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Applied Science and Advanced Materials International
Vol. 1 Issue 1 (September – October, 2014) ISSN: 2394-3173
Editorial Advisory Board
Prof. Madhab Ranjan Panigrahi Orissa Engineering College Bhubaneswar 751 007 Dr Swaminathan Sivaram National Chemical Laboratory Dr Homi Bhabha Road Pune 411 008 Dr. Swapan Kumar Dolui Department of Chemical Sciences School of Science and Technology
Tezpur University Napaam, Sonitpur, Assam–784 028 Dr. Sabbu Thomas Mahatma Gandhi University Priyadarshini Hills, Kottayam-686560 Kerala, India Dr. Amulya Kumar Panda National Institute of Immunology JNU Complex New Delhi – 110 067
Editorial Board
Dr. Pulickel Ajayan Rice University Houston, Texas,USA Dr. Ganesh Chandra Sahoo Central Glass and Ceramic Research Institute Kolkata Dr. Dipul Kalita CSIR-North Eastern Institute of Science and Technology Jorhat, Assam
Dr. Prakash P. Wadgaonkar National Chemical Laboratory Pune Dr. Maya Nayak Orissa Engineering College Bhubaneswar Dr. Balbir Singh Kaith National Institute of Technology Jalandhar
Editor: Dr. Biranchinarayan Tosh
E.mail: [email protected] Fax: 0091-06758-239723 Phone: 239737; 9437560248 Website: www.oec.ac.on
Published by Dr. Biranchinarayan Tosh on behalf of Hiranya Kumar Centre for Research & Development, Orissa Engineering College, Bhubaneswar 751 007 Applied Science and Advanced Materials International is issued bimonthly by HKCR&D – OEC and assumes no responsibility for the statements and opinions advanced by the contributors. The editorial staff in the work of examining papers received for publication is assisted, in an honorary capacity, by a large number of distinguished scientists and engineers. Communications regarding contributions for publication in the journal should be addressed to the Editor, Applied Science and Advanced Materials International, Hiranya Kumar Centre for Research and Development, Orissa Engineering College, Bhubaneswar 751 007 Correspondence regarding subscriptions and advertisements should be addressed to the Sales & Distribution Officer, Hiranya Kumar Centre for Research and Development, Orissa Engineering College, Bhubaneswar 751 007 Annual Subscription: Rs 1600.00 $ 300.00* Single Copy: Rs 320.00 $ 60.00* (*Inclusive of first class mail) For inland outstation cheques, please add Rs 50.00 and for foreign cheques, please add $ 10.00. Payments in respect of subscriptions and advertisements may be sent by cheque/bank draft, payable to Hiranya Kumar Centre for Research and Development, Orissa Engineering College, Bhubaneswar 751 007. Bank charges shall be borne by subscriber. Claims for missing numbers of the journal will be allowed only if received within 3 months of the date of issue of the journal plus the time normally required for postal delivery of the journals and the claim. © 2014 Hiranya Kumar Centre for Research and Development, Orissa Engineering College, Bhubaneswar 751 007
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Published by Dr. B Tosh on behalf of HKCR&D, OEC, Bhubaneswar 751 007 and printed at Devee Printers, Nuapatna, Cuttack - 754035
Applied Science and Advanced Materials International Vol. 1 Issue 1 (September – October, 2014)
CONTENTS
Editorial 2
Papers
Novel Composite Materials from Polymeric Waste and Modified Agro-Fiber 3
Himadri Das, Dipanka Dutta, Pallav Saikia, Dipul Kalita and Tridip Goswami
Clarification of tannery wastewater from beam house operation using ceramic 12
MF membrane
Ganesh C. Sahoo, Sourja Ghosh, Swachchha Majumdar and Sibdas Bandyopadhyay
Synthesis, Structural and Electrical Properties of Cu doped ZnO nanoparticles 16
Bikramkeshari Das, Tanushree Das,KajalParashar,S.K.S.Parashar
Low Density Polyethylene/Layered Silicate Nanocomposites: Influence of 21
MAH-g-PE as Compatibiliser on the Morphology, Physical Properties and
Crystallization Characteristics.
Sanghamitra Parija
Impedance Spectroscopy Of Zn0.98Nd0.02O Ceramic By High Energy Ball Milling 28
Tanushree Das, Bikram keshari Das, Kajal Parashar, S. K. S. Parashar,
Sequence Based Prediction of Kink in Transmembrane Helices by 32
Neural Network Method
N Mishra, A Khamari, M R Panigrahi, J K Meher, M K Raval
Author Index 37
Keyword Index 38
2
Applied Science and Advanced Materials International Vol. 1 Issue 1 (September – October, 2014)
Editorial…….
It was 2007, when I had a visit to National Chemical Laboratory, Pune where I had a
fruitful discussion with the then Director, Dr. Swaminathan Sivaram to open a new branch or
carry out research work on Advanced Materials at OEC. In the same year “Hiranya Kumar
Centre for Research and Development” was established in OEC to carry out research on
different thrust areas. The earlier concept was boosted after seven years, when Dr. Madhab
Ranjan Panigrahi, Director Academic/Principal, OEC, discussed with me to publish some in-
house journals. As a result of which, OEC now comes out with two new buds, “Applied Science
and Advanced Materials International” and “International Journal of Energy, Sustainability
and Environmental Engineering”.
While writing the editorial of the first issue, I wish to express my greatest respect to all
members of the editorial advisory board, especially to Dr. S. Sivaram and Dr. M. R. Panigrahi;
all members of the editorial board, especially to Dr. Prakash P. Wadgaonkar, Dr. G. C. Sahoo
and Dr. D. Kalita, whose constant moral support guided me to place the journals before you in
the present format.
I acknowledge to all the contributors, authors, who published their papers in our journal
and respond to my mails immediately for any help during editorial work.
A scientific journal’s greatest responsibility is to ensure that all contributions accepted
for publications are rigorously, but fairly reviewed. We gratefully acknowledge the valued
support of all scientists who have reviewed papers for our journal.
We wish you a very happy Foundation Day and welcome the submission of excellent
articles for the next issue.
Biranchinarayan Tosh
Editor
Applied Science and Advanced Materials International
Vol. 1 (1), September 2014, pp. 3-11
Novel Composite Materials from Polymeric Waste and Modified Agro-Fiber
Himadri Das, Dipanka Dutta, Pallav Saikia, Dipul Kalita* &Tridip Goswami
Cellulose Pulp & Paper Division
CSIR-North East Institute of Science and Technology, Jorhat-785006, Assam, India
Received 01 August 2014; accepted 28 August 2014
Abstract In the present study, an effort has been made to develop a quality composite material using coir fibre and waste
polyethylene by improving the surface properties of coir fibre with the help of chemical treatment under controlled
conditions. Chemical constituents of untreated and treated fibre were analysed by TAPPI standard method. Structural
analyses of these fibres were carried out by FTIR, Electron microscopy, Powder-XRD and Thermogravimetric analysis.
From powder-XRD crystallinity index was found to be higher for chemically modified fiber than untreated fibers. The
characteristics properties i.e. water absorption, total swelling values of the composite board made from different chemically
treated fibers reduced drastically and the mechanical strength properties i. e. ultimate tensile strength (UTS) and modulus of
rupture (MOR) increase significantly. Surface modifications of coir fiber increased the adhesion of fiber matrix which
improves the quality characteristics properties of the composite material.
Keywords Fibers, Composite, Electron microscopy, Modulus of rupture, Coir
In recent years, the use of lignocellulosic fibres or
plant fibres as a replacement for synthetic fibre such
as carbon, aramid, glass fibres in composite and
various areas of engineering have received increasing
attention in light of the growing environmental
awareness throughout the World. The use of natural
fibres as reinforcing materials in both thermoplastic
and thermoset matrix composites provides positive
environmental benefits with respect to ultimate
disposability and best utilization of raw materials1,2
.
Most of the developing countries are very rich in
agricultural fibre and a large part of agricultural waste
is being used as a fuel. India produces more than 400
million tonnes of agricultural waste annually and has
got a very large percentage of total world production
of rice husk, jute, stalk, baggase, groundnut shell and
coconut fibre etc3. These fibres often contribute
greatly to the structural performance of the composite
when used in plastic composites, can provide
significant reinforcement3. Natural fibres are very
attractive for composite materials because of their
advantages compared to synthetic fibres as it causes
lower levels of skin irritation and respiratory
problems during handling, reducing tool wear during
the processing, good recyclability, abundant supply,
low cost, low density, high specific strength to weight
ratio, non-toxicity and biodegrability4-6
. Bio
composite from plant and wood based fibres are used
in a different range of products, including aerospace
materials, automobile industry, building materials
etc7. Plastic materials are indispensable in our
livelihood but they are an important source of
environmental pollution. In order to reduce the
environmental pollution generated from the waste
polyethylene a suitable wood substitute composite
material can be developed from the mixture of natural
fibre and polyethylene waste material. Using biomass
fibres to reinforce plastics has several advantages
over synthetic fibre. They are low cost, low density,
have a high specific strength and modulus
comparatively easy to process due to their
nonabrasive, biodegradable and environment friendly
in nature. The efficiency of the fibre reinforced
composite depends on the fibre-matrix interface and
the ability to transfer stress from the matrix to the
fibre. This stress transfer efficiency plays a dominant
Corresponding Author:
Dipul Kalita
e-mail: [email protected]
4 Appl Sci Adv Mater Int, September 2014
role in determining the mechanical properties of the
composite8.
Coir is an important agro-fibre extracted from the
exocarp of the fruit of coconut palm (Cocosnucifera
L.). It mainly consists of lignin and cellulose. Lignin
is the main constituent and responsible ingredient for
the stiffness of the fibre. It is also responsible partly
for the natural colour of the fibre. Coir fibres are stiff
coarse, resilient, pliable and quite resistant to
bacterial attack. These fibres are widely available in
India, Srilanka, Malaysia, Indonesia and Philippines.
The performance of coir as reinforcement in polymer
composite is not satisfactory comparable to other
natural fibre, because of its low cellulose content,
brittle nature and high microfibrillar angle9. The
efficiency of coir as a reinforcement can be induced
by enhancing the interfacial adhesion between coir
and the polymer matrix. In order to improve the
mechanical properties of these composites, chemical
treatment has been considered as a good technique to
modify the fibre surface to obtain better adhesion
between the fibre and the matrix. Rout et al. (2001)9
studied the influence of fibre treatments (alkali,
blenching, vinyl grafting) on the performance of
coconut coir polyester composites. Rahman and
Khan8 subjected coconut coir fibres to alkali
treatment 5-50% for 0.5 h at temperatures ranging
from 0-100 °C. In the present study, various chemical
treatments like alkali, hydrochloric acid, ethanol-
benzene, acetic acid treatment has been done under
different conditions, in order to improve compatibility
of coir fibres, which are polar and hydrophilic due to
the presence of hydroxyl groups with non-polar and
hydrophobic thermoplastic matrix material. The
surface modification of coir fibres improves adhesion
of fibre-matrix interfaces in a composite, which in
turn improve the mechanical properties of the
composite9-12
.
The suitability of natural fibre composite in a
certain engineering application mainly depends on the
mechanical properties of composite. Therefore, the
present study has been conducted to study the
mechanical properties and in particular the interfacial
performance of composite based on coir fibres and
waste polyethylene as matrix. Ultimate tensile
strength (UTS) and modulus of rupture (MOR) are
two of the mechanical tests that can be made to find
significant basic mechanical properties of natural
fibre composites. Surface modification of coir fibre
by chemical treatment and its effect on mechanical
properties were studied and compared with untreated
fibre.
Experimental Procedure
Materials
Coir fibres were collected from the local market of
Jorhat, Assam. The fibres were cut to a length of
0.005-0.015m. The fibres were rinsed with water to
remove dust and impurities and then boiled in 40ml
of water per 1g fibre at room temperature and also for
killing the bacteria.13
.The polyethylene begs were
collected from the household waste, segregated,
cleaned with warm water. After these processes the
fibres and waste polyethylene were rinsed in tap
water and allowed to dry under sun. The dried fibres
were subjected to various chemical treatments like
sodium hydroxide, acetic acid, hydrochloric acid,
ethanol-benzene solution. All the chemicals were
purchased from spectrochem.
Proximate chemical constituents of coir fibre, was
carried out using the analytical method suggested by
Technical Association of Pulp and Paper Industry
(TAPPI, T-21 cm-86, T-222 om-83, USA) and
standard method of biochemical analysis. The fibres
were washed, dried in oven for 6-8 h at 40±5 °C
temperatures and then powdered in a Wiley mill. The
powder was then screened with 40 and 60 BSS mesh
and the powder fraction passed through 40 BSS mesh
and retained on 60 BSS mesh was taken for different
chemical analysis.
Lignin content was determined by Technical
Association of Pulp and Paper Industry (TAPPI, T-
222 om-83) standard method. Cellulose and
hemicelluloses content was determined by Standard
Methods of Biochemical Analysis by S.R.
Thimmaiah14
.
FT-IR studies were conducted by using a Perkin-
Elmer system 2000 FT-IR Spectrophotometer.
Powder XRD diffractions were carried out on a
Rigaku, UltimaIV X-ray diffractometer from 2-80°
2θ, using CuKα source (=1.54 Ǻ). The crystallinity
index (CI) was calculated using the following
equation, where I002 is the maximum intensity of the
I002 lattice reflection and I101 is the maximum intensity
of X-ray scattering broad band, due to amorphous
region of the sample. This method was developed by
Segal et al. 1959 15
and it is widely used for the study
of natural fibres.
CI (%) = [(I002─I101)/I002] ×100
The fibre samples were characterized for their
thermal stability using a thermogravimetric analyser
(TGA), TA, SDQ600. The samples were heated from
5
Das et al.: Novel Composite Materials
20 °C to 1000 °C at a heating rate of 10 °C/min under
a nitrogen environment flow of 100 ml/min.
Scanning Electron Microscopy (SEM) images were
analysed with JSM-6360 (JEOL). Tensile strength of
five composite specimens was analysed at 25 °C and
55% RH using Universal Testing Machine (UTM)
INSTRON Make, Model 5594. Ultimate tensile
strength, maximum load, tensile modulus values were
calculated by the software Merlin software version
V22054. The values of elongation at break were
calculated using the following equation: Tensile Strength
Elongation at break (%) = × 100
Tensile Modulus
For determination of Modulus of Rupture (MOR),
3 point flexural test additional attachment was used.
The MOR was then calculated using the following
equation and expressed in MPa by Equation: 3PL
R = (MPa)
2bd2
Where,
P - Maximum load applied on the test specimen (N)
L –Support span (mm)
b - Width of specimen tested (mm)
d –Thickness of specimen tested (mm)
Treatment of Coir Fibre
Screened coir fibres were treated with15% NaOH
solution at 100 °C for 4 h, 1.5 % HCl at 65 °C for 3 h,
1:1 ethanol-benzene solution at 80 °C for 6 h and
50% acetic acid solution at 100 °C for 3 h. After the
treatments, the fibres were washed properly with
distilled water and dried under sunlight.
Composite Board Preparation
Boards were made in the laboratory using untreated
and chemically treated fibre and polyethylene waste
cuttings. Polyethylene bags (PE) of lower density
were considered for the present investigation. The
wastes PE were first screened and after removal of
dust and foreign particles, these were washed with
water, dried under sunlight and cut in a chopping
machine. The cut pieces obtained from the chopper
were mixed with coir fibre for making the boards.
The size of the particles maintained at 0.01-0.0115 m
in length and 0.005- 0.0075 m width.
