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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 272
STUDY AND EFFECT OF ABRASIVE WEAR BEHAVIOR OF KEVLAR
Mohammad Faran Jamal1, Dr. Md Shadab Khan2, Er. Abdul Ahed Khan3
1Research Scholar, Department of Mechanical Engineering, Integral University, Lucknow, U.P., India
2,3Associate Professor, Department of Mechanical Engineering, Integral University, Lucknow, U.P., India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - Abrasive wear phenomena are simply caused by
the passage of relatively hard particles or asperities over a
surface. It directly affects the life of the component. A
systematic study of abrasive wear of Kevlar has been carried
out using a two body pin-on-disc wear machine. The objective
of this study was to evaluate the abrasive wear of Kevlar fiber
(after mixing it with epoxy resin) by grinding it at constant
load of 10N but at different rpm. A Kevlar often described as
being "five times stronger than steelonanequal weightbasis".
In particular, up to date aramid have been extensively used in
personal protection, tires, equipment, shoes, building
construction and marine application by virtue of their very
strong tensile strength. So, in this thesis a study of abrasive
wear of Kevlar at different speed were given to analyze the
possibility of wear. A review of abrasive wear behavior of
Kevlar using different wear rate speed has been discussed in
this thesis. Mainly focus on the varying wear condition during
varying rpm. As we all know that wear is very important
parameter which directly affects the life of a component. The
goal of this study was to evaluate abrasive wear only. The
result of the study indicates several measuring wear rate
technique till date.
It is concluded that-
 Wear volume increases with increasing
applied load.
 The loss in mass is maximum at zero degree
(horizontal position) for a particular load
 At horizontal position (zerodegree)twobody
abrasion takes place most of the time.
Key Words: Abrasive wear, Kevlar fibre, Epoxy resin,
Aramid, Asperities
1. INTRODUCTION
A synthetic material Kevlar® is a plastic strong enough to
stop bullets and knives—oftendescribedasbeing"fivetimes
stronger than steel on an equal weight basis. Unlike most
plastics it does not melt: it'sreasonablygoodatwithstanding
temperatures and decomposes only at about
450°C (850°F)." Kevlar is simply a super-strong plastic.
Kevlar's amazing properties are partly due to its internal
structure (how its molecules are naturally arranged in
regular, parallel lines) and partly due to the way it's made
into fibers that are knitted together. It's a proprietary
material made only bytheDuPont™chemical companyandit
comes in two main varieties called Kevlar 29 and Kevlar 49
(other varieties are made for special applications).
1.1 Properties of Kevlar
 It's strong but relatively light. The specific tensile
strength (stretching or pulling strength) of both
Kevlar 29 and Kevlar 49 is over eight times greater
than that of steel wire.
 Unlike its sister material, Nomex, Kevlar can be
ignited but burning usually stops when the heat
source is removed.
 Very low temperatures have no effect on Kevlar:
DuPont found "no embrittlement or degradation"
down to −196°C (−320°F).
 Kevlar can resist attacks from many different
chemicals, though long exposure to strong acids or
bases will degrade it over time.
There are two main stages involved in making
Kevlar. First you have to produce the basic plastic
from which Kevlar is made (a chemical called poly-
paraphenylene-terephthalamide no wonder they call
it Kevlar). Second, you have to turn it into strong
fibers. So the first step is all about chemistry; the
second one is about turning your chemical product
into a more useful, practical material.
Fig-1 Kevlar's monomer: C=carbon,H=hydrogen,O=oyxgen,
N=nitrogen, — is a single chemical bond, and = is a double
bond. This basic building block is repeated over and over
again in the very long chains that make up the Kevlar
polymer.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 273
1.2 Melting point of Kevlar
The melting point of Kevlar is above 500 °C (930 °F). The
higher melting point of Kevlar, as well as its greater stiffness
and tensile strength, partly results from the regular para-
orientation of its molecules.Insolutionthepolymerassumes
a liquid-crystal arrangement, whichorientsthemolecules so
that they can be spun and drawn into highly ordered fibres
of ultrahigh stiffness and strength
1.3 Abrasive wear
Abrasive wear takes place due torubbingofsoftersurface by
the harder surface. In the case of ductile materials, hard
particles or hard asperities results in plastic flow of softer
material. In brittle materials, wear occurs by brittlefracture.
