheel

Abbreviation

FEM Finite Element Method

RCF Rolling Contact Fatigue

OPEX The operational expenditure

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2Introduction

Ballast is considered as an essential component for “railway track structure “[1].It is because of its bending and snapping back readily without breaking down and because of its mechanical properties in construction and maintenance [2].In the earlier century, the concentration for maintenance and modeling was strongly based on superstructure of the track (vehicle, rails, sleepers, and fasteners) and less care has been devoted on substructure of the track (ballast, sub-ballast, and sub- grade). The operational expenditure (OPEX) in terms of preventive maintenance of substructure is increased because of the difficulties occurred when the ballast is fouled and how it is possible to keep the ballast clean. Keeping the ballast is essential in maintenance. The process of removing and cleaning the ballast is costly and interrupts the transporting service of the train. To shrink these costs, a cleaning machine is used to clean up the ballast. According to statistics, most deformation on track structure is due to ballast where the vibration leads to change in track geometry [1]. Therefore, it is important to minimize the vibration during studying the properties of ballast.

Figure2.1.Granular ballast [1]

Ahlbeck [3] assumed that load coincides with the cone distribution when transmitted from sleeper to ballast as seen in Fig. 1[1].

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Ballast’s vibration is not easy to be analyzed due to its granular configuration and dynamic action of the railway track. Theoretical modelling based on dynamic behavior of the system of railway track is studied to model the ballast with the moving loaded vehicle through excitation of the system. The modelling is established to build up a series of springs, dampers and masses system under sleeper to provide a better understanding of modelling the structure in order to get an effective result that can be used to avoid as possible as the noise of vibration and changing of track geometry. Nevertheless, the dynamic modelling of the ballast (springs, dampers, masses) with the superstructure of the track is better understood by analyzing the dynamics of the whole system and how to perform coupling between ballast and superstructure and similarly coupling of system as series of masses-springs-dampers in parallel with other same system during the dynamic behavior of the train-track interaction. Figure 2 illustrates the modelling of springs-dampers-masses in parallel with others [1].

Figure2.2.Simplified of Model

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In this work, the effect of the shear will be analyzed to see how much it plays an important issue to the system if it is added or not. However, MATLAB software is used to carry out the simulations of the mathematical modeling of the superstructure and substructure. The main purpose is to build and improve the simulation model of Vehicle-Track System by lump parameter method, then predict the ballast behavior excited by a moving train and research the impacts of system parameters. Some assumptions are used in theoretical modelling to predict the ballast behavior excited by moving train.

A basic static analysis carried on the rail part, calculation result is compared with the one simulated in software ABAQUS. If there is a crack in track, the vibration and contact force will affected the track structure deeply. It’s not only a potential threat in our system, but also an important security problem for maintenance in railway engineering. This part is preliminary work for deep analysis with a dynamic model, with the supports of theoretical and experimental results can get closer to the accurate situation. This is a good topic worth studying as a future work.

2.1Literature Review

As earlier mentioned, the improvement of modelling the ballast has been changed over the years, and a few studies have been done on modelling the ballast in railway track. In this thesis, many resources were used to understand the concept of ballast modelling and how the theoretical modelling can be established.

The work done by W.M. Zhai, et al. in 2003 [1] carried the mathematical modelling and experimental work of railway ballast vibrations by analyzing and testing the vibration of the granular ballast with using five parameters focused on the load transmission intersects fully with cone distribution through the transmission from the ballast to the sleeper. To highlight the

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continuity of the “interlocking ballast granules” the effect of shear to the stiffness and damping of the ballast is included .Ballast acceleration is measured by a moving train over continoues welded rails to verify the result of the theoretical modelling and to see how much the results are identical [1].

2.2Aim and Scope

In this thesis, the mathematical modelling is based on the dynamic behavior of train-track interaction after excitation of the loaded system. Many parameters are used in the model to establish an effective model, and then mathematical modelling is introduced by writing the differential order ordinary equations to implement it in Matlab software and then lump-parameter method is used to carry the modeling. Validate and compare the result with previous experiment. Also, complete the static analysis of track fracture to show different crack lengths are safety or not, and indicate the ultimate load in the most dangerous situation.

Th0065 numerical result will show the results as graph deformation, velocity and acceleration. The main objective of this work is to improve the modelling of ballast in a way to modify the parameters and geometry of the structure.

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3Ballasted Railway Model

3.1Background

Railway is an important source for transportation that connects many places to other across the world. The history of railway track includes systems with horse power and other systems in the past centuries until 1820s, the first mechanized land transport came out. In the recent 200 years, the railway track has become more advanced. Modern railway track takes into account several aspects [4]:

• safety and accuracy • Increasing the load capacity • Avoiding physical degradation to get the system more stable

Figure3.1.Track components of railway track [5]

The axle load and stresses are transferred from one layer to other layer such as from rail to the foundation and the magnitude of load and stresses become lower till reaching the sub grade.

Track components consist of: the superstructure and substructure. The superstructure includes the rails, fastening system and the sleepers, while the substructure includes the ballast, the sub ballast and the subgrade.

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3.2Track and its Components

3.2.1 Rails

Rails are made of longitudinal steel on which the wheels are running on contact with rail’s surface. The distribution of load from wheel to the sleeper and guidance of the train along the track are the main missions of rails. However, rails should be smooth and also decrease rolling contact fatigue. Higher rails are better than lighter rails in supporting the load and giving higher speed to the train. Rails should be highly strength, massive and joint less, with some given weight to provide convenient resistance to axle loads in order to avoid different problems (such as fatigue, wear).

The most common profile used in rail is Vignoles profile and the weight is in the range between 40-70 kg/m [6].

Figure3.2.Vignoles profile [13]

As mass Mr and the area moment of inertial I increase, the dynamic of the track system decrease quickly, but the contact force and the vehicle dynamic decrease very lightly. The rail cannot change the frequency content of the dynamic system.

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Table 3.1.the impact of rail parameters

Parameters T38 T43 T50 T60 T75

mr(kg/m) 38.73 44.65 51.5 60.64 74.414

I( 10-5m4) 1.2044 1.489 2.037 3.217 4.49

Figure3.3.PSD of acceleration of vehicle with different rail

The figure shows the acceleration PSD of the vehicle which is almost same in the five different types of rail, meaning that the rail has very slight impact for the vibration of the vehicle.

100.1

100.2

100.3

100.4

0

0.005

0.01

0.015

0.02

0.025

Frequency Hz

The PSD of acceleration of the vehicle in different rail

PSD

(m/s

2 )2 /Hz

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Figure3.2.The PSD acceleration of ballast by different rail

As the increase of I and mr can decrease the track dynamic, but the resonance frequencies are constant, just as the ballast show in the figure, other parts of the track have the similar results.

3.2.2Rail pads

Rail pads are an important part of railway track. It is located between the rail and the sleeper to decrease “Dynamic wheel/rail interaction forces” that protect the whole system from unbalance stresses [7].However, it supply electrical isolation and separate vibration of high frequency [3].

3.2.3Fastening System

Fastenings system is the structural connections of the three components; rail, rail pads and sleepers. It is elasticity transferred the load to sleeper after absorption it from rail and rail pads. Moreover, fastening system gives electrical insulation for concrete sleepers and it resists different movements of rails [3].

101.4

101.5

101.6

0

2

4

6

8

10

12

14

16x 10-4

X: 29.45Y: 0.001603

Frequency Hz

The PSD of acceleration of the ballast in different rail

PSD

(m/s

2 )2 /Hz

T38

T43

T50

T60

T75

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Figure3.4.Fastening System

3.2.4Sleepers

The sleepers transfer wheel load from rails and fastening system to ballast

and control the movement of rails. There are two kinds’ well-known sleepers;

the wooden railway sleepers and concrete railway sleeper.

Wooden railway sleepers have been used in the past but recently concrete railway sleepers are replaced and become more popular in railway industry. Wooden railway sleepers will change in structure due to different conditions (freezing, water, dry, etc.) and the behavior of anisotropy will occur. There are many advantages of wooden railway sleepers.

• able to bend easily • decrease vibration and noise

• absorb forces

However, concrete railway sleepers become more used in railway industry. It can be easily obtained than timber, carry higher axle –weights and achieve higher speed. It has less maintenance, longer life than wooden railway sleepers, and less deformation in geometry.