Approximately 0.5 kg of coir fibre was taken and
mixed with 0.25 kg of waste polyethylene (PE) bag
cuttings. These were mixed with coir fibres in such a
way that the cut pieces were uniformly distributed all
around the fibre mass. The mixture was put into the
wooden mould size 0.3 × 0.3 m and hot pressed at
115 ± 5 °C for 20 min and at 4.903 ± 5 N/mm2
pressure. A releasing agent was spread on both sides
of the fibre mass before hot pressing. After that, the
pressure was released from the hot press and the
board was kept for some time in open air for
conditioning. The properties of the boards made from
each treated coir fibre and PE waste bag cuttings were
studied.
Results and discussion
Fibre Characterization
The surface treatment of the coir fibre was carried out
by hydrochloric acid, acetic acid, ethanol-benzene
and sodium hydroxide at different concentrations
under controlled condition.
Table 1 shows the chemical constituents of both
untreated and treated coir fibre. It has been observed
from the Table 1 that the lignin content was recorded
40% for hydrochloric acid treated fibre, while 39%,
35% and 24% recorded for acetic acid, ethanol-
benzene and sodium hydroxide treated fibre
respectively. In case of untreated fibre lignin content
was recorded 44%. The higher lignin content makes
the fibre more rigid and stiff compare to other natural
fibre. Lignin provides plant tissue and individual
fibres with compressive strength and protects the
carbohydrates from chemical and physical damage16
.
But after treatment removal of lignin decreases
rigidity and stiffens of the fibre and enhanced the
surface roughness which will ultimately help in
compatibility of fibre to bond with the polyethylene
matrix for making composites. Hemicellulose content
of untreated fibre was recorded 18%, while after
chemical treatment it was reduced to 8% in
hydrochloric acid treatment, 15% in acetic acid
treatment, 13% in ethanol-benzene treatment and 6%
after sodium hydroxide treatment. Among all the
treatments, alkali treatments remove higher
percentage of hemicellulose content and as a result
showed a greater exposure of cellulose has taken
place and thereby increase in thermal stability.
Hemicellulose is strongly bound to cellulose fibrils by
hydrogen bonds. Hemicellulosic polymers are
branched, fully amorphous and have a significantly
lower molecular weight than cellulose. Because of its
open structure containing many hydroxyl and acetyl
groups, hemicelluloses is partly soluble in water and
hygroscopic17
.
6 Appl Sci Adv Mater Int, September 2014
So also, cellulose content was recorded 36.36 %
for untreated fibre, while 36.53 %, 37.21%, 37.50%
and 38.53 % for hydrochloric acid, acetic acid,
ethanol-benzene, and sodium hydroxide treated
respectively. Presence of hydroxyl groups of the
cellulose in coir is responsible for its inherent
hydrophilic nature. Treatments were done to reduce
the number of free hydroxyl groups of cellulose. This
would result in the reduction of the polarity of
cellulose molecules and in the improvement of its
compatibility with the thermosetting matrix used in
composites18
. Among all the treatment used for
modification of surface properties of coir fibre, the
alkali treatment showed better result in terms of
quality and strength. Chemical treatment decreases
the amorphous region of the fibres resulting in the
increase in crystalline portion. Because of higher
crystallinity of cellulose improves the bonding
property as well as ultimate tensile strength.
The treatment process removed lignin,
hemicellulose and other soluble parts like wax, tannin
and other non-cellulosic polysaccharides on the
surface of the fibre and made the fibre soft to adhere
easily with the polyethylene matrix been observed.
The fibrils get separated from each other because of
lignin, the cementing component had been removed
by the action of chemical treatment, leading to an
increase of the surface area and potentially improving
the fibre-matrix adhesion in composite.
The FTIR spectra (Fig. 1) of treated and untreated
coir fibre showed a broad and intense band centring
at ~3400 cm-1
due to the hydrogen bonded O-H
stretching vibration from the cellulose. The IR band at
~2925 cm-1
for untreated fibre is assigning to -
CH2antisymmetric stretching. This band at ~2925 cm-
1 shifted to ~2900 cm
-1 for treated coir fibre with
decrease in intensity, which concluded that carbon
atoms attached to carbon or hydrogen (-C-C- or –C-
H) decrease. The untreated coir fibre also showed an
absorption band at ~1735 cm-1
due to -C=O stretching
of the carbonyl and acetyl groups in the 4-O-methyl-
glucuronoacetyl xylan component of hemicelluloses
in coir fibre. The band is disappeared for the treated
fibre indicating removal of hemicelluloses
component. The treated and untreated fibre also
showed an absorption band at ~1607 cm-1
due to
adsorbed water molecule. The intensity of this band
increased upon treatment under controlled condition.
The band at ~1510 cm-1
for untreated fibre due to
presence of aromatic rings of lignin which shifted to
~1498 cm-1
with decrease in intensity for treated fibre
indicating partial removal of the lignin. A band at
~1250 cm-1
was observed for untreated coir fibre
which may be attributed to -C-O-C- bond in the
cellulosic chain. This band shifted to ~1258 cm-1
for
treated fibre indicating the change in the bonding
environment due to dissolution of hemicelluloses
during treatment.
Fig. 1 – FT-IR spectra of untreated and treated coir fiber
The effect of chemical treatment on surface
properties of fibre was examined under scanning
electron microscopy. Fig. 2 compares SEM of
untreated and treated coir fibre. SEM image of
untreated fibres Fig. 2(a) indicate that fibre surface
was covered with a layer of substances like oils,
waxes and extractives, part of natural constituents of
fibres. This layer was also observed by Vilay et al.19
Table 1 Chemical constituents of untreated and treated coir fibre
Particulars
Untreated
(%)
HCl treated
(%)
CH3COOH
treated (%)
Alcohol-benzene
treated (%)
NaOH
treated (%)
Ash 2.00 5.00 4.00 3.00 4.00
Cellulose 36.36 36.53 37.21 37.50 38.53
Lignin 44.00 40.00 39.00 35.00 24.00
Hemicelluloses 18.00 8.00 15.00 13.00 6.00
7
Das et al.: Novel Composite Materials
in the analysis of untreated sugarcane bagasse
micrographs and by Huang Gu5 in the analysis of the
tensile behaviour of brown coir fibre. But after
treatment Fig. 2(b)-(e) showed the pits and globular
marks which reveal chemical treatments removes
extractives, waxes and oils from fibre surfaces and it
increases the overall roughness of surface. With the
removal of these substances it indicates the presence
of parenchyma cells that are the natural constituents
of lignocellulosic fibres as well as the presence of
globular protusions, which are fatty deposits called
“tylose”19
. The presence of pits and globular marks
after chemical treatment are important for an increase
in the effective surface area and higher increase of the
roughness, consequently improving mechanical
bonding with the polymer matrix 20, 21
. For untreated
condition, poor adhesion between the fibre and
polyethylene matrix leads to existence of debonding
gap around the fibre. Partial removal of lignin, silica
and pith from the fibre helped in better bonding
between fibre and matrix and improved the surface
properties of fibre.
Fig. 2 – SEM image of a) Untreated b) Acetic acid treated
c) Alcohol-benzene treated d) HCl treated and e) NaOH
treated coir fibre
The TGA curves of untreated and treated coir fibre
are shown in Fig. 3. Two prominent weight loss were
invariably found for all the fibres. One was around
30-138 °C and other is around 220-457 °C. The
lower temperature thermal peak may be accounted for
evaporation of absorbed and crystal water molecule
associated with the cellulose fibre22
. The weight loss
occurred in this stage were 7.81% for untreated fibre,
14.45% for NaOH, 10.66% for acetic acid, 10.30%
hydrochloric acid and11.20% for ethanol-benzene
treated fibre respectively. The weight loss due to
moisture was found higher for treated fibre than
untreated one because, the treated fibre contains more
pores which substantiate the finding from SEM
image. Control treatment of coir fibre leads to
removal of fatty wax materials, pectins as well as
hemicelluloses ultimately makes the fibre more
hydrophilic in nature. Therefore, moisture loss is
easier and weight loss is more compared to untreated
one. The main degradation peak occurred 220-4570C.
It has been observed that for untreated fibre the
weight loss between 221-397 °C is 50.82%, which
may be assign for degradation hemicelluloses and α-
cellulose 23
. The main degradation peak was observed
60.99% for sodium hydroxide treated, 66.10% for
acetic acid treated, 68.00% for hydrochloric acid
treated, 62.85% for ethanol benzene treated
respectively in the temperature range 227-457 °C.
The degradation temperature for treated fibres shifted
to higher temperature well over 221°C to 457 °C
compared to the untreated fibre (397 °C) indicating
the higher thermal stability of treated fibre.
Fig. 3 – TGA of untreated and treated fiber
XRD studies of different treated and untreated
fibres were carried out to investigate the crystalline
behaviour of coir fibre (Figure 4). XRD analysis
showed two main peaks representing the planes 101
and 002 at 2θ around 16° and 22.4° respectively,
characteristic of cellulose crystalline phase of the
fibre21,24,25
. Crystallinity index (CI) was calculated
8 Appl Sci Adv Mater Int, September 2014
according to Equation 1, it was found 27.16 % in
case of untreated fibre whereas, it was recorded 30.07
%, 32.5 %, 28.71 % and 33.87 %, for acetic acid,
hydrochloric acid, ethanol- benzene, sodium
hydroxide treatment respectively. The higher CI of
treated fibre than untreated one due to removal of
residual lignin increased the exposure of the cellulose,
resulting in the crystalline index. X-ray graph shows
that the chemically treated fibre peaks were more
intense than untreated fibres i.e. treatments were able
to remove part of the amorphous material covering
the fibre.
Fig. 4 – X-ray diffraction spectra of untreated and treated
coir fibre
Characterization of Composite Boards
Table 2 represents the mechanical and physical
properties of composite boards made from both
untreated and chemically treated fibre using waste
polyethylene. Mechanical strength properties of
composite board viz. ultimate tensile strength (Fig. 5)
was recorded 3.099 MPa for untreated fibrewhich
attributed to lower crystallinity and considerably high
microfibrillar angle, while 6.345 MPa for NaOH
treated fibre. The minimum tensile strength 4.304
MPa was recorded in the composite board made of
HCl treated fibre among all treatment. Tensile
strength of composites made from treated fibre has
been improved and was capable of withstanding more
strain at maximum tensile stress. Composite made of
untreated fibre showed rapid decline of tensile stress
after attaining the ultimate strength. Likewise,
ethanol-benzene and acetic acid treated fibre
composite showed similar trend. Tensile strength
property of the HCl treated fibre composite showed
less tensile strength with high ductility. The
elongation at break (Fig. 6) of composite board found
maximum prepared from NaOH treated fibre. It was
visibly pronounced when treated with NaOH,
associated with the high lignin content and
consequently with the high values of microfibrillar
angles5. The coir fibre exhibited greater improvement
of tensile strength due to removal of hemicelluloses
and impurities from the coir fibre after the fibre
treatment. Cellulose content is responsible for a
consistent increased in tensile strength and elastic
modulus without exhibiting a decrease of the
elongation to break5. Modulus of rupture (MOR)
increased leading chemical treatment under controlled
conditions (Figure 7). MOR was recorded maximum
(15.4 MPa) for composites made from sodium
hydroxide treated fibre followed by acetic acid treated
(12.35 MPa), ethanol-benzene (11.62 MPa) and
hydrochloric acid treated (11.79 MPa) fibre
composite. During the progress of compression load,
the composite were not broken suddenly at certain
point but it could sustain the maximum load with
more extension.
Mechanical properties of composites were
strongly influenced by adhesion between the matrix
and fibre. The effects of the different chemical
treatments on the surface of fibre and the adhesion
between fibres and matrix were observed by scanning
electron microscope. SEM image of fracture surface
after tensile and compression test of untreated and
treated coir fibre composite are shown in Fig. 8-9. In
the case of the untreated fibres Fig. 8(a) & 9(a), they
seem to detach from the polymer matrix and have
relatively large pull-outs compared to other treated
fibres due to the poor interfacial adhesion with the
Table 2 Mechanical and physical properties of composite boards
Sample Density
(g/mm2)
UTS (MPa) MOR( MPa)
Untreated 0.733 3.099 ± 0.130 10.83 ± 0.459
HCl treated 0.740 4.304 ± 0.132 11.79 ± 0.459
Acetic acid treated 0.742 5.158 ± 0.168 12.35 ± 0.455
Alcohol-benzene
treated
0.771 4.853 ± 0.140 11.62 ± 0.500
NaOH treated 0.914 6.345 ± 0.093 15.4 ± 0.512
9
Das et al.: Novel Composite Materials
matrix. It is due to the presence of impurities like
waxy layer over the coconut fibre causes the poor
bonding. But after treatment Fig. 8(b) & 9(b), it was
observed that the fracture surfaces are uneven matrix
cracking and less void formation takes place due to
the good laminar bond between treated coir fibre and
binding matrix.
Fig. 5 – Tensile strength properties of treated coir
polyethylene composite board
Fig. 6 – Elongation at break of untreated and treated coir
polyethylene composite board.
Fig. 7 – 3-point flexural test (MOR) of treated coir
polyethylene composite board
Fig. 8 – SEM image of fracture surface of (a) Untreated
coir fiber composites after tensile test (b) Treated coir fiber
composites after tensile test
Fig. 9 – SEM image of fracture surface of a) Untreated coir
fibre composites after compression test b) Treated coir
fibre composites after compression test
Fig. 10 – Water absorption test of untreated and treated coir
polyethylene composite board
Fig. 11 – Total swelling test of untreated and treated coir
polyethylene composite board
10 Appl Sci Adv Mater Int, September 2014
Fig. 10 and Fig. 11 depict the water absorption and
swelling properties of composites. Water absorption
value of composite board was determined by
immersing the samples in distilled water for 24 h at
room temperature, after every 24 h the composite
board was taken out and excess of water on the
surface was removed. Three replicate data were
recorded and the average results were presented. The
water absorption was found higher in the boards made
from untreated fibre (8.07 %) due to less compactness
of the composite board. SEM micrograph of the
surface of untreated and treated coconut fibre (Fig. 2)
also support this statement. Figure 2a exhibits the
SEM micrograph of the untreated single fibre surface,
which indicates that it is full of randomly distributed
organic materials, whereas after treatment, the
hemicellulose and lignin are removed and pits are
revealed on the surface of the fibre (Fig. 2b-e)9,26
.
This statement was also supported by FTIR that
shows the peak at 1735 cm-1
(-C=O stretching of the
carbonyl and acetyl groups hemicelluloses) and
disappears after treatment. The fibre after
modification shows significant changes in water
absorption. Minimum water absorption was recorded
5.89 % in the composites made from sodium
hydroxide treated fibre while the composite made
from hydrochloric acid and acetic acid treated fibre
show 6.82 % and 6.38 %. Because of treatments
coating the fibre surface, therefore decreasing the
water absorption of the composites themselves 19, 27
.
