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This document summarizes a study that uses an Eulerian finite element approach to simulate the thermomechanical behavior of disc brakes over multiple braking cycles while accounting for pad wear. The study finds that considering pad wear leads to different temperature distributions on the disc with two hot bands appearing after several cycles, consistent with experiments. The Eulerian approach requires significantly less computational time than a Lagrangian approach. Pad wear is updated after each cycle and influences contact pressures and heat generation in subsequent cycles.

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0% found this document useful (0 votes)
22 views10 pages

Fulltext01 4

This document summarizes a study that uses an Eulerian finite element approach to simulate the thermomechanical behavior of disc brakes over multiple braking cycles while accounting for pad wear. The study finds that considering pad wear leads to different temperature distributions on the disc with two hot bands appearing after several cycles, consistent with experiments. The Eulerian approach requires significantly less computational time than a Lagrangian approach. Pad wear is updated after each cycle and influences contact pressures and heat generation in subsequent cycles.

Uploaded by

Om Singh
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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EB2013-MS-007

THERMOMECHANICAL SIMULATION OF WEAR AND HOT BANDS


IN A DISC BRAKE BY ADOPTING AN EULERIAN APPROACH
Rashid, Asim*, Strömberg, Niclas
Department of Mechanical Engineering, Jönköping University, Sweden.

Keywords: Eulerian framework, frictional heat, hot band, wear history, pad wear, repeated braking

Abstract: In this paper frictional heating of a disc brake is simulated while taking wear into account. By performing
thermomechanical finite element analysis, it is studied how the wear history will influence the development of hot
bands. The frictional heat analysis is based on an Eulerian formulation of the disc, which requires significantly
lower computational time as compared to a standard Lagrangian approach. A real disc-pad system to a heavy
truck is considered, where complete three-dimensional geometries of the ventilated disc and pad are used in the
simulations. A sequential approach is adopted, where the contact forces are computed at each time step taking the
wear and thermal deformations of the mating parts into account. After each brake cycle, the wear profile of the pad
is updated and used in subsequent analysis. The results show that when wear is considered, different distributions
of the temperature on disc are obtained for each new brake cycle. After a few braking cycles two hot bands appear
on the disc surface instead of only one. These results are in agreement with experimental observations.

1. INTRODUCTION

Disc brakes are used to adjust the speed of a vehicle by pressing a set of pads against a rotating disc. It converts the
kinetic energy of the moving vehicle mainly into heat. This heat causes the disc and the pad surface temperature
to rise in a short period of time. Due to relative sliding, both the pad and disc wear, which affects the behavior of
disc-pad system over time. Since the pad material is softer as compared to the brake disc, the wear of the pad is
dominant [1]. Higher temperature of the pad surface during braking also affects life of the pad negatively due to
increased wear rate.
Tribological contact in disc brakes has been studied both by physical experiments and numerical simulations. Both
techniques have their own roles and importance to understand the disc-pad system fully. Lee and Barber [2] per-
formed an experimental investigation of thermoelastic instability in disc brakes. They observed that temperature
initially rises faster at the inner and outer radii of the pad after many repeated test runs. They attributed this behavior
to the concentrated wear at the center of the pad during previous runs. Eriksson et al. [3] provided a comprehensive
overview of different processes, both at micro and macro scale, causing the contact surface variations. Panier et
al. [4] performed an experimental investigation of railway disc brakes and proposed a classification of hot spots
observed on a brake disc surface based on thermographs. They also studied the influence of pad stiffness and pad
contact length on hot spots development. Österle et al. [5] performed a pin-on-disc test and showed that a third
body with a different structure and composition from the first bodies was trapped in a gap between the pin and the
disc. The pin was cut from a commercial brake pad and the disc material was cast iron. Hong et al. [6] compared
the friction and wear characteristics of three friction materials with different binder resins. In their study, the wear
rate below a critical temperature showed a slow increase, but above it the wear rate increased rapidly. Furthermore
below the critical temperature binder played a minor role in the wear resistance of the friction material, but above it
the wear rate was strongly influenced by the thermal decomposition of the resin.
Contact pressure distribution is an important parameter for disc-pad systems. For the experimental study of the dis-
tribution of contact pressure, pressure sensitive films [1] have been used. These methods can only be used for static
analysis. Due to wear and other thermomechanical changes, contact pressure distribution does not stay constant dur-
ing braking operation so numerical simulations become an obvious choice to determine the evolution of the contact
pressure. Many researchers have used numerical simulations to enhance the understanding of the disc-pad system.
Dufrénoy and Weichert [7] implemented a two-dimensional (2D) fully coupled thermomechanical algorithm taking
wear into account. Kao et al. [8] developed a three-dimensional (3D) FE model capable of performing fully coupled
thermomechanical analysis. They took the effect of wear on contact pressure distribution into consideration. They
used this model to study hot judder in a disc brake. Koetniyom et al. [9] performed sequentially coupled thermo-
mechanical finite element analysis of disc brakes under repeated braking conditions. They considered only a small
segment of the disc taking the cyclic symmetry into account and assumed a uniform heat flux. In [10], Dufrénoy
and Weichert developed an uncoupled 3D FE model. They simulated only one-twelfth of the disc by considering the
axial and rotational symmetries of the disc and used temperature dependent material data. Gao et al. [11] developed
a fully coupled 3D thermomechanical FE model to investigate the fatigue fracture in disc brakes. They assumed
that thermal properties of the materials for disc and pad are invariant with temperature. Abubakar and Ouyang [1]
performed wear simulation of a brake pad by using a commercial FEA software and compared their results with