As the same to the change of the rail parameters, the interval of the sleepers Ls affect the dynamic of the track system strongly, but for the vehicle, the

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contact force, the impact is very tiny. We can check the sleeper vibration when Ls changes (Ls=450,500,545,600,650,750,850mm)

Figure3.3.PSD acceleration of the sleeper

The vibration intension of the sleeper changes as the sleeper interval changes, but the resonance frequencies remain the same.

Figure3.4.PSD of sleeper at 29.49 Hz

101.4 101.5 101.6

0

0.5

1

1.5

2

2.5

3

3.5

4

4.5

x 10-3

Frequency Hz

The PSD of acceleration of the sleeper in different sleeper interva PSD

(m/s

2 )2 /Hz

X: 29.49Y: 0.004626

WoodConcrete

450 500 545 600 650 750 8500

0.5

1

1.5

2

2.5

3

3.5

4

4.5

5x 10-3 PSD of sleepers for different sleeper interval at 29.49Hz

Interval of sleepers mm

PSD

(m

/s2 )

2 /Hz

ConcreteWood

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The figure shows the vibration intension of the sleepers at resonance frequency f=29.49 Hz when the interval changes. For instance, when Ls=545mm, the intension vibration is the weakest and the wood sleeper has weaker than the concrete.

From the figure above, when the ls=545mm, the vibration of sleeper is the weakest; this is why the interval of sleeper is about 550mm in practice. Though the vibration of wood sleeper is weaker than concrete, wood is more experience, more vulnerable and less sustainable, so the concrete is used more and more popularly.

3.2.5Ballast

Ballast bed is often formed of angular, crushed, hard stones and rocks of ballasted railway track [5]. It is located on the top layer of substructure and to the sides, in between sleepers, outside the rails to form the shoulders and ends down to form a ballast layer. The depth of ballast is placed at 0.3 meters [3]. Figure (4.7) shows the ballast and how it is placed.

The main functions of ballast are:

• resist longitudinal forces applied in sleepers • stability and elasticity of the track • draining to avoid irregularities • reduce stresses during transferring to next layers

In this thesis, our attention goes to figure out the important of this task due to the different effects to the railway as a whole and how much it leads to changing in the track geometry and track maintenance according to recent statistics.

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3.2.6Sub ballast

Sub ballast is the layer placed between ballast and subgrade to separate those two layers. It decreases the stresses and prevents interpenetration between ballast and subgrade [3].

Figure3.5.Ballast bed

Figure3.6.the PSD of acceleration of the ballast

101.4

101.5

101.6

0

1

2

3

4

5

6

7

8

x 10-4

Frequency Hz

The PSD of acceleration of the ballast in different ballast thickness

PS

D

(m/s

2 )2 /Hz

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Figure 3.7.Vibration of different ballast thickness

From the figure above, it can be obtained that the dynamic ballast vibration increases when the ballast thickness also increases. But the ballast can keep the track shape constant, and keeps the track from the damage of environment. So the ballast can’t be too thick.

Pick the value of the PSD at 29.45 Hz from the left figure, the result show the vibration intension increases as the ballast thickness increases.

250 350 450 550 6500

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1x 10-3

X = 250Y = 0.000607

The ballast vibration for different ballast thickness at 29.45Hz

Ballast thickness mm

PS

D

(m

/s2 )2 /H

zX = 350Y = 0.000625

X = 450Y = 0.000663

X = 550Y = 0.000723

X = 650Y = 0.000809

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3.3Shear Stiffness and Shear Damping

Figure 3.8.Influence of ballast shear damping and stiffness in ballast

From the figure obtained by adding the shear damping and stiffness can decrease the vibration of the ballast, for example at 29.44 Hz, the PSD for ignoring shear stiffness and damping is about 0.000995 (m/s2)2/Hz which is 3 times larger than 0.00033(m/s2)2/Hz for considering Shear stiffness and damping.

The vibration will affect the adjacent blocks of ballast more than the level of one ballast block due to friction and effect of ballast stones that cause to arise towards the motion of adjacent blocks of ballast in case of the present of shearing effect, otherwise no effect is occurred and ballast mass vibrate freely .However, if shear damping and shear stiffness of ballast are considered, then the vibration towards adjacent blocks will be weakening in force and it produces higher attenuating effect ballast blocks, implies that less vibration. Shearing parameters play an important role in analysing dynamic behavior of train-track system. [1]

0 5 10 15 20 25 30 35 400

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1x 10-3

Resonance frequency Hz

PSD

(m

/s2 )

2 /Hz

The impact of ballast shear damping and stiffnesss for the ballast vibration

Without Shear C KWith Shear C K

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3.4Main Forces act on Ballast

3.4.1Vertical and Squeezing Forces

Many forces disturb on the ballasted railway track. Every component has some forces exerted on it. Ballast has two main forces which act on it: vertical force and squeezing force. The vertical force is formed of compounding two loading: static and dynamic loading. Static loading refers as “dead load” of the top part of the track (superstructure) and the moving train [7]. Dynamic loading depends upon the situation of the track and the speed of the train. On the other hand, squeezing force excited during the maintenance tamping which leads to further damage to ballast.

The train weight divided by the number of wheels is defined as the vertical dead wheel. However, the limit of static load of the train’s loading is between 53 k N to 174 k N for “light rail passengers” in North America of heavy haul trains [5]. Also, these forces create vibration into the track structural and then disturb as stresses to the different components until reaching the subgrade layer. Figure3.9 shows the deflection of rail after uploading the rails by dead wheel load.

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Figure3.9.Load and stresses distribution of track structure [14]

3.4.2 Lateral and Longitudinal Forces

Ballast has lateral and longitudinal forces exerted on it. These two forces are difficult and complex to predict. Lateral wheel forces are occurred by the lateral force and lateral component acts on wheel flange towards rail and by friction force between rail and wheel respectively. Lateral wheel forces are geometry deviation from train reaction and weaving motions which result from instability at high speed train. While, buckling reactions force happens against lateral direction and buckling occurs by “high longitudinal rail compressive stress” as the increasing of rail’s temperature.

However, Longitudinal forces are in parallel to the rails of track way. These forces come from locomotive force, braking force, thermal expanding and compression of rails, and rail wave action.

In United States, two different measurements occurred on vertical wheel load.

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The measurements on the two figures show static and dynamic forces verses percent level exceeded for the track of Colorado test and the track of the mainline between Washington and New York respectively, and plotted as cumulative frequency distribution curves .About 20000 axles had been recorded during the measurements of dynamic force [5].

Figure3.10.Static and dynamic load for Colorado test track [5]

Figure3.11.Static and dynamic load for mainline

betweenWashington andNew York [5]

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3.5Maintenance Tamping

Maintenance tamping is an important tool that returns the track geometry to its original situation. This mechanism has tamping tines that remove the ballast and gather it under the sleeper. The mechanism lifts the sleeper and then insets tamping tines into the ballast.

Figure3.12.Maintenance tamping [5]

3.6Main Factors Effecting Modelling of Ballast

3.6.1Vertical Loads Transmission

The static and dynamic loads should transmit perfectly from superstructure starting from loading of wheel’s contact with rail and continuous to ballast and ending in subgrade layer without any failure. It is important to study the effect of increasing the axle load in which the settlement should be satisfied to maintain the track performance. A track settlement is mostly ascribed by the underlying subgrade of vertical settlement and partly due to ballast broken. Stresses are increased in the ballast layer as an increase of axle loads.

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3.6.2Train’s speed

It is essential to highlight the effect of increasing the speed of train in the track of railway which influence the “dynamic augment” and in turns change the load moving along the track [12]. However, stresses remain the same with higher speed of the train.

Figure3.13.Acceleration of vehicle in different speed

The speed will impact the dynamic of the whole system, the system dynamic and wheel-rail contact force will increase quickly, as the speed increase.

0

2

4

6

8

50

100

150

200

250-2

0

2

Time s

The acceleration of the vehicle in different speeds

Speed km/h

A m

/s2

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Figure3.14.Vehicle vibration in different speed at 1.997 Hz resonance frequency

A very strange phenomenon is obtained the vehicle vibration is the weakest case when the speed is 120km/h, after 120km/h, the vibration increases rapidly as the speed increases.