The reaction result can be seen from FTIR, which is
shown at peak ~2925 cm-1
for untreated fibre is
assigning to -CH2antisymmetric stretching. This band
at ~2925 cm-1
shifted to ~2900 cm-1
for treated coir
fibre with decrease in intensity, which concluded that
carbon atoms attached to carbon or hydrogen (-C-C-
or –C-H) decrease.The reduction of water uptake by
the composite made from sodium hydroxide treated
fibre is due to the mechanical bonding between
cellulose and polyethylene matrix at higher
temperature and higher compactness of the
composites. By replacing some of the hydroxyl
groups on the cell wall polymers with bonded
chemical groups (e.g. NaOH), hygroscopicity of the
lignocellulosic material are reduced 28
. Total swelling
value (Figure 11) due to surface absorption was
recorded 5.16 %, 2.24 %, 3.47 %, 3.45 % and 4.82 %
in untreated, sodium hydroxide, hydrochloric acid,
acetic acid and ethanol benzene treated fibre board
respectively. The swelling of the fibre caused by
water uptake, which fills gaps and enhance the
friction between the fibre and polyethylene matrix.
Untreated coir fibre boards have more void space than
treated one so that more water can absorbed and
causes swelling.
Conclusions The adhesion properties of coir fibre as such with
polyethylene material are very poor. However, these
properties can be enhanced by applying chemical
treatments to the fibre. From the above study it is
revealed that treated coir fibre is found suitable for
mixing with waste polyethylene for making
composite. Chemical treatments improve the fibre
properties which ultimately enhance mechanical
strength to the finished product. Among the
chemicals, NaOH treated coir fibre composites were
found better in all the quality characteristics.
Therefore, it can be concluded modified coir fibre
may suitably be used for development of composite
material for building and furnishing material in near
future.
Acknowledgements The authors are grateful to the Director, CSIR-North
East Institute of Science and Technology, Jorhat for
his kind permission to publish this paper. They are
also thankful to Coir Board for the financial assistant
to carry out the research work at CSIR-NEIST,
Jorhat.
References
1. Singha A S, Kaith B S & Kumar S, Int J Chem Sci, 2
(2004) 472.
2. Kaith B S, Singha A S & Kalia S, AUTEX Res J, 7
(2007) 119.
3. Gu R, Kumarappa S & Gaitonde V N, J Mater Environ
Sci, 3 (2012) 907.
4. Spinace M A S, Lambert C S, Fermoselli K K G &
Paoli M A D, Carbohyd Polym, 77 (2009) 47.
5. Gu H, Mater Des, 30 (2009) 3931.
6. John M J & Anandjiwala R D, Compos A, 40 (2009)
442.
7. Hariharan A B A & Khalil H P S A, J Compos Mater,
39 (2005) 663.
8. Rahman M M & Khan M A, Compos Sci Technol, 67
(2007) 2369.
9. Rout J, Misra M, Tripathy S S, Nayak S K & Mohanty
A K, Compos Sci Technol, 61 (2001) 1303.
10. Li X, Lope G T & Satyanarayan P, J Poly Environ,
15(1) (2007) 25.
11. Mizanur R M & Mubarak A K, Comp Sci Tech 67(11-
12) (2007) 2369.
12. Brahmakumar M, Pavinthran C & Pillai R M, Comp Sci
Tech, 65(3-4) (2005) 563.
11
Das et al.: Novel Composite Materials
13. Suardana N P G, Lokantara I P & Lim J K, Mater Phys
Mechan, 12 (2011) 113.
14. Thimmaiah S K, Standard methods of biochemical
analysis (Kalyani publishers) 1999.
15. Segal L, Creely J J, Martin Jr A E & Conrad C M, J
Text Res, 29 (1959) 786.
16. Frederick T W & Norman W, Natural fibre plastics and
composites (Kluwer Academic Publishers, New York)
2004.
17. Carvalho K C C, Mulinari D R, Voorwald H J C &
Cioffi M O H, Bio Res, 5 (2010) 1143.
18. Pietak A, Korte S, Tan E, Downard A & Staiger M P,
Appl Surface Sci, 253 (2007) 3627.
19. Vilay V, Mariatti M, Taib R M & Todo M, Comp Sci
Techol, 68 (2008) 631.
20. d’Almeida J R M, Aquino R C M P & Monteiro S N,
Compos A, 37 (2006) 1473.
21. Xiao B, Sun X F & Sun R C. Polym Degrad Stabil, 74
(2001) 307.
22. Ray D, Sarkar B K, Basak R K & Rana A K, J Appl
Polym Sci, 85 (2002) 2594.
23. Maldas D & Shiraishi N, Biomass and Bioenergy, 12
(1997) 273.
24. Pereira R, Filho S P C, Curvelo A A S & Gandini A,
Cellulose, 4 (1997) 21.
25. Vijayalakshmi R, Ashokan P V & Sridhar M H, Mater
Sci Eng A, 281 (2000) 213.
26. Gonzalez A V, Cervantes-Uc J M, Olayo R & Herrera-
Franco P J, Compos Part B, 30 (1999) 309.
27. Bessadok A, Marais S, Gouanve F, Colasse L,
Zimmerlin I, Roudesli S & Metayer M, Compos Sci
Technol, 67 (2007) 685.
28. Jayabal S, Sathiyamurthy S, Loganathan K T &
Kalyanasundaram S, Bull Mater Sci, 35 (2012) 567.
Applied Science and Advanced Materials International
Vol. 1 (1), September 2014, pp. 12 -15
Clarification of tannery wastewater from beam house operation using ceramic
MF membrane
Ganesh C. Sahoo*, Sourja Ghosh, SwachchhaMajumdar and SibdasBandyopadhyay
Ceramic Membrane Division, CSIR-Central Glass & Ceramic Research Institute
196 Raja S. C. Mullick Road, Jadavpur, Kolkata 700032
Received16 August 2014; accepted 30 August 2014
Abstract Clarification study of sectional stream and composite effluent from beam house operation of tannery
industry was carried out using tubular ceramic membrane following cross-flow membrane filtration (CMF) technique.
In order to minimize the interaction between foulants and membrane layer, composite effluent was also pretreated and
membrane filtered using the same technique. Two types of pretreatment viz gravity settling and chemical treatment
under optimized dose followed by gravity settling were studied. Sectional stream, composite effluent and pretreated
supernatants were analyzed before and after membrane filtration study. Zirconia and alumina coated membrane over
low-cost clay-alumina based membrane support were used. Physical properties of the elements were also determined.
Membrane flux varied from 25 to 350 l/m2h depending on the feed turbidity and membrane type at 1.2 bar, and
permeate turbidity down to 1 NTU was achieved with 99% removal.
Keywords Tannery wastewater, beam house, pretreatment, cross-flow membrane filtration, tubular ceramic
membrane, flux, turbidity.
Processing of leather in tannery industry generates
wastewater at various stages like soaking, bating,
liming, deliming, pickling, skin degreasing, tanning
etc. are called ‘Beam House’ operation. Effluent
contains two types of contaminants viz. chemical
contaminants like sodium chloride, sodium
sulphide, lime, chromium etc. and organic matters
like, proteins, fats, coloring compounds etc. with
high biological and chemical oxygen demand.
Developments are being carried out to reduce water
consumption during the leather processing, adopt
green process without toxic chemicals and recovery
and reuse of wastewater.
Existing treatment processes include treatment
of effluent with the chemicals like sodium
hydroxide, magnesium oxide, etc, which results a
sludge and liquor. In the common effluent treatment
plant (CETP), the effluent generated from different
sectional streams are mixed and subjected to
primary, secondary and tertiary treatment steps to
recover and reuse of tannery wastewater.
Microfiltration (MF), ultrafiltration (UF),
nanofiltration (NF) and reverse osmosis (RO)
membranes have been used for clarification of
various effluent streams of the ‘beam house’ have
been examined extensively1. Application of UF and
RO for treatment of effluents from liming,
degreasing2,3
, soaking, bating and pickling1 steps
has been reported. CSIR-CGCRI, Kolkata have
been working on development of low-cost clay-
alumina based ceramic membranes, their
characterization and application for wastewater
treatment4-8
. Porous ceramic membranes have
excellent chemical resistance, operable at higher
temperature, stability to organic solvents, are
expected to be used in the separation and filtration
of both aqueous and non-aqueous solutions9-15
.
Objective of the present study is clarification of
sectional stream and composite effluent from ‘beam
house’ operation using tubular ceramic membrane
following cross-flow membrane filtration (CMF)
technique. Minimization of membrane fouling by
pretreatment of effluentwas also carried out. Two
types of pretreatment were studied viz. gravity
settling and chemical treatment under optimized
dose followed by gravity settling.
Corresponding Author:
Ganesh C. Sahoo
e-mail: [email protected]
13 Sahoo et al.: Clarification of Tannery Waste Water
Experimental Procedure Physical properties of 200 mm long ceramic
elements were determined using buoyancy method
(Table 1). Waste water from various tannery
operations and membrane permeate samples were
characterized w.r.t. turbidity (NTU), total dissolved
solid (TDS), pH and conductivity (mS/cm) using
Turbidity Meter and Multiparameter, HACH Co.,
USA (Table 2). Composite sample (CTE) was
prepared by mixing 4-sectionalstreams viz. 1st
soaking, 2nd
soaking, 3rd
soaking and liming at a
fixed volume ratio (2:2:2:1.5). Pretreatment
condition of CTE was optimized. Pretreatment of
composite sample was done by gravity settling for
24 hours of raw effluent and chemical treatment
followed by gravity settling for 24 hours.
Optimization of chemical pretreatment of composite
sample was done on the basis of lowering of
supernatant turbidity by varying coagulant dose at a
fixed flocculent concentration (1.0 ml/l). CMF
study was carried out at variable transmembrane
pressure (TMP) and at constant transmembrane
pressure of 1.2 bar for two hrs. A feed of 40 l batch
of 4-sectional streams was treated using 19-channel
ceramic membrane. Clarification study of CTE and
supernatants of composite samples (SCTE) using
single-channelsupport, alumina and zirconia coated
membranes was donefor 10 L batch.
Results & Discussion
Properties of sectional streams, composite effluent
and pretreated effluents are given in Table-2.
Particle size distribution study shows that average
particle size ranges from 0.1 to 90 m (Fig. 1) can
be separated using microfiltration membrane.
Microfiltration of sectional streams of 40 l batch in
bench scale unit using 19-channel ceramic element
showed that permeate flux (70 – 170 l/m2h, LMH)
and turbidity were varied according to feed turbidity
and permeate turbidity down to 16 NTU was
achieved at 1.2 bar TMP from feed of 150 NTU
(Fig. 2). Apparent porosity of single Channel
elements are higher compare to 19-channel element
as shown in Table 1.
Table 1Properties of Ceramic Elements.
Properties 19-channel
element
Single channel
element
Zirconia coated
membrane
Alumina coated
membrane
Outer diameter (mm) 35 36 36 36
Channel diameter (mm) 4.2 29 29 28
Tube length (mm) 200 200 200 200
Dry weight (g) 313.4 160.6 162.3 163.8
Bulk density (g/cc) 2.4 2.1 2.2 2.1
Apparent porosity (%) 23 36.1 36.8 37.7
Water absorption (%) 9.6 17.0 17.1 17.9
Table 2 Properties of sectional streams and composite of beam house operation.
Properties Sectional Stream Composite (2:2:2:1.5)
First
Soaking
Second
Soaking
Third
Soaking Liming
As such
Pretreated
Settling Chemical
treatment &
settling
Turbidity (NTU) 553 146 112 6,000 1241 160 30.2
TDS (g/l) 48.4 33.7 8.1 18.3 13.3 14.0 16.4
pH 6.7 7.8 7.6 12.5 7.5 8.4 7.1
Conductivity (mS/cm) 74.0 6.8 15.1 29.6 30.2 29.4 27.7
DO (ppm) 8.6 8.5 10.9 7.6 --- --- ---
BOD (g/l) - 2.3 - 6.1 --- --- ---
COD (g/l) - 0.8 - 4.5 --- --- ---
Av. Particle size (m) 9.9 24.8 89.6 0.1 6.3 --- ---
14 Appl Sci Adv Mater Int, September 2014
Fig. 1 Particle size distribution of tannery wastewater
samples collected from different stages of operation
using Zetasizer Nano-S (Malvern, UK).
Fig. 2 Membrane flux comparison with feed turbidity for
different sectional stream using 19-channel ceramic MF
membrane.
Crossflow membrane filtration of composite sample
for 10 l batch showed similar membrane flux of 80
LMH at 1.2 bar TMP at the initial stage using
single-channel membranes, but it came down to ~
45 LMH within 1.5 hrs of filtration may be due to
membrane fouling (Fig. – 3). Performance of
zirconia coated membrane element was found to be
better w. r. t. flux and turbidity removal (98%) as
shown in the Fig. - 3.
Fig. 3 Change in permeate flux and turbidity through
various single channel tubular ceramic elements at 1.2
bar TMP using lab unit.
Optimization of chemical pretreatment of
composite sample was performed by measuring the
turbidity of supernatant with varying coagulant dose
at a fixed flocculent concentration (1.0 ml/l).
Supernatant turbidity obtained was minimum (~25
NTU) for coagulant dose of 1.0 g/l as shown in
figure 4. Turbidity down to 30 NTU was achieved
at optimized chemical doses.
Fig. 4 Variation of turbidity in supernatant with variation
of coagulant dose.
Settling velocity (cm/s) was calculated (cm/s)
and plotted against time (hr) up to 40 hrs as shown
in fig. 5. The result shows that settling occurred
within 4 hrs under optimized doses of coagulant and
flocculant.
Fig. 5 Compression of settled mass with time during
coagulation of the composite tannery effluent.
Fig. 6 Variation of permeate flux and turbidity with time
of composite tannery effluent obtained after various
pretreatment through alumina coated ceramic membrane
at 1.2 bar TMP using lab unit.
15 Sahoo et al.: Clarification of Tannery Waste Water
Alumina coated membrane provided comparable
flux (25 LMH at 1.2 bar TMP) using composite
sample and gravity settled supernatant of composite
sample, and much higher flux (350 LMH at 1.2
bar TMP) using chemically treated supernatant
while permeate turbidity down to 1 NTU was
achieved using both type of pretreatment methods
as shown in Fig. 6.
Conclusion
Pretreatment of composite effluent from beam
house operation may be an alternative method of
clarification using ceramic membrane from the
points of turbidity removal and permeate
throughput. Membrane permeate of sectional stream
may be recycled after addition of balanced amount
of chemical to the same operation or to the
operation using similar chemicals. Solid waste
generated may be used as wealth such as fertilizer,
adsorbent preparation etc.
References 1. Cassano A, Molinari R, Romano M & Drioli E, J
Membr Sci, 181 (2001) 111.
2. Cassano A, Drioli E & Molinari R, J Soc Leather
Technologists Chemists, 82 (1998) 130.
3. Cassano A, Criscuoli A, Drioli E & Molinari R,
Clean Product Processes 1 (4) (1999) 257.
4. Sahoo G C, Bandyopadhyay S, Roy S N & Maiti H S,
National Seminar on Membrane Science
&Technology : Challenges and Opportunities,
Regional Research Laboratory, Jorhat, India,
February 12-13, 2004.
5. Sahoo G C, Roy S N & Bandyopadhyay S;
Proceedings of 9th
International Conference on
Inorganic Membranes (ICIM9), edited by R Bredesen
& H Ræder (Lillehammer, Norway) June 25-29,
2006.
6. Bandyopadhyay S, Sahoo G C, Roy S N & Maiti H S,
Indo-US Joint Conference, Mumbai, December 28-
30, 2004.
7. Bandyopadhyay S, Roy S N & Maiti H S, 12th
Annual
Meeting of North American Membrane Society,
2001.
8. Sahoo G C, Roy S N & Bandyopadhyay S, Int J
Scientific Engg Technol, 2(8) (2013) 803.
9. Tsuru T, Sep Purif Methods, 30 (2001) 191.
10. Roy S N, Bandyopadhyay S, Ghosh B P & Maiti H S,
Indian Patant (File No. NF/234/2001), 2001.
