International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 07 | July 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2052
TRIBOLOGICAL INVESTIGATION OF Al7075/TIC/MOS2 HYBRID
COMPOSITE MATERIAL
Ms. Kanchan A. More
1
, Prof. Suyash Y. Pawar
2
1
PG Student, M.E. (Mechanical) (Design Engineering), NDMVPs KBT College of Engineering, Nashik, Maharashtra,
India
2
Asst. Professor, Mechanical Department, NDMVPs KBT College of Engineering, Nashik, Maharashtra, India
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Abstract - In this paper, wear behavior of hybrid composites
of Al7075 alloy reinforced with TiC & MoS2 was investigated at
ambient & elevated temperature. Al7075/TiC/MoS2 specimens
were prepared by the method of stir casting. The pin on disc
apparatus was used to evaluate the wear behavior of
specimens. Taguchi technique was used for optimization.
Minitab 18 software was used for the statistical analysis
purpose. An orthogonal L9 arrays were formed. The influence
of various parameters such as applied load, temperature,
sliding distance & % of reinforcement were investigated by
ANOVA. For analysis, MINITAB 18 software was used. Further
regression equations were used to determine the correlation
between the parameters. The most influencing parameters
found by S/N ratio. Results revealed that reinforcement shows
negative influence on weight loss. weight loss decreases with
increasing reinforcement. Applied load, sliding distance &
temperature was influencing factors in wear resistance.
Key Words: ANOVA, MINITAB 18, regression analysis, S/N
ratio, orthogonal array, wear behavior, Taguchi technique.
1. INTRODUCTION
Today’s technology offers materials which were light in
weight and cost effective. This leads to development of
advanced materials which possesses excellent properties
like high stiffness, high specific strength along with superior
wear resistance. Durability of any machine part is vital
design consideration. There are many factors that directly
influence the life of machine component. So, the biggest
challenge in front of design engineer is careful material
selection for particular application. Many engineering
components in aviation, marine and automobile industries
like rock climbing equipment, bicycle components, inline
skating-frames and hang glider airframes has to possesses
properties like high strength to weight ratio, improves wear
resistance, corrosion resistance, high toughness both at
ambient and elevated temperature condition.
Therefore, hybrid metal matrix composites are now a day
considered to be smart alternative because of their superior
tribological properties at both ambient and elevated
temperature condition. Reinforcing aluminium alloy with
other materials increases its temperature range in wear
limited application like crankshaft, piston, cylinder heads,
manifolds and heat exchangers. So, the present work focuses
on development and tribological characterization of hybrid
aluminium metal matrix composites for automobile and
aerospace application.
2. LITERATURE REVIEW
Belete Sirahbizu Yigezu et al. had studied the abrasive wear
characteristics of the in situ synthesized Al–12% Si/TiC
composites were investigated based on the plan of full
factorial design. During the experiment applied load, sliding
distance, and weight percentage of reinforcement
considered as input parameters and weight loss and
coefficient of friction are considered as response parameters.
The experimental result revealed that for the coefficient of
friction sliding distance and weight percentage of
reinforcement are most dominating factors. On the hand, for
weight loss applied load was most dominating factor [1]. R.
Anand Kumar et al. had studied Al–12% Si aluminium matrix
reinforced with TiC powder and composite was prepared by
the process of metal cladding. SiC, TiC, TaC, B4C, WC were
most widely used reinforcement materials in MMC. TiC was
mostly attractive due to its high hardness, low heat
conductive coefficient, high elastic modulus, high melting
point, especially it’s thermodynamic stability and good
wettability with molten aluminium [2]. S. Jerome et al. had
studied in situ Al-TiC (5 wt.%, 10 wt.%, 15 wt.%) composites
were produced. The wear tests were conducted at room
temperature 120
0
c & 200
0
c. Reinforcement shows the
negative influence on the weight loss. Weight loss decreases
with increasing reinforcement percentage of TiC at all
temperature. On the other hand, wear rate increases with
the increase in applied load. Results revealed that at room
temperature transfer layer formation mechanism dominates
the wear rate while at the elevated temperature wear rate
reduces with oxidative layer formation [3]. Anand Kumar et
al. were investigated abrasive wear modeling of in-situ Al-
4.5% Cu /TiC metal matrix composite based on full factorial
design. In the experiment applied load, sliding distance &
weight % of reinforcement in the metal matrix were treated
as control factors. It has also been observed that sliding
distance was most dominating factor for the coefficient of
friction. As sliding distance increases coefficient of friction
also increases. On the other hand, weight loss increases with
increase in applied load and sliding distance. Whereas
reinforcement shows the negative influence on the weight
loss, weight loss decreases with increasing reinforcement.