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International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME
521
DRY SLIDING STUDIES OF POROSITY ON SINTERED CU-BASED
BRAKE MATERIALS
Glenn Kwabena GYIMAH1,a
*, Dong CHEN1,b
, Ping HUANG1,c,
School of Mechanical and Automotive Engineering, South China University of Technology,
Guangzhou, 510640, P. R. China.1
ABSTRACT
Cu-based composites with its promising engineering application due to their excellent
thermophysical properties coupled with better high temperature mechanical properties as
compared to pure copper and copper alloys. An investigation on a Cu-based composite
frictional material re-inforced with other elements for train brake was treated under P/M route
for its wear behavior in terms of sintering temperature and porosity. The dry sliding wear
characteristics investigation test with a high pressure pad-on-disc tester was developed for the
three different sintering temperatures samples. The optimal porosity was obtained at the
highest sintering temperature of 950o
C. That same optimal porosity gave the lowest wear
frictional coefficient, and the highest coefficient of friction. Three forms of wear mechanisms
were observed during the dry sliding process, namely, delamination wear, plowing wear and
abrasive wear. High wear rates were found on samples sintered at 850o
C and 900o
C. Abrasive
wear and the delamination wear were the main cause of high wear coefficient, low wear
number and low coefficient of friction. The nature of abrasive surfaces observed were
classified into three divisions, namely, smooth abrasive surfaces; rough abrasive surface; and
the highly abrasive surface. The dominance of wear is discussed in the light of SEM
photography of the worn surfaces.
Keywords: Brake materials; Wear; Porosity; Wear mechanism; Sintering temperature.
INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING
AND TECHNOLOGY (IJMET)
ISSN 0976 – 6340 (Print)
ISSN 0976 – 6359 (Online)
Volume 4, Issue 2, March - April (2013), pp. 521-529
© IAEME: www.iaeme.com/ijmet.asp
Journal Impact Factor (2013): 5.7731 (Calculated by GISI)
www.jifactor.com
IJMET
© I A E M E
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME
522
1. INTRODUCTION
Recently, much attention has been given to the effect of porosity on Cu-based matrix
composites, due to its indispensable influence on tribological and mechanical behavior of
sintered composites. The influence of Porosity is very high in the determination of a
material’s application. The porosity of material influences its ability to withstand wear since
it has an impact on the properties of the Cu-based composite material. In view of this, powder
metallurgist has devoted much into minimized porosity because of higher porosity results in
lower values in all mechanical properties of sintered steels. [1] In comparison with the
numerous studies concerned with other mechanical properties, the influence of porosity on
wear behavior of sintered steels has not been extensively investigated. [1] The principal
factors that influence the sliding wear of the composites include: extrinsic factors such as
sliding distance, sliding velocity, applied load, atmosphere temperature, etc. and intrinsic
factors such as reinforcement type, shape, size, volume fraction and distribution, interface
between reinforcement and matrix, matrix material, heat treatment, porosity, etc. [2] The use
of different copper and nickel particle sizes provided the ability to modify the porosity size
and spacing. [3] Lee et al. [4] studied the effect of sintered porosity in powder metallurgy
(PM) 6061 monolithic alloy and 6061: SiCp composites on dry abrasive wear, indicating that
the wear rate of 6061 alloy increases drastically with increasing porosity, while for its
composites, the porosity effect is not significant.
The effect of porosity on the wear and friction of metals has been studied by
Vardavoulias et al. [5]. They claimed that the pores enhance the surface roughness of the
materials and decrease the real area of contact between two sliding surfaces and consequently
increase the contact pressure and promote particle detachment during sliding. Suh [6] has
argued that the increase in porosity content of the composite reduces the required length of
crack propagation to link-up with other cracks in order to cause delamination. Thus, porosity
decreases the wear resistance and coefficient of friction of the composite. For different
sintered composites materials those effects are not constant depending on factors such as the
composition and heat treating condition. Therefore, until now, it has been very difficult to
make a universal conclusion about the influence of pores on various sintered materials.
In this paper, a careful evaluation of the samples wear behavior before and after
practical application was done. The influence of sintering temperature on the porosity during
the dry sliding wear behavior of sintered novel Cu-based composite train brake material was
investigated.
2. EXPERIMENTAL DETAILS
2.1 Sample preparation
The specimens used for this study are made by powder metallurgy technique, which
process includes mixing, compacting and sintering. The first step was the selection of powder
materials categorized under based metal as the matrix, frictional components, lubricants and
alloying elements. These were based on the outcome of Kryachek [7] review and Yao et
al[8,9]. The newly developed bronze based brake pad powder material with its chemical
composition is given in Table 1.
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME
523
Table 1. Chemical compositions of material in mass (wt. %)
Ingt: Matrix Frictional
component
Lubricant component Alloying
element
Cu (SiO2 & Fe) (Graphite &MoS2) (Mn & Sn)
Wt%. 50-60 15-20 15-20 5.0
The powders listed in Table 1 were weighed in a Sartorius BS224 S (Max 220g
d=0.0001g) with their given proportion, the well prepared powder were mixed in a V-cone
mixer or double cone mixture machine. The rotating speed of double cone mixture was
maintained at 150 rpm for nine hours. After the mixing process, the mixtures were compacted
in a hardened steel die using a hydraulic press machine (SANS DCS-300 Digital Hydraulic
Compacting machine) under the pressure of 650Mpa.