11. Das N, Bandyopadhyay S, Chattopadhyay D & Maiti
H S, J Materials Sci, 31 (1996) 5221.
12. Bhanushali D, Kloos S, Kurth C & Bhattacharyya D,
J Membrane Sci, 189 (2001) 1.
13. Dey T, Sahoo G C, Roy S N & Bandyopadhyay S, Int
J Scientific Res Pubs (ISSN 2250-3153), 3(10) (2013)
1.
14. Criscuoli A, Majumdar S, Figoli A, Sahoo G C,
Bafaro P, Bandyopadhyay S & Drioli E, J Hazard
Mater, 211-212 (2012) 281.
15. Roy B, Dey S, Sahoo G C, Roy S N &
Bandyopadhyay S, J Am Oil Chemists Soc, 91(8),
(2014), 1453.
Applied Science and Advanced Materials International
Vol. 1 (1), September 2014, pp. 16-20
Synthesis,Structural and Electrical Properties of Cu doped ZnO nanoparticles
Bikramkeshari Das*, Tanushree Das,KajalParashar,S.K.S.Parashar
Nano Sensor Lab, School of Applied Sciences, KIIT University, Bhubaneswar-751024,Odisha, India.
Received 21 August 2014; accepted 3September 2014
Abstract Single phaseZn0.99Cu0.01O ceramic nanopowder was successfully synthesized by solid state reaction
technique. X-ray diffraction studies of synthesized powder reveals single phase, hexagonal wurtzite structure and
belongs to space group of p63mc. No secondary peak in the XRD pattern shows the incorporation of Cu2+
ion into the
ZnO lattice rather than the interstitial one. Compare with pure ZnO(50nm),the average crystallite size of Zn0.99Cu0.01O
(55nm) is higher. The substitution of Cu in ZnO results in contraction of the atoms. Electrical properties of the material
has been studied by using Impedance Spectroscopy in the frequency range100Hz-1MHz and temperature range (3000c-
5000c) follow non-Debye relaxation process. The ac conductivity of Zn0.99Cu0.01O . lesser than ZnO which follow
universal power law s
dcac A within frequency range 1kHz to 1MHz.
Keywords XRD, Impedance Spectroscopy, Zn 0.99Cu0.01O , ac conductivity
ZnO is a well known of the II–VI compound
semiconductor which has a large direct band gap of
3.37 eV and high exciton binding energy of 60
meV, excellent chemical and thermal stability1-3
. It
has a stable wurtzite structure with lattice spacing a
= 0.325 nm and c = 0.521 nm and composed of a
number of alternating planes with tetrahedrally co-
ordinated O2-
and Zn2+
ions, stacked alternately
along the c-axis4. Furthermore, ZnO semiconductor
material has generated a lot of interest among
researchers and technologists for device
applications. For its unique properties, low cost and
environmental friendliness5 and optical properties
can be tuned by quantum confinement effects at
nano sizes6. Thus, zinc oxide can be a promising
candidate for novel applications such as UV
detectors7, field emission devices
8, high sensitivity
gas sensors9,biosensors
10,dye-sensitized solar
cells11
, photoluminescent materials12
, photocatalytic
degradation of pollutants13
and antibacterial
purposes14
,piezoelectric devices and spintronics4
These important properties make ZnO has a great
potential in the field of nanotechnology. Nano zinc
oxide is non-toxic, with wide band gap has also
been identified as a promising semiconductor
material for exhibiting ferromagnetism (RTFM) at
room temperature when doped with most of the
transition metal elements15
. Properties of ZnO can
be tuned, by doping with various metal atoms to suit
specific needs and applications16
. Doping is a
widely used means to tailor the band structures of
bulk semiconductors, facilitating the construction of
various devices essential for the development of
microelectronics17
.The metal doping induces drastic
changes in optical, electrical and magnetic
properties of ZnO by altering its electronic
structure. Many authors have reported the changes
induced by incorporation of transition metal ions
into ZnO lattice18-20
.Some reports addressed room-
temperature ferromagn- etic behaviour of transition
metal[Fe, Mn, Ni, Co, Cr] doped semiconductor
oxides,20-22
and the behaviour of ferromagnetism is
caused mainly by intrinsic defects or impurity
phases or ferromagnetic precipitates23-
24.Substitution of copper into the ZnO lattice has
shown to improve properties such as photocatalytic
activity, gas sensitivity and magnetic semi
conductivity25-28
. Copper doped zinc oxide
Zn0.95Fe0.03Cu0.02O was found to exhibit
ferromagnetic performance at room temperature 29
.But this Cu incorporation reduced the saturation
magnetization of Fe doped ZnO magnetic
semiconductors. Photoluminescence (PL) of Cu
doped ZnO nanocrystals were found to show
pronounced UV emission and negligible visible
emission with peak positions coinciding with that of
Corresponding Author:
Bikramkeshari Das
e-mail:[email protected]
17 Das et al.: Synthesis, Structural and Electrical Properties
undopedZnO30
. Among transition metals,Cu is an
especially interesting dopant because that Cu-
related compounds are not strongly ferromagnetic.
Recently, a few research groups have synthesized
and studied the physical properties of Zn1−xCuxO
thin films31-35
. Several methods are available for the
synthesis of ZnO nanoparticles,such as a chemical
or physical method37
hydrothermal process38
sol−gel
method39
and co-precipitation method40
.However,
there are still much less report on Cu doped ZnO36
.
Owing to the importance of Cu doped ZnO
nanoparticlecs, the current study involves the
analysis of phase, structure and electrical properties
of Zn1-xCuxO with x = 0, 0.01 by solid state reaction
route.
Experimental procedure Cu doped ZnO ceramic powder abbreviated as
Zn0.99Cu0.01O was prepared by using a simple solid
state reaction technique. High purity precursor ZnO
and CuO were weighted according to their atomic
ratio, used as a raw material to achieve the desired
product .The sample was prepared by thoroughly
grinding these powders in an agate mortar and was
calcined at 8500C for 2hr with a heating rate of
20C/min using air atmosphere. The calcined powder
was mixed with PVA which act as a binder to make
pellet at a pressure of 437Mpa using hydraulic
press. Finally,the pellet was sintered at 10000C for
2hr in air atmosphere and was coated with silver
paste on both sides heated at 7000C for 15 minute.
Crystal structure,phase identification and unit
cell parameters of Zn0.99Cu0.01O was investigated by
using XRD. The electrical properties were analysed
by using a computer cotrolled analyzer (Hioki LCR
Hi-tester-3532-50) as a function of temperature,(30
– 5000C) over a wide range of frequency ( 100Hz-
1MHz).
Result and Discussion
Structural Analysis Fig. 1 illustrates the XRD patterns of ZnO and
Zn0.99Cu0.01O ceramic nanopowder calcined at
8500C for 2hr.The XRD patterns of
Zn0.99Cu0.01Oshows the reflection planes indexed to
wurtzite hcp structure of ZnO(space group of
p63mc, JCPDS:36-1451).No extra peak in the
pattern shows the formation of single phase5. This
indicates that Cu2+
ion successfully occupy the
lattice site rather than interstitial one. This is due to
the fact that ionic radius of Cu2+
(0.73Å) is very
close to that of Zn2+
(0.74Å),due to which Cu can
easily penetrate into ZnO crystal lattice17
.
Fig. 1 (a)X-ray diffraction patterns of ZnO and
Zn0.99Cu0.01O nanoparticles; (b) Rietveld refinement plot
of ZnO; (c)Zn 0.99 Cu0.01 O nanoparticle
18 Appl Sci Adv Mater Int, September 2014
The average crystallite size has been estimated by
Debye-Scherrer equation17
d=0.9λ/βcosθ
Where d is the average crystallite size, λ is the
wavelength of the incident X-ray beam, θ is the
Braggs diffraction angle and β is the angular width
of the diffraction peak at the half-maximum in
radians on 2θ scale.The average crystallite sizes of
the samples havebeen found to be 50nm(ZnO) and
55nm(Zn0.99Cu0.01O) respectively.
The Lattice parameters are calculated by
Rietveld refinement using Maud software. For ZnO
the values are a=3.2493Å, c=5.2056Å and
microstrain=35.4 x 10-4
and for Zn0.99Cu0.01O the
values are, a=3.2504Å,c=5.2060Å, microstrain =
81.03 x 10-4
respectively. From Fig-1(c),it can be
seen that the fit between observed and calculated
profiles is very good inZn0.99Cu0.01O which
indicates that Cu occupying Zn sites confirms that
Cu is indeed substituting Zn in the formation of
Zn0.99Cu0.01O41
.It is observed from a-value that the
base atoms along X and Y axis lies closer to each
other in ZnO then Zn0.99Cu0.01O and also from c-
value there is a elongation of base atom along Z-
axis of Zn0.99Cu0.01O then pure ZnO.
Impedance Analysis Complex impedance spectroscopy(CIS) is anon-
destructive method to study the microstructure and
electrical properties of solids. It is a powerful
technique for the characterization of grain and grain
boundaries in ceramics42
. Measurement of
impedance parameter helps in the identification of
various electrical parameters appropriate for the
system43
. Polycrystalline materials usually shows
both grain and grainboundary effects with different
time constants, leading to two successive
semicircles43
. The semicircular pattern in the
impedance spectrum is representative of electrical
process taking place in the material which can be
thought of as resulting from the cascanding effect
of a parallel combination of resistive and
capacitance elements arising due to the bulk
properties of the material and the grainboundary
effects. The high frequency semicircle is due to the
bulk property of the material and the low frequency
semicircle to be due to grain boundary effects42
.
Fig2 shows the variation of real part of impedance
Z' with frequency, imaginary part of impedance
with Z" with frequency and real part w.r.t.
imaginary part ( Z' vs Z'') at different temperature
(3000c-500
0c) in ZnO and Zn0.99Cu0.01O.
From Fig. 2, it can be shown that, for both the
sample, the magnitude of Z' decreases with increase
in temperature, indicating increase in ac
conductivity, further at law frequencies the value of
Z' decreases with rise in temperature, showing
negative temperature co-efficient of resistance
(NTCR) effect45
. The value of Z' for all temperature
may merge after1MHz for Zn0.99Cu0.01O due to the
release of space charge45
.
The plot of imaginary part of impedance Z'' with
frequency shows the Z'' peak shifts to the higher
frequencies with increasing temperature and
existing of peak broadening indicating the
relaxation process in the system43
. The relaxation
species may possibly be electrons at low
temperature and defects at high temperature43
.
From Z' Vs Z'' it was observed that Zn0.99Cu0.01O
follow the non-Debye relaxation phenomena, ZnO
it does not have any clear semicircular arcs at
different temperature. The semicircular arcs are
generated during the temperature interval between
3000C – 375
0C indicates the major contribution of
grain boundary resistance. Again the magnitude of
semicircular arc decreases with increase in
temperature for both ZnO and Zn0.99Cu0.01O
indicates temperature dependant nature.
Fig. 2 CIS plots ofZnO and Zn0.99Cu0.01Onanoarticles
19 Das et al.: Synthesis, Structural and Electrical Properties
AC Conductivity The variation of AC Conductivity as a function of
temperature(1kHz-1MHz) at a temperature range
3000C – 500
0Cfor ZnO and Zn0.99Cu0.01O is shown
in Fig 3. The conductivity is found to be frequency
independent in low frequency regions and is
illustrated as dc conductivity.AC conductivity
measurement is an important tool for studying the
transport properties of materials45
. The frequency
dependent AC conductivity can be described by
Jonscher's power law as follows45
.
s
dcac A
Where n is a frequency exponent in the range 0
and 1
σdc is temperature dependent dc conductivity
related to the drift mobility of the charge carrier A
is a temperature dependent constant.
The AC conductivity value increases with
increase in temperature indicates the electrical
conduction in the material. The electrical
conduction in the sample is a thermally activated
process result by the release of space charge.
Further, one more possible reason is the native point
defects in ZnO(oxygen and zinc interstial)46
.The
increasing conductivity w.r.t temperature indicates
the negative temperature co-efficient of
resistance(NTCR). From graph it was found that
AC conductivity decreases with Cu doping to ZnO.
Conclusion Zn0.99Cu0.01O polycrystalline nanopowder was
synthesized by solid state reaction method.The
incorporation of Cu2+
ion into ZnO lattice rather
than the interstitial was observed from XRD
analysis. Contraction of base atom along all axis
was observed from Rietveld analysis.CIS plot of
Cu2+
doped ZnO shows relaxation phenomena in the
material.Increasing AC conductivity in ZnO
thanZn0.99Cu0.01O was observed due to release of
space charge and native point defect in ZnO.
References
1 Deepa M, Bahadur N, Srivastava A K, Chaganti P &
Sood K N, J Phys Chem Solids, 70 (2009) 291.
2 Chikoidze E, Dumont Y, Jomard F & Gorochov O,
Thin Solid Films, 515 (2007) 8519.
3 Li X Z, Zhang J & Sellmyer D J, Solid State
Commun, 141 (2007) 398.
4 Chauhana R, Kumar A & Chaudharya R P, J Chem
Pharm Res, 2(4) (2010) 178.
5 Senthilkumaar S, Rajendran K, Banerjee S, Chini T
K & Sengodan V, Mater Sci Semicond Process, 11
(2008), 6.
6 Sabri N S,Yahya A K & Talari M K, J
Luminescence, 7 February 2012.
7 Safa S, Sarraf-Mamoory R & Azimira R D, Physica
E, 57 (2014) 155.
8 Zhu Y W, Zhang H Z, Sun X C, Feng S Q, Xu J,
Zhao Q, Xiang B, Wang R M & Yu D P, Appl Phys
Lett, 83(1) (2003) 144.
9 Xu J, Pan Q, Shun Y & Tian Z, Sensors and
Actuators B: Chemical, 66(1) (2000) 277.
10 Zhang F, Xiaoli W, Shiyun A, Zhengdong S, Qiao
W, Ziqiang Z, Yuezhong X, Liton J & Katsunobu Y,
Analytica Chimica Acta, 519( 2) (2004) 155.
11 Repins I, Contreras A, Egaas B, De H, John S, Craig
L, Perkins B & Rommel N, Prog Photovolt Res Appl,
16(3) (2008) 235.
12 Lawrie B J, Haglund R F & Mu R, Opt Express,
17(4) (2009) 2565.
13 Behnajady M A, Modirshahla N & Hamzavi R, J
Hazard Mater, 133(1) (2006) 226.
14 Akhavan O, Azimirad R & Safa S, Mater Chem Phys,
130(1) (2011) 598.
15 Herng T S, Lau S P, Yu S F, Yang H Y, Wang L,
Tanemura M & Chen J S, Appl Phys Lett, 90 (2007)
032509.
16 Singhal S, Kaur J, Namgyal T & Rimi S, Physica B,
407 (2012) 1223.
17 Ohno H, Science, 281 (1998) 951.
18 Bhat S V & Deepak F L, Solid State Commun, 135
(2005) 345.
19 Deka S & Joy P A, Solid State Commun, 142 (2007)
190.
20 Jing C, Jiang Y, Bai W, Chu J & Liu A, J Magn
Magn Mater, 322 (2010) 2395.