1
physical tests. They considered the real surface topography of the pad while building the finite element model by
measuring height distributions with a gauge. Söderberg and Andersson [12] performed a simulation of wear and
contact pressure distributions of the brake pad using a general purpose finite element analysis software. Vernersson
and Lundén [13] studied the behavior of brakes numerically for repeated brake cycles. They used a 2D fully coupled
FE model while considering the coefficient of friction as being constant and a temperature dependency of the wear
rate. They found out that wear of the pad strongly depends on the stiffness of the friction material and its mounting.
Today, the prevalent way to simulate frictional heating of disc brakes in commercial softwares is to use the La-
grangian approach in which the finite element mesh of a disc rotates relative to a brake pad. Although this approach
works well, it is not feasible due to extremely long computational times. Particularly, for simulating repeated brak-
ing this approach is of little importance for practical use. Sometimes two-dimensional FE models are used to reduce
the computational time but this approach is not sufficient to model complex behavior. The rotational symmetry
of the disc makes it possible to model it using an Eulerian approach, in which the finite element mesh of the disc
does not rotate relative to the brake pad but the material flows through the mesh. This requires significantly lower
computational time as compared to the Lagrangian approach. Nguyen et al. [14] developed an Eulerian algorithm
for sequentially coupled thermal mechanical analysis of a solid disc brake. First they performed a 3D contact cal-
culation to determine the distribution of the pressure. Then a sequentially coupled analysis is implemented by first
performing a transient heat transfer Eulerian analysis followed by a steady-state mechanical analysis. Recently,
Strömberg [15] developed a finite element approach using an Eulerian framework for simulation of frictional heat-
ing in sliding contacts. In his approach, the fully coupled problem is decoupled in one mechanical contact problem
and a frictional heat problem. For each time step the thermoelastic contact problem is first solved for the temperature
field from the previous time step. Then, the heat transfer problem is solved for the corresponding frictional power.
In another paper [16] this approach was implemented for simulating frictional heating in disc-pad systems.
In this work, frictional heating of a disc brake, while taking the wear into account, is simulated by implementing an
Eulerian approach. A toolbox developed by Strömberg, which is based and described in his earlier work [16] but
now extended to include wear of the pad, is used to perform the frictional heat analysis. In this Eulerian approach
the contact pressure is not constant, but varies at each time step taking into account the wear and thermomechanical
deformations of the disc and the pad. This updated contact pressure information is used to compute wear, and heat
generation and its flow to the contacting bodies at each time step. In such manner, the wear and nodal temperatures
are updated accurately and their history is recorded at each time step. Then a Python script is used to write the wear
and temperature history to an output file for subsequent use. The disc-pad system is simulated for several brake
cycles. After each brake cycle pad geometry reflects the material removed by accumulated wear and this updated
geometry of the pad is used in subsequent brake cycles. Because the finite element mesh of the disc does not rotate
relative to the pad, the contact region is always well defined and a node-to-node based approach can be adopted.
This allows the mesh to be refined only in the region where the brake pad is in contact with the disc, which results in
lower computational time. The output file with temperature history can be used e.g. in a sequentially coupled stress
analysis.
The results show the appearance of two hot bands on the disc surface after several brake cycles which cannot be
predicted when wear is ignored. The Eulerian approach has proved tremendously cheap in terms of computational
time when compared to a fully coupled Lagrangian approach. This is demonstrated by presenting numerical results.