The compacts were subsequently transferred into a sintering furnace for sintering. The
sintering took 90 mins in a controlled atmosphere furnace saturated with carbon at 850-950o
C
at 0.01MPa constant pressure. The sintered materials were then driven out when oil-cooled.
Finally, the resulting rectangular bar with thickness of 5mm was cut and grounded to a size of
14mm × 14mm test specimens. Nine pairs of specimens were prepared for the friction and
wear test.
2.2 Testing Procedures
I. Characterisation test
The density of friction materials was determined according to a procedure proposed in
ASTM D792, which is based on Archimedes’ principle. This was done on all the samples at
different sintering temperatures and the average results are recorded in Table 3a.
A digital microhardness tester HVS - 1000 instrument was used for the hardness and the
hardness values were taken in the Vickers scale using 10N within 20 seconds. Prior to the
hardness test, the samples were ground and polished with sand paper of grit 180, 240, 320,
600, 800, 1000, and 1200 successively, and were also cleaned in alcohol in an ultrasonic
cleaner. For each specimen, the hardness measurements were repeated ten times and an
average of the ten was taken.
A microstructure and tribosurfaces analysis was carried out with OM and SEM. An
optical microscope (OM) and a scanning electron microscope (SEM) were employed to
examine microstructures of the specimen before and after the wear test. The surfaces of the
specimens were first polished with sand paper of grit 180, 240, 320, 600, 800, 1000, and 1200
successively, followed by two polishing stages of 3µm and 0.05µm, respectively. The OM
and the SEM helped analyze the nature of the microstructure for the likely pores available
and the wear surfaces, and they were done both before and after the wear test.
II. PERFORMANCE TEST
The schematic diagram of the test rig is shown in Figure 1. During the tribotests, the
performance test includes the determination of coefficient of friction, friction force, wear loss
and type of wear. These were tested according to the China National Standard GB5763-1998
using an X-MSM Constant Speed Friction Material Tester with constant speed 7.54ms−1 and
constant pressure 3.13MPa. As a rotor, the disc made of cast iron (grade HTA5/HB with
Brinell hardness in the range of 196) was used. The test rig is composed of the following
parts: the control and monitoring unit; the disc; and the sample holder. The friction test was
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME
524
performed at these selected temperatures (150, 200, 250, 300 and 350o
C). Two specimens
were pressed against a gray cast iron rotating disk with a total contact area of approximately
3.92cm2
and rotated for 5000 revolution. The machine was originally made to apply 0.98MPa
and cover 25×25mm of surface area. Modification of the sample holder was done, reducing
the surface area to 14×14 mm and thereby increasing the pressure on the sample to 3.13MPa.
The friction coefficient data was obtained automatically by the tester. Five sample
pairs were tested for each specimen and an average of the experimental data was taken as the
result. The wear coefficient k in mm3
N−1
m−1
was calculated after 5000 revolutions of the
disc. Since the system cannot measure the wear loss directly, the volume wear rate by pad-on-
disk wear testing (ASTM G99-95a) was used.
Figure 1 Schematic Diagram of Test Rig
It is now generally recognized that materials suitable for unlubricated tribological
application (e.g. bearing, brake, wheel/rail, cam/tappet, piston/cylinder, work piece/tool, etc.)
under the operating conditions (load Fa, speed v, temperature T, operating duration t, sliding
distance s), various friction and wear processes may occur and must fulfill the following
criteria:[13]
.
.
distslidingload
volumewear
coeffwear
×
= (1)
afforcefrictionaverage
changevolume
Rn
k
,2
1
×=
π
(2)
the volume change is A(d1-d2).
where R is the distance from the center of the rotating disk to the center of the
specimen (=0.15m), n is the number of rotations of the disk during testing (5,000 rev), A is
the area of the specimen (196mm2
), d1 is the average thickness of the specimen before the
experiment (mm), d2 is the average thickness of specimen after the experiment (mm), and fa
is the automatically obtained average force of sliding friction (N) from the test rig. They were
obtained at temperatures of 100, 150, 200, 250, 300 and 350o
C, respectively. The test rig was
equipped with a temperature control unit with a pump to circulate water under the disc to
maintain a controlled temperature. The average force was also recorded from the test rig at
every operating temperature. The volume change was obtained by calculating the difference
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME
525
between initial volume before test and the final volume after test. These and the other
parameters of the test rig were entered into equation (2) to obtain the results in Table 3.
Also, wear numbers were also adopted. These were calculated, and used as a means of
knowing the wear resistance level of the design material. The mass of the specimen was
measured before and after the wear test to obtain the mass loss after 5,000 revolutions, at
temperatures of 100, 150, 200, 250, 300 and 350o
C, respectively. The densities were obtained
by the procedure proposed by ASTM D792 after the tribo test. This was done and the wear
number was obtained as:
VolumelossMass
Density
WnumberWear n
1
)( == (3)
where Wn is the wear number. Physically, it is per unit volume of the sample. The
higher the wear number, the more effective the wear resistance of the material [17]. The
results are tabulated in Table 3.
General porosity means the fraction of pore volume to the total volume. The porosity
calculations were done using equation (4) after obtaining the various densities.
1001, ×





−=
t
PPorosity
ρ
ρ
(4)
where, P is the porosity, ρ is the density of brake material and ρt is the density of
corresponding bulk material.
III. TEST CONDITION
All tests were done under strict laboratory environmental and experimental standards.