100 1000 10000 100000
0.0
5.0x10-2
1.0x10-1
1.5x10-1
2.0x10-1
2.5x10-1
ZnO
300 0C 325
0C
350 0C 375
0C
400 0C 425
0C
450 0C 475
0C
500 0C
Frequency (Hz)
AC
Con
duct
ivity
(ac
)
AC
Con
duct
ivity
(ac
)
100 1000 10000 100000
0.0
5.0x10-2
1.0x10-1
1.5x10-1
2.0x10-1
2.5x10-1
Zn0.99
Cu0.01
O
300 0C 325
0C
350 0C 375
0C
400 0C 425
0C
450 0C 475
0C
500 0C
Frequency (Hz)
Fig. 3 Frequency dependent AC Conductivity of ZnO and Zn0.99Cu0.01O nanoparticles
20 Appl Sci Adv Mater Int, September 2014
21 Radovanovic P V and Gamelin D R,Phys RevLett, 91
(2003) 157202.
22 Norberg N S, Kittilstved K R,Amonette J E,
Kukkadapu RK, Schwartz DA & Gamelin D R, J Am
Chem Soc, 126 (2004) 9387.
23 Ueda K, Tabata H & Kawai T, Appl Phys Lett, 79
(2001) 988.
24 Cho Y M, Choo W K, Kim H, Kim D & Ihm Y, Appl
Phys Lett, 80 (2002) 3358.
25 Saeki H, Tabata H & Kawai T, Solid State Commun
120 (2001) 439.
26 Sonawane Y S, Kanade K G, Kale B B & Aiyer R C,
Mater Res Bull, 43 (2008) 2719.
27 Buchholz D B, Changa R P H, Song J H & Ketterson
J B, Appl Phys Lett, 87 (2005) 082504.
28 Kanade K G, Kale B B, Baeg J O, Lee S M, Lee C
W, Moon S & Chang H, Mater Chem Phys, 102
(2007) 98.
29 Liua H, Yanga J, Huaa Z, Liua Y, Yanga L, Zhanga
Y & Caoa J, Mater Chem Phys, 125 (2011) 656.
30 Jayanthi K, Chawla S, Sood K N, Chhibara M &
Singh S, Appl Surf Sci, 255 (2009) 5869.
31 Chakraborti D, Narayan J & Prater J T, Appl Phys
Lett, 90 (2007) 062504.
32 Hou D L, Ye X J, Meng H J, Zhou H J, Li X L, Zhen
C L & Tang G D, Appl Phys Lett, 90 (2007) 142502.
33 Herng T S, Lau S P, Yu S F, Yang H Y, Ji X H,
Chen J S, Yasui N & Inaba H, J Appl Phys, 99 (2006)
086101.
34 Buchholz D B, Chang R P H, Song J H & Ketterson J
B, Appl Phys Lett, 87 (2005) 082504.
35 Cr C H O, Jy H, Jp K I M, Sy J, Ms J, Wj L E E &
Dh K I M, Journal Code: F0599B, 43 (2004),
L1383.
36 Xu C X, Sun X W, Zhang X H, Ke L & Chua S J,
Nanotechnol, 15 (2004) 856.
37 Niedegrberger M, J Mater Chem, 18 (2008) 5208.
38 Zhang L, Liu X, Geng C, Fang H, Lian Z, Wang X,
Shen D & Yan Q, Inorg Chem, 52 (2013) 10167.
39 Chakraborti S, Sarwar S & Chakrabarti P, J Phys
Chem B, 117 (2013) 13397.
40 Zhang S, Hu F, He J, Cheng W, Liu Q, Jiang Y, Pan
Z, Yan W, Sun Z & Wei S, J Phys Chem C, 117
(2013) 24913.
41 Singh J, Hudson M S L, Pandey S K, Tiwari R S and
Srivastava O N, Int J Hydrogen Energy, 37 (2012)
3748e374.
42 Sen S, Pramanik P and Choudhary R N P, Appl Phys
A, 83(3) (2005) 549.
43 Sen S, Choudhary R N P & Paramanik P, British
Ceramic Trans, 103 (2004) 6.
44 Sahoo P S, Panigrahi A, Patri S K & Choudhary R N
P, Bull Mater Sci, 33(2) (2010) 129.
45 Das T, Das B, Parashar K, Parashar S K S and
Nagamalleswararao A, Adv Mater Res, 938 (2014)
63.
46 Janotti A & deWalle C G V, Rep Prog Phys, 72
(2009) 126501.
Applied Science and Advanced Materials International
Vol. 1 (1), September 2014, pp. 21-27
Low Density Polyethylene/Layered Silicate Nanocomposites: Influence of MAH-g-
PE as Compatibiliser on the Morphology, Physical Properties and Crystallization
Characteristics.
Sanghamitra Parija
Templecity Institute of Technology & Engineering, F-II, Knowledge campus, Khordha-752057
Received 11 August 2014; accepted 25 August 2014
Abstract In the present investigation nanocomposites have been prepared from the LDPE, octa decyl amine modified
montmorillonite (Nanomer 1.30P grade) and maleic anhydride grafted polyethylene (EpoleneE-142 ) as reinforcement and
compatibiliser. LDPE along with three different nanomer loading (1,3 and 5 wt %) were melt intercalated with and without
compatibiliser. Different material properties i.e. melt behavior, mechanical properties and thermal characteristics were
assessed and compared with the virgin polymer. The TEM analysis of the uncompatibilised and compatibilised hybrids was
carried out to evaluate the clay dispersion in the resulted hybrids. It is observed that the nanomer addition leads to decrease
in MFI and shear rate with increase in viscosity of base polymer. The nanocomposites show improved mechanical
properties as compared to the virgin polymer. However, the elongation at break decreased significantly with the increased
addition of nanomer. Experimental findings revealed that MAH-g-PE being used as a compoatibiliser is instrumental in the
property enhancement of the resulted hybrids. Compatibilised LDPE/layered silicate hybrid showed improved thermal
stability and crystallization characteristics as compared to the base polymer.
Key words Montmorillonite, Viscosity, E-142, intercalation, Nanocomposites, Compatibiliser,
The polymer melt intercalation of mica type layered
silicate is a viable approach to the synthesis of a
variety of polymer/layered silicate
nanocomposites1-5
. Since 1996 the preparation of
intercalated nanocomposites without in situ
intercalative polymerization became the mainstream
of the nanotechnology after being reported by
Giannelis and co workers6,7
. The melt intercalation
involves mixing the layered silicate with the base
polymer above its softening temperature. Interest in
polyolefin nanocomposites has gained a large
momentum due to their promise of improved
performance in packaging applications8-12
. The
polyolefin nanocomposites preparation by melt
compounding is considerably more difficult due to
the weak interaction between the mineral surface
and the low energy material i.e. polyolefin.
Grafting of pendant anhydride groups has been used
successfully for the chemical modification of these
resins to overcome the poor phase adhesion in
polyolefin/clay systems. The role of maleated
polyolefin in preparation of polyolefin-based
nanocomposites has already been well described by
various researchers 13-23.
As low-density polyethylene found rapid
acceptance because of its high toughness, tensile
strength, puncture resistance and elongation at break
it can be used as base polymer for nanocomposites
preparation. In this communication nanocomposites
from LDPE and organophilic montmorillonite
(Nanomer 1.30P) were prepared by implementing
melt intercalation technique. Comparative accounts of
the melt flow characteristics; mechanical properties &
analytical characterization of the virgin and resulted
hybrids were carried out. The influence of epolene-
C16 (maleic anhydride grafted PE) as compatibiliser
on the mechanical performance, thermal
Corresponding Author:
Sanghamitra Parija
e-mail: [email protected]
22 Appl Sci Adv Mater Int, September 2014
characteristics and melt behavior of nanocomposites
were also evaluated.
Experimental Procedure
Materials
Low density polyethylene (Grade: with MFI 4.0 and
density 0.925 gm/cc from IPCL Ltd. (India) was used
as base polymer for the study.
Octa- decyl amine modified montmorillonite
(Nanomer -1.30P) with specific gravity 1.7g/cm3, 70-
75% montmorillonite clay and 25-30% octa -decyl
amine obtained from Nanocor Inc. U.S.A., was used
as reinforcing filler.
Maleic anhydride (MA) grafted Polyethylene (E-
142) with <1wt% MA content, acid number 5 and
Mw = 16,000 obtained from Eastman Chemicals Co.,
Germany was used as compatibiliser without further
modification.
Nanocomposite Preparation
Nanomer was kept in vacuum oven at 80°C for 2 h in
order to remove the absorbed moisture. The
nanocomposites samples were prepared in two stages.
At the first stage different LDPE/layered silicate
hybrids were prepared by melt compounding
technique taking three different weight percentage of
nanomer (1,3 and 5%), pre-weighed quantity of
LDPE with and without compatibiliser. Melt
intercalation was done at 50rpm rotor speed by using
torque rheometer (Haake Rheocord 9000,Germany)
having sigma roller rotors blades and a chamber size
of 69 cm3
volumetric capacities. The compounding
temperature was 160°C for a period of 15 min in all
the cases.
Subsequently these premixes were brought to
room temperature and separately molded by
compression molding using a 100T press, Delta
Malikson, India, for 10 minutes at 160°C with
molding tonnage of 10T to produce sheets of 3±
0.1mm thickness. Virgin LLDPE was compression
moulded under similar conditions of temperature for
comparison of mechanical properties. A Counter cut-
Copy milling machine 6490(CEAST, Italy) was used
for the preparation of test specimens from the sheets
as per ASTM-D-638, 790 and 256 using calibrated
templates24
.
Melt Flow Characteristics
The melt behavior of the nanocomposites as well as
virgin polymer was studied by melt flow index tests
using MFI tester (CEAST, Italy) as per the ASTM-D-
123824
. The molten sample was allowed to flow
through a standard die (2.095 mm diameter, length
8mm) keeping the temperature at 190°C and load 2.16
Kg. The MFI, shear rate and viscosity of the samples
were measured at a constant shear stress
Mechanical Property Evaluation
The specimens were prepared and subjected to the
influence of standard laboratory temperature of 23±1°
and relative humidity of 55±2% for 24 hours to bring
the materials into equilibrium before testing as per
ASTM- D-61824
to analyze various mechanical
properties with testing condition of 23± 1°C and
55±2% RH.
Tensile Properties
Specimens of virgin LLDPE, uncompatibilised and
compatibilised nanocomposites having dimensions
165x12.7x3mm were subjected to tensile tests as per
ASTM-D-63824
using universal testing machine
(UTM), LR-100K (Lloyd Instruments Ltd, U. K.) at
100 mm/min crosshead speed and 50mm gauge
length.
Flexural Modulus
The specimens of virgin, uncompatibilised and
compatibilised hybrids with 80 X 12.7 X 3mm
dimensions were subjected to flexural testing as per
ASTM-D-790 under three point bending using
universal testing machine (UTM) LR 100K Lloyds
Instruments Ltd. UK. The tests were carried out with
span length of 50mm and crosshead speed of
1.3mm/min.
Impact Strength
The izod impact strength of the nanocomposites and
virgin LLDPE was determined from the specimen
having dimensions 63.5X12.7X3mm with a V notch
with notch depth of 2.54mm and notch angle of 45° as
per ASTM-D- 256 by using Impactometer 6545
(CEAST, Italy).
Each mechanical data reported was the average of
five tests of the same specimen.
Thermal Characteristics Measurement
Differential Scanning Calorimetric (DSC) Analysis
Melting and isothermal crystallization behavior of the
nanocomposites and virgin LDPE were carried out by
differential scanning calorimeter (DSC, Perkin Elmer-
Pyris-6- USA). Samples with <5mg weight was
heated for the non-isothermal changes the samples
23 Parija S: Low Density Polyethylene/Layered Silicate Nanocomposites
from 50 to 225°C at the rate of 10°C/min under
nitrogen atmosphere. For isothermal change the
sample was kept at 225°C for 5 minutes in order to
remove the thermal history and then subjected to
cooling to 50°C at the rate of -10°C/min for the
crystallization temperature. For isothermal change the
samples were kept at 50°C for 5 minutes and then
heated up to 225°C for the melting point.
Thermo Gravimetric Analysis (TGA)
The TGA analysis of nanocomposites and virgin
polymer was studied in order to analyze the effect of
nanomer and compatibiliser on the thermal stability of
the base polymer by using a thermo gravimetric
analyzer (Mettle 4000). The samples of <10mg
weight were heated from 50°C to 600°C at the rate of
20°C/minutes under a protective nitrogen atmosphere.
The weight loss percentage was measured and
compared with the virgin polymer.
Nanocomposite Microstructure
Nanocomposite microstructure was investigated by
transmission electron microscopy using TEM –
Philips CM-20. Specimens of 75nm were cut from the
middle section of a compression-molded bar by using
a reichert microtome under cryogenic conditions and
then the film was retrieved onto Cu grids.
Results and Discussion
Melt behavior
The MFI, shear rate and viscosity data of the
LDPE/Clay nanocomposites and virgin polymer were
showed a decreased MFI and shear rate with
increased viscosity along with the increase in
nanoclay addition. The increase in viscosity is
attributed to the added nanoclay, a particulate filler
leading to the confinement of the polymer chains
those intruded in to the inter layer galleries of the
layered silicates
thereby affecting the flow
characteristics of the base polymer25
. Experimental
findings revealed that the melt behavior of the
resulted hybrids was not changed appreciably by the
addition of nanomer thereby unaffecting the
processibility of the base polymer.
The compatibilised nanocomposites showed
increased shear rate with decreased viscosity as
compared to the uncompatibilised one. The decrease
in viscosity is observed due to the increasing amount
of MAH-g-PE in the compatibilised LDPE/clay
hybrids containing low molecular weight oligomeric
fraction thereby increasing the flow of the LDPE.
Mechanical Properties
Tensile Properties
The tensile properties of the nanocomposites were
illustrated in Fig 1. It is well observed that the
nanocomposites show improved strength and modulus
values with reduced elongation at break than the
virgin LDPE. However, the strength and modulus of
the LDPE/ Clay hybrid has been increased up to 3%
nanomer loading (13.72%, 5.17% for 1% and
43.85%, 10.01 increment in tensile strength and
tensile modulus respectively for 3%) then decreased
for further increasing the clay loading to 5% (38.55 &
0.0% increment in tensile strength and modulus
respectively). The increment in strength and modulus
is attributable to the reinforcing and toughening
characteristics of dispersed nanolayers with high
aspect ratio. With large number of reinforcing
nanoclay platelets present in the polymer matrix
which act as efficient stress transfer agents in
nanocomposites induce plastic deformation into the
host polymer. It is expected that the macromolecules
contacted to the solid silica would have different
responses from those matrix because of the
mechanical displacement resulting from elongation,
which is responsible for the increased modulus of
nanocomposites26
. For higher percent clay loadings
corresponding strength and modulus of the hybrids
started to decrease mainly because of the
agglomeration of clay particles27,28
.
Fig. 1 Effect of nanomer loading on modulus of elasticity
of nanocomposites
Compatibilised nanocomposites showed linear
improvement in tensile modulus than the
uncompatibilised one (Fig. 2) up to 2% compatibiliser
loading and thereafter decreased drastically with
increase in epolene loading. The improvement is
attributable to the reinforcing effect of intercalated
nanolayers achieved through strong hydrogen
0
50
100
150
200
0 2 4 6
Nanomer(wt%)
Ela
sti
c M
od
ulu
s(M
Pa)
0
50
100
150
200
0 2 4 6
Nanomer(wt%)
Ela
sti
c M
od
ulu
s(M
Pa)
24 Appl Sci Adv Mater Int, September 2014
bonding between the OH groups of the maleic
anahydride group of MAH-g-PE and the oxygen of
the silicates thereby increasing the inter gallery space
of the nanoclay29
. At higher epolene loading the
nanocomposites showed decreased tensile modulus
due to the introduction of appreciable amount of low
molecular weight (MA-g-PE) fraction into the hybrid.