3.6.3Drainage

Drainage factor is necessary for ballast to drain the track system in order to satisfy the performance of ballast material and maintenance of the track. While, unclear or wet ballast will lead to the growth of plant, such as grasses, that affects the reduction of drainage from ballast bed. Therefore, drainage should be taking into consideration to maintain the settlement of the track.

3.6.4Vibration of running train

At high speed of the train, the track ballast will be influenced which in turns

60 90 120 150 180 210 2400

0.05

0.1

0.15

0.2

0.25

0.3

0.35The vehicle vibration for different vehicle speed at first resonance frequency 1.997 Hz

PS

D

(m

/s2 )2 /H

z

Speed km/h

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leads to high vibration of the ballast bed and affects the other components of the railway track. Ballast bed should be Equipped with such modelling to not let the ballast lifted from its position under high pressure coming from vibration of train’s speed and also it can be occurred by using larger particles of ballast and replace in away by keeping the ballast level low with relation to the top of sleeper.

3.6.5Stability

The track of the train should achieve the stability by giving well performance for various functions of ballast. Also, ballast has to carry and transmit vertical loads (static and dynamic loads) in all direction. Moreover, vertical loads are uniformly distributed to substructure section especially ends in subgrade layer.

3.6.6Resistance

The ballast material should have the ability to resist any empty voids in order not to produce any kind of fines between particles that stopping drainage to occur. Also, if the ballast material losses its function of resistance the strength to withstand, then the ballast section will become more detritions and loss the meanings of supporting the whole system to stay stable all the time.

3.7Stresses acts on ballast bed

Vertical loads are exerted in different components of railway track and especially come from wheel load over the rail that leads to deflections and creating stresses which distributed over ballast and subgrade layers. However, over loading acts on ballast layer may leads to deterioration of the quality of the track due to the rapid increase of axle loads.

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Zimmermann’s theory states that the compressive stresses distributed from sleeper to ballast can be calculated by choosing the maximum stress between these two layers under wheel loads and by applying Dynamic Amplification Factor due to the speed of the rolling stock as per Eisenmann’s model [12].

However, Eisenmann’s model can be written as follow:

sb= DA ) ( / /Asb = 3.1

The above formula is used to find the stresses of ballast bed due to the force that is coming from the sleeper. However, this formula is used specific contact area between sleeper and ballast bed for half sleeper.

3.8Specifications of Ballast

Table 3.1.The specification of ballast

Shape Quality Depth Water

Absorption

Width of Shoulder Ballast

• Angular • Hard stones • Crushed rocks• Not

contaminant

• Sharp at corners

0.3 meters

50/100 %

=0.5% maximum

700 mm on

curves and 500 mm on straight

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3.9Friction coefficient of Wheel-rail

There are many factors affect the dynamic behavior of the train. Coefficient of friction is one factor which causes greater crawling forces and then RCF and probability of wear will increase more [8].Further, coefficient of friction varies from season to other season relying upon climate condition. For examples, the friction drops down to small value about 0.1 while it is raining and increases up to higher value about 0.6 in a freezing winter [4]. The coefficient of friction of wheel-rail is changing during a year as seen in the graph depending climate condition.

Figure 3.15.Variation of coefficient of friction of wheel-rail in a year [4]

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4Theoretical Modelling

4.1Introduction

In 1867, Winkler advanced the Elastic foundation beam theory which was used for modeling of the track soon, and then in 1926, Timoshenko researched the vibration of the rail by The Elastic foundation beam firstly. with the rapid development of Railway in all of the world, and the scientists have made great achievements for modeling the dynamic of the rail system, in the 1970s, Ahlbeck from American, Birmann from Germany, and Gant of France used the lumped parameters method to create the vehicle-track model which include the compositions of the vehicle and the track, as well as the wheel-rail contact, to study the vibration questions [16]. Afterwards the model as the figure 4.1 shown has been presented, which is quite popular, and can get good results matched with experiment.

One of the main goals of this work is to get much better understanding of different parameters and how it should be used in train-track system in order to get a better enhancement of modelling ballast.

To do this work, modelling of train-track system should be presented using the fundamentals of physics and mathematics by differential second order ordinary equations to create the desired modelling.

However, to reach the final modelling of the system, some theories should be studied and analyzed and then achieve the mathematical modelling of train-track system

Firstly, SDOF composed of spring-mass-damper system is analyzed in this chapter to give a clear idea about the modelling of train-track system and then writing possible various differential equations. Then, Euler’s beam

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theory introduces in details as a theory that can be used to couple the beam with different components of the whole system. Finally, the mathematical modelling of train-track interaction can be created after knowing the basic concept of SDOF, Euler’s beam theory, other important theories (D’Alembert principle, and non-linear Hertzian spring elements) and how to couple of each of them.

4.2Simplifications

Following assumptions are made to achieve the desirable modelling of the whole system. These assumptions are:

• Assume Rail is Euler’s beam with two fixed ends • The ballast can be divided to many rigid masses • The velocity and deformation of ballast at the first mass and the last mass

are zero • Track is symmetrical about the middle line between the two rails • The loading is distributed in symmetric in both rails • The contact force between wheels and rail can be ruled by Hertzian non

linear contact theory • The components of train-track are rigid bodies • Dynamic movement in the direction of vertical plane is studied • All damper should be viscous • The parameters of the vehicle–track system are constant

The system is composed of two parts: the vehicle part and the track part. The vehicle is represented by the train and the track part is composed of rail-sleeper-pads-ballast-subgrade. However, vehicle model is an series masses-springs-dampers also called multiple degree of freedom systems (MDOF), and the track model with rail assumed as Euler’ beam . Sleeper, ballast and subgrade are also MODF system. The both parts are coupled by

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wheel-rail contact force which is ruled by non-linear Hertzian contact theory.

Figure4.1.Train-Track System Simplified Model

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4.3Single Degree of Freedom

4.3.1Introduction

Single degree of freedom (SDOF) is composed of mass-damper-spring. This system is well-known as basic in mechanics that can be used to study more complicated system. Figure (3.2.) shows the model of SDOF.

Figure4.2.SDOF Model

After knowing the properties of the single-degree-of-freedom system, it will be clearer to know the modelling of the whole system.

4.3.2Differential Equation

From Newton second law, sum of the all forces acting on the object;

F m x 4.1

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Where m is the mass, c is the viscous damping coefficient, k is the stiffness, is the absolute displacement of the mass. Then, derive the differential equation of motion for the SDOF system, it written as:

m x cx xk 4.2

Take all components of the equation to the left, it would be written like this:

m x cx kx 0 4.3

Divide equation (4.3) by m, then it is written in the form:

xcm x

km x 0 4.4

Where,

cm 2ξω 4.5

Finally, wn is easily found,

km ω 4.6

whereω is the natural frequency (radians/sec), andξis the damping ratio.

And the damped natural frequency:

ω ω 1 ξ (4.7)

4.4 Euler’-beam theory and Timoshenko-beam heory

Euler-Bernoulli beam theory gives the equation of motion as:

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4 2

4 2

( , ) ( , ) ( , )d w x t d w x tEI m q x tdx dt

+ = (4.8)

In the Euler-Bernoulli beam theory influence of shear is neglected. As the beam height over length ratio increases this approximation becomes less and less valid [9]. A way of considering shear deformations but still keep a one-dimensional description of a beam structural element.

While Timoshenko- beams theory gives:

2 22

2 2 2b s sd v d v qd v M

dx dx dx EI GAα

= + = − − (4.9)

If the shear modulus of the beam material approaches infinity - and thus the beam becomes rigid in shear - and if rotational inertia effects are neglected, in this case, it is almost the same as the ordinary beam theory [9].

Timoshenko beam theory is higher order than the Euler-Bernoulli theory; it is known to be superior in predicting the transient response of the beam. The superiority of the Timoshenko model is more pronounced for beams with a low aspect ratio. It is shown that use of an Euler-Bernoulli based controller to suppress beam vibration can lead to instability caused by the inadvertent excitation of unmodelled (this is means that the system which without definition) modes [9].