During the experiments, a constant rotation of 480rpm was maintained (sliding velocities of
7.54ms-1
); and the constant pressure was 3.13MPa based on the surface area of the specimen.
The test rig is equipped with a temperature controlling unit with a pump to circulate water
under the disc to maintain a controlled temperature.
1. RESULTS AND DISCUSSION
3.1. Porosity Effect on Friction and Worn surface
The effect of porosity and the sintering temperature on friction and worn surfaces of
the sintered Cu-based composite rubbing against a rotor, the disk made of cast iron (grade
HTA5/HB with Brinell hardness in the range 196), are shown at figure 3. The worn surfaces
of the composite specimen and wear debris were examined by SEM. The operating condition
for pressure and sliding speed for all the samples are 3.13MPa and 7.4m/s.
The typical SEM microphotographs of the worn surface for Cu-based composite are shown in
Figure 3(a) to (c). The sections marked A on the microphotograph indicates the destructive
wear sections during the tribo testing. The B sections are the relatively medium wear
surfaces, which indicate mild wear occurred during sliding. The section C has low wear
surface, glassy luster and integrated friction film, which shows this section has better wear
resistance property. The surface sintered at 850o
C (a) containing 17.53% porosity, shows
abrasive scratches, indicating abrasive wear. The groove (in a) reveals plowing wear also
occurred during sliding; this is material displacement to the side of the wear track. The
surface sintered at 900o
C (b) containing 15.82% porosity, shows flake-like fragments, and
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME
526
pits. These are a result of stress caused by high pressure exerted on the material during
operation which results in delamination wear of medium-large flake-like fragments. The
larger the flakes the more severe the delamination and therefore the greater the rate of wear
observed. The surface (c), sintered at 950 o
C containing 14.04% porosity, shows iron
particles rich in carbon on the surface. The iron rich carbon formation increased resistance to
wear and this resulted in a very smooth surface as shown.
The higher the porosity value of the samples, the lower coefficient of friction, lower
wear number and high wear coefficient resulting to high volume loss.
From the discussions above, the general observation of the worn surfaces may be grouped
into three types; namely, destructive wear (found mostly on (a) and (b)); medium wear
(mostly on (a) and (c)); and low wear (only on (c)).
Fig. 3 Shows cross-sectional SEM micrograph of the nature of smoothness of friction
surfaces at different sintering temperatures: (a) 850o
C, (b) 900o
C and (c) 950o
C.
3.2. Porosity Effect on Hardness and Wear
Table 2 shows the physical properties of the Cu-based composite. The wear rate
changes through the repeated contact process under constant load and velocity (3.13PMa and
7.54m/s respectively) [10]. Wear rates are often quoted in terms of a wear coefficient or
dimensionless wear coefficient as derived from the Archard treatment of wear processes [11].
The average hardness values measured with a Vickers hardness tester (Table 3) on all the
materials shows a similar tendency as the results of the sintering as shown in Figure 3. The
materials with less porosity and sintered at high sintering temperature exhibited high hardness
as shown in Table 3 with low porosity at low sintering temperature. This confirmed the fact
that, porosity influences the hardness, and therefore, affects the rate of wear of the material.
From the same table, the wear rate was also greatly affected by the porosity values obtained
at their respective sintering temperatures.
The wear volume rate (Vw) is calculated as shown in equation (1); where K is the wear
coefficient (dimensionless), W the normal load and H the hardness. The Archard treatment of
wear has been shown to be valid for cases where mechanical influences are dominant [12].
Wear is often associated with hardness of the materials in contact. Basically, the harder the
material, the more wear resistant it is, but it is also more brittle and therefore more sensitive
to the detachment of particles. According to Table 3, the lowest wear rate was observed at the
950o
C sintered material. This could be attributed to the fact that there was sufficient heating
to reduce porosity, which also brought about increase in hardness to optimize the wear
properties of the material.
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME
527
Table 2 Physical properties of Cu-based composite
Rule Of Mixture
( )3
. −
cmgtρ 3
.973.7 −
cmg
Experiment Data
Average ( )3
. −
cmgρ 6.714 3
. −
cmg
Average Microhardness (HV) 294
Average Porosity %, 





−=
t
P
ρ
ρ
1 15.79%
Table 3. Properties of the Cu-based composite material
Sint.
Tem.
Tsin
Density, ρ Porosity, P Hardness,
Hv
Wear Coeff.
k
Wear num.
Wn
Coeff.
Frict. µ
850o
C 6.51 17.53 272 0.000154 8.7191 0.336
900o
C 6.71 15.82 287 0.000166 9.8499 0.343
950o
C 6.85 14.04 304 0.000044 10.128 0.404
3.3. Abrasive Surfaces Classification
In view of the advancement of technology, the application of computer-based
technology and image-processing methods have lead to a fully automated classification
system of tribological surfaces. Such a system has been useful in classifying (i) surfaces
during manufacturing processes (quality control), (ii) wear surfaces in the failure analysis of
engineering components, or (iii) wear particles in machine condition monitoring. The hybrid
fractal-wavelet method is used here to demonstrate how an unknown abrasive surface can be
classified into one of three classes of abrasive surfaces [13]. 3-D surface morphology images
are shown in Figure 4 to identify the different kinds of abrasive surfaces.
In Figure 4, our investigation shows that the abrasive surfaces can be classified into
three divisions, named as smooth abrasive surface (mirror surface and integrated friction
film) which has better wear resistance property because it demonstrated minimal wear rate,
rough abrasive surface (rough surface) indicates moderate wear rate and a highly abrasive
surface (much rough surface) showing excessive wear. Examples of the 3-D surface
morphology images of the surface from each division are shown in Figure 4.
