Evaluation of mechanical properties of retrogression and reaged al 7075 alloy reinforced with sicp composite material

IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
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Volume: 03 Issue: 11 | Nov-2014, Available @ http://www.ijret.org 117
EVALUATION OF MECHANICAL PROPERTIES OF
RETROGRESSION AND REAGED AL 7075 ALLOY REINFORCED
WITH SICP COMPOSITE MATERIAL
Janardhana K1
, D. N. Drakshayani2
1
Assistant Professor, Department of Mechanical Engineering, Sir M.VIT, Bangalore-562157
2
Professor, Department of Mechanical Engineering, Sir M.VIT, Bangalore-562157
Abstract
The metal matrix composites offers a spectrum of advantages that are important for their selection and use as structural
materials. A few such advantages are high strength, high elastic modulus, high toughness and impact resistance, low sensitivity to
changes in temperature or thermal shock, high surface durability, low sensitivity to surface flaws, high electrical and thermal
conductivity, minimum exposure to the potential problem of moisture absorption resulting in environmental degradation and
improved machinability with conventional metal working equipment. The aim of the present study is to investigate the mechanical
properties of Silicon Carbide particulate (SiCp) reinforced Aluminum matrix composite after retrogression and re-aging.
Aluminum 7075 alloy with 10%, 15% and 20% SiCp were studied.
Keywords: Retrogression and Re-aging, Aluminum 7075 alloy, heat treatment.
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1. INTRODUCTION
Particulate reinforced aluminum alloy matrix composites
have received attention over many years due to their
excellent yield and tensile strengths, high specific elastic
modulus and isotropic properties compared with the
conventional alloy materials, which is very good candidate
for structural applications in the field of aerospace,
automotive and electronics.
The particulate-reinforced metal-matrix composites have
emerged as attractive materials for use in a spectrum of
applications such as industrial, military and space related.
The renewed interest in metal matrix composites has been
aided by development of reinforcement material which
provides either improved properties or reduced cost when
compared with existing monolithic materials. [1-2]
Particulate reinforced metal-matrix composites have
attracted considerable attention on account of the following
aspects: 1. Availability of a spectrum of reinforcements at
competitive costs. 2. Successful development of
manufacturing processes to produce metal matrix
composites with reproducible microstructures and
properties. 3. Availability of standard and near standard
metal working methods which can be utilized to produce
these materials.
During the last decade, considerable efforts have been made
to improve the strength of precipitation hardened aluminum
alloy matrix composites, such as developing new
preparation technologies with suitable heat-treatments.
7XXX series aluminum alloys are lightweight materials that
are widely used in the aerospace industry because of their
superior specific strength. The main strengthening
mechanism for these alloys is artificial aging commonly
known as T6 temper. Although T6 tempered 7XXX series
alloys are satisfactorily used in many engineering
applications, they suffer from stress corrosion cracking,
especially when working in environments containing
chloride. Another aging route known as T73 [3] temper has
been developed to overcome the drawback. However, T73
temper is accompanied by a loss in strength of about 10-
15%. In 1974, Cina [3] proposed new aging process known
as retrogression and reaging to improve the Stress
Corrosiom Cracking (SCC) resistance of 7075 alloy without
significance loss in strength when compared to the T6
temper state.
RRA is applied to T6 tempered 7XXX series alloys into 2
successive steps, namely, retrogression and reaging. [20].
Taguchi technique is used for design of experiments. The
L18 array for each weight percentage of SiC(p) has been
chosen and the factors for each specimen will be varied as
required.
2. EXPERIMENTATION:
The nominal composition of Al-7075 alloy is given in Table
1.
Table 1: Composition of Al-7075
Elements Wt (%)
Cu 1.2 - 2
Mg 2.1 - 2.9
Zn 5.1 - 6.1