4.5Modeling of Train-Track System

4.5.1Introduction

Mathematical modeling of train-track system is used to band together all components in a way of investigating dynamic analysis of whole system. In fact, it is hardly possible to create a mathematical modeling of any component without taking into consideration a visible feature of train-track

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interaction. However, the interaction of all components within a system leads to the results of dynamic behavior that can be investigated by several mathematical modeling. Further, it is possible in this mathematical modeling to find out such as calculation of velocity, acceleration, etc for any components of train-track interaction. To established ballast model, the rail is assumed as Euler’s beam for calculations and non-linear Hertzian spring elements are used in this work to model the wheel-rail contact. Moreover, Euler’s beam is more effective and useful than Timoshenko beam where ratio of height over length is very small of beam. In this model, velocity, acceleration and deformation of vehicle, rail, sleeper and ballast are presented as the result on graphs by implementation on Matlab software. Dynamic behavior of train-track system is changing all the time depending on many factors speed of train, the irregularity level of rail and other important factors.

Then the dynamic situation of the vehicle C62A will be presented in the chapter, with the running speed V=60km/h on the rail with 6 level irregularity.

4.5.2Modeling of Vehicle

In most cases, all parts of the system should be rigid bodies through studying the dynamic behavior of vehicle. In general; a rigid body has six degree of freedom. In the presented model, the rigid body has two degree of freedom. The first one corresponds to vertical deformation, while the other rolling in rotation direction. Therefore, the vehicle is modeled with six degrees of freedom including a body of a car, the two bogie masses and their moment of inertia. Figure (4.1) shows the schematic of the vehicle that consists of a car body, four wheels and truck frames.

4.5.2.1Differential Equation

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By applying D’Alembert principle, the governing equations describe a body of car. These equations can be entirely described as second order ordinary differential equations.

In this work, two degree of freedom of a rigid body is studied. Then, car-body has vertical deformation and rotational. These equations written [18] as follow:

Car body’s deformation:

2 2 0 (4.10)

is the gravity of the car body

and

Car body’s rotational:

2 2 2 21 2 1 2 0

(4.11)

However, the first bogie frame mass is subjected to deformation and rotational.

First bogie mass deformation:

22 2

(4.12)

and

First bogie mass rotation:

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2 21 1 2

0 4.13

Also, the second bogie mass is subjected to deformation and rotational as the first bogie.

Second bogie mass deformation:

22

2 4.14

Second bogie mass rotation:

J 2M l φ p t p t l 0 (4.15)

However, the wheels are replaced under the two bogie frame masses without any suspension of springs.

The equation of wheels depends on the deformation, the velocity, and the acceleration of the two bogie frame masses. Moreover, these four equations can be derived from equations (4.12), (4.13), (4.14) and (4.15).

For first wheel, the equation can be written as follow:

Z Z l φ 4.16

For second wheel, the equation can be written as follow:

(4.17)

For third wheel, the equation can be written as follow:

(4.18)

For fourth wheel, the equation can be written as follow:

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4.19

where, Zw1, Zw2, Zw3 and Zw4 are deformations for first, second, third and fourth wheels respectively, and , ,are rotational for first and second bogie frame respectively.

Consequently, it is convenient to write these equations in the form of matrixes which it can facilitate the solution of the presented work and then implement it in MATLAB to get the results.

These equations are written in the form of the given equation matrix:

MZ’’+CZ’+KZ=0 (4.20)

where,Z describes as the given matrix:

(4.21)

M, C and K are given in matrix form in appendix 2

At speed 60 km/h, different graphes are obtained using different variable.

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Figure4.3.The acceleration of the vehicle with speed 60 km/h

Figure4.4.PSD acceleration of vehicle with speed 60 km/h

0 1 2 3 4 5 6 7-0.8

-0.6

-0.4

-0.2

0

0.2

0.4

0.6

0.8

X: 4.447Y: 0.6613

Time s

The acceleration of the vehicle in speeds V=60km/h A

m/s

2

X: 4.173Y: -0.7208

10-1 100 101 102 103 104 1050

0.005

0.01

0.015

0.02

0.025

X: 1.997Y: 0.02452

Frequency Hz

The PSD of acceleration of the vehicle in speeds V=60km/h

PSD A

(m

/s2 )2 /H

z

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Figure4.5.The displacement of vehicle with 60 km/h

Figure4.6.The velocity of vehicle with 60 km/h

0 1 2 3 4 5 6 70.065

0.07

0.075

0.08

Time s

The displacement of the vehicle in speeds V=60km/h X

m

0 1 2 3 4 5 6 7-0.06

-0.04

-0.02

0

0.02

0.04

0.06

0.08

Time s

The velocity of the vehicle in speeds V=60km/h

V m

/s

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Figure4.7.The rotary acceleration of vehicle with 60 km/h

Figure4.8.PSD rotary acceleration of vehicle with 60 km/h

From the figures, the resonance frequency is very low 1.997 Hz the magnitude is quite small 0.02452 m/s and 0.005778 Hz respectively for vertical acceleration and rotary acceleration.

0 1 2 3 4 5 6 7-0.2

-0.15

-0.1

-0.05

0

0.05

0.1

0.15

Time s

A

r

ad/s

2

The rotaty acceleration of the vehicle in speeds V=60km/h

10-1 100 101 102 103 104 1050

1

2

3

4

5

6x 10-4

X: 1.997Y: 0.0005778

Frequency Hz

PS

D A

(ra

d2 /s)2 /H

z

The PSD of rotaty acceleration of the vehicle in speeds V=60km/h

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Figure4.9.The rotary velocity with 60 km/h

Figure4.10.The rotary displacement of vehicle with 60 km/h

0 1 2 3 4 5 6 7-0.015

-0.01

-0.005

0

0.005

0.01

0.015

Time s

V ra

d/s

The rotaty velocity of the vehicle in speeds V=60km/h

0 1 2 3 4 5 6 7-1.5

-1

-0.5

0

0.5

1

1.5x 10-3

Time s

X ra

d

The rotaty displacement of the vehicle in speeds V=60km/h

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4.6Modeling of Track

The railway track is described in the presented model as a rail, sleeper, and ballast as illustrated in figure (4.1). The numerical method is used to find a vertical model of a track with different elements. Accordingly, the rail is treated by Euler’s beam theory with a defined boundary conditions and the sleeper is under the rail through coupled springs-dampers.

In fact, to establish the final solution of different parts of a railway track, mathematical and physical theories are used in this model. Here we consider the unloaded track as the equilibrium position (in other words, without consider the gravity of the track)

4.6.1Modeling of Rail

The continuous beam is assumed to be treated by Euler’s beam theory and it is supported at ends by simply supports. Two rails are connected in parallel and symmetrical about the middle line.

4.6.1.1Differential Equation

In fact, the rail should be considered as infinite beam, but in calculation finite length is used, and value the length about 160 m. Figure (4.1) shows the beam with boundary conditions at the ends.

Since the rail is described as Euler’s beam. Therefore, the dynamic equation is described [18] as follow:

, ,

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4.22

With boundary conditions:

Z 0, t =0, Z L, t =0 (4.23)

Z 0, t 0, Z L, t 0 4.24

Where,Fi is the support force from the discrete sleeper i to rail

Gj is the load or contact force of the wheel j.

However, Fi is obtained by using the given equation:

, , 4.25

Moreover, Gj is described as the following equation:

0 (4.26)

Figure4.11.Rail Model

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To find the values and ; different equation written as follow:

2 (4.27)

2 (4.28)

2 (4.29)

(4.30)

4.31

In this model, , may be given as:

, 4.32

Where, is the generalized deflection of the nth mode and is the nth eigenfunction of a simply supported beam described as:

(4.33)

where, Yk is the k mode shape

Solving equation (4.32) into (4.22) and by the orthogonality of different modes, it becomes as:

0 4.34

And by the property of the Dirac function:

The given equation can be obtained:

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q tEIm

kπL q t F

N

t Y x

G t Y xG 4.35

However, if equation (3.25) is solved with equation (4.35), the following equation is obtained:

∑ ∑

∑ ∑ ∑∑ ∑ (4.36)

Figure4.12.Acceleration of rail with 60 km/h

The maximum vertical acceleration of the rail is 2.539 m/s2, when the wheels just pass the sampling point.