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME
528
Figure 4 shows 3-D surface morphology images of the surface (a) at 850 o
C, (b) at 900 o
C
and (c) at 950 o
C.
The (a) is observed to be the one with a highly abrasive surface; this is as a result of
having fewer peaks that are ironic or hard to withstand pressure from the braking system. The
(b) was also observed as the rough abrasive surface with moderate peaks withstanding the
exerted pressure of the braking system. The (c) is the one that was observed as having enough
ironic peaks to withstand the exerted pressure and therefore given a smooth abrasive surface.
4. CONCLUSION
The wear resistance properties of the novel Cu-based composite material against a
cast iron disc (grade HTA5/HB with Brinell hardness in the range 196) tested under a full
laboratory condition, reveals a strong influence of porosity over the mechanical and
tribological characteristics of the material. Investigation and observations concerning the
effect of porosity on the mechanical and tribological characteristics have led to the following
conclusions:
The porosity level affects the mechanical properties. High porosity is not the best if
optimizing the performance of the novel material, which leads to weakening of the materials
as a result of low sintering temperatures but this can be further improved and considered for
manufacturing commercial brake pads. On the other hand, low porosity samples gave a high
resistance to wear. This was as a result of the high sintering temperature which ensured
complete diffusion.
Much lower wear coefficient, high wear number and high coefficient of friction were
obtained at low porosity samples (14.04% at 950o
C) tested. These show high resistance to
wear; given good tribological characteristics and good mechanical properties.
The dominant wear mechanisms found were plowing, delamination and abrasive
wear. Abrasive wear and the delamination wear were the main cause of high wear coefficient,
low wear number and low coefficient of friction. The nature of abrasive surfaces observed
were classified into three divisions, namely, smooth abrasive surfaces (mirror surface and
integrated friction film) which has better wear resistance properties because it demonstrates
minimal wear rate; the rough abrasive surface (rough surface) indicates moderate wear rate;
and lastly, the highly abrasive surface (much rough surface) showing excessive wear and has
a high degree of surface destruction. This is as a result of the rate of wear that occurred
during the dry sliding.
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME
529
5. ACKNOWLEDGMENT
We are grateful to the staff of The Key Laboratory of Specially Functional Materials
and Advanced Manufacturing Technology, Ministry of Education, South China University of
Technology. We are also value the support of the staff of the Analytical and Testing Center
of South China University of Technology particularly Prof. Zhang Da Xue and Mr. Zhu Fan
Kang (Chang Zhang) where we carried out the Experiments and the test.
6. REFERENCES
[1] J. Wang, Y. He, and H. Danninger, Influence of Porosity on the Sliding Wear Behavior
of Sintered Fe-1.5Mo-0.7C Steels, ASM International, JMEPEG (2003) 12:339-344
[2] M. Gui, S. B. Kang, J. M. Lee, Influence of porosity on dry sliding wear behavior in
spray deposited Al–6Cu–Mn:SiCp composite, Materials Science and Engineering,
A293 (2000) 146–156
[3] T. M. Cimino, A. H. Graham and T. F. Murphy, The effect of microstructure and pore
morphology on mechanical and dynamic properties of ferrous P/M materials, Presented
at pM2TEC '98
[4] H.L. Lee, W.H. Lu, S.L. Chan, Abrasive wear of powder metallurgy Al alloy 6061-SiC
particle composites. Wear 159 (1992) 223
[5] M. Vardavoulias, C. Jouannt-Tresy, M. Jeandin, Sliding wear behaviour of ceramic
particle reinforced high-speed steel obtained by powder metallurgy, Wear 165 (1993)
141–149.
[6] N.P. Suh, An Overview of the Delamination Theory of Wear, Wear 44 (1977) 1–16.
[7] V. M. Kryachek, Sintered Metals and Alloys Friction Composites: Traditions and New
Solutions (Review). Powder Materials, Powder Metallurgy and Metal Ceramics, Vol.
43, Nos. 11-12, 2004 Spring Science + Business Media, Inc.
[8] Xiong X., Sheng H, Chen J, Yao P, Effects Of Sintering Pressure And Temperature on
Microstructure and Tribological Characteristic of Cu-Based Aircraft Brake Material,
Trans. Nonferrous Met. Soc. China 17(2007) 669-675
[9] Yao P, Sheng H, Xiong X., Huang B., Worn Surface Characteristics of Cu-Based
Powder Metallurgy Brake for Aircraft, Trans. Nonferrous Met. Soc. China 17(2007) 99-
103.
[10] Kato K,. Classification of Wear Mechanisms/Models, Wear – Materials, Mechanisms
and Practice, Edited by G. Stachowiak , 2005, 9-20,.
[11] Williams J. A., Engineering Tribology Oxford Science Publications, Oxford University
Press, New York 1994.
[12] Neville A. and Morina A., Wear and Chemistry of Lubricants, Wear – Materials,
Mechanisms and Practice, Edited by G. Stachowiak , 2005, 71-94.
[13] G. W. Stachowaik, G. B. Stachowiak, D. De Pellegrin, P. Posiadlo. Characterization
and Classification of Abrasive Particles and Surfaces, Wear–materials, mechanisms and
practice. Edited by G. Stachowiak 2005 339-368.
[14] ASTM B611.