Fig. 2 Effect of epolene loading on modulus of elasticity of
nanocomposites
Flexural Modulus
Fig. 3 Effect of nanomer loading on Flexural modulus of
nanocomposites
The reinforcing benefit of nanomer loading on the
flexural modulus of the nanocomposites was reported
in Fig. 3. The nanocomposites showed increment in
flexural modulus (57.6,192.6 and 157% increment)
than the neat polymer for 1, 3 and 5% nanomer
loading respectively. However, modulus value
lowered for 5% than 3% clay loading. Increased
modulus for 1 and 3% nanomer loading is attributable
to the high stiffness of nanolayers with high aspect
ratio and anisotropy, which is acting as stress transfer
medium in the nanocomposites. The entanglement of
the polymer chain intruded into the inter gallery is
responsible for induced plastic deformation in the
hybrids. Similar observations were observed for other
nanocomposite systems30
. The toughness of
nanocomposites at higher nanomer loading might be
decreased due to the nanoparticle clusters inhibiting
plastic deformation of matrix by the constraining
effect of nanomer agglomerates31
.
Fig. 4 Effect of epolene loading on Flexural modulus of
nanocomposites
Compatibilised nanocomposites showed improved
flexural modulus (Fig. 4), which increased linearly
(4.19 increment for 1 % and 32.7increment for 2 %
respectively) with the epolene loading up to 2%
thereafter decreased drastically for further increasing
the MAH-g-PE. The improvement in toughness is
attributable to the reinforcing effect of separated
nanolayers achieved through intercalation of the
intruding MA-PE groups in the inter gallery space of
nanoclay inducing plastic deformation of the polymer
matrix. . However, at higher epolene loading the
nanocomposites showed decreased flexural modulus,
which is attributed to the introduction of appreciable
amount of low molecular weight (MA-PE) fraction
with lower toughness into the hybrid.
Impact Strength
The Impact strength (IS) values of nanocomposites
were shown in Fig. 5. IS increased by 43.8% than the
virgin LDPE for 1% nanomer and it is further
increased by 48.8% for 3% nanomer and then the
increment was reduced to 45.7% for 5% namomer
loading. The increment in impact strength suggested
that the resistance to crack propagation is enhanced
owing to the extensive plastic deformation of the
matrix bound to the nanomer. Circles of matrix
around the nanoparticles agglomerates, which was
proved to be substantially critical for consuming
failure energy45, t
is clearly a function of rate of
loading due to the viscoelastic nature of the inter
25 Parija S: Low Density Polyethylene/Layered Silicate Nanocomposites
phase. The decreased impact strength at higher clay
loading (5%) is attributed to detrimental effect of
nanomer clusters leading to non-uniform dispersion
of clay nanolayers in polymer matrix 32
.
Fig. 5 Effect of nanomer loading on impact strength of
nanocomposites
Fig. 6 Effect of epolene loading on Impact strength of
nanocomposites
The influence of added compatibiliser on the
impact strength was represented in Fig. 6. It is
observed that the impact strength of the
compatibilised nanocomposites improved linearly
(2.82% for 1% and 42.7% for 2%) with
compatibiliser addition up to 2% epolene and after
that the hybrids with higher epolene content showed
detrimental decrease in impact strength. The
improvement in IS might be due to the chain
entanglement by the intruded MAH-g-PE
macromolecules forming H-bonding with the oxygen
atom of the silicate tetrahedra inside the inter gallery
space of the clay. The interaction between the
grafted polymer and the base polymer also
contributed significantly towards the strength
increment33
. At higher epolene loading the
nanocomposites show decreased impact strength due
to the presence of appreciable amount of low
molecular weight (MAH-g- PE) fraction, which is
responsible for the decreased impact strength of the
hybrid.
Thermal Characteristics
Melting Point
Fig. 7 DSC Thermograms of nanocomposites for melting
behavior(Tm)
Melting point of LDPE, uncompatibilised and
compatibilised hybrids were reported in Fig. 7.
Uncompatibilised and compatibilised nanocomposites
showed higher melting point than the virgin polymer,
which is due to the higher thermal resistance of the
nanoclay. However, the difference in melting point
between both hybrids and virgin polymer were not
significant. This insignificant change in the melting
point is attributed to ineffectiveness of the nano filler
in changing the crystallite size of the base polymer34
.
Crystallization Characteristics
The crystallization exotherms of pure LDPE,
LDPE/Org-MMT and LDPE/MAH-g-PE/Org -MMT
systems were also reported. It is observed that the
LDPE/Clay nanocomposites exhibits a narrow
isothermal crystallization peak as compared to LDPE.
The crystallization process of LDPE seems to be
accelerated in the presence of clay platelets as
evidenced by the reduced peak width. The
crystallization temperature (Tc) of the
nanocomposites shifted to the higher side. The Tc for
the uncompatibilised nanocomposites is higher than
that of pure LDPE, which is explained by the
heterogeneous nucleation effect of the org-MMT
particle on the LDPE macromolecule segments35
.
Melted LDPE macromolecules can easily which leads
to the crystallization of LDPE molecules at a higher
26 Appl Sci Adv Mater Int, September 2014
temperature. From the result it is well observed that
the LDPE/MAH-g-PE/Org-MMT nanocomposites
showed higher Tc value than the uncompatibilised
one. The difference in crystallization temperature
between the LDPE/Org-MMT and LDPE/MAH-g-
PE/LDPE indicates the synergistic heterogeneous
nucleus effect of MAH-g-PE and Org-MMT on the
crystallization temperature of LDPE.
Thermal Stability
The dispersion of the clay is known to improve the
thermal stability of polymers. Fig. 8 presented the
results of the TGA analysis of LDPE samples. The
LDPE/clay hybrid showed increased thermal stability
than the pure LDPE. The increased thermal stability
of the uncompatibilised hybrid is due to the
introduction of inorganic clay with good thermal
stability as well as the interaction between the clay
particles and the polymer matrix36,37
.
Improved thermal stability of nanocomposites has
been attributed to the decreased permeability of
oxygen by the intercalated clay. Ogata et el reported
that the clay seemed to hinder the degradation of the
PLA hybrids at low temperature38
. The thermal
stability of the compatibilised nanocomposites was
more than the virgin and uncompatibilised one. The
higher thermal stability of the compatibilised hybrid
is attributed to the synergistic effect of the inherent
high heat resistance of the clay and the increased
interfacial interaction resulted between the clay
nanolayers, grafted polymeric fraction and the base
polymer. These results are in good agreement with the
PP/clay nanocomposites reported by Zanetti et al39
and Hambir et al40
.
Fig. 8 TGA Thermograms of nanocomposites
Nanocomposites Microstructure
The internal structure of the nanocomposites in the
nanometer scale was directly observed via TEM
analyses. Fig. 9a and b showed the result of the TEM
bright field images of the uncompatibilised as well as
compatibilised nanocomposites. It is revealed that the
clay layers are stacked to form intercalated structure
in case of uncompatibilised nanocomposites
contributing to the reduced benefits of the nano filler.
On the other hand the TEM image revealed that
layered silicates with smaller stacks were dispersed to
give a well interacted with strong flocculation
structure giving good adhesion between the nano
layers, LDPE and MAH-g-LDPE in case of
compatibilised hybrid.
Fig. 9 TEM micrograph of nanocomposites
Conclusion The incorporation of org-MMT in the LDPE matrix
leads to concurrent improvement in the mechanical
properties of the organoclay /LD hybrid for a
relatively lower nanomer loading (3%) without
affecting the processibility of the base polymer.
LDPE showed marginal decrease in MFI, shear rate
and increased viscosity with nanomer addition. The
nanomer as well as compatibiliser loading play
important roles in producing LDPE/ layered silicate
nanocomposites with superior mechanical properties
through intercalation of base polymer in the inter
gallery space of the layered silicates by mechanical
shear.
References 1 Lee J, Takekoshi T & Giannelis E P, Mater Res Sympo
Proc, 57 (1997) 513.
2 Gilman W J, Appl Clay Sci, 15 (1999) 31.
3 Vaia R A, Price G, Ruth P N, Nguyen H & Lichetenhan
T, Appl Clay Sci, 15 (1999 67.
4 Krishnamoorti R, Vaia R A & Giannelis E P, Chem
Mater, 8 (1996) 1728.
5 Okamoto M, Moitra S, Taguchi H, Kim Y H & Kotaka
T, Polymer, 41 (2000) 3887.
27 Parija S: Low Density Polyethylene/Layered Silicate Nanocomposites
6 Frones T D, Yoon P J, Keskula J H & Paul D R,
Polymer, 42 (2001) 9929.
7 Vaia R A, Jandt K D, Kramer E J and Giannelis E P,
Chem Mater, 8 (1996) 2628
8 Liu L M, Qu Z N & Zau X G, J Appl Polym Sci, 63
(1997) 137.
9 Zhang Q & Fu Q, Polym Int, 49 (2000) 1561.
10 Reichert P, Nitz H, Klinke S, Brangsch R, Thomann R
and Mulhaupt R, Macromol Mater Eng, 275 (2000) 8.
11 Fisher H, Geigens L, & Koster T, Nanocomposites from
Polymer and Layered silicate materials TNO-TOPD
report, 1998.
12 Giannelis E P, Adv Mater, 6(8) (1996) 29.
13 Vaia R A & Ishii G, Chem Mater, 5 (1993) 1694.
14 Gilman J W & Jackson C L, Chem Mater, 12 (2000)
1866.
15 Pavilkova S, Thomann R, Reichert P, Mulhaupt R,
Marcincin A & Borsig E, J Appl Polym Sci, 89 (2003)
604.
16 Somwangthanaroj A, Lee E C & Solomon M J,
Macormol, 36 (2003) 2333.
17 Balazs A, Singh C & Zhulina E, Macromol, 31 (1998)
8370.
18 Kato M, Usuki, A & Okada A, J Appl Polym Sci, 66
(1997) 1781.
19 Galgali G, Ramesh C & Lele A, Macromol, 34 (2001)
852.
20 Wang K H, Choi M H, Koo C M, Choi Y S & Chung I
J, Polymer, 42 (2001) 9819.
21 Karukawa Y, Yasuda H & Oya A, J Mater Sci Lett, 16
(1997) 1670.
22 Hasewaga K M, Kato M, Usuki A & Okada A, J Appl
Polym Sci, 67 (1998) 87.
23 Seo Y, Kim J, Kim K U & Kim Y C, Polymer, 41
(2000) 2639.
24 Annual Book of ASTM standards,(08-01)-Plastic-C(1)-
2343. (1988 )
25 Ji X L, Jing J K, Jiang W & Jiang B Z, Polym Eng Sci,
42 (2002) 983
26 Chang J H & An A U, J Polym Sci Part B: Polym Phys,
40 (2002) 670.
27 Masenelli-Varlot K, Reynaud E, Vigier G & Varlet J, J
Polym Sci, Part B: Polym Phy, 40 (2002) 272.
28 Zhang M Q, Rong M Z, Zhang H B & Friedrich K,
Polym Eng Sci., 43(2) (2003) 490.
29 Parija S, Nayak S K, Verma S K & Tripathy S S, Polym
Composites, 25(6) (2004,) 646.
30 Rong M Z, Zhang M Q, Zheng Y X, Zeng H M, Walter
R & Friedrich K, Polym, 42 (2001) 167.
31 Chang J H, Park K D, Cho D, Yang H S & Inh K J,
Polym Eng Sci, 41 (2001) 1514.
32 Kurokawa Y, Yusuda H & Oya A, J Mater Sci Lett, 15
(1996) 1481.
33 Yasue K, Katihara S, Yashikawa M & Fusimota K, “In
Situ Polymerization Route to Nylon-6
Nanocomposites” in Polymer-Layered silicate
Nanocomposites Ed Pinnavaia T J & Beall G W,
Wiley (2000).
34 Maity P, Nam P H, Okamoto M, Kotaka T, Hasegawa
N & Usuki A, Polym Eng Sci, 42 (2002) 1864.
35 Xu Wliang G, Wang W, Tang S, He P & Pan W P, J
Appl Polym Sci, 88 (2003) 3093.
36 Dho J G & Cho I, Polym Bull, 41 (1998) 511:8.
37 Wen J & Wikes G L, Chem Mater, 8 (1996) 1667.
38 Ogata N, Jimenez G, Kawai H & Ogihara T, J Polym
Sci Part B: Polym Phy, 35 (1997) 389.
39 Zanetti M, Camino G, Reichert P & Mulnaupt R,
Macromol Rapid Comm, 22 (2001) 176.
40 Hambir S, Bulakh N & Jog J P, Polymer Engg Sci, 42
(2002) 1800.
Applied Science and Advanced Materials International
Vol. 1 (1), September 2014, pp. 28-31
Impedance Spectroscopy Of Zn0.98Nd0.02O nano Ceramic By
High Energy Ball Milling
Tanushree Das*, Bikram keshari Das, Kajal Parashar, S.K.S. Parashar,
Nano Sensor Lab, School of Applied Sciences, KIIT University, Bhubaneswar-751024,Odisha, India.
Received 21 August 2014; accepted 5 September 2014
Abstract The electrical properties of Zn0.98Nd0.02O nano ceramic synthesized by high energy ball milling technique
was investigated by Impedance spectroscopy in the frequency range 100Hz to 1MHz and temperature range 3000c-
5000c.Complex Impedance Spectroscopy(CIS) plot reveals the presence of both bulk and grain boundary effect,
Negative temperature co-efficient of resistance (NTCR) and follow non-Debye relaxation phenomena. Variation of
AC conductivity as a function of frequency increases with increase in temperature.
Keywards Zn0.98Nd0.02O,Impedance spectroscopy,AC conductivity
The promise of nanocrystals as a technological
material for applications including wavelength
tuneable lasers1, bioimaging
2, and solar cells
3 may
ultimately depend on tailoring their behaviour by
adding impurities through doping. Impurities are
reported to modify electronic, electrical, optical,
and magnetic properties of bulk semi-conductors.
Zinc oxide (ZnO) is an important semiconductor
material both in the form of a ceramic or a powder.
Intrinsically, ZnO is a n-type semiconducting
compound with a wide band gap energy of about
3.37 eV and a large exciton binding energy of 60
meV at room temperature4. Due to its unique
properties, ZnO can be used for many applications
including the production of paint5, ceramics
6,
photocatalysis7 and electronics
8.It is well known
that ZnO nanoparticles can be fabricated through
two major routes, namely (1) the top-down route
that includes conventional9, mechanochemical
10 and
mechanical milling11
and (2) the bottom-up route
that includes solvothermal12
,sol–gel13
and
precipitation methods14
. Both these major routes
have different advantages and disadvantages; but
each can be used to produce high quality ZnO
nanoparticles. Rare earth elements(REEs), such as
Eu,Er,and Gd,are characterized by abundant energy
levels and multi-substrate and exhibit very sharp
and temperature independent luminescence in the
ultra violet(UV) and visible light range15–17
. REEs
such as Eu, Er and Tb doped into the ZnO
semiconductor can be tuned over the entire
ultraviolet(UV) and visible light range18–20
. For
example, Eu doped ZnO exhibits red light15
, while
Er doped ZnO exhibits a green emission21
. REE
Gd3+
is of particular interest because its scintillation
properties22
, which allow it to be used to make
phosphor films23-24
. Amornpitoksuk et al.25
investigated the effects of Ag doped ZnO
nanoparticles, prepared by a precipitation method,
on their structural, photocatalytic and antibacterial
properties. They reported that the particle sizes
decreased, and the photocatalytic efficiency for
degradation of methylene blue increased as a
function of the Ag concentration. Benhebal et
al.26
showed that the band gap energy was reduced
when ZnO was doped with 10% lithium, sodium or
potassium due to an increase in its crystallinity. The
Na- and Li-doped ZnO particles also had an
improved efficiency to degrade phenol and benzoic
acid, but the K-doped ZnO particles had reduced
degradation efficiency. Anandan et al. prepared La-
doped ZnO nanoparticles by a co- precipitation
method and they showed that the rate of degradation
of monocrotophos in aqueous solution for La doped
ZnO nanoparticles increased with an increase of the
La content up to 0.8 wt% and then decreased27
. In
addition, the properties of other metal dopants such
Corresponding Author:
Tanushree Das
e-mail:[email protected]
29 Das et al.: Impedance Spectroscopy
as Al, Ta, Sn, Cu, Cd, Pd, Cr and Mn on the ZnO
properties were also investigated28-35
.
