DENSIFICATION AND DEFORMATION BEHAVIOUR OF SINTERED POWDER METALLURGY COPPER-7_TUNGSTEN COMPOSITE DURING COLD UPSETTING by iaemedu

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									International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 1, Jan - Feb (2013) © IAEME
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ISSN 0976 – 6340 (Print)
ISSN 0976 – 6359 (Online)
Volume 4 Issue 1 January- February (2013), pp. 01-07
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 DENSIFICATION AND DEFORMATION BEHAVIOUR OF SINTERED
  POWDER METALLURGY COPPER-7%TUNGSTEN COMPOSITE
                DURING COLD UPSETTING
                            N.Vijay ponraj1, Dr.G.Kalivarathan2
                1
                  Research Scholar, CMJ University, Meghalaya, Shillong, India
    2
      Principal/Dept of Mech. Engg, PSN Institute of Technology and Science, Tirunelveli,
              Tamilnadu, India, Supervisor CMJ University, Shillong, Meghalaya.
                               Email:vijay_ponraj@yahoo.com


ABSTRACT

        Studies were conceded out to evaluate the initially preformed density and initial
aspect ratio on the densification behavior of sintered Copper 7% Tungsten composite. The
preform possessed 0.85 is the initial theoretical density. Aspect ratio varied from 0.4, 0.6 and
0.8. Properties of Copper Tungsten composites with respect to linear strain, lateral strain and
true stress were evaluated and plotted. Studies exposed that higher stress and higher strain
values are obtained in composite when compared to the Tungsten powder. The composite of
Copper 7%W obtained at 750oC. The Composite obtained at lower aspect ratio acquired the
highest stress and strain when compared to the composites preforms obtained at other aspect
ratio

KEYWORDS: Powder Metallurgy, Metal Matrix Composites, Preform, Sintered Copper-
7%Tungsten Composite, Nano Structure.

1. INTRODUCTION

        The term “composite” broadly refers to a material system which is tranquil of discrete
constituents (the reinforcement) distributed in a continuous phase (the matrix). It derives its
individual characteristics from the properties of its ingredients, from the geometry and
architecture, and also from the properties of the restrictions (interfaces) of its different
constituents. Composite materials are usually classified on the basis of physical or chemical
nature of their matrix phase, like polymer matrix, metal-matrix and ceramic composites etc.
Among the materials that are extended to an increasing scope of metal matrix composites.
The space industry was the first sector captivated in the usage of these materials. Another
fragment of even superior fiscal importance for the development of new metal matrix
composites (MMC s) is the automotive industry. The suppleness allied with MMC’s in

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International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 1, Jan - Feb (2013) © IAEME

tailoring their physical and mechanical properties as compulsory by the users have made
them suitable candidates for a gamut of applications related to automobile and aeronautical
sectors. The preface of fine dispersed particles into the metal matrix has crucial reinforcing
effects when maintained at prominent temperatures. Powder forging technique is
conventional as the most inexpensive and efficient procedure leading to aperture elimination
and superior mechanical strength. Although a number of processes are available for
producing MMC's, the powder metallurgy technique was found to be the most appropriate
because it yields better mechanical properties. Research on dispersion strengthened materials
points out the implication of the properties of the starting metallic powders and also the
importance of the preliminary structure in preserving the structure of the concluding
manufactured goods. A very important aspect of scattering strengthening is the even
allotment of tungsten particles, their fine distribution, especially in nanometer scale, and the
introduction of a possible amount of dispersed particles into the volume of the base metal.
The powder metallurgy sintered parts possesses 20-40% porosity which can be
advantageously used, but the mechanical properties of the component are adversely effected
by the presence of porosity. Therefore, the parts intended for dynamic applications, the final
compaction should be close (up to about 1.5-2%) to that of fully dense material. Forging of
the sintered preforms result in a precision component with the reduction or elimination of
porosity. The lessening in porosity during forging, results in a decrease in preform volume.
The compliant of porous materials, thus, does not follow the laws of number constancy.
Further, the “material parameters” (such as, modulus of elasticity and modulus of rigidity) are
functions of density of the buckling body and as such the “material parameters” also feel a
variation along with a change in porosity (density). Initially, there had been some
experimental, semi-experimental or analytical looms using slab method for obtaining the
density of porous formed metal parts. Thereafter, several researchers studied the forging of
porous materials and garrison by using finite element method taking material to be rigidly
plastic. A challenge to use numerical method for the analysis of powder metal forging
operation has also been studied by various researchers using a unyielding plastic approach.
Rigid plastic approach could be adequate for large deformation by excluding the effect of
resilient behaviour of the material. Subsequently, there have been some attempts to develop
elastic-plastic approach to study the deformation of porous materials. The aim of the present
work is to study the mechanics of cold forging of powder metal preforms taking into account
its plastic strains as the work material which undergoes deformation. The model developed
was applied to study the forging of an axis symmetric short frozen cylindrical part under
simple upsetting. The analysis was carried out for the press forging with slow rates of
deformation where inertia and temperature effects were negligible. The total results predicted
the densification pattern of the work material and the loads required to produce the desired
deformation.