[15] P. Kurmi, S. Rathod and P. Jain, “Abrasive Wear Behavior of 2014al-Tic in Situ
Composite”, International Journal of Mechanical Engineering & Technology (IJMET),
Volume 3, Issue 3, 2012, pp. 229 - 240, ISSN Print: 0976 – 6340, ISSN Online:
0976 – 6359.

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Dry sliding studies of porosity on sintered cu based brake materials

  • 1. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME 521 DRY SLIDING STUDIES OF POROSITY ON SINTERED CU-BASED BRAKE MATERIALS Glenn Kwabena GYIMAH1,a *, Dong CHEN1,b , Ping HUANG1,c, School of Mechanical and Automotive Engineering, South China University of Technology, Guangzhou, 510640, P. R. China.1 ABSTRACT Cu-based composites with its promising engineering application due to their excellent thermophysical properties coupled with better high temperature mechanical properties as compared to pure copper and copper alloys. An investigation on a Cu-based composite frictional material re-inforced with other elements for train brake was treated under P/M route for its wear behavior in terms of sintering temperature and porosity. The dry sliding wear characteristics investigation test with a high pressure pad-on-disc tester was developed for the three different sintering temperatures samples. The optimal porosity was obtained at the highest sintering temperature of 950o C. That same optimal porosity gave the lowest wear frictional coefficient, and the highest coefficient of friction. Three forms of wear mechanisms were observed during the dry sliding process, namely, delamination wear, plowing wear and abrasive wear. High wear rates were found on samples sintered at 850o C and 900o C. Abrasive wear and the delamination wear were the main cause of high wear coefficient, low wear number and low coefficient of friction. The nature of abrasive surfaces observed were classified into three divisions, namely, smooth abrasive surfaces; rough abrasive surface; and the highly abrasive surface. The dominance of wear is discussed in the light of SEM photography of the worn surfaces. Keywords: Brake materials; Wear; Porosity; Wear mechanism; Sintering temperature. INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING AND TECHNOLOGY (IJMET) ISSN 0976 – 6340 (Print) ISSN 0976 – 6359 (Online) Volume 4, Issue 2, March - April (2013), pp. 521-529 © IAEME: www.iaeme.com/ijmet.asp Journal Impact Factor (2013): 5.7731 (Calculated by GISI) www.jifactor.com IJMET © I A E M E
  • 2. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME 522 1. INTRODUCTION Recently, much attention has been given to the effect of porosity on Cu-based matrix composites, due to its indispensable influence on tribological and mechanical behavior of sintered composites. The influence of Porosity is very high in the determination of a material’s application. The porosity of material influences its ability to withstand wear since it has an impact on the properties of the Cu-based composite material. In view of this, powder metallurgist has devoted much into minimized porosity because of higher porosity results in lower values in all mechanical properties of sintered steels. [1] In comparison with the numerous studies concerned with other mechanical properties, the influence of porosity on wear behavior of sintered steels has not been extensively investigated. [1] The principal factors that influence the sliding wear of the composites include: extrinsic factors such as sliding distance, sliding velocity, applied load, atmosphere temperature, etc. and intrinsic factors such as reinforcement type, shape, size, volume fraction and distribution, interface between reinforcement and matrix, matrix material, heat treatment, porosity, etc. [2] The use of different copper and nickel particle sizes provided the ability to modify the porosity size and spacing. [3] Lee et al. [4] studied the effect of sintered porosity in powder metallurgy (PM) 6061 monolithic alloy and 6061: SiCp composites on dry abrasive wear, indicating that the wear rate of 6061 alloy increases drastically with increasing porosity, while for its composites, the porosity effect is not significant. The effect of porosity on the wear and friction of metals has been studied by Vardavoulias et al. [5]. They claimed that the pores enhance the surface roughness of the materials and decrease the real area of contact between two sliding surfaces and consequently increase the contact pressure and promote particle detachment during sliding. Suh [6] has argued that the increase in porosity content of the composite reduces the required length of crack propagation to link-up with other cracks in order to cause delamination. Thus, porosity decreases the wear resistance and coefficient of friction of the composite. For different sintered composites materials those effects are not constant depending on factors such as the composition and heat treating condition. Therefore, until now, it has been very difficult to make a universal conclusion about the influence of pores on various sintered materials. In this paper, a careful evaluation of the samples wear behavior before and after practical application was done. The influence of sintering temperature on the porosity during the dry sliding wear behavior of sintered novel Cu-based composite train brake material was investigated. 2. EXPERIMENTAL DETAILS 2.1 Sample preparation The specimens used for this study are made by powder metallurgy technique, which process includes mixing, compacting and sintering. The first step was the selection of powder materials categorized under based metal as the matrix, frictional components, lubricants and alloying elements. These were based on the outcome of Kryachek [7] review and Yao et al[8,9]. The newly developed bronze based brake pad powder material with its chemical composition is given in Table 1.