Through mechanical milling technique, the
particle size down can easily reduce to nanoscale
level, the solubility limit of doping metal can be
extended at low temperature and amorphous phase
can be easily produced36
.It appears from our
literature survey that synthesis of Zn0.98Nd0.02O
material by ball milling and its electrical
characterization through Impedance analysis have
received little attention. In view of this, we have
carried out complex Impedance spectroscopy
studies on Zn0.98Nd0.02O with an aim to investigate
the picture of electrical properties prepared by high
energy ball milling.
Experimental Procedure Nanocrystalline Zn0.98Nd0.02O ceramic was
synthesized by high energy ball milling
technique(HEBM, PM 400Retsch,Germany). High
purity ZnO and Nd2O3 used as a raw material was
weighed according to their atomic ratio. The
powder was milled in tungsten carbide vials with
tungsten carbide balls by taking ball to powder ratio
10:1 for 10 hr at 300rpm in wet milling condition. It
is well known that the proper choice of milling
parameters such as milling time, ball to powder
mass ratio and rotation speed have major role in the
preparation of ZnO nanoparticles37
.The mixture was
milled for 1hr, alternating with a stop of 30 min to
prevent over heating and to reduce engine wear.
Generation of heat during mill is due to the kinetic
energy of grinding medium and secondly due to the
exothermic process occurring during milling38
.The
mixture powder was calcined at 11000C at a heating
rate of 20c per minute to obtain the desired product.
The calcined powder was pressed into circular disc
(pellet) using PVA as binder. The role of PVA is to
reduce the brittleness and to have better
compactness among the granuals of the material.
Finally the pellet was sintered at 12000C for 2 hr
and coated
with silver paste on both side and heated at 7000C
for 15min, for electrical measurement. The
electrical properties of sintered sample was
characterized by computer controlled Impedance
analyser (Hioki LCR Hi-tester-3532-50).
Result and Discussion
Impedance analysis
Impedance spectroscopy is an experimental tool for
the characterization of electrical behaviour of
electrochemical cells or electronic materials. It is an
important technique in view of its simplicity and
clarity in describing the electrical processes
occurring in a system on applying an ac signal as
input perturbation. The output response, when
plotted in a complex plane plot, appears in the form
of a succession of semicircles representing electrical
phenomena due to bulk material, grain boundary
effect and interfacial phenomena if any. In view of
this specialty, CIS makes it possible to separate the
contribution due to different components in a
polycrystalline sample, that of course have different
time constants, in the frequency domain. The
frequency dependent properties of a material is
normally described in terms of any of the formalism
expressed as: 39
Complex impedance,
Z* = Z'− jZ "= Rs– j/ωCs
Complex admittance,
Y*= Y'+ jY" = 1/Rp+ jωCp= G(ω) + jB(ω)
Complex permittivity (dielectric constant),
ε* = ε' − jε"
Complex modulus,
M*= 1/ε*= M '+ jM"= jωC0Z*
and tan δ = −Z'/Z" = Y'/y" = ε "/ε' = M" /M'
where (Z',Y', ε', M') and (Z", Y", ε", M") are the
real and imaginary components of impedance,
admittance,permittivity and modulus respectively,
G: conductance, B:susceptance,and tan δ: dielectric
loss. They are interrelated with each other.
Fig. 1 shows the variation of real part of
impedance (Z') wit frequency at different
temperature (3000C - 500
0C). It is observed that, the
curves display decrease in the value of Z' with the
increase in both frequency as well as temperature,
indicating an increase in AC conductivity with the
rise in temperature and frequency 40
. Again, at low
frequencies the value of Z' decreases with rise in
temperature40
.
Fig. 2 shows the variation of imaginary part of
impedance (Z'') with frequency at different
temperature. This plot is most suitable for
evaluation of relaxation frequency.Each
semicircular arc in the impedance has a
characteristics peak occurring at a unique relaxation
frequency(ωmax) attributed to electrical phenomena
due to different components in the sample. It can be
expressed as: 39
ωmaxRC= ωmaxτ= 1
⇒ ωmax = 1/τ = 1/RC
⇒ fmax = 1 / 2πτ= 1 / 2πRbCb
Relaxation frequency and hence relaxation time
(τ) is a parameter that depends only on the intrinsic
properties of the material and not on the sample
geometrical factors. The term intrinsic properties of
the material refer to the properties attributed to
structure/microstructure (i.e. grain interior or bulk,
grain boundary, etc.). It can be seen that, The
magnitude value of resonance frequency decreases
30 Appl Sci Adv Mater Int, September 2014
and shifting towards high frequency side with
increase in temperature. This indicates the
temperature dependence of electrical relaxation
phenomena of the material. Again a typical peak
broadening is observed with rise in temperature
suggesting a spread of relaxation time40
.
Fig. 1 Variation of real part of impedance(Z') of
Zn0.98Nd0.02O with frequency at different temperature.
Fig. 2 Variation of imaginary part (Z'') of impedance of
Zn0.98Nd0.02O with frequency at different temperature.
Fig-3 shows the CIS plot(z' vs z'' ) of
Zn0.98Nd0.02O nano ceramic measured at different
temperature( 3000c- 500
0c ). The complex
impedance spectrum comprised at high frequency
semicircle as well as low frequency semicircle, This
is due to contribution of both bulk and grain
boundary effects. The proposed material
Zn0.98Nd0.02O has semicircular arc and plots with
centre located below the real axis, describe non-
Debye relaxation.
AC conductivity
Conductivity analysis provides significant
information related to transport of charge carriers,
i.e electron/hole or cations /anions that
predominates the conduction process and their
response as a function of temperature and
frequency41
. Fig-4 shows the variation of AC
conductivity of Zn0.98Nd0.02O as a function of
frequency at different temperature. The frequency
dependent conductivity of material exhibit both low
and high frequency dispersion phenomena. This
follows the Jonscher's power law42
. s
dcac A
Where s is frequency exponents in the range of
0<n<1.Both the σdc and Aare thermally activated
quantities and indicate that the conduction is a
thermally activated process.From fig it is observed
that the AC conductivity value increases with
increase in temperature, indicating electrical
conduction in the material. The increasing
conductivity w.r.t. temperature indicates the
negative temperature co-effecient of resistance of
(NTCR) behaviour due to the grain and grain
boundary resistance.
Fig. 3 Variation of (Z' and Z'') of impedance of
Zn0.98Nd0.02O with frequency at different temperature
Fig. 4 Variation of Ac conductivity of Zn0.98Nd0.02O as a
function of frequency at different temperature
100 1000 10000 100000 1000000
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000 Zn0.98
Nd0.02
O,12000C Sint
Z'
Frequency(Hz)
3000c
3250c
3500c
3750c
4000c
4250c
4500c
4750c
5000c
100 1000 10000 100000 1000000
0
-500
-1000
-1500
-2000
-2500Zn
0.98Nd
0.02 O,1200
0C Sint
Frequency(Hz)
3000c
3250c
3500c
3750c
4000c
4250c
4500c
4750c
5000c
Z''
0.0 2.0x103
4.0x103
6.0x103
8.0x103
1.0x104
1.2x104
0.0
-2.0x103
-4.0x103
-6.0x103
-8.0x103
-1.0x104
-1.2x104
Zno.98
Nd0.02
O,12000c sint 300
0c
3250c
3500c
3750c
4000c
4250c
4500c
4750c
5000c
Z''
Z'
100 1000 10000 100000 1000000
-2.0x10-2
0.0
2.0x10-2
4.0x10-2
6.0x10-2
8.0x10-2
1.0x10-1
1.2x10-1
1.4x10-1 Zn
0.98Nd
0.02 O,1200
0C Sint
Frequency(Hz)
3000c
3250c
3500c
3750c
4000c
4250c
4500c
4750c
5000c
Ac C
on
du
cti
vit
y
31 Das et al.: Impedance Spectroscopy
Conclusion Nanocrystalline Zn0.98Nd0.02O ceramic synthesized
by high energy ball milling technique. From the
Impedance spectroscopic studies the material
showed relaxation effects which are non- Debye
type and NTCR effect The relaxation frequencies
shifted to higher frequency side with increase in
temperature. The CIS plots reveals the contribution
of both bulk and grain boundary effect.The AC
conductivity increases with increase in temperature.
References 1 Klimov V I, Ivanov S A, Nanda J, Acher-mann A,
Bezel I, McGuire J A & Piryatinski A, Nature, 447
(2007) 441.
2 Michalet X, Pinaud F F, Bentolila L A, Tsay J M,
Doose S, Li J J, Sundaresan G, Wu A M,Gambhir S
S & Weiss S, Science, 307 (2005) 538.
3 Gur I, Fromer N A, Geier M L & Alivisatos A P,
Science, 310 (2005) 462.
4 Suwanboon S, Amornpitoksuk P & Muensit N,
Ceramics Int, 37 (2011) 2247.
5 Mikhailov M M, NeshchimenkoV V, Dedov N
V,Chundong L & Shiyu H, J Surf Invest, 5 (2011)
1152.
6 Kushnirenko V I, Markevich IV V & Zashivailo T
V, J Lumine Sci, 132 (2012) 1953.
7 Amornpitoksuk P, Suwanboon S, Sangkanu S,
Sukhoom A & Muensit N, Super Lattic Microstruct,
51 (2012) 103.
8 Vishwas M, NarasimhaRao K , ArjunaGowda V K &
Chakradhar R P S, Spectrochimi Acta, PartA:
Molecul Biomolecul Spectr, 5 (2012) 423.
9 Chang Y S, Chang Y H, Chen I G, Chen G J,Chai Y
L, Fang T H & Wu S, Ceramics Int, 130 (2004)
2183.
10 Sabri N S , Yahya A K & Talari M K, J Lumine Sci,
132 (2012) 1735.
11 Suwanboon S, Amornpitoksuk P & Bangrak P,
Ceramics Int, 37 (2011) 333.
12 Ye N & Chen C C, Optic Mater, 34 (2012) 753.
13 Suwanboon S, Sci Asia: J Sci Soc Thailand, 34
(2008) 31.
14 Samaele N, Amornpitoksuk P & Suwanboon S,
Powder Technol, 203 (2010) 243.
15 Wang D, Wang J Y, Cao J, Lang J, Gao M & Liu X,
Chem Res Chinese Univ, 27 (2011) 174.
16 Guo C, Ding X & Xu Y, J Am Ceram Soc, 93 (2010)
1708.
17 Kaur G, Dwivedi Y & Rai S B, J Fluoresc, 21 (2011)
423.
18 Ji S,Yin L, Liu G, Zhang L & Ye C, J Phys Chem, C
113 (2009) 16439.
19 Armelao L,Heigl F, Jurgensen A, Blyth R I R,Regier
T and Zhou X T, et al.,JPhysChem, 2007, C111,
10194.
20 Li G,Dawa C,Lu X,Yu X,Tong Y,Langmuir, 2009,
25, 2378.
21 Chao L C,Chiang P C,Yang S H,Huang J W,Liau C
C, and Chen J S, et al.,JapJApplPhys, 2006, 45, 938.
22 Kobayashi Fu M and Parker J M,JLuminesc, 2001,
94, 321.
23 Seo S Y,Lee S, Park, H D, Shin N and Sohn K
S,JApplPhys, 2005, 92, 5248.
24 Bae J S,Jeong J H,Yi S S and Park J C,ApplPhysLett,
2003, 82, 3629.
25 Amornpitoksuk P, Suwanboon S, Sangkanu S,
Sukhoom A, Muensit N andBaltrusaitis J, Powder
Technol, 2012, 219, 158.
26 Benhebal H, Chaib M, Leonard A, Lambert S D and
Crine M, Mater SciSemiconducProc, 2012, 15, 264.
27 Anandan S, Vinu A, Sheeja Lovely K L P,
Gokulakrishnan P, Srinivasu P, MoriT, Murugesan V,
SivamuruganV,andAriga K, JMoleculCataly A:
Chem, 2007, 266, 149.
28 Hsiao K C,Liao S C and Chen Y J,MaterSciEngg, A:
StructurMater:Properties,MicrostructProces, 2007,
447, 71.
29 Kong J Z,Li A D,Zhai H F,Gong Y P,Li H and Wu
D,JSolid StateChem, 2009, 182, 2061.
30 Jia X,Fan H,Afzaai M,Wu X and Brien P O,J Hazard
Mater, 2011, 193, 194.
31 Mohan R,Krishnamoorthy K and Kim S
J,SolidStateComm, 2012, 152, 375.
32 Karunakaran C,Vijayabalan A and Manikandan
G,SuperlatticMicrostruct, 2012, 51, 443.
33 Zhong J B, Li J Z, He X Y, Zeng J, Lu Y, Hu W and
Lin K, Current ApplPhys, 2012, 12, 998.
34 Wu C, Shen L, Zhang Y C and Huang Q, MaterLett,
2011, 65, 1794.
35 Ullah R and Dutta J,JHazardMater, 2008, 156, 194.
36 Suryanarayana C, Prog Mater Sci, 2011, 46, 1.
37 Vojisavljevic K,Scepanovic M, Sreckovic T, Grugic-
Brojcin M,Brankovic Z and Brankovic G ,
JPhys:Condens Matter, 2008, 20, 475202.
38 Suryanarayana C,Prog Mater Sci 2001:46, 1.
39 PradhanDillip K, Samantaray B K, Choudhary R NP
and Thakur A K.,Mater SciEngg, 2005, B 116, 7.
40 Sahoo P S , Panigrahi A, patri S K & Chaudhary R N
P, Bul Mater Sci, 33(2) (2010) 129.
41 Shukla A & Chaudhary R N P, Physica B, 405 (2010)
99.
42 Jonscher A K, Nature, 276 (1977) 673.
Applied Science and Advanced Materials International
Vol. 1 (1), September 2014, pp. 32-36
Sequence Based Prediction of Kink in Transmembrane Helices by Neural
Network Method
N. Mishra1, A. Khamari
2, M. R. Panigrahi
3, J. K. Meher
4, M. K. Raval
5
1Dept of Chemistry, Rajendra College, Balangir, Odisha, India -767002 2Dept of Physics, Rajendra College, Balangir, Odisha, India – 767002
3Department of Chemical Engineering, Orissa Engineering College, Bhubaneswar, India
4Dept of Computer Science and Engineering, Vikash College of Engg for Women, Bargarh, India-768028
5Department of Chemistry, Gangadhar Meher College, Sambalpur, Odisha, India – 768004,
Received 01 September 2014; accepted 10 September 2014
Abstract The kinks (bends) in helices play an important role in functions of transmembrane proteins. Kinked helices
are believed to be required for appropriate helix-helix and protein-protein interaction in membrane protein complexes.