2.2 2.4 2.6 2.8 3 3.2 3.4 3.6 3.8-2

-1.5

-1

-0.5

0

0.5

1

1.5

2

2.5X: 2.776Y: 2.533

Time s

The acceleration of the rail in speeds V=60km/h

A m

/s2

X: 3.284Y: 2.539

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Figure4.13.PSD acceleration of rail with 60 km/h

Figure4.14.Velocity of rail with 60 km/h

For the nonlinear contact force, the low frequencies are quite chaotically, but after 40Hz, two resonance frequencies can be obtained at 716.8Hz and 1198Hz.

10-1

100

101

102

103

104

105

0

0.5

1

1.5

2

2.5x 10

-3

X: 27.62Y: 0.002135

Frequency Hz

The PSD of acceleration of the rail in speeds V=60km/h

PSD A

(m/s

2 )2 /Hz

X: 716.8Y: 0.0001954 X: 1198

Y: 0.0001244

2.4 2.6 2.8 3 3.2 3.4 3.6 3.8

-0.02

-0.01

0

0.01

0.02

0.03

Time s

The velocity of the rail in speeds V=60km/h

V m

/s

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4.6.2Modeling of Sleeper

The sleeper lies between the rails and ballast layer. The distance of discrete sleepers is usually about 0.5 meters and the system behaviors under sleeper mass as spring-damper that are connected in parallel.

4.6.2.1Differential Equation

In the presented work, sleepers can describe as the interaction of train-track system as the dynamic equation that can be presented from figure (4.1).

In general, the dynamic equation of sleeper is written for any chosen sleeper i (i=1: N)

Then, for the sleeper (ith), the following equation [18] can be established

, , 0 (4.37)

Then, equation (4.38) is obtained after solving equation (4.32) into equation (4.37):

0 4.38

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Figure4.15.Acceleration of sleeper with 60 km/h

Figure4.16.PSD acceleration of sleeper with 60 km/h

2.5 2.6 2.7 2.8 2.9 3 3.1 3.2 3.3 3.4 3.5

-1

-0.5

0

0.5

1X: 3.282Y: 1.036

Time s

The acceleration of the sleeper in speeds V=60km/h

A m

/s2

X: 2.653Y: -1.283

X: 3.161Y: -1.263

101 102 103

0

5

10

15

x 10-4

X: 40.93Y: 9.244e-009

Frequency Hz

The PSD of acceleration of the sleeper in speeds V=60km/h

PSD A

(m/s

2 )2 /Hz

X: 29.45Y: 0.001563

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Figure4.16.PSD acceleration of sleeper with 60 km/h

4.6.3 Modeling of Ballast

4.6.3.1Analysis of Ballast Vibration

Ballast can be considered as one of the most components that forms main source of vibration from the system as a whole. The reason is related to the changing of geometry of track and stability of ballast. However, it so difficult to study the dynamic behavior of ballast according to recently studies has been accomplished in this domain work. Actually, ballast vibration is analyzed as series of spring and damper under sleeper component [1], [3]. In fact, Ahlbeck supposed that the analysis of ballast vibration can be represented as mathematical modeling if it is considered that these stresses are distributed within the cone region. From this point of view, it can be accepted to create the modeling depending in this assumption. Therefore, it can possible be analyzed the ballast masses just under each sleeper as the form of cone region to carry the modeling of each parameter [1].

4.6.3.1.1Non-Overlapping Case

2.2 2.4 2.6 2.8 3 3.2 3.4 3.6-0.015

-0.01

-0.005

0

0.005

0.01

0.015

Time s

The velocity of the sleeper in speeds V=60km/h V

m/s

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As shown in figure (1), the modeling of ballast represents as a cone region under a sleeper.

Figure4.18.Ballast Mass Simplified Model [1]

According to definition, the ballast mass is written in the form:

mb=ρ vb (4.39)

Where,

is the density of ballast;

vb is the volume of ballast;

And the volume of ballast can be easily found from the given geometry in figure (1). Thus, the volume of ballast is equal [1]:

vb= h tan γ+( xb + xe ) hbtanγ+xexb (4.40)

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Where,

hb ,the height of ballast;

xe ,the length of half sleeper;

xb ,the width of sleeper;

, the angel of stress distribution for ballast

Therefore, the ballast mass is:

mb= ρ [ h tan γ+ ( + ) hbtanγ+ ] (4.41)

Similarly, the ballast stiffness can be determined from ballast mass simplified model as the following equation:

Kb = /

.Eb (4.42)

Eb is the modulus elasticity of ballast. However, the ballast damping is difficult to be calculated analytically because of the reasons that mentioned before. However, the ballast damping was established by Sato in the famous test which called “Wheel set-dropping test” [5, 11].

4.3.1.1.2Overlapping Case

In the previous section, overlapping wasn’t taken into consideration in choosing the parameters of ballast. However, an overlapping can be existed in cone region for changing in angel distribution or properties of ballast component and maybe also the distance between two sleepers. Furthermore, this case will lead to changing in the given variables as well as in the results of parameters.

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Thus, the height will become as follow:

h h x x2 tan γ 4.43

wherexs the distance between two sleepers

Therefore, the ballast mass becomes as:

M = (xe + ) +xs ( - ) + ( - (4.44)

Figure4.19.Ballast model in case of overlapping

Furthermore, the ballast stiffness can be written as two parts due to the overlapping as seen in figure (2).

The ballast stiffness is composed of two parts:

The first part of ballast stiffness is:

= /

Eb (4.45)

And the second part:

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=

Eb (4.46)

The combination of the two parts becomes as follow:

= (4.47)

In addition, ballast is described as dynamic equation like sleeper due to the interaction of train-track system which leads to result of dynamic behavior. However, using the schematic of modeling in train-track system in figure (3.1), the given dynamic equation can be represented using the parameters of dampers, masses and stiffness at different components of the sleeper, ballast, shear ballast and subgrade in vertical direction of model.

In general, the dynamic equation of ballast is:

2 2

0 (4.48)

With boundary conditions:

0 (3.49)

0 (3.50)

By using the dynamic equation in eq (4.48) at the boundary conditions given in eq (3.49) and (3.50), then these equations are implemented in Matlab to obtain the deformation, the velocity, and the acceleration of ballast.

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Figure4.20.Acceleration of ballast with 60km/h

Figure 4.21.PSD acceleration of ballast with 60km/h

2.4 2.6 2.8 3 3.2 3.4-0.8

-0.6

-0.4

-0.2

0

0.2

0.4

0.6

X: 3.161Y: -0.7801

Time s

The acceleration of the ballast in speeds V=60km/h

A

m/s

2

X: 2.653Y: -0.7872

101.2 101.3 101.4 101.5 101.6 101.7

0

1

2

3

4

5

6

x 10-4

Frequency Hz

The PSD of acceleration of the ballast in speeds V=60km/h

PSD A

(m/s

2 )2 /Hz

X: 29.45Y: 0.0006631

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Figure 4.22.the vertical velocity of the ballast with the speed 60km/h

Figure4.23.The comparison of displacement for rail, sleeper and ballast when the vehicle speed V=60 m/s and the rail irregularity level is 6 level

2.6 2.8 3 3.2 3.4 3.6-8

-6

-4

-2

0

2

4

6

8

10

x 10-3

Time s

The velocity of the ballast in speeds V=60km/h

V m

/s

2 2.5 3 3.5 4 4.5

0

0.5

1

1.5

2

2.5x 10-3

X: 2.759Y: 0.002361

The displacements for rails,sleeper and ballast

Dis

plac

emen

t

m

Time s

X: 2.756Y: 0.001311

X: 2.725Y: 0.0008158

rail

sleeper

ballast

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From the figure, we can obtain that the displacement of rail is almost 3 times larger than the ballast.

Figure4.24.Comparison of vibration intension of the

different parts of the system at resonance frequencies

The figure show, the comparison of the accelerations of different parts of the dynamic system, the vehicle body have the most largest value at resonance 1.998Hz, and in the track system, the vibration of rail is the most serious, all the three parts of track system, rail sleeper, ballast get their pick value at 29.75Hz

100 101 102 103 10410-5

10-4

10-3

10-2

10-1

X: 1.998Y: 0.02434

The resonance frequency for the different parts of the dynamic system

Resonance Frequency Hz

PSD (

m/s

2 )2 /Hz

Vehicle bodyRailSleeperBallast

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4.7 Wheel/Rail Bonding Force

We assume the wheel/rail bonding force can be governed by Hertz nonlinear contact force theory.