2. FRICTIONAL HEAT ANALYSIS

The workflow of the approach used for frictional heat analysis is shown in Fig. 1. An input file, which contains the
meshed geometry with appropriate boundary conditions and loads is required for the frictional heat analysis. During
this analysis linear thermo-elasticity is adopted and the problem is decoupled in two parts. In the first part, for a

Input file

In-house software

ODB file

Figure 1: Workflow of sequential approach.

2
Specify initial temperatures of
‫ݐ‬ൌͲ disc and pad.

Thermoelastic contact problem


is solved while taking the wear
into account and contact pressure
distribution is determined.
‫ ݐ‬ൌ ‫ ݐ‬൅ ο‫ݐ‬

Wear gaps are updated.

Heat transfer problem is solved


and new nodal temperatures are
determined.

Figure 2: Sequential approach used during frictional heat analysis to determine temperature history.

Table 1: Material properties for frictional heat analysis.

Disc Pad Plate


Thermal conductivity [W/mK] 47 0.5 46
Young’s modulus [GPa] 92.9 2.2 210
Poisson’s ratio [-] 0.26 0.25 0.3
Thermal expansion coefficient [10−5 /K] 1.55 1 1.15
Density [kg/m3 ] 7200 1550 7800
Heat capacity [J/kgK] 507 1200 460

given temperature distribution the contact problem is solved while taking the wear of the pad into account to obtain
the nodal displacements and contact pressure distribution. The new contact pressure distribution is used to update
the wear gaps. In the second part, for the obtained contact pressure distribution the energy balance is solved and new
nodal temperatures are determined. These equation systems are then solved sequentially and, wear and temperature
histories are developed. The nodal temperatures determined at a time step are taken into account in the next time
step to update the deformed geometry of the disc and pad. This is shown schematically in Fig. 2. The wear and
nodal temperature history is then written in an output file (called ODB file) by using a Python script. Details about
the governing equations can be found in [16].
Three parts are considered for the frictional heat analysis. Materials assumed for the disc and the back plate are cast
iron and steel, respectively. Friction material used as brake pad is a composite. Temperature independent material
properties used for these parts are listed in Table 1.

3. NUMERICAL RESULTS

The assembly of the disc-pad system considered in this paper is shown in Fig. 3. This is an assembly of a disc-
pad system of a heavy Volvo truck. The outer diameter and thickness of the disc are 434 [mm] and 45 [mm],
respectively. The ventilated disc is geometrically symmetric about a plane normal to the z-axis. It is assumed
that thermomechanical loads applied to the system are symmetric so only half of this assembly is considered for
the simulation and symmetry constraints are applied on the nodes lying on the symmetry plane. Some detailed
geometry at the inner radius has been removed to simplify the model as that is not important for this analysis. The
displacements along x and y directions of the nodes located at the inner radius of the disc are set to zero. All the
surfaces of the disc, except the one lying on the the symmetry plane are considered to lose heat by convection.
The brake pad is supported by a steel plate at the back side as shown in Fig. 4. Some detailed geometry of the back
plate which is not necessary for the simulation has been removed. Two cylindrical pins apply a normal force on the
back surface of the back plate which transmits it to the pad. Displacements at the back surface of the back plate,
other than along the force direction, are fixed. Furthermore temperature is set to zero on the back surface.