2. PROBLEM FORMULATION

        Present exploration focused on the densification behavior of sintered copper 7%
tungsten powders when taken in varying quantities. Frictionless compression tests are used to
find out the fundamental plastic flow characteristics of porous metals. Studies expose that the
deformation was uniform with barreling of cylindrical surfaces. The proposed study also
carries out to evaluate the initial preformed density and initial aspect ratio on the
densification behavior of sintered copper 7% tungsten composites. The preform obsessed
0.85 as initial density and three aspect ratio varied from 0.4, 0.6, and 0.8. Four performs, each

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International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 1, Jan - Feb (2013) © IAEME

of different aspect ratio were taken for each temperature. A critical literature survey reveals
that several attempts has been made in producing components through powder metallurgy
route, which may contain one or the other type of impurifier. These perhaps could not be
verified during the course of several investigations as the fine dispersion of self oxidized
material in the component perchance induced enhanced properties. A wide variety of research
in the area of elemental powder and its own oxide composite has been carried out. But earlier
investigations have shown that extruding the sintered preform containing the self oxidized
dispersions in different proportions on extrusion may encourage improved mechanical
properties. It is well established that in the metal forming operations the deformation is never
sternly homogeneous and therefore pores present on the surface of the component can never
be closed either due to the predominance of tensile forces or due to hydrostatic forces present
in the dead metal zones. Therefore, it is more likely that the particulate structure will be
customary at the surface of the component irrespective of preform design for any upsetting
test. For studying the behavior of copper 7% tungsten composite during cold upsetting,
mechanical properties should be given precedence. In most of the methods adapted for
studying the strengthening of the composite, strengthening metal must have higher melting
point than matrix metal. In this method, we have developed tungsten as a strengthening
component, but it possesses higher melting temperature than Copper (matrix metal). The
basic advantage of dispersion strengthened materials is that it does not improve yield strength
at ambient temperature or work hardening rate. The present investigation on composite
carried out at temperatures of 7500c with three aspect ratios of 0.4, 0.6 and 0.8.

3. EXPERIMENTAL PROCEDURE

3.1. Materials Required:
The materials required for this investigation are: Copper and Tungsten powder for composite
preparation, graphite for using as lubricant, high carbon die steel punch and die, two flat
plates heat treated to Rc 53 to 56 and tempered to Rc 46 to 49, a stainless steel tray, and an
electric muffle furnace.

3.2. Preparation of Copper-7% Tungsten Composite:
Copper and Tungsten powders were used in the present investigation. These powders were
purchased from M/s. Metal Powder Company (P) Ltd., Tirumangalam, Madurai, Tamilnadu,
India. Electrolytic copper and atomised tungsten were obtained with 100% and 99.73% purity
respectively. The individual powders were pulverized in a high energy ball mill (Fritsch,
Germany - Pulverisette - 6) for four hours after that it was mixed on weight basis with 7%
Tungsten and rest Copper powder. These composite powders were pulverized in a high
energy ball mill and after 10 hours milling, the obtained particle size was approximately
below 400nm. SEM was used for evaluation of morphological changes of the particles after
milling and is shown in Fig. 1(a-c). Fig. 1(a) shows the SEM image of the Cu particles at
9500X magnification and has a structure of a cluster of tiny particles and like small flattened
flake particles due to severe plastic deformation of copper, micro-welding and fracture of the
large flakes due to typical mechanical milling. Fig. 1(b - c) shows the SEM image of the W
powders at 6000X and 2000X magnification respectively, It is in the formation of flattened
particles with pancake structure. Fig. 1(d) shows the SEM image of the Cu-7%W Powder
Composite at 8000X particles. It shows the morphological changes of Cu-7%W powder
mixture after 10 hours milling. No significant difference between the Cu morphology in the
composite and the monolithic W powder is observed at low milling times; that means the fine

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International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
                                                                        )
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 1, Jan - Feb (2013) © IAEME

                                  the
W elements distributed throughout the Cu matrix and represents the particle size in the range
between 200-400nm.




                    (a)                                             (b)
   Fig. 1 SEM micrograph after ball milling (a) Cu powder 9,500 X (b) W powder 6,000X


3.3. Characteristics of Oxidized Powder:
The characteristic of the copper and Tungsten powder is shown in Table 1 (a        (a-b). The
individual powders were pulverized in a high energy ball mill (Fritsch, Germany -
                                                                               %
Pulverisette - 6) for four hours after that it was mixed on weight basis with 7% Tungsten and
rest Copper powder.