P (t) [ Z (t) (4.51)

G is the wheel rail contact constant;

δZ t is the elastic compression between wheel and rail.

G 4.57R-0.149×10-8 for the worn-type wheel

G 3.86R-0.115×10-8for the cone-type wheel

R is the radius of the wheel

Z(t) Zwj(t) – Zr(xwj, t ) ( j 1~4 (4.52)

Zwj (t) is the vertical displacement of the wheel j at time t;

Zr (xwj,t) is the vertical displacement of rail under the wheel j.

IfδZ t 0 meaning the rail and wheel is not contacted, then the contact force p (t) =0.

Input the irregularity of rail Z0(t), the contact force p(t):

pj (t) ,0 δZ t 0

(4.53)

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Figure4.25.The wheel rail contact force with 60 km/h

Figure4.2.PSD of wheel rail contact force

0 1 2 3 4 5 6 71.6

1.7

1.8

1.9

2

2.1

2.2

2.3

2.4x 105 The wheel-rail contact force in speed V=60km/h

Time s

Con

tact

forc

e N

10-1 100 101 102 103 104 1050

2

4

6

8

10

12x 10

6

X: 1.83Y: 1.043e+007

The PSD of the wheel-rail contact force

Frequency Hz

PSD

N

2 /Hz

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4.8Track Irregularities

4.8.1Introduction

Track irregularities are precursor safety occurrences which under specific circumstances lead to an accident, and main dynamic exacting resource Track irregularities can occur due to any deviation of geometry of the track. Types of track irregularities are mentioned by the Swedish track recording vehicle STRIX [4]:

• Geometrical track errors in lateral and vertical directions • Deviation from nominal track gauge • Deviation from nominal cant

Figure4.27.Types of track irregularities [4]

4.8.2 Differential Equation and Analysis of Track Irregularities

The feature of cracks outgrowth in wheel and rail Vertical irregularities is due to the dynamics analysis of forces. The lateral irregularities can manage control of the track when outer wheels are unstable guidance against outer rail. These two types of irregularities produce uncomfortable behavior [10].

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The American rail department PSD equation:

ΩΩ Ω Ω

4.54

Sv is the rail irregularity power spectral density;

Av is the Roughness constant (cm^2.rad/m);

Ωc isthe cut off spatial frequency (rad/m);

k is the safety factor:0.25-1.0 (in our article, k=0.25)

Table 4.1.Parameters of American rail power spectral density

Parameters

The level of rail

1 2 3 4 5 Level6

Av/(cm2.rad/m)

1.2107 1.0181 0.6816 0.5376 0.2095 0.0339

As/(cm2.rad/m)

3.3634 1.2107 0.4128 0.3027 0.0762 0.0339

Ωs 0.6046 0.9308 0.8520 1.1312 0.8209 0.4380

Ωc 0.8245 0.8245 0.8245 0.8245 0.8245 0.8245

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Figure4.28.Comparison of irregularity PSD for the

simulation value and the resolvable value in level 6

As shown in figure (4.28), irregularities have big effect on changing dynamic track of the whole system. As a result, irregularities with wavelengths range between 0-50 meters where it is transferred from PSD to irregularity in time domain with using random phase to get the following dynamic analysis.

As seen in figure above, nonlinearities are taken into account in this work just during studying rail pads which have nonlinear behavior opposite to other parts of train-track system.

In the previous analysis, the simulation was carried of US at level 6 after transfer track irregularity PSD between time domain and frequency domain. Now, the simulation result will be based just from PSD to irregularity in time domain using a function random in MATLAB.

10-1 100 101 10210-14

10-12

10-10

10-8

10-6

10-4The Track Irregularity PSD

f/Hz

PS

D m

2 /Hz

The simulation valueThe resolvable value

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We use a wavelength in range between 0.5m-50m with running speed v and specific excitation frequency to avoid noise. Irregularities are so many types with different wavelength [track irregularities reference]. Selection will be done in the suitable one to carry the dynamic analysis of track irregularities.

Here, the equations for track irregularities [17] as follow :

N| |

N X k X k (4.55)

The irregularity in time domain x (n):

x(n) N

∑ X k exp N

N (4.56)

X(k) N ∆ ∆ (4.57)

∆ (4.58)

Φ ) (4.59)

Where Φ is normal distribution from 0~2pi.

Using these equation and the numerical methods, then implement them into MATLAB to get the graph of the railway track irregularity.

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Figure4.2.Tthe vertical absolute irregularities As function of the position on the rail

1.30.The wheel-rail contact force in different speeds of vehicle

20 40 60 80 100 120 140 160-6

-4

-2

0

2

4

6

8x 10-3 The railway track irregularity

x/m

irreg

ular

ity Z

/m

0

2

4

6

8

1

2

3

4

5

6

70

2

4

x 105

Time s

The wheel-rail contact force in different speeds of vehilce

Irregularity level

Con

tact

forc

e N

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The wheel rail contact forces for the different rail irregularity level when the vehicle running speed V=60kg/h, the level 7 mean the rail is perfectly smooth. So from the 2 figures below, the wheel-contact force increase as the rail

Figure 4.31.The amplitude of contact force PSD at the first resonance frequency

Figure31 shows first resonance frequency at 18.3 Hz, and for level 3 4 the first resonance frequency is 1.997 Hz, level 7 is 15.31Hz. It becomes rougher, then the vibration of the system will increase, and the safety and comfortableness decrease surely. But the smoother rail needs higher cost and technological request.

1 2 3 4 5 6 70

1

2

3

4

5

6x 108The amplitude of contact force PSD at the first resonance frequency

Am

plitu

de

N2 /2

Irregularity level

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4.8.3 Comparison between Experiment and Simulation Data

Figure4.32.Comparison of simulation and experiment data of ballast

Figure4.33.Comparison between simulation and experiment data

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2-6

-4

-2

0

2

4

6The simulation vaule of ballast acceleration

Time s

The

acce

lera

tion

of b

alla

st g

Simulation valueExperiment value

0 50 100 150 200 250 300 350 4000

0.05

0.1

0.15

0.2

0.25

Frequency Hz

The

acce

lera

tion

dens

ity g

/Hz

Simulation valueExperiment value

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A rail surface on a joint has detected as the shape of cosine function during the dynamic analysis of the system. During loading the wheels of a train, the irregularity will be affected by such that excitation. However, the depth of wave of irregularity is about 0.4 mm and the wave length is 80 mm [1].

The pick value of simulation: 5.248g and the experiment value is 4.69g.

From the figure the frequency range have a very good agreement with each other between the experiment value and simulation value.

4.8.4 Conclusion and Result

When the train passes at passes with speed 60 km/h, it shows approximately the same result for simulation data and experiment data and the acceleration of the ballast was almost the same.

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5Simulation Part in ABAQUS

5.1 Overview

Conventional simulation of the whole system has been done in ABAQUS, due to the bounded less reason such as working capacity and the own limitations of the software, the overall model needs improvement and expansion as a part of future work; In another way, an interesting question is brought up: statics fracture analysis of track. As we know, the Vibration situation will be changed if there any deformation occurs in any part of our system. Track is the part connects the train-track system and ballast system, and it’s also the transmitter of force and vibration. So crack on the track can be seen as an initiator of vibration source. When crack appears, it will impact on the vibration original force and transmit it to the ballast part, and the affected load will change the attribute of the crack, in turn. For this, the problem is an important research subject in ballasted track system-the interaction of crack and vibration. The elemental task is prepared for dynamic analysis and more available models, as well as the successors in this area. As conclusion, hand calculation result is compared with the one from simulation; the reasons why there are some differences are given.

5.2Fundamental Fracture Analysis of Track

5.2.1 Problem Description

A local problem in our system: fracture analysis of track is studied. The damage of track crack, as an engineering problem, also occupies an important position in railway engineering. The track is a constituent part in our system; its stability affects the safety and efficacy directly.

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5.2.2 Background

On the basis of our assumptions, the track used in the system is ideal quality without any damage, such as corrosion or crack. But in the real-life engineering, the impact from construction, environmental and many other reasons, it has the possibility of fracture occur.