Abrasion is categorized dependingonthetypesofcontact, as
well as contact environment. Depending on the types of
contacts, abrasive wear can be classified as two-body and
three-body wear. The former occurs due to an abrasive
slides along a surface, and the later, due to an abrasive is
caught between one surface and another. Figure shows the
schematic representation of two body and three body wear
mechanisms.
Fig-2
Two-body abrasive wear involvestheremoval ofmaterial by
abrasive particles which are held fixed(asinabrasivepaper)
while being moved across a surface. This processproducesa
grooving form of wear.
Three-body abrasion involves loose particles which may
rotate as well as slide as they contact the wearing surface.
Compared to two-body abrasion, three-body abrasion is
much more common and also much more complicated than
two-body abrasion.
2. PROBLEM FORMULATION
The problem stated above is based on mathematical model
proposed by Fillot et al, according to Fillot et al thepresence
of wear particles in the system will act as a dry lubricant. To
formulate an analytical model the author first composes a
particular definition of the third body concept stating that
wear is a process characterized by three distinct phases:
material detachment from the surface of a body, the mass of
particles within the contact area and finally the ejection of
particulate matter from the system; referring to figure 1
these are Qs, Mi and Qw respectively. As a result the change
in mass of particles within the system can be written as a
function of the two volume flow rates, as given in equation;
the author refers to this as the mass equilibrium equation
(i.e. it is a mass balance).
dMi/dt = Qs – Qw
Subsequently the authordefinedtworelationshipsthatwere
essential in this wear analysis, these are the connection
between Qs and Mi and secondly between Qw and Mi. Fig.
shows graphical representation of three body concept.
The first relationship (Qs - Mi) is referred to as the source
flow activation and represents the particle generation
process; as discussed, this was the sole concern of Archard’s
wear law. The author considers this in three stages. Firstly
he states that the normal pressureappliedacrossthecontact
will be equally shared by the surfaces and the third body.
Furthermore he states that the total sliding distance
occurring in the system will be composed of the sliding
distance of the two surfaces and the sliding distance of the
third body, which represents the shear occurring between
particles, and uses this definition to arrive at equation 1.
dXtotal = dXFB + dXTB (1)
Where dXtotal is the total sliding distance, dXFB is the
sliding distance of the contacting surfaces and dXTB is the
sliding distance of Mi. The total velocity of the system is the
rate of change of distance with respect to time and therefore
can be written in equation 2.
V = dXFB/dt + dXTB/dt (2)
Where V is the total velocity of the system. The author now
considers the occurrence of shear within the system, stating
that, as a preference, shear will occur in the third body
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 274
rather than at the contacting surfaces as long as it is “easier”
to do so. This will cease to be the case when the maximum
value of shear stress has been obtained within the third
body; hence at τmax. The shear rate can then be expressed
as a function of the max shear stress andthereforea function
of the velocity within the third body and its thickness as
shown in equation 3.
ν = 1/HTB * dXTB/dt (3)
Where ν is the shear rate, HTB is the height of the third
body. If the shear rate of the system is assumed to be a
constant then the velocity of the third body is proportional
to its height. Therefore the mass of the third body can be
related to the sliding velocity:
dXTB/dt = aMi (4)
Where ‘a’ is a constant of proportionality. The variable Qs is
considered with respect to the sliding velocity of the bodies
in contact. Referring to Archard the volume of material
removed from the body is proportional to the sliding
distance; hence the rate of change of volume produced
(volume flow-rate Qs) will be proportional to the rate of
change of sliding distance (i.e. velocity)
dXFB /dt = bQs (5)
Where ‘b’ is a constant of proportionality. Equations5,4and
2 can now be combined to find a relationship between Qs
and Mi and it is given as:
Qs = Cs (Mimax - Mi ) (6)
From this last equation (eq. no. 6) it can be seenthattheflow
of material from the contact surfaces is proportional to the
mass of material already trapped in the contact area. The
author does not examine the process of material removal
from the surfaces in great detail but he proposes that
material removal will occur when the energy present in the
system cannot be absorbed by the third body.