Therefore, knowledge of kink and its prediction from amino acid sequences is of great help in understanding the
function of proteins. However, determination of kink in transmembrane α-helices is a computationally intensive task. In
this paper we have developed Neural Network method based on radial basis function for prediction of kink in the
helices with a prediction efficiency of 85%. A feature vector generated using three physico-chemical properties such as
alpha propensity, coil propensity, and EIIP constituted in kinked helices contains most of the necessary information in
determining the kink location. The proposed method captures this information more effectively than existing methods.
Keywords Kink, Transmembrane α-helices, RBF, Feature vector, Physico-chemical properties.
Knowledge of segments of transmembrane proteins
and the bends in helices help in the study of tertiary
structure and hence understanding the role played
by that protein. 20-30% of all the proteins in any
organism are membrane proteins. These are of
particular importance because they form targets for
over 60% of drugs on the market. Transmembrane
α-helix bundle is a common structural feature of
membrane proteins except porins, which contains
β-barrels. Membrane spanning α-helices differ
from their globular counterpart by the presence of
helix breakers, Pro and Gly, in the middle of
helices. Pro is known to induce a kink in the
helix1,2
. A hypothesis suggests that Pro is
introduced by natural mutation to have a bend and
later further mutated leaving the bend intact for
required function during the course of evolution3.
The role of Pro and kinks in transmembrane helices
were extensively investigated both experimentally
and theoretically to unravel the nature's
architectural principles2,4
. Another observation
suggest induction of kink at the juncture of α-
helical and 310 helical structure in a
transmembrane helix2-6
. Mismatch of
hydrophobicity of lipid bilayer and peptide may
also result in distortion of α-helical structure7.
Sequences of straight and kinked helices were
further subjected to machine learning to develop a
classifier for prediction of kink in a helix from
amino acid sequences. Support vector machine
(SVM) method8 projects that helix breaking
propensity of amino acid sequence determines kink
in a helix. DWT has been applied on
hydrophobicity signals in order to predict
hydrophobic cores in proteins10
. Protein sequence
similarity has also been studied using DWT of a
signal associated with the average energy states of
all valence electrons of each amino acid11
. Wavelet
transform has been applied for transmembrane
structure prediction12
. Signal processing methods
Corresponding Author:
N Mishra
e-mai: [email protected]
A Khamari
e-mai: [email protected]
M R Panigrahi
e-mail: [email protected]
J K Meher
e-mail: [email protected]
M K Raval
e-mail: [email protected]
33 Mishra et al.: Sequenced Based Prediction of Kink
such as Fourier transform and wavelet transform
can identify periodicities and variations in signals
from a background noise. The presence of kink in
amino acid sequence is determined effectively in
transform domain analysis13
.
Kinked and straight helix of protein Type-4
Pilin and Chlorophyll A-B binding protein
respectively are shown in Fig.1.
Fig. 1 Backbone representation of (a) kinked helix of
type-4 pilin protein (2pil) (b) straight helix (second helix)
of chlorophyll a-b binding protein (1rwt
A kink in a helix may be formed by helix-helix
interaction. In such cases the intrinsic kink forming
or helix breaking tendency may not be required.
Even a helix forming tendency may be overridden.
This possibility clamps a theoretical limit to predict
a kink with high accuracy. Hence there is a need to
develop advanced algorithm for faster and accurate
prediction of kink in transmembrane helices. This
motivates to develop novel approach based radial
basis function neural network (RBFNN) to
effectively predict kink in transmembrane α-helices.
Materials and Methods
Database.
List of transmembrane proteins and their coordinate
files were obtained from the Orientation of Proteins
in Membranes (OPM) database at College of
Pharmacy, University of Michigan
(http://www.phar.umich.edu).
Determination of α-helical regions.
Dihedral angles were computed using
MAPMAK from coordinate files and listed for each
residue along with assignment of conformational
status of the residue namely right or left helical, β-
strand. Molecular visual tools RasMol were used to
visually confirm the transmembrane α-helical
regions.
Computation of helix axis.
Helix axis was computed from the approximate
local centroids θi’(xi0,yi
0,zi
0) of the helix by taking
a frame of tetrapeptide unit [9].
(1)
where xi, yi, and zi are the coordinates of Cα atoms
of the tetrapeptide frame. Unit vector in the
direction of resultant of vectors θ'iθ'i+1 yields
direction cosines (l, m, n) of axis of helix (A). The
axis pass through the centroid of the helix θ0 = (X
0,
Y0, Z
0).
(2)
where n is the number of residues in a helix.
Refined local centers θi of helix are then calculated
for each Cα by computing the foot of perpendicular
drawn from Cαi to A.
Location of hinges.
Hinges were located in a helix by a distance
parameter d(CiNi+4), where Ci is the backbone
carbonyl carbon of ith residue and Ni+4 is backbone
peptide nitrogen of i+4th residue [9]. Value of
d(CiNi+4) beyond the range 4.227±0.35$ Å reflects
a hinge at the ith residue in the helix. Hinge was
quantified by two parameters kink and swivel [3].
Calculation of Feature Parameters Here physico-chemical properties of amino
acids are used to draw the feature vector. These are alpha, coil and Electron ion pseudpotential interaction potential (EIIP) as shown in Table 1.
Radial basis function neural network
classifier (RBFNNC). In this paper we have introduced a low complexity radial basis function neural network (RBFNN) classifier to efficiently predict the sample class [14,15] . The potential of the proposed approach is evaluated through an exhaustive study by many benchmark datasets.
The experimental results showed that the proposed method can be a useful approach for classification. A radial basis function network is an artificial neural network that uses radial basis functions as activation functions. It is a linear
3
03
03
0
4
1 ,
4
1 ,
4
1 i
i
ii
i
i
ii
i
i
ii zzyyxx
n
i
i
n
i
i
n
i
i zn
Zyn
Yxn
X1
0
1
0
1
0 1 ,
1 ,
1
34
Appl Sci Adv Mater Int, September 2014
combination of radial basis functions. The radial basis function network (RBFNN) is suitable for function approximation and pattern classification problems because of their simple topological structure and their ability to learn in an explicit manner. In the classical RBF network, there is an input layer, a hidden layer consisting of nonlinear node function, an output layer and a set of weights to connect the hidden layer and output layer. Due to its simple structure it reduces the computational task as compared to conventional multi layer perception (MLP) network. The structure of a RBF network is shown in Fig. 1.
Table 1 Physicochemical parameters of amino acid
residues used in algorithm for prediction of Ni-binding
sites in proteins
Amino acid Alpha Coil EIIP
A 1.372 0.824 0.0373
R 0.694 0.893 0.0959
N 0.473 1.167 0.0036
D 0.416 1.197 0.1263
C 1.021 0.953 0.0829
Q 0.765 0.947 0.0761
E 0.704 0.761 0.0058
G 0.913 1.251 0.0050
H 1.285 1.068 0.0242
L 1.471 0.810 0.0000
I 1.442 0.886 0.0000
K 0.681 0.897; 0.0371
M 1.448 0.810 0.0823
F 1.459 0.797 0.0946
P 0.526 1.540 0.0198
S 0.903 1.130 0.0829
T 0.910 1.148 0.0941
W 1.393 0.941 0.0548
Y 0.907 1.109 0.0516
V 1.216 0.772 0.0057
In the RBFNN based classifier, an input vector x is used as input to all radial basis functions, each with different parameters. The output of the network is a linear combination of the outputs from radial basis functions.
For an input feature vector x, the output y of the jth
output node is given as.
Fig.1 The structure of a RBF network
k
2k
x(n) CN N
2
j kj k kj
k 1 k 1
y w w e
(3)
The error occurs in the learning process is
reduced by updating the three parameters, the
positions of centers (Ck), the width of the Gaussian
function (σk) and the connecting weights (w) of
RBFNN by a stochastic gradient approach as
defined below:
ww(n 1) w(n) J(n)w
(4)
k k c
k
C (n 1) C (n) J(n)C
(5)
k k
k
(n 1) (n) J(n)
(6)
Where, 21J(n) e(n)
2
, e (n)=d(n) - y(n)
is the error, d(n) is the target output and y(n) is the predicted output. w C and are the learning parameters of the RBF network.
Simulation Studies and Discussions In order to compare the efficiency of the proposed
method in predicting the class of the kink data we
have used standard datasets. All the datasets
categorized into two groups: binary class to assess
the performance of the proposed method. The
dataset consists of amino acid sequences of 9
characters. 400 sequences from kink dataset and
400 sequences from non-kink dataset are taken as
35 Mishra et al.: Sequenced Based Prediction of Kink
training set. The feature selection process proposed
in this paper includes alpha, coil and EIIP as shown
in the Table 1. To implement the RBFNN classifier,
we first read in the file of protein sequence which is
represented with numerical values. The
performance of the proposed feature extraction
method is analyzed with the neural network
classifiers: RBFNN. The leave one out cross
validation (LOOCV) test is conducted by
combining all the training and test samples for the
classifiers with datasets [16]. LOOCV is a
technique where the classifier is successively
learned on n-1 samples and tested on the remaining
one. i.e., it removes one sample at a time for testing
and takes other as training set. It involves leaving
out all possible subsets so the entire process is run
as many times as there are samples. This is repeated
n times so that every sample was left out once.
Repeating these procedure n times gives us n
classifiers in the end. Our error score is the number
of mispredictions. Out of 400 sequences from kink
dataset all 400 samples are detected as true positive
whereas out of all 400 sequences from non-kink
dataset,all 400 samples are detected as true
negative. The prediction accuracy has been analyzed in
terms of two measuring parameters such as accuracy (A), precision (P) and recall (R). These are defined in terms of four parameters true positive (tp), false positive (fp), true negative (tn) and false negative (fn). tp denotes the number of kinks and are also predicted as kinks, fp denotes the number of actually Non-kinks but are predicted to be kinks, tn is the number of actually Non kinks and also predicted to be kinks, and fn is the number of actually kinks and predicted to be Non kinks.
Accuracy
The accuracy of prediction of kinks in amino acid sequence is defined as the percentage of kinks correctly predicted of the total sequences present. It is computed as follows:
(7)
Precision
Precision is defined as the percentage of kinks
correctly predicted to be one class of the total kinks
predicted to be of that class. It is computed as:
(8)
Recall
Recall is defined as the percentage of the kinks that
belong to a class that are predicted to be that class.
Recall is computed as:
(9)
A query sequence of 35 kink samples and 35 non-
kink samples are tested for validation and the result
obtained is shown in table 2.
Table 2 Measuring parameters for prediction
accuracy
Actual
Predicted
Kink Non-kink
Kink 30 (tp) 5 (fp)
Non-kink
6(fn) 29 (tn)
The accuracy, precision and recall are 0.85,
0.84, and 0.84 respectively. The accuracy of sequence based classifiers reported so far is about 85%. Hence the present classifier appears to have high accuracy compared to existing sequence based classifiers.
Conclusion
Neural network approach based on radial basis
function plays a vital role in the prediction of kink
in transmembrane α-helix. The proposed method is
not only fast but also has improved accuracy (85%)
as compared to SVM learning system (80%)
reported by us earlier8. However prediction of kink
in a helix depends on the features of amino acid
sequence. Feature vector with propensities of
residues in helix and coil along with EIIP are only
used for numerical representation in the present
study. Although kink prediction has its own
limitations, the present work is primary report in
the area of helix kink prediction from amino acid
sequence based on neural network algorithms.
Acknowledgment
The authors wish to thank management members
and the principal of the college for all kinds of
supports to complete this work.
nnpp
np
ftft
ttA
pp
p
ft
tP
np
p
ft
tR
36
Appl Sci Adv Mater Int, September 2014
References
1. Ramachandran G, Ramakrishnan C & Sasisekharan
V, J Mol Biol, 7 (1963) 95.
2. Sankararamakrishnan R & Vishveshwara S,
Biopolym, 30 (1990) 287.
3. Cordes F, Bright J & Sansom M P, J Mol Biol, 323
(2002) 951.
4. Von Heijne G, J Mol Biol, 218 (1991) 499.
5. Yohannan S, Faham S, Whitelegge J & Bowie J, The
Evolution of Transmembrane Helix Kinks and the
Structural Diversity of G-protein Coupled Receptors,
in Proc. Natl. Acad. Sci. U.S.A. 101, 959-963 (2004).
6. Pal L, Dasgupta B & Chakrabarti P, Bioploym, 78
(2005) 147.
7. Daily A, Greathouse D, van der Wel P & Koeppe R,
Biophys J, 94 (2008) 480.
8. Mishra N, Khamari A, Mohapatra P K, Meher J K &
Raval M K. Support Vector Machine Method to
Predict Kinks in Transmembrane α-Helices (Excel
India Publishers, India), 2010.
9. Mohapatra P K, Khamari A & Raval M K, J Mol
Model, 10 (2004) 393.
10. Hirakawa H, Muta S & Kuhara S, Bioinformatics, 15
(1999) 141.
11. de Trad C, Fang Q & Cosic I, Protein Eng, 15 (2002)
193.
12. Murray K B, Gorse D & Thornton J, J Mol Biol, 316
(2002) 341.
13. Meher J K, Mishra N, Mohapatra K, Raval M K,
Meher P K & Dash G N, Signal Processing
Approach for Prediction Kink in Transmembrane α-
Helices, in proceeding of in the International
Conference on Advances in Information Technology
and Mobile Communication (AIM-2011)-Springer
CCIS, ISBN 978-3-642-20572-9, pp. 170-177, April-
2011. 14. Chen S, Cowan C F N & Grant P M, IEEE Trans
Neural Networks, 2 (1991) 302. 15. Powell M J D, Radial basis functions
formultivariable interpolation: A review. IMA Conference on Algorithms for the Approximationof Functions and Data, RMCS, Shrivenham, Englan, 1985.
16. Lachenbruch P A & Mickey M, Technometrics 10 (1986) 1.
Applied Science and Advanced Materials International Vol. 1 Issue 1 (September – October, 2014)
Author Index
Bandyopadhyay, S 12
Das, B K 28
Das, B 16
Das, H 3
Das, T 28
Das, T 16
Dutta, D 3
Ghosh, S 12
Goswami, T 3
Kalita, D 3
Khamari, A 32
Majumdar, S 12
Meher, J K 32
Mishra, N 32
Panigrahi, M R 32
Parashar, K 16
Parashar, K 28
Parashar, S K S 16
Parashar, S K S 28
Parija, S 21
Raval, M K 32
Sahoo, G C 12
Saikia, P 3
Applied Science and Advanced Materials International Vol. 1 Issue 1 (September – October, 2014)
Keyword Index
Ac conductivity 16, 28
Beam house 12
Coir 3
Compatibiliser 21
Composite 3
Cross-flow membrane filtration 12
E-142 21
Electron microscopy 3
Feature vector 32
Fibers 3
Flux 12
Impedance Spectroscopy 16, 28
Intercalation 21
Kink 32
Modulus of rupture 3
Montmorillonite 21
Nanocomposites 21
Physico-chemical properties 32 Pretreatment 12
RBF 32
Tannery wastewater 12
Transmembrane α-helices 32
Tubular ceramic membrane 12
Turbidity 12
Viscosity 21
XRD 16
Zn 0.99Cu0.01O 16
Zn0.98Nd0.02O 28