Figure5.1.Crack on the track

In railway engineering, the situation of track fracture is not what we hope. Fracture is the most potential of danger and maintenance. In order to avoid or retard the occurrence of fracture, we need to research the influence on the track, which form the contact force and vibration. There are two sources: top-down, train-track system initiated; the other one is bottom-up, come from track and ballast system. The two directions transmission of energy, the track will be influenced, if there is a crack, it will gradually be changed with the input such as force and vibration. From here we can see the internal relations between each part.

5.2.3Rationale from Fracture Mechanics

To get start our study of track fracture, we should introduce our model, a simplified model, the same as the model ‘three point bending test’ we studied

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in fracture mechanics. The test sample here is our track, the two end supports are the sleepers. Here we add a crack with length a in the middle point between the two supports, as the figure below.

Figure5.2.The three point bending test sample

The three point bending method can calculate the fracture (intensity) factor , use the result compared with the normalized value , we can indicate the situation we analyzed is safe or not, also we can point out the maximum value of the load when there is crack propagation.

We also know that this model we use belongs to Ι type (opening mode) in fracture mechanics. For this type of model, the fracture factor is influenced by three factors: stress, crack length and form coefficient. The relationship between them can be performed as below.

√ (5.1)

Where, σ is the nominal stress, α is form factor and is the crack length.

5.2.3.1Rudimentary Knowledge of Hand Calculation

For Ι type (opening mode), we have the equations to calculate the fracture

a

2W

W

P

2W

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factor .

(5.2)

And,

. . . . (5.3)

Where: P-load, S-span of the test sample, B-thickness of the sample, W-height of the sample, a -crack length.

Under the theoretical direction, we can calculate if we have all the parameters needed.

5.2.4Fracture Analysis Model in ABAQUS

In our model, we assume the test sample is a piece of track between two sleepers, so logically the two supports in our three point bending test are the sleepers. The material of the track is low carbon high manganese steel, which is used in normal railway construction. Adding a static load in our system, keep the magnitude of load same as the value we used in theoretical modelling, P= 200K N each wheel (four wheels totally).

We have designed two different beams as our testing samples in ABAQUS, the first model we used is a rectangular beam, and the second model is an I-beam. The dimensions showed as below. Because of continuity reason of result comparison, there we use the rectangular beam as a transition model, instead of compare the I-beam and hand calculation. This will be described in details in subsection 5.35.

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As tabovmid

5.2.

For of threal

Figure5.3

the same with ve, in simulati

ddle between tw

5 Comparison

three points bhe test sample ity case we us

3.The outline a

Figure5.4.Cr

the theoreticalion part the crawo sleepers, sh

n of Crack An

ending experimis rectangle, soe in engineerin

75

and the dimens

ack added in a

l model in fracack in add in chow as figure

nalysis Result

ment, we shouo the specimenng, the track is

sion of two test

all situations

cture mechaniccross section, th5.4.

ts

uld notice that n thickness is as I-beam. In ad

t samples

c we mention he position is

the cross-sectia constant, but ddition to this,

the

ion the , in

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hand calculation part, there is no guidance of the case with variable cross-section sample. So first we compare the results from hand calculation and model one (rectangular beam), both with rectangular cross-section, then compare the results of two models simulated in ABAQUS. This is a reparative way to put the incalculable practical engineering case together with the simulation result.

5.2.5.1 Results of Rectangle Beam

Figure5.5.The Different Crack Length Demonstrate in ABAQUS

Form figure 5.5 we know that under the same load, the stress and fracture factor all change a lot with the increasing of the crack length. From this figure, it can be seen clearly that the maximum stress and fracture factor show at crack tip in every crack length case.

After we pick all the maximum values of fracture factor in each case, put together with the hand calculation result, the figure 5.6 shows the variation tendency with the increasing of the crack length.

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Figure5.6.Facturefactor form calculation and simulation

From figure 5.6 above, we can see that tack the crack length equal to 10mm as an watershed, before 10mm the two result keep a good agreement with each other, but after this crack length, the gap will increase much faster and faster.

To explain this compare conclusion, we should awaken equation 5.1.

From this we know fracture factor under the control of three factors, -the nominal stress, -form factor and -the crack length. In calculation case we think the -form factor is unconverted, but in practical case when the crack length change, the angle of the crack will change, the X is no longer the one we used in previous case. But from this figure, even though the numerical value can’t keep the same with the increasing of crack length, but we can see they keep a good agreement in tendency.

5.2.5.2 Results of Different Models in ABAQUS

Since the I-beam is the practical type we used in real railway engineering,

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and we also know the theoretical basis of I-beam case calculation is difficult to realize, so compare the I-beam simulation result in ABAQUS with the simulation result of square beam is very necessary.

Figure5.7.Fracturefactor two model in simulation

From figure5.7 we know the I-beam’s fracture factor will increase with the increasing of the crack length before 25mm, the same conclusion as the calculation and first model, but after 25mm, it presents a great different behavior. Here gives the explanations of this phenomenon, as follow.

• The I-beam’s cross section dimensions is varying along the longitudinal height;

• The internal force from varied-sized parts is much complicated then the rectangular beam.

5.2.6 Elementary Ensemble Model

From figure 5.7 we can get that when the crack length is 25mm, the fracture

factor is the maximum value 508.637N/ .

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Infact, the maximum value is still within the security range, because the

industrial standard of the material used in track is 1176N/ 15 , that

means under a static load as we made, there will no crack propagation.

It is mentioned before, as a condition, the load we add is 20K N on each wheel. So, the bearable load in daily life is 80 tons, but just in case the train is used for special mission, what is the allowable load? In this case, there will be crack propagation at the most dangerous crack length is 25mm. The load can’t afford for normal track we use in our model is 190 tons(475 K N on

each wheel), since at this condition, the fracture factor is 1201N/ ,

which is bigger than the standard value, it’s an acceptable carrying capacity for a single section of the train.

5.2.7 Objective Evaluation of Comparison

As conclusion, we can indicate that in the interval range of 0 to 20mm, the simulation result keep pace with each other, basically. After the crack length reaching 25mm, fracture factor of rectangular beam is much smaller than the I-beam. The main reason of this problem is geometric dimension and unavoidable error between calculation and simulation. It can be a worthy intensive study topic.

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7 Conclusion and Future Work

7.1Conclusion

This thesis attempts to study the equivalent dynamics model of ballasted track bed. For this reason, theoretical modeling is carried to build the dynamic behavior of train-track system by lump-parameter method and then implement that model in MATLAB software to permit the result of the calculation of deformation, velocity and acceleration at a desirable layer and especially at ballast layer according to the given requirements listed in this thesis. Previous work has been done by W.M. Zhai, et al. in 2003 [1] was carried experiment and mathematical work on modelling ballast. While in the presented work, theoretical modelling is done and also simulation on cad Inventor was studied to compare the results between them and moreover to modify the parameters used as possible as to improve the modelling. To establish this work, many assumptions are taken into account due to the difficulties of analyzing the dynamic behavior of the whole system as changing of the track geometry most of the time.

To sum up, mathematical modelling and the simulation carried in MATLAB and ABAQUS permit the following results listed below.

• Using the simplified model that allows to come up with mathematical modelling equations of train-track system

• Writing the modelling equation of ballast as well as the parameters such as damping and stiffness and then lump-parameter method is used

• Calculation of deformation, velocity and acceleration of ballast and represent on graphs as dynamic analysis curve due to the vibration and track geometry change.

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• Comparing the experimental part with theoretical part to verify the results.

• The vibration of the vehicle is affected by the running speed of the vehicle and the irregularity of the rail badly, but by other parts of the track slightly. The parameters of the track such as the thickness of the ballast, the types of the rail, the interval of the sleepers, can influence the vibrations of the track obviously, so getting reasonable parameters of the track is very important for the maintenance and working time of the track.

• Simulation in ABAQUS and complete the static analysis of track fracture situation, find out the critical load of general train, and the fracture situation in different crack length on the track.

7.2Future Work

In the present work, the theoretical part is established as the use of

mathematical and physical theories and then compares it to the simulation

part to validate the result. However, it is possible to perform experiment to

obtain the dynamic response of ballast excited by passing train instead of

comparison to simulation part. Moreover, different numerical method such

as discrete element method can be used to solve mathematical modelling.

Develop a packaging simulation program on MATLAB GUI to simulate

vehicle-track.