3
The disc is meshed such that it has smaller elements where it contacts the pad as shown in Fig. 5 (only a small
portion of the disc is shown). This is an advantage of the Eulerian approach because the finite element mesh of the
disc does not rotate relative to the brake pad but the material flows through the mesh. The heat flux generated at the
interface of the stationary pad and the disc is considered with convective heat transfer in the disc. In a Lagrangian
approach a fine mesh should be applied on the complete surface of the disc because the finite element mesh of the
disc rotates relative to the brake pad or some adaptive strategy should have to be applied. All the parts considered
for the simulation are meshed with 4-node linear tetrahedron elements in HyperMesh (HyperWorks 10.0). These
meshed parts are then used to prepare input file with boundary conditions and loads in Abaqus/CAE. The disc
assembly is meshed with 269438 elements that has 64957 nodes and 185697 degrees of freedom.
Now the results of frictional heat simulations will be described for two different cases. In the first case, a brake
application is simulated for one cycle and wear is not considered. Figure 6 shows the surface temperature as a
function of time and disc radius for this case. The nodes of the disc chosen for this plot are located at 180◦ away
from the middle of the pad. A brake force of 24.5 [kN] is applied for 45 [s] on the back surface of back plate. The
angular velocity of the disc is 45 [rad/s] and held constant throughout the simulation. This loadcase corresponds to a
truck moving downhill with a constant speed. The force is ramped up by using a log-sigmoid function during 20 time
increments and then held constant for next 70 increments with time step = 0.5 [s]. The friction coefficient is µ = 0.3,
contact conductance coefficient is ϕ = 0.1 [W/NK] and convection coefficient is set to 50 [W/m2 K]. The brake
force generates an average brake moment of 1240 [Nm] after the ramping up. The total CPU time is 4272 [s] on a
workstation with Intel Xeon X5672 3.20 GHz processor. In the graph it can be seen that temperature is not uniformly
distributed over the disc instead a narrow band with relatively higher temperature appears in approximately middle
of the disc surface.
In the second case, brake application is simulated for several cycles and material removed due to wear in each cycle
is considered in subsequent braking operations. During each brake cycle, the wear coefficient is set to 10−10 [m2 /N]
and rest of the parameters are same as for the first case. The total CPU time for a single cycle is 4289 [s] on a
workstation with Intel Xeon X5672 3.20 GHz processor. Each brake cycle requires almost the same CPU time for
each simulation. In Fig. 7, temperature of the disc surface is shown at the end of brake operation for first cycle.
A ring of high temperatures, called a hot band, is evident in the middle of the disc. Figure 8a shows the surface
temperature as a function of time and disc radius for the first cycle of brake application. The nodes of the disc
chosen for this plot are located at 180◦ away from the middle of the pad. In the graph it can be seen that during the
cycle there is only one hot band on the disc surface.
By intuition it can be thought that the high temperature ring should form near the outer radius of the disc. But
the ring appeared approximately in the middle of the disc surface. It might be understood by studying the contact
pressure plots at different time steps as shown in Fig. 10. In Fig. 10a the contact pressure plot for the first time
increment or at the moment when the pad comes into contact with the disc is shown. It can be seen that the contact
pressure is not the highest at the outer radius of the pad. The region where contact pressure is higher generates more
heat and causes further expansion of the disc and the pad material near this area which in turn causes higher contact
pressure. In the meantime convex bending caused by thermal deformation of the pad and the back plate, as shown
in Fig. 9, also plays a major role in concentration of contact pressure towards the middle of the pad surface. This

X
Z

Figure 3: An assembly of the disc-pad system, also showing the cylindrical pins used to push the back plate.