  • 3. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME 523 Table 1. Chemical compositions of material in mass (wt. %) Ingt: Matrix Frictional component Lubricant component Alloying element Cu (SiO2 & Fe) (Graphite &MoS2) (Mn & Sn) Wt%. 50-60 15-20 15-20 5.0 The powders listed in Table 1 were weighed in a Sartorius BS224 S (Max 220g d=0.0001g) with their given proportion, the well prepared powder were mixed in a V-cone mixer or double cone mixture machine. The rotating speed of double cone mixture was maintained at 150 rpm for nine hours. After the mixing process, the mixtures were compacted in a hardened steel die using a hydraulic press machine (SANS DCS-300 Digital Hydraulic Compacting machine) under the pressure of 650Mpa. The compacts were subsequently transferred into a sintering furnace for sintering. The sintering took 90 mins in a controlled atmosphere furnace saturated with carbon at 850-950o C at 0.01MPa constant pressure. The sintered materials were then driven out when oil-cooled. Finally, the resulting rectangular bar with thickness of 5mm was cut and grounded to a size of 14mm × 14mm test specimens. Nine pairs of specimens were prepared for the friction and wear test. 2.2 Testing Procedures I. Characterisation test The density of friction materials was determined according to a procedure proposed in ASTM D792, which is based on Archimedes’ principle. This was done on all the samples at different sintering temperatures and the average results are recorded in Table 3a. A digital microhardness tester HVS - 1000 instrument was used for the hardness and the hardness values were taken in the Vickers scale using 10N within 20 seconds. Prior to the hardness test, the samples were ground and polished with sand paper of grit 180, 240, 320, 600, 800, 1000, and 1200 successively, and were also cleaned in alcohol in an ultrasonic cleaner. For each specimen, the hardness measurements were repeated ten times and an average of the ten was taken. A microstructure and tribosurfaces analysis was carried out with OM and SEM. An optical microscope (OM) and a scanning electron microscope (SEM) were employed to examine microstructures of the specimen before and after the wear test. The surfaces of the specimens were first polished with sand paper of grit 180, 240, 320, 600, 800, 1000, and 1200 successively, followed by two polishing stages of 3µm and 0.05µm, respectively. The OM and the SEM helped analyze the nature of the microstructure for the likely pores available and the wear surfaces, and they were done both before and after the wear test. II. PERFORMANCE TEST The schematic diagram of the test rig is shown in Figure 1. During the tribotests, the performance test includes the determination of coefficient of friction, friction force, wear loss and type of wear. These were tested according to the China National Standard GB5763-1998 using an X-MSM Constant Speed Friction Material Tester with constant speed 7.54ms−1 and constant pressure 3.13MPa. As a rotor, the disc made of cast iron (grade HTA5/HB with Brinell hardness in the range of 196) was used. The test rig is composed of the following parts: the control and monitoring unit; the disc; and the sample holder. The friction test was
  • 4. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME 524 performed at these selected temperatures (150, 200, 250, 300 and 350o C). Two specimens were pressed against a gray cast iron rotating disk with a total contact area of approximately 3.92cm2 and rotated for 5000 revolution. The machine was originally made to apply 0.98MPa and cover 25×25mm of surface area. Modification of the sample holder was done, reducing the surface area to 14×14 mm and thereby increasing the pressure on the sample to 3.13MPa. The friction coefficient data was obtained automatically by the tester. Five sample pairs were tested for each specimen and an average of the experimental data was taken as the result. The wear coefficient k in mm3 N−1 m−1 was calculated after 5000 revolutions of the disc. Since the system cannot measure the wear loss directly, the volume wear rate by pad-on- disk wear testing (ASTM G99-95a) was used. Figure 1 Schematic Diagram of Test Rig It is now generally recognized that materials suitable for unlubricated tribological application (e.g. bearing, brake, wheel/rail, cam/tappet, piston/cylinder, work piece/tool, etc.) under the operating conditions (load Fa, speed v, temperature T, operating duration t, sliding distance s), various friction and wear processes may occur and must fulfill the following criteria:[13] . . distslidingload volumewear coeffwear × = (1) afforcefrictionaverage changevolume Rn k ,2 1 ×= π (2) the volume change is A(d1-d2). where R is the distance from the center of the rotating disk to the center of the specimen (=0.15m), n is the number of rotations of the disk during testing (5,000 rev), A is the area of the specimen (196mm2 ), d1 is the average thickness of the specimen before the experiment (mm), d2 is the average thickness of specimen after the experiment (mm), and fa is the automatically obtained average force of sliding friction (N) from the test rig. They were obtained at temperatures of 100, 150, 200, 250, 300 and 350o C, respectively. The test rig was equipped with a temperature control unit with a pump to circulate water under the disc to maintain a controlled temperature. The average force was also recorded from the test rig at every operating temperature. The volume change was obtained by calculating the difference
  • 5. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME 525 between initial volume before test and the final volume after test. These and the other parameters of the test rig were entered into equation (2) to obtain the results in Table 3. Also, wear numbers were also adopted. These were calculated, and used as a means of knowing the wear resistance level of the design material. The mass of the specimen was measured before and after the wear test to obtain the mass loss after 5,000 revolutions, at temperatures of 100, 150, 200, 250, 300 and 350o C, respectively. The densities were obtained by the procedure proposed by ASTM D792 after the tribo test. This was done and the wear number was obtained as: VolumelossMass Density WnumberWear n 1 )( == (3) where Wn is the wear number. Physically, it is per unit volume of the sample. The higher the wear number, the more effective the wear resistance of the material [17]. The results are tabulated in Table 3. General porosity means the fraction of pore volume to the total volume. The porosity calculations were done using equation (4) after obtaining the various densities. 