To conclude the author restates that the aim of this work
was not to refine or continueexistingwearlawsandthinking
but to look at this problem from a new angle in order to
better describe, predict and understand wear. The author
also raises the question surrounding the pin on disc test: i.e.
why the wear process is dependent on the orientation in
which the apparatus is configured. Therefore the author
incorporates the way in which a particle leaves the contact
area to try and account for this phenomenon. He suggests
that a large amount of time has been spent in defining and
investigating the various wear mechanisms but there is a
distinct dearth of information on the methods of material
expulsion.
3. METHODOLOGY
Numerous researches have been doneinthefieldofabrasive
wear. This work is also an experimental design in the fieldof
abrasive wear evaluation via a newly designed wear test rig.
In view of the objective a set-up was needed to be designed
which can calculate wear rate at different speed (rpm) of
work piece with respect to the main frame (horizontal
position). A pin on disc wear test technique was adopted to
test the wear behavior of specimens.
Wear rate and wear mass were evaluated at different
orientation of the specimen. The tests were conducted for
seven different orientations namely 400rpm, 500rpm,
600rpm, 700rpm, 800rpm, 900rpm, 1000rpm. The wear
mass of above said specimen evaluated at a constant time of
5min (300 sec).
The set up has following different parts-:
(1)Controller (2)D.C. Motor (3)Flange Coupling (4)Bearing
(5)Main Frame (6)Frame(Angular) (7)Acrylic Sheet (8)
Grinding Wheel (9) Specimen (10) Screw Jack (11)LoadCell
(12) Angular Lever.
Fig-3
3.1 Working of set-up
DC motor is connected to regulator through a suitable
electrical wiring. Further, flange coupling connects D.C
motor to a shaft. A key is provided for connecting DC motor
and shaft. Grinding disc is connected to one end of the shaft
which is supported by two bearings. The specimen is fitted
in specimen holder. The specimen holder is made of wood;a
slot equal to the size of cross-section of specimen is made in
it, to properly hold the same. The samples are fastened with
the fixture in these slots, one at a time and the wear test is
performed. The fixture is fitted in acrylic sheet having
multiple holes along the radius of the sheet. These holes are
made in such a way to get fresh surface along grinding disc.
At the end of the acrylic sheet there is attachment to apply a
load. The load is applied with help of screw jack, as the
screw jack moves forward it pushes the acrylic sheet with
help of shaft which connects screw jack and acrylic sheet.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 275
3.2 Specimen’s material
The specimen was selected for present investigation is a
mixture of two materials namely Kevlar & Resin.
As Kevlar is in the form of fibers, it is not possible to apply
abrasion process on fibers in pin on disc setup. To resolve
this issue Epoxy Resin is used which holds the fibers on its
exact shape and location.
Resin-- Generally it is a viscous (liquid or semi liquid)
substance that reacts to certain conditions (usually heat) or
another substance (aka a hardener). The reaction is
polymerization, which is the formation of long molecular
chains transforming the substance into a solidwithadhesive
properties during the transitioning.
4. RESULT
The results on weight loss have been presentedasa function
of sliding distance against grinding Disc. The wear rate has
been evaluated in term of weight loss in the entire specimen
investigated.
All the calculations is investigated by weighting the
specimen before grinding and after grinding and then the
loss of weight after abrasion is considered as the wear rate.
The wear rate increases gradually at different rpm.
As the wear studies were conducted against the abrasive
media (grinding disc). The selection of applied load and the
position of the specimen for wear studies were takenas10N
and 0º. Seven reading of wear were taken from seven
specimens at different rpm. The result shows that as the
speed (rpm) increases the wear rate of the specimen
increases for a same load.
