Upload
lydung
View
215
Download
2
Embed Size (px)
Citation preview
http://www.iaeme.com/IJMET/index.asp 225 [email protected]
International Journal of Mechanical Engineering and Technology (IJMET) Volume 7, Issue 6, November–December 2016, pp.225–235, Article ID: IJMET_07_06_023
Available online at
http://www.iaeme.com/ijmet/issues.asp?JType=IJMET&VType=7&IType=6
ISSN Print: 0976-6340 and ISSN Online: 0976-6359
© IAEME Publication
PRODUCTION AND MECHANICAL
CHARACTERIZATION OF AL-7075-T6 AND FLY ASH
COMPOSITE BY STIR CASTING HOT DIE PROCESS
F. Anand Raju
Assistant Professor, Siddharth Institute of Engineering & Technology, Puttur, A.P, India.
Dr. M.L.S. Deva Kumar
Professor & Vice Principal, JNT University College of Engineering, Anthapuramu, A.P, India.
ABSTRACT
Today the engineering metals are mutable their properties with high mechanical properties by
the combination of different metals and other process. One of the most recent developments in the
field of metals improves mechanical properties and reduce the weight density to utilize day- today
life is composite materials. In this Aluminum metal matrix composite (AMMC) has gain more
predominate role in metal matrix composite. After the usage of iron the second largest metal that
use in the engineering, industrial, domestic works is aluminum. Fly ash (15%, 20% and 25%)
particles are added in the Al-7075-T6 to produce Aluminum metal matrix composite by hot die
casting process. Fly ash act as the reinforce metal in the aluminum metal matrix. This is added in
the molten metal by stirring the ash particles to mix thoroughly and spared in the aluminum metal.
Fly ash is the industrial waste by product converted in to usable metal so it reduce the storage
problem and reduce the weight ratio of the AMMC. In this work the composition of the fly ash is
varied to get the best mechanical properties and reduce the weight density of the AMMC. This type
of AMMC is widely used in light weight vehicles, building elevation materials and aerospace
application.
Key words: Aluminum 7075-T6, Fly Ash, Mechanical Properties, Stir Casting, Chemical analysis
of Aluminum and Fly Ash.
Cite this Article: F. Anand Raju and Dr. M.L.S. Deva Kumar, Production and Mechanical
Characterization of Al-7075-T6 and Fly Ash Composite by Stir Casting Hot Die Process.
International Journal of Mechanical Engineering and Technology, 7(6), 2016, pp. 225–235.
http://www.iaeme.com/ijmet/issues.asp?JType=IJMET&VType=7&IType=6
1. INTRODUCTION
Aluminum is the second largest metal in the engineering materials. This is the oldest metal and most usable
metal from house hold to aerospace. Aluminum fly ash metal matrix composite is strengthen composite in
which soft and ductile aluminium matrix is strengthen by the hard and brittle fly ash particles.
Discontinuously reinforced aluminium based metal matrix composites are improving their high strength,
high isotropic and goodwear resistance. Discontinuously reinforcement aluminium composites have been
developed in the various fields like aerospace, automotive and many other engineering applications [1].
F. Anand Raju and Dr. M.L.S. Deva Kumar
http://www.iaeme.com/IJMET/index.asp 226 [email protected]
Fly ash particles are potential discontinuous dispersoids used in metal matrix composites due to their
low cost and low density reinforcement which are available in large quantities as a waste by productin
thermal power plants [2].
MMCs offer a unique balance of physical and mechanical properties. Aluminium MMCs have received
increasing attention in recent years as engineering materials with improved strength, hardness and impact
resistance. The stair casting method is widely used among the different process.
Fly ash is a naturally-cementatious coal combustion by-product. About 130 coal based thermal power
plants that available in India are producing about 120 million tonne fly ash per year. Fly ash has been
considered as an “Industrial waste” and was being disposed of in ash ponds. In Indian coal has high ash
content and low calorific value as result huge amount of fly ash is generated. According to ASTM C-618
Fly ash is broadly classified into two major categories: Class F and Class C fly ash. The chemical content
of the ash differ the type of ash i.e., the amount of calcium, silica, alumina and iron [4].Fly ash utilization
improved and reduces the pollution in environment, now in present day’s fly ash is focusing and improving
their investigation in various fields like AMMC’s, brick, roads, agriculture and etc.
Production of AMMC’s has nemours advantages which are lightweight materials used in aerospace and
automobile industry. The production of AMMC’s gives good mechanical characteristics and less in cost.
2. EXPERIMENTAL WORK
2.1. Raw Material
In this work, aluminum 7075-T6 alloy has been used as matrix and fly ash particle with average size of (1-
53µm) were used as reinforcement material and its chemical composition was shown in the table 1. The fly
ash is collected from Lanco Industry at Srikalahasti.