1001, ×      −= t PPorosity ρ ρ (4) where, P is the porosity, ρ is the density of brake material and ρt is the density of corresponding bulk material. III. TEST CONDITION All tests were done under strict laboratory environmental and experimental standards. During the experiments, a constant rotation of 480rpm was maintained (sliding velocities of 7.54ms-1 ); and the constant pressure was 3.13MPa based on the surface area of the specimen. The test rig is equipped with a temperature controlling unit with a pump to circulate water under the disc to maintain a controlled temperature. 1. RESULTS AND DISCUSSION 3.1. Porosity Effect on Friction and Worn surface The effect of porosity and the sintering temperature on friction and worn surfaces of the sintered Cu-based composite rubbing against a rotor, the disk made of cast iron (grade HTA5/HB with Brinell hardness in the range 196), are shown at figure 3. The worn surfaces of the composite specimen and wear debris were examined by SEM. The operating condition for pressure and sliding speed for all the samples are 3.13MPa and 7.4m/s. The typical SEM microphotographs of the worn surface for Cu-based composite are shown in Figure 3(a) to (c). The sections marked A on the microphotograph indicates the destructive wear sections during the tribo testing. The B sections are the relatively medium wear surfaces, which indicate mild wear occurred during sliding. The section C has low wear surface, glassy luster and integrated friction film, which shows this section has better wear resistance property. The surface sintered at 850o C (a) containing 17.53% porosity, shows abrasive scratches, indicating abrasive wear. The groove (in a) reveals plowing wear also occurred during sliding; this is material displacement to the side of the wear track. The surface sintered at 900o C (b) containing 15.82% porosity, shows flake-like fragments, and
  • 6. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME 526 pits. These are a result of stress caused by high pressure exerted on the material during operation which results in delamination wear of medium-large flake-like fragments. The larger the flakes the more severe the delamination and therefore the greater the rate of wear observed. The surface (c), sintered at 950 o C containing 14.04% porosity, shows iron particles rich in carbon on the surface. The iron rich carbon formation increased resistance to wear and this resulted in a very smooth surface as shown. The higher the porosity value of the samples, the lower coefficient of friction, lower wear number and high wear coefficient resulting to high volume loss. From the discussions above, the general observation of the worn surfaces may be grouped into three types; namely, destructive wear (found mostly on (a) and (b)); medium wear (mostly on (a) and (c)); and low wear (only on (c)). Fig. 3 Shows cross-sectional SEM micrograph of the nature of smoothness of friction surfaces at different sintering temperatures: (a) 850o C, (b) 900o C and (c) 950o C. 3.2. Porosity Effect on Hardness and Wear Table 2 shows the physical properties of the Cu-based composite. The wear rate changes through the repeated contact process under constant load and velocity (3.13PMa and 7.54m/s respectively) [10]. Wear rates are often quoted in terms of a wear coefficient or dimensionless wear coefficient as derived from the Archard treatment of wear processes [11]. The average hardness values measured with a Vickers hardness tester (Table 3) on all the materials shows a similar tendency as the results of the sintering as shown in Figure 3. The materials with less porosity and sintered at high sintering temperature exhibited high hardness as shown in Table 3 with low porosity at low sintering temperature. This confirmed the fact that, porosity influences the hardness, and therefore, affects the rate of wear of the material. From the same table, the wear rate was also greatly affected by the porosity values obtained at their respective sintering temperatures. The wear volume rate (Vw) is calculated as shown in equation (1); where K is the wear coefficient (dimensionless), W the normal load and H the hardness. The Archard treatment of wear has been shown to be valid for cases where mechanical influences are dominant [12]. Wear is often associated with hardness of the materials in contact. Basically, the harder the material, the more wear resistant it is, but it is also more brittle and therefore more sensitive to the detachment of particles. According to Table 3, the lowest wear rate was observed at the 950o C sintered material. This could be attributed to the fact that there was sufficient heating to reduce porosity, which also brought about increase in hardness to optimize the wear properties of the material.
  • 7. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME 527 Table 2 Physical properties of Cu-based composite Rule Of Mixture ( )3 . − cmgtρ 3 .973.7 − cmg Experiment Data Average ( )3 . − cmgρ 6.714 3 . − cmg Average Microhardness (HV) 294 Average Porosity %,       −= t P ρ ρ 1 15.79% Table 3. Properties of the Cu-based composite material Sint. Tem. Tsin Density, ρ Porosity, P Hardness, Hv Wear Coeff. k Wear num. Wn Coeff. Frict. µ 850o C 6.51 17.53 272 0.000154 8.7191 0.336 900o C 6.71 15.82 287 0.000166 9.8499 0.343 950o C 6.85 14.04 304 0.000044 10.128 0.404 3.3. Abrasive Surfaces Classification In view of the advancement of technology, the application of computer-based technology and image-processing methods have lead to a fully automated classification system of tribological surfaces. Such a system has been useful in classifying (i) surfaces during manufacturing processes (quality control), (ii) wear surfaces in the failure analysis of engineering components, or (iii) wear particles in machine condition monitoring. The hybrid fractal-wavelet method is used here to demonstrate how an unknown abrasive surface can be classified into one of three classes of abrasive surfaces [13]. 3-D surface morphology images are shown in Figure 4 to identify the different kinds of abrasive surfaces. In Figure 4, our investigation shows that the abrasive surfaces can be classified into three divisions, named as smooth abrasive surface (mirror surface and integrated friction film) which has better wear resistance property because it demonstrated minimal wear rate, rough abrasive surface (rough surface) indicates moderate wear rate and a highly abrasive surface (much rough surface) showing excessive wear. Examples of the 3-D surface morphology images of the surface from each division are shown in Figure 4.