4
Back Plate Brake Pad

Figure 4: Brake pad with back plate.

convex bending can be explained by the expansion of the pad surface material due to the increase in temperatures.
The frictional heat causes the pad surface temperature to rise in a short period of time as compared to the inner
region of the pad and the back plate as shown in Fig. 9. Consequently, the surface expands more than the inner
region of the pad and the back plate which results in the convex bending. These phenomena combined with the
ramping up of brake force in later increments, causes the higher contact pressure in an area which is away from the
outer radius of disc as shown in Fig. 10d.
In Fig. 11 contact pressure plots are shown for further time steps when the brake force is held constant for the first
cycle and Fig. 12 shows the wear on the pad for corresponding time steps. It can be seen that the contact pressure
keeps on concentrating towards the middle of the pad with increasing time increments. It can also be observed that
wear is higher in the areas where contact pressure is higher.
Figure 8b shows the surface temperature as a function of time and disc radius for the 41st cycle of brake application.
It can be seen that in the beginning there are two hot bands which converge to one as the temperature increases with
time. In Figure 13 which shows temperature of the disc surface at 13th time increment for the 41st cycle of brake
application, two hot bands can be seen. In Fig. 14, temperature of the disc surface is shown at the end of brake
operation for the 41st cycle of brake application. By comparing with Fig. 7, it can be concluded that after 41 brake
cycles the maximum temperature has decreased and the hot band becomes wider at the end of brake operation. The
appearance of two bands can be explained by the shifting of high contact pressure areas. Due to the concentrated
wear in the middle of the pad during repeated brakings, a depression appears when the pad cools down and returns
to its undeformed state at the end of a brake operation. So during next brake cycle, the high contact pressure first
builds on the outer regions of the pad surface. In Fig. 15 accumulated wear of the pad is shown at the end of the
40th brake cycle. Fig. 16 shows the distribution of contact pressure during the 41st cycle. It can be seen that contact
pressure first builds on the outer regions which are less worn out and then due to thermomechanical deformations of
the pad, as discussed before, moves to the middle of the pad surface with increasing time increments. By comparing
the results of the first case with those obtained for the first brake cycle of the second case, it can be concluded that
for a pad without wear history there is no noticeable influence during braking due to wear. But accumulated wear
does have a significant influence on the distribution of temperature after some brake cycles.

4. DISCUSSION

The temperatures predicted by the in-house software have been compared with the temperatures recorded by a
thermal imaging camera during a physical test and found to be relatively higher. Moreover, two hot bands predicted
after repeated brake cycles are not as distinct as observed in the thermographs. These differences could be due
to temperature independent material data, friction coefficient, and wear coefficient used during the frictional heat
analysis. For more realistic results, temperature dependent material data should be used. Furthermore, the friction

Figure 5: Mesh of the disc.

5
1000

800

Temperature [ oC]
600

400

200
40

0 20
220 200 180 160 140 120 0
100 Time [s]
Radius [mm]

Figure 6: Temperature as a function of time and disc radius obtained by frictional heat simulation.

NT11
1121
1064
1007
950
894
837
780
723
667
610
553
496
440

Figure 7: After the brake application at the first cycle, a ring of high temperature develops on the disc surface.

coefficient of a brake pad is generally dependent on temperature, velocity and contact pressure [17] but in this work
it is assumed to be constant at µ = 0.3 to represent an average behavior. Similarly, the wear coefficient is generally
dependent on temperature and velocity [6, 18] but in this work it is assumed to be constant at 10−10 [m2 /N]. In
a very near future, we will extend this work such that a temperature dependent behavior of the friction and wear
coefficients is included in the proposed method. At present the in-house software assumes constant angular velocity
of the disc that corresponds to a vehicle moving downhill with a constant speed but in the future it could also be
extended to non-constant angular velocities.