Figure 2.1 Fly Ash Figure 2.2 Aluminum 7075-T651 plate
2.2. Dimensions of the Die
The die is prepared by mild steel plate and square rods. The bottom plate is of 300×150×25mm and the top
plate of 300×150×10 mm, the side bars on four side of different length, and two are 250×25×25 mm and
the two short length of 150×25×25 mm is machined and polished to avoid the sticking of the cast. The bars
were firmly bolted to the bottom and top plates to form as a rectangular cavity of size 250×100×15 mm. At
the center of the top plate a 30mm diameter hole is drilled to pour the molten metal into the cavity. The one
Production and Mechanical Characterization of Al-7075-T6 and Fly Ash Composite by Stir Casting Hot Die Process
http://www.iaeme.com/IJMET/index.asp 227 [email protected]
side of the top plate a 10mm hole is drilled to form as a riser and escape the molten hot gases evolved in
the casting.
Figure 2.3 Open Die Figure 2.4 Closed Die
2.3. Preparation of Specimen by Stir Casting Process
In this, the electric induction titling furnace is chosen to produce the specimens. The furnace is fully
equipped with a stirrer and a DC motor to move the stirrer up and down. The motor movement is operated
by pneumatic system. The control of temperature is done by digital control system. The speed of motor is
controlled by DC regulator.
Figure 2.5 Tilting Induction furnace Figure 2.6 Stirrer
The aluminum of 7075-T6 was melted at the temperature of 800°C then the stirrer is start to stir the
molten aluminium. Fly ash particles were added to the melt at the time of vortex formation (15%,20%,and
25%) by weight %.The fly ash particles average size of (1-52µm) is obtained by sieving the collected ash
from the industry. Before mixing the fly ash it is pre heated at the temperature of 600°C to remove the
wettability in the muffle furnace. The melt temperature is maintained 800°C to 1000°C during the addition
of the fly ash particles. The mixed AMMC is poured in the metal die which is maintained at hot condition.
Then the die is allowed to solidification to produce the given specimen.
F. Anand Raju and Dr. M.L.S. Deva Kumar
http://www.iaeme.com/IJMET/index.asp 228 [email protected]
Figure 2.7 Digital Temperature Control Figure 2.8 Digital DC speed control
(a) 15% Fly ash (b) 20% Fly ash (c) 25% Fly ash
Figure 2.9 Cast specimen of Al7075-T6 and Fly ash.
The cast specimens were prepared for mechanical test
3. MECHANICAL TEST ON SPECIMEN
3.1. Tensile Test
The Al-7075-T6is preparing according to the ASTM C-618and also AMMC. The plate size of aluminum
prepared in the die of 250×150×15mm plate is cut to 250× 25×12.5 mm to test tensile strength of the
specimen at different composition with parent material.
Production and Mechanical Characterization of Al-7075-T6 and Fly Ash Composite by Stir Casting Hot Die Process
http://www.iaeme.com/IJMET/index.asp 229 [email protected]
Figure 3.1 Cutting of parent plate Figure 3.2 Universal testing machine with specimen
Figure 3.3 Tensile Test specimen with Dimensions
Figure 3.4 Test Specimen before Test Figure 3.5 Test specimen after test
F. Anand Raju and Dr. M.L.S. Deva Kumar
http://www.iaeme.com/IJMET/index.asp 230 [email protected]
Figure 3.6 Load VS Displacement
3.2. Hardness Test
Hardness is the property of a material that enables it to resist plastic deformation, usually by penetration.
However, the term hardness may also refer to resistance to bending, scratching, abrasion or cutting. The
hardness test was conducted on the Brinell hardness testing machine for all the samples with composite
specimens.
Figure 3.7 Specimen under test
3.3. Impact Strength
The toughness is the energy requires breaking the material. The energy is calculated in jouls. The energy
consumed is calculated by the difference between total energy supplied to the energy available at the end.
The measure of toughness can be found with the help of Charpy and Izod impact tests. The standard
specimen size for Charpy impact testing is 10mm×10mm×55mm.
Figure 3.8 Test specimen before testing Figure 3.9 Test specimen after testing
0
3
6
9
12
15
18
21
24
27
30
0 2 4 6 8 10 12 14 16
Load
kN
Displacement mm
Load Vs Displacement
Production and Mechanical Characterization of Al
http://www.iaeme.com/IJMET
Impact test was carried out at room temperature using Impact tester to calculate toughness. The
specimen is supported at two end like a
breaking the specimen due to the impact of the pendulum.
Figure 3.10
4. RESULT AND DISCUSSIO
4.1. Chemical Analysis of Al7075
The chemical analysis of the parent
Spark or arc atomic emission spectroscopy is used for the analysis of metallic elements in solid samples.