Wear Initiated at Different rpm
(rpm) Weight
before
grinding
Weight
after
grinding
Total
weight loss
At 400 rpm 9.487 gm 8.883 gm 0.604 mg
At 500 rpm 7.459 gm 6.722 gm 0.737 mg
At 600 rpm 9.203 gm 7.970 gm 1.233 gm
At 700 rpm 8.876 gm 7.047 gm 1.829 gm
At 800 rpm 10.056 gm 7.114 gm 2.942 gm
At 900 rpm 9.659 gm 6.245 gm 3.414 gm
At 1000 rpm 8.386 gm 5.060 gm 3.326 gm
5. CONCLUSION
It is concluded from the above discussion that wear is
function of orientation and applied load. Initially, it was
understood that wear depends upon applied load, surface
parameters and mechanical properties such as hardness,
toughness etc. But now it clear that it not only dependsupon
the above said parameters but also depends on orientation
of surface in contact with the abrasive media with the
horizontal surface. The movement of the debri particles
plays an important role in this regard. At horizontal position
the weight and centrifugal force are parallel to each other
and most of the debri particles falls due this resultant force
from abrasive media , due to this the specimen gets fresh
abrasive surface most of the time which results in higher
abrasive wear. If orientation changes from 0º to 90º the
wear resistance increases or wears decreases.
It is concluded that:
 The loss in mass is maximum at zero degree
(horizontal position) for a particular load.
 The loss in mass is minimum at 90 degree (vertical
position) for a particular load.
 Maximum wear occur when the test specimen is
held at 0º angle
 Minimum wear occur when the specimen is held at
90º angle for given applied load
 At horizontal position (zero degree) two body
abrasion takes place most of the time.
 Two body abrasion converted intothreebodywhen
orientation of set up changes from 0 to 90 degree
due change in the behavior of debri particles.
 It was also apparent from the quadratic regression
equations that regression coefficients positive in
case of applied load and negative in case of
orientation hence wear rate is directlyproportional
to the applied load andinverselyproportional tothe
orientation as it changes from 0º to 90º. of the
model surface to be best fitted, as the regression
equation was highly significant . Thus, the fitted
mathematical equation gives fairly accurate
prediction of wear rate.
6. REFERENCES
[1] "What is Kevlar". DuPont. Retrieved 2007-03-28.
[2] "Wholly aromatic carbocyclic polycarbonamide fiber
having orientation... - US 3819587 A - IP.com". ip.com.
[3] "Stephanie Louise Kwolek Biography". Bookrags.
Archived from the original on May 24, 2009.
Retrieved May 24, 2009.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 276
[4] How Kevlar® works: a simple introduction.
Explainthatstuff.com (2009-12-07). Retrieved on2012-
05-26.
[5] Michael C. Petty, Molecular electronics: from principles
to practice, John Wiley & Sons, 2007, p. 310
[6] KEVLAR Technical Guide. dupont.com. Retrieved on
2012-05-26.
[7] Kevlar – DuPont Personal Protection. .dupont.com.
Retrieved on 2012-05-26.
[8] Gong (Ed), RH (2011). Specialist Yarn and Fabric
Structures: Developments and Applications. Woodhead
Publishing. p. 349. ISBN 9781845697570.
[9] B. Suresha, G. Chandramohan, Three-body Abrasive
Wear Behaviour of Particulate-filled Glass–vinyl Ester
Composites, Journal ofMaterialsProcessingTechnology,
200 (2008), pp. 306–311.
[10] J. R. Davis, Surface Engineering for Corrosion and Wear
Resistance, ASM International, USA (2001).
[11] J. K. Lancaster, Abrasive Wear of Polymers, Wear, 14
(1969), pp. 223-239.
[12] J. K. Telford, A Brief Introduction to Design of
Experiments, Johns Hopkins Apl Technical Digest, 27
(2007), pp. 224-232.
[13] T., Jankauskas, V.; Skirkus, R.; Martinkus, N. 2011 ‘The
Abrasive Wear Research Of Arc Welded Surfaces Into
Embedded Abrasive , Journal Zemes Ukio Inzinerija,
Mokslo Darbai Vol. 43 No. 4 Pp. 28-37 Issn 1392-1134
Record Number 20123116718.
[14] Williams, J. A. (2005). "Wear And Wear Particles - Some
Fundamentals." TribologyInternational,38(10)Pg863-
870.
[15] Zaamout M.S., (2004 A.D./1425 A.H.) Investigating The
Abrasive Wear Behaviour Of Locally Used Automotive
Paint, Kau: Eng. Sci.,Vol. 15 No. 2, Pp. 81-96 .
[16] Q Wang, Z H Chen, Z X Ding And Z L Liu (2008).