5. CONCLUDING REMARKS
ODB: Brake3P.odb Abaqus/Standard 6.9−EF1 Mon Feb 27 12:24:27 W. Europe Standard Time 2012

In this work frictional heat analysis of a disc brake has been performed taking into account wear of a pad. This
Step: heat, Step with own NT11 data
analysis is performed in an in-house
Increment 90:software based on the Eulerian approach. It has been shown that braking
Step Time = 0.989010989011
Primary Var: NT11
history affects the evolution ofDeformed
Y
temperature
Var: not set distribution during
Deformation Scale Factor: not seta brake cycle. The analysis predicts concentrated

wear in the middle of the pad which results in the appearance of two hot bands after repeated brake cycles.
Z
X

It has been shown that other than the local factors e.g. thermal expansion, convex bending of the pad and the back
plate also plays a major role in the contact surface evolution. Phenomenon of convex bending has been described
in other works [2, 3], to the best of our knowledge, but no experimental observation or numerical simulation results
have been presented to support it. In this paper it has been shown with numerical simulations that convex bending
plays a major role in the concentration of contact pressure to the middle of pad.
This method has proved tremendously cheap in terms of computational time when compared to the Lagrangian
approach. In the future this approach can be used to study the influence of different geometries of the pad and the
disc on the maximum temperature with a reasonable simulation time. It can be very useful when studying new
designs for real disc brake systems.

6
1000 1000

800 800
Temperature [ oC]

Temperature [ oC]
600 600

400 400

200 200
40 40

0 20 0 20
220 200 220 200
180 160 180 160
140 120 0 140 120 0
100 Time [s] 100 Time [s]
Radius [mm] Radius [mm]

(a) Cycle =1 (b) Cycle =41

Figure 8: Temperature as a function of time and disc radius with the consideration of wear.

NT11
669
614
558
502
446
390
335
279
223
167
112
56
0

Figure 9: Thermally induced deformations of the pad and back plate during brake operation shown in different
projections. The deformation is exaggerated for visual clarity.

NT11 NT11
0.057 0.674
0.052 0.618
0.048 0.561
0.043 0.505
0.038 0.449
0.033 0.392
0.029 0.336
0.024 0.279
0.019 0.223
0.014 0.166
0.010 0.110
0.005 0.054
0.000 −0.003

(a) t = 0.5 s (b) t = 2.5 s


NT11 NT11
50.522 99.797
46.312 91.480
42.102 83.164
37.891 74.847
33.681 66.531
29.471 58.215
25.261 49.898
21.051 41.582
16.840 33.265
12.630 24.949
8.420 16.633
4.210 8.316
−0.000 0.000

(c) t = 7.5 s (d) t = 10 s

Figure 10: Nodal contact forces represented as pressure plots on the pad surface shown at different time steps for
the first cycle during ramping up of the brake force. The legend is given in [N].

7
ODB: Brake3P_PN.odb Abaqus/Standard 6.9−EF1 Wed Jan 25 15:03:56 W. Europe Standard Time 2012 ODB: Brake3P_PN.odb Abaqus/Standard 6.9−EF1 Wed Jan 25 15:03:56 W. Europe Standard Tim
NT11 NT11
+1.6e+02 +1.8e+02
+1.4e+02 +1.7e+02
+1.3e+02 +1.5e+02
+1.2e+02 +1.4e+02
+1.0e+02 +1.2e+02
+9.1e+01 +1.1e+02
+7.8e+01 +9.1e+01
+6.5e+01 +7.6e+01
+5.2e+01 +6.0e+01
+3.9e+01 +4.5e+01
+2.6e+01 +3.0e+01
+1.3e+01 +1.5e+01
+0.0e+00 +0.0e+00

(a) t = 17.5 s (b) t = 25 s


NT11 NT11
+2.1e+02 +2.3e+02
+1.9e+02 +2.1e+02
+1.7e+02 +1.9e+02
+1.5e+02 +1.7e+02
+1.4e+02 +1.5e+02
+1.2e+02 +1.3e+02
+1.0e+02 +1.1e+02
+8.6e+01 +9.4e+01
+6.9e+01 +7.5e+01
+5.2e+01 +5.6e+01
+3.4e+01 +3.8e+01
+1.7e+01 +1.9e+01
+0.0e+00 +0.0e+00

(c) t = 35 s (d) t = 45 s

Figure 11: Nodal contact forces represented as pressure plots on the pad surface shown at different time steps for
the first cycle while the force is held constant. The legend is given in [N].