Expand the ABAQUS model into the dynamic analysis, consider the vibration source and get the result which press close to the physical truth.

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8. References

[1] W. M. Zhai, K. Y. Wang and J. H Lin, (2004), Modelling and Experiment

of Railway Ballast Vibrations, Journal of Sound and Vibration, Elsevier.

[2] G. Saussine a,*, C. Cholet a, P.E. Gautier a, F. Dubois b,C. Bohatier b

and J.J. Moreau b,(2004), Modelling ballast behaviour under dynamic

loading. Part 1: A 2D polygonal discrete element method approach, Journal

of Sound and Vibration, Elsevier.

[3] K. Knothe, Gleisdynamik, Ernst & Sohn, Berlin, 2001, pp. 77–85.

[4]Nia, S, Dynamic Modelling of Freight Wagons, Master’s degree Thesis,

ISRN:BTH-AMT-EX-2011/D-04-SE

[5] Wee Loon Lim, (2004), Mechanics of Railway Ballast Behaviour,

University of Nottingham

[6]Akke Simon Johanna SUIKER, (2002), The Mechanical Behaviour of

Ballasted Railway Tracks, de TechnischeUniversiteit Delft,

[7]X. Lei, N, A., Noda,(2002), Analysis of Dynamic Response of vehicle and Track coupling System with Random Irregularity of Track Vertical Profile, Journal of Sound and Vibration, Elsevier.

[8] A. Ekberg, E. Kabo and H. Andersson, An Engineering Model for

Prediction of rolling Contact Fatigue of Railway Wheels, Department of

Applied Mechanics /Charmec, Chalmers University of Technology, Sweden.

[9]Göran Broman, (2003), Computational Engineering, Department of

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mechanical Engineering, Blekinge Institute of Technology, Karlskrona,

Sweden.

[10] Tomas Karis, Track Irregularities for High-Speed Trains, Master’s degree Thesis, TRITA-AVE 2009:95, ISSN 1651-7660,ISBN 978-91-7415-547-1

[11] Hai Huang, (2009), Discrete Element Modelling of Railroad Ballast Using Imaging Based Aggregate Morphology Characterization Department of Civil and Environmental Engineering, University of Illinois at Urbana Champaign.

[12]A.V. Mittal,S.K.Maurya, Ballast Specification,Session No. 721

[13]http://www.google.dk/imgres?q=vignoles+rail+profile

[14] http://en.wikipedia.org/wiki/Newmark-beta_method

[15]Qingfen Li1; Shifan Zhu2, Fracture Mechanics and Engineering

Application, ISBN: 978-7-81007-863-4, Harbin engineering university press

[16]AhLbeck D R,Meachan H C, Prasue RH, The development of the analytical models for rail road track dynamics, Railroad Track Mechanics& Technology(Kerr A D, editor) [17] Garg V K, Dukkipati RV,Dynamic of railway vehicle systems, New York: Academic Press [18]Wang Ming, Zhai, Vehicle-Track Coupling dynamics, 3th Edition, Science Press.Beijing, 2007

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Appendix

Appendix 1

These nomenclatures are used in this thesis.

Cb Ballast Damping lc Half Length of Car

Cf Subgrade Damping le Support Length of Half Sleeper

Cp Rail Pad Damping ls Sleeper Spacing

Cs Sleeper Damping lt Half Length Bogie

Cw Ballast Shear Mb Ballast Mass

Ct Bogie Damping Mc Car Mass

Eb Ballast Modulus Mp Pad Mass

Ef Subgrade K30 Modulus Ms Sleeper Mass

Jc Mass Moment Inertia of Car Mt Bogie Mass

Jt Mass Moment Inertia of Bogie Mw Wheel Mass

Kp Rail Pad Stiffness Zc Car-Body Vertical Deformation

Kw Ballast ShearStiffness Zbi Vertical Deformation ith Ballast

Kt Bogie Stiffness Zsi Vertical Deformation ith Sleeper

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lb Sleeper Width Zt1 Vertical Deformation at First Bogie

Appendix 2

The mass, damping and stiffness matrices are expressed as:

Diag Mi = , , 2 , 2 , 2 , 2

M=

⎥⎥⎥⎥⎥⎥⎥⎥

⎢⎢⎢⎢⎢⎢⎢⎢

++

++

2

2

2000000200000020000002000000000000

twt

wt

twt

wt

c

c

lMJMM

lMJMM

JM

C=

⎥⎥⎥⎥⎥⎥⎥⎥

⎢⎢⎢⎢⎢⎢⎢⎢

−−−

−−

00000000000000000000200002

2

2

2

tctt

tctt

ttttct

ttt

ClCC

ClCClClClC

CCC

,

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K=

⎥⎥⎥⎥⎥⎥⎥⎥

⎢⎢⎢⎢⎢⎢⎢⎢

−−−

−−

00000000000000000000200002

2

2

2

tctt

tctt

ttttct

ttt

KlKK

KlKKlKlKlK

KKK

Appendix 3

3.1Introduction

Nowadays, engineer is using numerical methods as a basic in ordinary differential equations to solve complex problems which is really difficult to find a solution of it by analytical methods in some time, especially when these problems related to approximation or three dimensions. However, analytical methods are useful to get clear idea and much understanding about several numerical methods in order to show the final analysis result in given software [9].

As it known, numerical methods depend of something that called in studying of science “ Guessing”[9].These methods must consider the following important issues:

• Accurate, means errors must be negligible • Effective, means solution with definite time

• Stable, means errors must be defined very well

3.2Newmark-Beta Method

Newmark-Beta method is considered as one of several numerical methods which used to solve several differential equations. However, this method is

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87

found to evaluate the dynamic response of different field such as finite element analysis for modeling a given dynamic system.

Use mean value theorem and equation of motion to derive the Newmark-Beta method [14].

For the dynamic equation: MX CX KX P, the Newmark_beta method procedure is shown below:

(1), predict the displacement and velocity at n+1 step

X , X X Δt12 ψ X Δt ψ A Δt

X , X 1 φ X Δt φ X Δt

(2) Predict the acceleration:

X , M P , K X , C X ,

(3)The iteration procedure:

X , X X Δt12 β X Δt β A , Δt

X , X 1 φ X Δt φ X , Δt

and the acceleration:

X , M P , K X , C X ,

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Where m is the iteration number and when m=1, the m iteration takes the

value of prediction step as: X , X ,

The iteration procedure at each time stop is continued until the difference

between two successive acceleration is smaller than the given tolerance [9].

3.3Runge-Kutta Method

Runge-Kutta method is a numerical method that used to solve differential

equation with a good accuracy; the total truncation error is of O h [the

computational engineering page32].

For the project, the Runge-Kutta method can be described by

Xk1 2 k2 2 k3 k4

6Δt

X Xk1 2 k2 2 k3 k4

6

X X X Δt

n=1, 2, 3…

where

k1 M P C X K X Δt where Pn P X

k2 M P C X 0.5k1 K X X Δt 0.5Δt k1 /2

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where P P X X Δt 0.5Δt k1 /2

k3 M P C X 0.5k2 K X X Δt 0.5Δt k2 /2

where P P X X Δt 0.5Δt k2 /2

k4 M P C X k3 K X X Δt 0.5Δt K3

P P X X Δt 0.5Δt k3

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FigureA.1.The algorithm chart

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FigureA.2.Comparison of acceleration of ballast in the different numerical method

Figures above show the results of the both methods for model2where the

velocity of vehicle is 60km/h (model: the ballast without shear damping and

shear stiffness and model2: the rail with shear damping and shear stiffness.

Here it can be possible to obtain results from the two different methods. But

Newmark-Beta just take half time than the Runge-Kutta method, therefore

the Newmark-Beta was chosen as the main method.

2.2 2.4 2.6 2.8 3 3.2 3.4 3.6-1

-0.8

-0.6

-0.4

-0.2

0

0.2

0.4

0.6

0.8

1

Time s

The

acce

lera

tion

of b

alla

st

m/s

2The comparison of the different numerical method

The newmark-betaThe rungekutta

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School of Engineering, Department of Mechanical Engineering Blekinge Institute of Technology SE-371 79 Karlskrona, SWEDEN

Telephone: E-mail:

+46 455-38 50 00 [email protected]