‘Performance Study Of AbrasiveWearAndErosiveWear
Of Wc-12co Coatings Sprayed By Hvof’. In Proceedings:
2nd Ieee International Nanoelectronics Conference
(Inec) Pp 340- 344.
[17] J.M. Wu , Z.Z. Li, ( 2000) “Contributions Of The
Particulate Reinforcement To Dry Sliding Wear
Resistance Of Rapidly Solidified Al-Ti Alloys”,Wear244,
147–153,.

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  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 272 STUDY AND EFFECT OF ABRASIVE WEAR BEHAVIOR OF KEVLAR Mohammad Faran Jamal1, Dr. Md Shadab Khan2, Er. Abdul Ahed Khan3 1Research Scholar, Department of Mechanical Engineering, Integral University, Lucknow, U.P., India 2,3Associate Professor, Department of Mechanical Engineering, Integral University, Lucknow, U.P., India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - Abrasive wear phenomena are simply caused by the passage of relatively hard particles or asperities over a surface. It directly affects the life of the component. A systematic study of abrasive wear of Kevlar has been carried out using a two body pin-on-disc wear machine. The objective of this study was to evaluate the abrasive wear of Kevlar fiber (after mixing it with epoxy resin) by grinding it at constant load of 10N but at different rpm. A Kevlar often described as being "five times stronger than steelonanequal weightbasis". In particular, up to date aramid have been extensively used in personal protection, tires, equipment, shoes, building construction and marine application by virtue of their very strong tensile strength. So, in this thesis a study of abrasive wear of Kevlar at different speed were given to analyze the possibility of wear. A review of abrasive wear behavior of Kevlar using different wear rate speed has been discussed in this thesis. Mainly focus on the varying wear condition during varying rpm. As we all know that wear is very important parameter which directly affects the life of a component. The goal of this study was to evaluate abrasive wear only. The result of the study indicates several measuring wear rate technique till date. It is concluded that-  Wear volume increases with increasing applied load.  The loss in mass is maximum at zero degree (horizontal position) for a particular load  At horizontal position (zerodegree)twobody abrasion takes place most of the time. Key Words: Abrasive wear, Kevlar fibre, Epoxy resin, Aramid, Asperities 1. INTRODUCTION A synthetic material Kevlar® is a plastic strong enough to stop bullets and knives—oftendescribedasbeing"fivetimes stronger than steel on an equal weight basis. Unlike most plastics it does not melt: it'sreasonablygoodatwithstanding temperatures and decomposes only at about 450°C (850°F)." Kevlar is simply a super-strong plastic. Kevlar's amazing properties are partly due to its internal structure (how its molecules are naturally arranged in regular, parallel lines) and partly due to the way it's made into fibers that are knitted together. It's a proprietary material made only bytheDuPont™chemical companyandit comes in two main varieties called Kevlar 29 and Kevlar 49 (other varieties are made for special applications). 1.1 Properties of Kevlar  It's strong but relatively light. The specific tensile strength (stretching or pulling strength) of both Kevlar 29 and Kevlar 49 is over eight times greater than that of steel wire.  Unlike its sister material, Nomex, Kevlar can be ignited but burning usually stops when the heat source is removed.  Very low temperatures have no effect on Kevlar: DuPont found "no embrittlement or degradation" down to −196°C (−320°F).  Kevlar can resist attacks from many different chemicals, though long exposure to strong acids or bases will degrade it over time. There are two main stages involved in making Kevlar. First you have to produce the basic plastic from which Kevlar is made (a chemical called poly- paraphenylene-terephthalamide no wonder they call it Kevlar). Second, you have to turn it into strong fibers. So the first step is all about chemistry; the second one is about turning your chemical product into a more useful, practical material. Fig-1 Kevlar's monomer: C=carbon,H=hydrogen,O=oyxgen, N=nitrogen, — is a single chemical bond, and = is a double bond. This basic building block is repeated over and over again in the very long chains that make up the Kevlar polymer.