NT11 ODB: Brake3P_PN.odb Abaqus/Standard 6.9−EF1 Mon Jan 30 15:07:46 W. Europe Standard TimeNT11
2012 ODB: Brake3P_PN.odb Abaqus/Standard 6.9−EF1 Mon Jan 30 15:07:46 W. Europe Standard Time 2012
+2.0e−06 +4.0e−06
+1.8e−06 +3.7e−06
+1.7e−06 +3.3e−06
+1.5e−06 +3.0e−06
+1.3e−06
Y Step: heat, Step with own NT11 data +2.7e−06
Y Step: heat, Step with own NT11 data
Z
+1.2e−06 Increment 35: Step Time = 0.388888888889 Z
+2.3e−06 Increment 50: Step Time = 0.555555555556
+1.0e−06 Primary Var: NT11 +2.0e−06 Primary Var: NT11
+8.3e−07 X Deformed Var: not set Deformation Scale Factor: not set +1.7e−06 X Deformed Var: not set Deformation Scale Factor: not set
+6.7e−07 +1.3e−06
+5.0e−07 +1.0e−06
+3.3e−07 +6.7e−07
+1.7e−07 +3.3e−07
+0.0e+00 +0.0e+00

(a) t = 17.5 s (b) t = 25 s


NT11 ODB: Brake3P_PN.odb Abaqus/Standard 6.9−EF1 Mon Jan 30 15:07:46 W. Europe Standard TimeNT11
2012 ODB: Brake3P_PN.odb Abaqus/Standard 6.9−EF1 Mon Jan 30 15:07:46 W. Europe Standard Time 2012
+7.0e−06 +1.0e−05
+6.4e−06 +9.2e−06
+5.8e−06 +8.3e−06
+5.3e−06 +7.5e−06
+4.7e−06
Y Step: heat, Step with own NT11 data +6.7e−06
Y Step: heat, Step with own NT11 data
Z
+4.1e−06 Increment 70: Step Time = 0.777777777778 Z
+5.8e−06 Increment 90: Step Time = 1.0
+3.5e−06 Primary Var: NT11 +5.0e−06 Primary Var: NT11
+2.9e−06 X Deformed Var: not set Deformation Scale Factor: not set +4.2e−06 X Deformed Var: not set Deformation Scale Factor: not set
+2.3e−06 +3.3e−06
+1.8e−06 +2.5e−06
+1.2e−06 +1.7e−06
+5.8e−07 +8.3e−07
+0.0e+00 +0.0e+00

(c) t = 35 s (d) t = 45 s

Figure 12: Wear on the pad surface, shown in [m], at different time steps for the first cycle.

Viewport: 1 ODB: E:/DiscBrakes/Results/No_..._Simulation_1/Brake3P.odb

NT11
ODB: Brake3P_WEAR.odb
212 Abaqus/Standard 6.9−EF1 Mon Jan 30 15:12:00 W. Europe Standard Time 2012 ODB: Brake3P_WEAR.odb Abaqus/Standard 6.9−EF1 Mon Jan 30 15:12:00 W. Europe Standard Time 2012
NT11195
177
1129
159
1071
Y Step: heat, Step with
142 own NT11 data
1014 Y Step: heat, Step with own NT11 data
Z Increment 35: Step124 Time = 0.388888888889 Z Increment 50: Step Time = 0.555555555556
Primary Var: NT11106
956 Primary Var: NT11
X
Deformed Var: not set899Deformation Scale Factor: not set X
Deformed Var: not set Deformation Scale Factor: not set
88841
71784
53726
35669
18612
0554
497
439