                              Table 1 Characteristics of powder

                                     (a) Copper Powder
 Test           IS 5461                      ASTM B-417         ASTM         B- ASTM       E-
 Standard                                                       213             194
 Property       Sieve analysis, %            Apparent           Flow rate      Acid
                +75µm +45µm -45µm            density (g/cc)     Sec(50g-1)     Insoluble

 EC/86          0.42        5.43     94.24   1.58               Nil            Nil
 Grade

                                    (b) Tungsten Powder
 Characteristics                        Test Standard                  Value
 Sieve analysis : - 45 µm               ASTM D-185                     99.00
 Average Particle Size,    Fisher ASTM B-330                           3.92
 Number
 Oxygen Content (Hydrogen Loss)   ASTM E-159                           1.85
 Other Impurities                 AAS                                  0.21
 Purity                                                                97.93


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International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 1, Jan - Feb (2013) © IAEME

3.4. Compaction of Zinc-Zinc Oxide Powder:
Cylindrical compacts of 20 mm diameter with an aspect ratio of 0.40, 0.60 and 0.80 were
prepared. The compacts were prepared using ball milled Cu-7% W composite. The composite
powders were compacted by using suitable punch and die set assembly on a Universal
Testing machine having 1 MN capacity. Compacting pressure was applied gradually and it
was 1.2 GPa for three aspect ratios. Graphite was used to lubricate the punch, die and the
butt. When preparing the compacts, the initial density and aspect ratio were maintained by
precisely controlling the mass and accurately monitoring the compacting pressure employed

3.5 Sintering
After the compaction, the compacts were immediately taken out from die set assembly and
loaded into the furnace for sintering. To prevent oxidization, the green compacts were
initially covered with inert argon atmosphere in the furnace. The sintering was carried out in
an inert gas circulated electric muffle furnace at 750°C for a holding period of one hour. As
soon as the sintering schedule was over, the sintered preforms were cooled inside the furnace
itself to the room temperature. After the completion of sintering, the preforms were cleaned
by using a fine wire brush.

3.6 Cold Deformation Experiments
Deformation experiments were carried out by using flat faced dies and a hydraulically
operated compression testing machine of having 1MN capacity. The flat dies were machined
and tempered. Flat faces of the dies were ground after heat treatment in a grinding machine,
in order to obtain the final dimensions and surface quality and its hardness was measured as
90 HRB after tempering. Graphite was well applied as lubricant on the ends of preforms and
contacting surfaces of flat dies, which created a situation for almost frictionless ideal
deformation. In general, each compact was subjected to an incremental compressive loading
in steps of 50kN until the appearance of visible cracks on the free surface. Immediately, after
the completion of each step of loading, the height, the contact diameters at the top and
bottom, the bulged diameter and the density were measured for each of the deformed
preforms. The density measurements were carried out using Archimedes principle.
Experimental measurements were also used to calculate the various parameters namely the
stresses, the Poisson’s ratio, density ratio and the strain.

4. RESULTS AND DISCUSSIONS

        The sintered P/M Copper-7% W composite was made under the temperatures of
7500c. Cylindrical preforms of three different aspect ratios were employed in the compression
tests. Plots were drawn for copper-7% W between the hoop strain and the axial strain to
compare with different aspect ratios. The rate of change of hoop strain with respect to axial
strain was not the same for all aspect ratios. This indicates that each aspect ratio had different
slope and the hoop strain increased with axial strain. Among the three aspect ratios, sintered
preforms oxidized at aspect ratio of 0.8 had more strain values. Similarly, the aspect ratio of
0.8 also had high strain values when compared with others. From the plots it was also evident
that the strain increased with higher aspect ratios. The deformation of the composites under
lower aspect ratio is less. Due to the low value of hoop and axial strain, composites have the
low ductile property .This composite is more suitable for the compressive load applications.
Plots between the true stress and true strain are shown in figure 3. It is observed that the true
axial stress increases rapidly as the true axial strain is increased, followed by a gradual

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International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 1, Jan - Feb (2013) © IAEME

increase in the true axial stress with further increase in the axial strain. Further, it is found
that the 0.80 preform improved load bearing capacity compared to that for other aspect ratios,
while the initial fractional density remains constant.

                                                            Cu - 7%W
                                                 Initial Theoretical Density 0.85
                           1.6
                           1.4
                           1.2
             Hoop Strain




                             1
                           0.8                                                       Aspect Ratio 0.4
                           0.6
                                                                                     Aspect Ratio 0.6
                           0.4
                                                                                     Aspect Ratio 0.8
                           0.2
                             0
                                 0   200        400            600    800

                                           Axial Strain

        Fig.2 Axial Strain Vs Hoop Strain for different aspect ratio of 0.4, 0.6 and 0.8

                                                            Cu - 7% W
                                                  Initial Theoretical Density 0.85
                           1.6
                           1.4
                           1.2
            Axial Strain




                            1
                           0.8                                                       Aspect Ratio 0.4
                           0.6
                                                                                     Aspect Ratio 0.6
                           0.4
                                                                                     Aspect Ratio 0.8
                           0.2
                            0
                                 0   200        400            600    800
                                            Axial Stress


         Fig.3 Axial Strain Vs Axial Stress for different aspect ratio 0.4, 0.6 and 0.8

5. CONCLUSION

        The major findings of this investigation include the rate of change of hoop strain with
respect to the axial strain indicated high values for higher aspect ratios. The rate of change of
true stress with respect to true strain was different for different aspect ratios. Higher aspect
ratio had the maximum value of both true stress and true strain than lower aspect ratio.

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International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 4, Issue 1, Jan - Feb (2013) © IAEME

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