The parent aluminum piece is ground up and
through the sample, heating it to a high temperature to excite the atoms within it.
atoms emit light at characteristic wavelengths that can be dispersed with a monochromator and detected.
The detected elements are tabulated
Table 4.1
Element Silicon
Si
Iron
Fe
Copper
Cu
Required 0.4 0.5 1.2
Content 0.35 0.164 2.02
Element Zirconium
Zr
Na Tin
Sn
Required - -
Content - -
Production and Mechanical Characterization of Al-7075-T6 and Fly Ash Composite by Stir Casting Hot Die Process
IJMET/index.asp 231
Impact test was carried out at room temperature using Impact tester to calculate toughness. The
end like a simply supported beam in the test and reading was taken by
breaking the specimen due to the impact of the pendulum.
3.10 Charpy Impact test specimen with dimensions
RESULT AND DISCUSSIONS
nalysis of Al7075-T6
The chemical analysis of the parent Aluminum is tested by Spark or arc atomic emission spectroscopy
Spark or arc atomic emission spectroscopy is used for the analysis of metallic elements in solid samples.
ground up and burned during analysis. An electric arc or spa
through the sample, heating it to a high temperature to excite the atoms within it.
characteristic wavelengths that can be dispersed with a monochromator and detected.
The detected elements are tabulated below.
Table 4.1 Chemical Composition of Al 7075-T6
Copper
Cu
Manganese
Mn
Magnesiu
m
Mg
Chromiu
m
Cr
1.2-2.0 0.3 2.1-2.9 0.18-0.28
2.02 0.015 2.06 0.15
Tin
Sn
Bismut
h
Bi
Plambu
m
Pb
Co Other Element
Each
- - - - 0.05
- - 0.01 <0.002 0.05
T6 and Fly Ash Composite by Stir Casting Hot Die Process
Impact test was carried out at room temperature using Impact tester to calculate toughness. The
beam in the test and reading was taken by
specimen with dimensions
Spark or arc atomic emission spectroscopy.
Spark or arc atomic emission spectroscopy is used for the analysis of metallic elements in solid samples.
An electric arc or spark is passed
through the sample, heating it to a high temperature to excite the atoms within it. The excited analyte
characteristic wavelengths that can be dispersed with a monochromator and detected.
Nicke
l
Ni
Zinc
Zn
Titaniu
m
Ti
- 5.1-6.1 0.2
<0.01 5.989 0.05
Other Element Al
Total
0.15 Remainder
0.15 Remainder
F. Anand Raju and Dr. M.L.S. Deva Kumar
http://www.iaeme.com/IJMET/index.asp 232 [email protected]
4.2. Mechanical Properties
Table 4 2Al 7075-T6 Metal matrix samples with different compositions by weight ratio.
Sample Weight % of aluminum Weight % of fly ash
Sample-1 100 0
Sample-2 85 15
Sample-3 80 20
Sample-4 75 25
Table 4.3 Mechanical properties of the samples.
Sample Tensile
strength
(N/sq mm)
Yield
strength
(N/sq mm)
Elongation on
50mm G.L
(%)
Impact Test
‘V’ notch(J)
Size
10×10×55mm
Hardness
[ HBW /10 mm ball
dia / 3000 kgf load]
Density
g/cc
Sample-1 586 543 15 9 58 2.89
Sample-2 150 141 6 7 66 2.73
Sample-3 60 55 2 4 78 2.58
Sample-4 73 66 5 6 64 2.75
Figure 4.1 Samples Vs Tensile Strength
Figure 4.2 Samples Vs Yield Strength
0
100
200
300
400
500
600
700
Sample 1 Sample 2 Sample 3 Sample 4
Te
nsi
le S
tre
ng
th (
N/
sq m
m)
Samples
0
100
200
300
400
500
600
Sample 1 Sample 2 Sample 3 Sample 4
Yei
ld s
tren
gth
(N /
sq
mm
)
Samples
Production and Mechanical Characterization of Al-7075-T6 and Fly Ash Composite by Stir Casting Hot Die Process
http://www.iaeme.com/IJMET/index.asp 233 [email protected]
Figure 4.3 Samples Vs Elongation
Figure 4.4 Samples Vs Impact Strength
Figure 4.5 Samples Vs Brinell Hardness (BHN)
0
2
4
6
8
10
12
14
16
Sampe 1 Sample 2 Sample 3 Sample 4
Elo
ng
ati
on
%
Samples
0
1
2
3
4
5
6
7
8
9
10
Sample 1 Sample 2 Sample 3 Sample 4
Imp
act
Str
en
gth
(J)
Samples
0
10
20
30
40
50
60
70
80
90
Sample 1 Sample 2 Sample 3 Sample 4
Bri
ne
ll H
ard
ne
ss (
BH
N)
Samples
F. Anand Raju and Dr. M.L.S. Deva Kumar
http://www.iaeme.com/IJMET/index.asp 234 [email protected]
5. CONCLUSION
The investigation conducted, leads to the following conclusions:
Fly ash is added in the molten aluminum up to 25% by weight ratio by stir casting process for
production of composite material. So the industrial waste turns into industrial wealth. Addition of fly ash
as 15%, 20% and 25% by weight % the tensile strength of the samples reduces and hardness of the samples
is increased. By comparing the four samples, the sample3 with 20% fly ash has highest hardness BHN
78.The weight density of the material is decreased by 20% fly ash addition. By increasing of the hardness,
ware rates significantly reduced.