_______________________________________________________________________________________
Cr 0.18-0.28
Si <0.4
Al 87.1-97.4
Fe <0.5
Stir casting method is used to obtain the Al 7075/ SiC p
composite. Aluminum 7075 was introduced into the furnace
at 660 ºC, so as to obtain its liquid phase. After obtaining a
melt, silicon carbide powder pre heated at 300ºC for 30
minutes was added to it. Mechanical agitation was done to
get a homogenous melt. This mixture is then casted into
fingers of specific dimensions. Preaging is carried out at
temperatures of 125 ºC, 135 ºC and 145 ºC for time periods
of 12 hs, 24hs and 48 hs. Then Retrogression is carried out
at temperatures of 200 ºC, 220 ºC and 240ºC for 5 minutes,
10 minutes and 15 minutes followed by reaging at 125 ºC,
135 ºC and 145 ºC for 12 hs. The heat treatment is carried
out in a Muffle Furnace. These heat treated specimens are
then machined to the required dimensions (Fig. 3.) for the
tensile test. The results are plotted in L18 arrays and
Statistical Analysis Software MINITAB 16 by Taguchi
method is used for analysis.
2.1.1. Stir Casting
Casting Process was carried out to prepare the samples as
discussed in earlier paper. [20]
1. Aluminium 7075 of known weight was melted at 660ºC.
2. After obtaining a melt, pre heated (300 ºC for 30 minutes)
silicon carbide particles were added to it.
3. Mechanical agitation was done to get a homogenous melt.
4. Silicon carbide reinforced Aluminium 7075 was obtained
by Stir casting. At each casting operations, 4 fingers were
obtained.
5. All specimens were then coded as indicated in section
2.2.
Fig 1 Furnace with stirring apparatus
2.1.2. Heat Treatment
Retrogression and reaging treatment can improve the stress
corrosion behavior of the alloy while maintaining the
mechanical resistance of the T6 temper [4-12]. The
following are the steps involved in retrogression and re-
aging:
 Specimens are placed in the muffle furnace for
preaging. The temperature and time of heat
treatment is decided by the specimen coding as that
required by the Design of Experiments.
 Once the preaged specimens are naturally cooled to
room temperature, they are retrogressed at the
required temperature and time.
 The retrogressed specimens are then cooled
naturally to room temperature and then reaged as
required
Fig 2 Heat treatment in muffle furnace
2.2 Methodology
Experimental design using Taguchi method
Six factors and 3 levels for each parameter have been
chosen for each specimen composition as given in Table 2.
The L18 array for each weight % fraction of SiC has been
chosen and the coding of the specimen is done as follows.
Table 2: Six factors and 3 levels for each parameter
Percentage of
SiC,%
A - 0 B -10 C -
20
Preage
temperature, ºC
1 -
125
2 -
135
3 -
145
Preage time, hs A -
12
B - 24 C -
48
Retrogression
temperature, ºC
1 -
200
2 -
220
3 -
240
Retrogression time,
hs
A - 5 B - 10 C -
15
Reage temperature,
ºC
1 -
125
2 -
135
3 -
145
Reage time, hs A -
12
B - 24 C -
48
If a specimen is labeled A2B3C1A, then the specimen
condition is as indicated below:
1. 0% SiC 2. Pre-aged at 135 ºC 3. For 24 hs
4. Retrogressed at 240 ºC 5. For 15 minutes
6. Re-aged at 125 ºC 7. For 12 hs
2.3. Tensile Test
It was carried out as per ASTM standards E8- 95A. All the
samples were tested for strength.

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The samples were loaded till fracture.
Fig 3: Tensile test specimen
3. RESULTS AND DISCUSSION
3.1. Taguchi Method
Taguchi technique using Minitab 16 Statistical Software was
used to analyze the L18 array for each of the specimens.
Totally 4 arrays were used. In each 4 different percentages
(0%, 10%, 15% and 20%) of SiC were considered.
Main effects Graphs for means and S/N ratios were obtained
showing relationships between the output result and the
various factors.
For Tensile strength the larger the better condition is
selected.
3.2 Tensile Strength
3.2.1 Regression Equations (0% SiC):
TENSILE STRENGTH = - 324 + 2.48 PREAGE TEMP +
0.109 PREAGE TIME + 0.476 RETROGRESSION TEMP -
0.53 RETROGRESSION TIME - 0.239 REAGE TIME
………………………… 1
145135125
130
120
110
100
90
482412 240220200
15105
130
120
110
100
90
145135125 482412
preage temp
MeanofMeans
preage time retrogression temp
retrogression time reage temp reage time
Main Effects Plot for Means
Data Means
145135125
43
42
41
40
39
482412 240220200
15105
43
42
41
40
39
145135125 482412
preage temp
MeanofSNratios
preage time retrogression temp
retrogression time reage temp reage time
Main Effects Plot for SN ratios
Data Means
Signal-to-noise: Larger is better
Fig. 4: Main effects plot for Means and S/N ratios of 0%
SiC
From Fig.4 its observed that, the specimens which are
preaged at 145o
C for 24 hs, retrogressed at 240o
C for 5
minutes and reaged at 125o
C for 48 hs improved the tensile
strength of the composite material. Also, the specimens
which are preaged at 125o
C for 12 hs, retrogressed at
200o
C for 15 minutes and reaged at 145o
C for 24 hs
exhibited the poorer tensile strength.
The increase in the strength of the specimens are due to the
formation of the more stable interphases like MgZn2 [12-14]
and also refinement of the grains at the said elevated
temperature of retrogression for short interval of time.
Whereas the specimens which are subjected to lower
retrogressed temperature for short interval of time and
higher reaging temperature for longer reaging time resulting
in the coarsening of the interphases and formation of more
unstable precipitates.
3.2.2. Regression Equations (10% SiC):
TENSILE STRENGTH = - 95.1 - 0.317 PREAGE TEMP -
0.662 PREAGE TIME + 0.129 RETRO TEMP + 0.250
RETRO TIME + 2.06 REAGE TEMP + 0.0050 REAGE
TIME
………………………… 2
145135125
170
160
150
140
130
482412 240220200
15105
170
160
150
140
130
145135125 482412
PREAGE TEMP
MeanofMeans
PREAGE TIME RETRO TEMP
RETRO TIME REAGE TEMP REAGE TIME
Data Means
145135125
44.5
44.0
43.5
43.0
42.5
482412 240220200
15105
44.5
44.0
43.5
43.0
42.5
145135125 482412
PREAGE TEMP
MeanofSNratios
Data Means
SiC
preaged at 125o
C for 15
200o
C for 24 hs exhibits
poor tensile strength.
The increase in the strength of the specimens are due to the
formation of more stable interphases like MgZn2 [12-14]
and also refinement of the grains at the said elevated