  • 8. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME 528 Figure 4 shows 3-D surface morphology images of the surface (a) at 850 o C, (b) at 900 o C and (c) at 950 o C. The (a) is observed to be the one with a highly abrasive surface; this is as a result of having fewer peaks that are ironic or hard to withstand pressure from the braking system. The (b) was also observed as the rough abrasive surface with moderate peaks withstanding the exerted pressure of the braking system. The (c) is the one that was observed as having enough ironic peaks to withstand the exerted pressure and therefore given a smooth abrasive surface. 4. CONCLUSION The wear resistance properties of the novel Cu-based composite material against a cast iron disc (grade HTA5/HB with Brinell hardness in the range 196) tested under a full laboratory condition, reveals a strong influence of porosity over the mechanical and tribological characteristics of the material. Investigation and observations concerning the effect of porosity on the mechanical and tribological characteristics have led to the following conclusions: The porosity level affects the mechanical properties. High porosity is not the best if optimizing the performance of the novel material, which leads to weakening of the materials as a result of low sintering temperatures but this can be further improved and considered for manufacturing commercial brake pads. On the other hand, low porosity samples gave a high resistance to wear. This was as a result of the high sintering temperature which ensured complete diffusion. Much lower wear coefficient, high wear number and high coefficient of friction were obtained at low porosity samples (14.04% at 950o C) tested. These show high resistance to wear; given good tribological characteristics and good mechanical properties. The dominant wear mechanisms found were plowing, delamination and abrasive wear. Abrasive wear and the delamination wear were the main cause of high wear coefficient, low wear number and low coefficient of friction. The nature of abrasive surfaces observed were classified into three divisions, namely, smooth abrasive surfaces (mirror surface and integrated friction film) which has better wear resistance properties because it demonstrates minimal wear rate; the rough abrasive surface (rough surface) indicates moderate wear rate; and lastly, the highly abrasive surface (much rough surface) showing excessive wear and has a high degree of surface destruction. This is as a result of the rate of wear that occurred during the dry sliding.
  • 9. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 2, March - April (2013) © IAEME 529 5. ACKNOWLEDGMENT We are grateful to the staff of The Key Laboratory of Specially Functional Materials and Advanced Manufacturing Technology, Ministry of Education, South China University of Technology. We are also value the support of the staff of the Analytical and Testing Center of South China University of Technology particularly Prof. Zhang Da Xue and Mr. Zhu Fan Kang (Chang Zhang) where we carried out the Experiments and the test. 6. REFERENCES [1] J. Wang, Y. He, and H. Danninger, Influence of Porosity on the Sliding Wear Behavior of Sintered Fe-1.5Mo-0.7C Steels, ASM International, JMEPEG (2003) 12:339-344 [2] M. Gui, S. B. Kang, J. M. Lee, Influence of porosity on dry sliding wear behavior in spray deposited Al–6Cu–Mn:SiCp composite, Materials Science and Engineering, A293 (2000) 146–156 [3] T. M. Cimino, A. H. Graham and T. F. Murphy, The effect of microstructure and pore morphology on mechanical and dynamic properties of ferrous P/M materials, Presented at pM2TEC '98 [4] H.L. Lee, W.H. Lu, S.L. Chan, Abrasive wear of powder metallurgy Al alloy 6061-SiC particle composites. Wear 159 (1992) 223 [5] M. Vardavoulias, C. Jouannt-Tresy, M. Jeandin, Sliding wear behaviour of ceramic particle reinforced high-speed steel obtained by powder metallurgy, Wear 165 (1993) 141–149. [6] N.P. Suh, An Overview of the Delamination Theory of Wear, Wear 44 (1977) 1–16. [7] V. M. Kryachek, Sintered Metals and Alloys Friction Composites: Traditions and New Solutions (Review). Powder Materials, Powder Metallurgy and Metal Ceramics, Vol. 43, Nos. 11-12, 2004 Spring Science + Business Media, Inc. [8] Xiong X., Sheng H, Chen J, Yao P, Effects Of Sintering Pressure And Temperature on Microstructure and Tribological Characteristic of Cu-Based Aircraft Brake Material, Trans. Nonferrous Met. Soc. China 17(2007) 669-675 [9] Yao P, Sheng H, Xiong X., Huang B., Worn Surface Characteristics of Cu-Based Powder Metallurgy Brake for Aircraft, Trans. Nonferrous Met. Soc. China 17(2007) 99- 103. [10] Kato K,. Classification of Wear Mechanisms/Models, Wear – Materials, Mechanisms and Practice, Edited by G. Stachowiak , 2005, 9-20,. [11] Williams J. A., Engineering Tribology Oxford Science Publications, Oxford University Press, New York 1994. [12] Neville A. and Morina A., Wear and Chemistry of Lubricants, Wear – Materials, Mechanisms and Practice, Edited by G. Stachowiak , 2005, 71-94. [13] G. W. Stachowaik, G. B. Stachowiak, D. De Pellegrin, P. Posiadlo. Characterization and Classification of Abrasive Particles and Surfaces, Wear–materials, mechanisms and practice. Edited by G. Stachowiak 2005 339-368. [14] ASTM B611. [15] P. Kurmi, S. Rathod and P. Jain, “Abrasive Wear Behavior of 2014al-Tic in Situ Composite”, International Journal of Mechanical Engineering & Technology (IJMET), Volume 3, Issue 3, 2012, pp. 229 - 240, ISSN Print: 0976 – 6340, ISSN Online: 0976 – 6359.