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 273 1.2 Melting point of Kevlar The melting point of Kevlar is above 500 °C (930 °F). The higher melting point of Kevlar, as well as its greater stiffness and tensile strength, partly results from the regular para- orientation of its molecules.Insolutionthepolymerassumes a liquid-crystal arrangement, whichorientsthemolecules so that they can be spun and drawn into highly ordered fibres of ultrahigh stiffness and strength 1.3 Abrasive wear Abrasive wear takes place due torubbingofsoftersurface by the harder surface. In the case of ductile materials, hard particles or hard asperities results in plastic flow of softer material. In brittle materials, wear occurs by brittlefracture. Abrasion is categorized dependingonthetypesofcontact, as well as contact environment. Depending on the types of contacts, abrasive wear can be classified as two-body and three-body wear. The former occurs due to an abrasive slides along a surface, and the later, due to an abrasive is caught between one surface and another. Figure shows the schematic representation of two body and three body wear mechanisms. Fig-2 Two-body abrasive wear involvestheremoval ofmaterial by abrasive particles which are held fixed(asinabrasivepaper) while being moved across a surface. This processproducesa grooving form of wear. Three-body abrasion involves loose particles which may rotate as well as slide as they contact the wearing surface. Compared to two-body abrasion, three-body abrasion is much more common and also much more complicated than two-body abrasion. 2. PROBLEM FORMULATION The problem stated above is based on mathematical model proposed by Fillot et al, according to Fillot et al thepresence of wear particles in the system will act as a dry lubricant. To formulate an analytical model the author first composes a particular definition of the third body concept stating that wear is a process characterized by three distinct phases: material detachment from the surface of a body, the mass of particles within the contact area and finally the ejection of particulate matter from the system; referring to figure 1 these are Qs, Mi and Qw respectively. As a result the change in mass of particles within the system can be written as a function of the two volume flow rates, as given in equation; the author refers to this as the mass equilibrium equation (i.e. it is a mass balance). dMi/dt = Qs – Qw Subsequently the authordefinedtworelationshipsthatwere essential in this wear analysis, these are the connection between Qs and Mi and secondly between Qw and Mi. Fig. shows graphical representation of three body concept. The first relationship (Qs - Mi) is referred to as the source flow activation and represents the particle generation process; as discussed, this was the sole concern of Archard’s wear law. The author considers this in three stages. Firstly he states that the normal pressureappliedacrossthecontact will be equally shared by the surfaces and the third body. Furthermore he states that the total sliding distance occurring in the system will be composed of the sliding distance of the two surfaces and the sliding distance of the third body, which represents the shear occurring between particles, and uses this definition to arrive at equation 1. dXtotal = dXFB + dXTB (1) Where dXtotal is the total sliding distance, dXFB is the sliding distance of the contacting surfaces and dXTB is the sliding distance of Mi. The total velocity of the system is the rate of change of distance with respect to time and therefore can be written in equation 2. V = dXFB/dt + dXTB/dt (2) Where V is the total velocity of the system. The author now considers the occurrence of shear within the system, stating that, as a preference, shear will occur in the third body
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 274 rather than at the contacting surfaces as long as it is “easier” to do so. This will cease to be the case when the maximum value of shear stress has been obtained within the third body; hence at τmax. The shear rate can then be expressed as a function of the max shear stress andthereforea function of the velocity within the third body and its thickness as shown in equation 3. ν = 1/HTB * dXTB/dt (3) Where ν is the shear rate, HTB is the height of the third body. If the shear rate of the system is assumed to be a constant then the velocity of the third body is proportional to its height. Therefore the mass of the third body can be related to the sliding velocity: dXTB/dt = aMi (4) Where ‘a’ is a constant of proportionality. The variable Qs is considered with respect to the sliding velocity of the bodies in contact. Referring to Archard the volume of material removed from the body is proportional to the sliding distance; hence the rate of change of volume produced (volume flow-rate Qs) will be proportional to the rate of change of sliding distance (i.e. velocity) dXFB /dt = bQs (5) Where ‘b’ is a constant of proportionality. Equations5,4and 2 can now be combined to find a relationship between Qs and Mi and it is given as: Qs = Cs (Mimax - Mi ) (6) From this last equation (eq. no. 6) it can be seenthattheflow of material from the contact surfaces is proportional to the mass of material already trapped in the contact area. The author does not examine the process of material removal from the surfaces in great detail but he proposes that material removal will occur when the energy present in the system cannot be absorbed by the third body. To conclude the author restates that the aim of this work was not to refine or continueexistingwearlawsandthinking but to look at this problem from a new angle in order to better describe, predict and understand wear. The author also raises the question surrounding the pin on disc test: i.e. why the wear process is dependent on the orientation in which the apparatus is configured. Therefore the author incorporates the way in which a particle leaves the contact area to try and account for this phenomenon. He suggests that a large amount of time has been spent in defining and investigating the various wear mechanisms but there is a distinct dearth of information on the methods of material expulsion. 3. METHODOLOGY Numerous researches have been doneinthefieldofabrasive wear. This work is also an experimental design in the fieldof abrasive wear evaluation via a newly designed wear test rig. In view of the objective a set-up was needed to be designed which can calculate wear rate at different speed (rpm) of work piece with respect to the main frame (horizontal position). A pin on disc wear test technique was adopted to test the wear behavior of specimens. Wear rate and wear mass were evaluated at different orientation of the specimen. The tests were conducted for seven different orientations namely 400rpm, 500rpm, 600rpm, 700rpm, 800rpm, 900rpm, 1000rpm. The wear mass of above said specimen evaluated at a constant time of 5min (300 sec). The set up has following different parts-: (1)Controller (2)D.C. Motor (3)Flange Coupling (4)Bearing (5)Main Frame (6)Frame(Angular) (7)Acrylic Sheet (8) Grinding Wheel (9) Specimen (10) Screw Jack (11)LoadCell (12) Angular Lever. Fig-3 3.1 Working of set-up DC motor is connected to regulator through a suitable electrical wiring. Further, flange coupling connects D.C motor to a shaft. A key is provided for connecting DC motor and shaft. Grinding disc is connected to one end of the shaft which is supported by two bearings. The specimen is fitted in specimen holder. The specimen holder is made of wood;a slot equal to the size of cross-section of specimen is made in it, to properly hold the same. The samples are fastened with the fixture in these slots, one at a time and the wear test is performed. The fixture is fitted in acrylic sheet having multiple holes along the radius of the sheet. These holes are made in such a way to get fresh surface along grinding disc. At the end of the acrylic sheet there is attachment to apply a load. The load is applied with help of screw jack, as the screw jack moves forward it pushes the acrylic sheet with help of shaft which connects screw jack and acrylic sheet.
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 275 3.2 Specimen’s material The specimen was selected for present investigation is a mixture of two materials namely Kevlar & Resin. As Kevlar is in the form of fibers, it is not possible to apply abrasion process on fibers in pin on disc setup. To resolve this issue Epoxy Resin is used which holds the fibers on its exact shape and location. Resin-- Generally it is a viscous (liquid or semi liquid) substance that reacts to certain conditions (usually heat) or another substance (aka a hardener). The reaction is polymerization, which is the formation of long molecular chains transforming the substance into a solidwithadhesive properties during the transitioning. 4. RESULT The results on weight loss have been presentedasa function of sliding distance against grinding Disc. The wear rate has been evaluated in term of weight loss in the entire specimen investigated. All the calculations is investigated by weighting the specimen before grinding and after grinding and then the loss of weight after abrasion is considered as the wear rate. The wear rate increases gradually at different rpm. As the wear studies were conducted against the abrasive media (grinding disc). The selection of applied load and the position of the specimen for wear studies were takenas10N and 0º. Seven reading of wear were taken from seven specimens at different rpm. The result shows that as the speed (rpm) increases the wear rate of the specimen increases for a same load. Wear Initiated at Different rpm (rpm) Weight before grinding Weight after grinding Total weight loss At 400 rpm 9.487 gm 8.883 gm 0.604 mg At 500 rpm 7.459 gm 6.722 gm 0.737 mg At 600 rpm 9.203 gm 7.970 gm 1.233 gm At 700 rpm 8.876 gm 7.047 gm 1.829 gm At 800 rpm 10.056 gm 7.114 gm 2.942 gm At 900 rpm 9.659 gm 6.245 gm 3.414 gm At 1000 rpm 8.386 gm 5.060 gm 3.326 gm 5. CONCLUSION It is concluded from the above discussion that wear is function of orientation and applied load. Initially, it was understood that wear depends upon applied load, surface parameters and mechanical properties such as hardness, toughness etc. But now it clear that it not only dependsupon the above said parameters but also depends on orientation of surface in contact with the abrasive media with the horizontal surface. The movement of the debri particles plays an important role in this regard. At horizontal position the weight and centrifugal force are parallel to each other and most of the debri particles falls due this resultant force from abrasive media , due to this the specimen gets fresh abrasive surface most of the time which results in higher abrasive wear. If orientation changes from 0º to 90º the wear resistance increases or wears decreases. It is concluded that:  The loss in mass is maximum at zero degree (horizontal position) for a particular load.  The loss in mass is minimum at 90 degree (vertical position) for a particular load.  Maximum wear occur when the test specimen is held at 0º angle  Minimum wear occur when the specimen is held at 90º angle for given applied load  At horizontal position (zero degree) two body abrasion takes place most of the time.  Two body abrasion converted intothreebodywhen orientation of set up changes from 0 to 90 degree due change in the behavior of debri particles.  It was also apparent from the quadratic regression equations that regression coefficients positive in case of applied load and negative in case of orientation hence wear rate is directlyproportional to the applied load andinverselyproportional tothe orientation as it changes from 0º to 90º. of the model surface to be best fitted, as the regression equation was highly significant . Thus, the fitted mathematical equation gives fairly accurate prediction of wear rate. 6. REFERENCES [1] "What is Kevlar". DuPont. Retrieved 2007-03-28. [2] "Wholly aromatic carbocyclic polycarbonamide fiber having orientation... - US 3819587 A - IP.com". ip.com. [3] "Stephanie Louise Kwolek Biography". Bookrags. Archived from the original on May 24, 2009. Retrieved May 24, 2009.
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 08 | Aug 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 276 [4] How Kevlar® works: a simple introduction. Explainthatstuff.com (2009-12-07). Retrieved on2012- 05-26. [5] Michael C. Petty, Molecular electronics: from principles to practice, John Wiley & Sons, 2007, p. 310 [6] KEVLAR Technical Guide. dupont.com. Retrieved on 2012-05-26. [7] Kevlar – DuPont Personal Protection. .dupont.com. Retrieved on 2012-05-26. [8] Gong (Ed), RH (2011). Specialist Yarn and Fabric Structures: Developments and Applications. Woodhead Publishing. p. 349. ISBN 9781845697570. [9] B. Suresha, G. Chandramohan, Three-body Abrasive Wear Behaviour of Particulate-filled Glass–vinyl Ester Composites, Journal ofMaterialsProcessingTechnology, 200 (2008), pp. 306–311. [10] J. R. Davis, Surface Engineering for Corrosion and Wear Resistance, ASM International, USA (2001). [11] J. K. Lancaster, Abrasive Wear of Polymers, Wear, 14 (1969), pp. 223-239. [12] J. K. Telford, A Brief Introduction to Design of Experiments, Johns Hopkins Apl Technical Digest, 27 (2007), pp. 224-232. [13] T., Jankauskas, V.; Skirkus, R.; Martinkus, N. 2011 ‘The Abrasive Wear Research Of Arc Welded Surfaces Into Embedded Abrasive , Journal Zemes Ukio Inzinerija, Mokslo Darbai Vol. 43 No. 4 Pp. 28-37 Issn 1392-1134 Record Number 20123116718. [14] Williams, J. A. (2005). "Wear And Wear Particles - Some Fundamentals." TribologyInternational,38(10)Pg863- 870. [15] Zaamout M.S., (2004 A.D./1425 A.H.) Investigating The Abrasive Wear Behaviour Of Locally Used Automotive Paint, Kau: Eng. Sci.,Vol. 15 No. 2, Pp. 81-96 . [16] Q Wang, Z H Chen, Z X Ding And Z L Liu (2008). ‘Performance Study Of AbrasiveWearAndErosiveWear Of Wc-12co Coatings Sprayed By Hvof’. In Proceedings: 2nd Ieee International Nanoelectronics Conference (Inec) Pp 340- 344. [17] J.M. Wu , Z.Z. Li, ( 2000) “Contributions Of The Particulate Reinforcement To Dry Sliding Wear Resistance Of Rapidly Solidified Al-Ti Alloys”,Wear244, 147–153,.