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temperature of retrogression for short interval of time.
Whereas the specimens which are subjected to lower
retrogressed temperature for short interval of time and
higher reaging temperature for longer reaging time resulting
in the coarsening of the interphases and formation of more
unstable precipitates.
TENSILE STRENGTH = 173 + 0.367 PREAGE TEMP -
1.59 PREAGE TIME - 0.004 RETRO TEMP - 0.02 RETRO
TIME - 0.000 REAGE TEMP - 0.001 REAGE TIME
……………… 3
145135125
210
195
180
165
150
482412 240220200
15105
210
195
180
165
150
145135125 482412
PREAGE TEMP
MeanofMeans
Data Means
145135125
46
45
44
43
482412 240220200
15105
46
45
44
43
145135125 482412
PREAGE TEMP
MeanofSNratios
Data Means
SiC
TENSILE STRENGTH = - 785 + 1.17 PREAGE TEMP -
1.06 PREAGE TIME + 2.93 RETRO TEMP - 0.03 RETRO
TIME + 1.55 REAGE TEMP - 0.001 REAGE TIME
……………… 4
145135125
250
225
200
175
150
482412 240220200
15105
250
225
200
175
150
145135125 482412
PREAGE TEMP
MeanofMeans
Data Means
145135125
48
46
44
482412 240220200
15105
48
46
44
145135125 482412
PREAGE TEMP
MeanofSNratios
Data Means
SiC
From Equation 1, 2, 3 and 4 it’s observed that the
relationship between the stated parameters is established and
also able to estimate the tensile strength for the different
values of the parameters.
preaged at 145o
C for 15
220o
C for 48 hs exhibits
poor tensile strength.
preaged at 145o
C for 5
200o
C for 12 hs exhibit
poor tensile strength. The increase in the strength of the
specimens is due to the formation of the more stable
interphases like MgZn2 [12-14], dissolution of the unstable
precipitates and also refinement of the coarser grains at the
said elevated temperature of retrogression for short interval
of time. Whereas the specimens which are subjected to
lower retrogressed temperature for longer interval of time
and higher reaging temperature for longer reaging time
resulting in the coarsening of the interphases and formation
of more unstable precipitates resulting in the increase of
dislocation density as the percentage of SiC particles
increased.
4. CONCLUSIONS
From the present studies, the following conclusions were
obtained.
1. With increase in temperature and time of all 3 phases of
RRA, pre-aging, retrogression and reheating, the Tensile
Strength generally increases.
2. At higher pre-aging and re-aging temperatures, increase
in Tensile Strength can be due to the relieving of internal
stresses within the material and refinement of the grains.

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ACKNOWLEDGEMENTS
The authors sincerely thank the Management and Staff of
Department of Mechanical Engineering, Sir M.VIT and
Family members.
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alloy reinforced with SiCp Composite Material”, IJERT,
Volume. 3, Issue. 09, 406-409, September - 2014

Evaluation of mechanical properties of retrogression and reaged al 7075 alloy reinforced with sicp composite material

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