ODB: Brake3P_WEAR.odb Abaqus/Standard 6.9−EF1 Mon Jan 30 15:12:00 W. Europe Standard Time 2012 ODB: Brake3P_WEAR.odb Abaqus/Standard 6.9−EF1 Mon Jan 30 15:12:00 W. Europe Standard Time 2012

Y Step: heat, Step with own NT11 data Y Step: heat, Step with own NT11 data
Z Increment 70: Step Time = 0.777777777778 Z Increment 90: Step Time = 1.0
Primary Var: NT11 Primary Var: NT11
X X
Deformed Var: not set Deformation Scale Factor: not set Deformed Var: not set Deformation Scale Factor: not set

Figure 13: Two bands of high temperatures on the disc surface at t = 6.5 [s] during the 41st cycle of brake application.

8
Viewport: 1 ODB: E:/DiscBrakes/Results/No_..._Simulation_1/Brake3P.odb

NT11
1011
NT11963
914
1129
866
1071
818
1014
770
956
721
899
673
841
625
784
577
726
528
669
480
612
432
554
497
439

Figure 14: After the brake application at the 41st cycle, a ring of high temperatures develops on the disc surface.

NT11
169E−06
155E−06
141E−06
127E−06
113E−06
99E−06
85E−06
70E−06
56E−06
42E−06
28E−06
14E−06
0E+00
ODB: Brake3P.odb Abaqus/Standard 6.9−EF1 Wed Feb 01 14:29:11 W. Europe Standard Time 2012

ODB: Brake3P.odb Abaqus/Standard 6.9−EF1 Thu Jan 26 08:56:30 W. Europe Standard Time 2012
Step: heat, Step with own NT11 data
Increment 90: Step Time = 0.989010989011
Primary Var: NT11
Figure 15: Accumulated wear on the pad surface, shown in [m], at the end of the 40th cycle.
Y
Deformed Var: not set Deformation Scale Factor: not set
Step: heat, Step with own NT11 data
Z
X Increment 90: Step Time = 0.989010989011
Primary Var: NT11
Y
Deformed Var: not set Deformation Scale Factor: not set
Z
X

NT11 NT11
21.759 61.269
19.946 56.163
18.133 51.057
16.320 45.952
14.506 40.846
12.693 35.740
10.880 30.634
9.066 25.529
7.253 20.423
5.440 15.317
3.627 10.211
1.813 5.106
0.000 0.000

(a) t = 5 s (b) t = 15 s
NT11 NT11
77.166 145.546
70.736 ODB: Brake3P_WEAR.odb Abaqus/Standard 6.9−EF1
133.417 Wed Feb 01 14:19:08 W. Europe Standard Time 2012
64.305 121.288
57.875 109.159
51.444 97.030
45.014 84.902
38.583 Step: heat, Step with own NT11 data 72.773
Y
32.153 60.644
25.722
Z Increment 1: Step Time = 0.0111111111111 48.515
19.292 Primary Var: NT11 36.386
12.861 X 24.258 not set
Deformed Var: not set Deformation Scale Factor:
6.431 12.129
0.000 0.000

(c) t = 30 s (d) t = 45 s

Figure 16: Nodal contact forces represented as pressure plots on the pad surface shown at different time steps for
the 41st cycle. The legend is given in [N].

ODB: Brake3P_PN.odb Abaqus/Standard 6.9−EF1 Wed Feb 01 14:15:36 W. Europe Standard Time 2012 ODB: Brake3P_PN.odb Abaqus/Standard 6.9−EF1 Wed Feb 01 14:15:36 W. Europe Standard Time 2012

Z
Y Step: heat, Step with own NT11 data
Increment 10: Step Time = 0.111111111111
9 Z
Y Step: heat, Step with own NT11 data
Increment 30: Step Time = 0.333333333333
Primary Var: NT11 Primary Var: NT11
X X
Deformed Var: not set Deformation Scale Factor: not set Deformed Var: not set Deformation Scale Factor: not set
6. ACKNOWLEDGEMENT
This project was financed by Vinnova (FFI-Strategic Vehicle Research and Innovation) and Volvo 3P.

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