The study gives the further addition of fly ash and study of microstructure and tribological studies.
Casting the materials in to blooms and slabs to be rolled and extruded as different components for all
applications.
REFERENCE
[1] Mahendra.K.V and Radhakrishna. K, Castable composites and their application in automobiles, Proc.
IMechE Vol. 221 Part D: J. Automobile Engineering, (2007): pp. 135-140
[2] B.VijayaRamnath et al “Aluminium Metal Matrix Composite –A Review” published in Advanced
material science, 38(2014) pp 55-60.
[3] P. Shanmughasundaram1, R. Subramanian2 “Some Studies on Aluminium-Fly Ash Composites
Fabricated by Two Step Stir Casting Method”, European Journal of Scientific Research ISSN 1450-
216X Vol.63 No.2 (2011), pp.204-218.
[4] J.Alam and MN Akhtar “Fly ash Utilisation in different sector in india scenario” published in Internation
journal of emerging trends in Engineering and Development, vol-1 Augest 2011, pp1-14.
[5] P. K. Rohatgi and R. Q. Guo, “Low Cost Cast Aluminium – Fly Ash Composites for Ultra-light
Automotive Application”, TMS Annual Meeting, Automotive Alloys, (1997)
[6] Deepak singla1, S.R. Mediratta2, “Evaluation of Mechanical Properties of Al 7075-Fly Ash Composite
Material”, International Journal of Innovative Research in Science, Engineering and Technology ISSN:
2319-8753 Vol. 2, Issue 4, April 2013
[7] H.C. Anilkumar1, H.S. Hebbar2 and K.S. Ravishankar3 “Mechanical Properties of Fly Ash Reinforced
Aluminium Alloy (Al6061) Composites”, International Journal of Mechanical and Materials
Engineering (IJMME), Vol.6 (2011), No.1, 41-45
[8] sankar.L1, Srinivasan.R2, Viswanathan.P3 and Subramanian.R4, “Comparison Study of Al-Fly Ash
Composites In Automobile Clutch Plates”, from internet
[9] Vivekananthan1 M. and Senthamarai2 k., “Experimental Evaluation of Aluminium-Fly Ash Composite
Material to Increase the Mechanical &Wear Behaviour by Stir Casting Method”,CARE Journal of
Applied Research (ISSN 2321-4090)
[10] K.V. MAHENDRA1, K. R ADHAKRISHNA2, “Fabrication of Al–4.5% Cu Alloy with Fly Ash Metal
Matrix Composites and Its Characterization”, material science-poland, Vol.25, No.1 2007
[11] Hull D, Clyne T W, “An Introduction to Composite Materials, Cambridge”, UK: Cambridge Univ.
Press, 1996
[12] Matthews F.L., Ralwlings R.D, “Composite materials engineering and science”, Glasgow, UK,
Champaman and hall, 1994
Production and Mechanical Characterization of Al-7075-T6 and Fly Ash Composite by Stir Casting Hot Die Process
http://www.iaeme.com/IJMET/index.asp 235 [email protected]
[13] DRDO “Composite Materials”, Popular Science & Technology (PST) series is being published by
DESIDOC, was published in the year 1990
[14] Rohatgi P.K, Metal-matrix Composites, Defence Science Journal, Vol 43, No 4, (1993): pp 323-349.
[15] R.Maguteeswarana, Dr. R.Sivasubramanian and V.Suresh, “Study and Investigation of Analysis of
Metal Matrix Composite”, International Journal of Mechanical Engineering & Technology (IJMET),
Volume 3, Issue 2, 2012, pp. 171 - 188
[16] R.Maguteeswarana, Dr. R.Sivasubramanian and V.Suresh, “Methodology Study and Analysis of
Magnesium Alloy Metal Matrix Composites”_ International Journal of Mechanical Engineering &
Technology (IJMET), Volume 3, Issue 2, 2012, pp. 217 - 224