Advanced Materials And Engineering Taufiq Yap Yun Hin
Advanced Materials And Engineering Taufiq Yap Yun Hin
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7. Advanced Materials
and Engineering
Selected, peer reviewed papers from the
Annual International Conference on
Intelligent Materials and Nanomaterials
(AIMN 14),
April 18-19, 2014, Seoul, South Korea
Edited by
Taufiq Yap Yun Hin
8. Copyright 2014 Trans Tech Publications Ltd, Switzerland
All rights reserved. No part of the contents of this publication may be reproduced or
transmitted in any form or by any means without the written permission of the
publisher.
Trans Tech Publications Ltd
Churerstrasse 20
CH-8808 Pfaffikon
Switzerland
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Volume 983 of
Advanced Materials Research
ISSN print 1022-6680
ISSN cd 1022-6680
ISSN web 1662-8985
Full text available online at http://www.scientific.net
Distributed worldwide by and in the Americas by
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9. Preface
In order to be organized as a leading annual international conference of
IAMR for researchers, scientists to participate all over the world, Annual
International Conference on Intelligent Materials and Nanomaterials
(AIMN14) is successfully held on April 18-19, 2014 in Seoul, South
Korea.
AIMN14 serves as the important and influential platform for authors to
publish manuscripts in excellent international proceedings and exchange
new ideas face to face. AIMN14 is the unique conference with its strong
organization team, dependable reputation and wide sponsors all around
the world.
All accepted papers of AIMN14 have been strictly selected for the quality
and the relevance to the conference. We sincerely hope that the current
selected papers provide a good overview of the research activities related
to advanced materials and engineering. These new materials includes,
intelligent materials, nanomaterials synthesis and properties, nano devices
and system, nano materials, technologies for applications,
materials/nanufacturing processes, etc.
The volume of AIMN14 is expected to boast future research activities
within the new actions, meetings and conferences and this volume is
provided not only for the readers abroad overview of the latest research
results on material science and related fields, but also for those who wish
to have a valuable summary and reference in these fields.
We would like to express our sincere appreciations to all the authors for
their contributions to this volume. We are indebted to all the referees for
their constructive comments on the papers. Many thanks are also warmly
given to Trans Tech Publications, the distinguished publisher of AIMN14.
All staffs of AIMN14 Organizing Committees from IAMR look forward
to your continuous attention and support to this Annual International
Conference in the future.
AIMN14 Organizing Committees
10. Committees
Honorary Chairs
Prof. Vikas Tomar, Purdue University, USA
Editorial Chairs
Prof. Taufiq Yap Yun Hin, Universiti Pertanian Malaysia
(UPM), Malaysia
PC Co-Chairs
Prof. Elias Saion, Universiti Pertanian Malaysia (UPM),
Malaysia
Prof. Razali Ismail, Universiti Teknologi Malaysia (UTM),
Malaysia
Prof. Jeonghoon Yoo, Yonsei University, South Korea
Prof. Min Chen, Aalborg University, Denmark
Dr. Xufeng Dong, Dalian University of Technology, China
Prof. Mohd Sapuan Salit, Universiti Pertanian Malaysia (UPM),
Malaysia
Prof. Kurapati Srinivas, GMR institute of technology, India
Prof. Jayabalan M, Biomaterials Subject Group of MRSI, India
Prof. Avishai Yshai, Ben-Gurion University of the Negev, Israel
Dr. Othman Inayatullah, Universiti Pertanian Malaysia (UPM),
Malaysia
Steering Committee Chairs
Prof. Choi Changhwan, Hanyang University, South Korea
Prof. Kun Zhao, China University of Petroleum (Beijing)
11. Table of Contents
Preface and Committtess
Chapter 1: Advanced Materials, Technologies and Applications
Gangue as Flame Retardants for Flexible Poly(Vinyl Chloride)
M. Gao, C.G. Song, D. Rong and Y.W. Ji 3
Novel Thermo Thickening Smart Gel with Interpenetrating Polymer and Surfactant
Network
J. Yang, Y.N. Zhou, Y.J. Lu, W.X. Cui, X.H. Qiu, B.S. Guan and Y.H. Ding 7
Smart and Robust Composite Tube Columns Frames for Offshore Sub-Structure
Construction
T.M.B. Albarody, Z.B. Mustaffa and M.S. Liew 11
The Research Process and Application Prospect of the Smart Piezoelectric Materials
X.L. Fang, W.F. Zhang and H.X. Wang 16
Reusable and Efficient Polystryrene-Supported Acidic Ionic Liquid Catalyst for the
Synthesis of n-Butyl Acetate
Y.H. Cheng, B. Zhang, S.J. Dai, H.L. Tong and L.X. Li 20
An Exploration of Factors Affecting the Preparation of SiO2-Coated α-Al2O3 Pearlescent
Pigment
N. Wu, Q.H. Chen, W.M. Zhou, M.Z. Ke, Q.R. Qian and Z.H. Yuan 26
Assessment of Engineering Properties of Geosynthetics with Seaming Methods
H.Y. Jeon 30
Comparative Study of Physico-Chemical Properties of Pure Polyurethane and Polyurethane
Based on Castor Oil
M.A. Alaa, K. Yusoh and S.F. Hasany 39
Temperature Effects and pH Value on Free Swell Behaviors of Bentonite Solutions
H.Y. Jeon 44
The Thermal Properties of Unsaturated Polyester Resin Treated with Intumescent Flame
Retardants
M. Gao, D. Rong, C.G. Song and Y.W. Ji 52
Chapter 2: Nanomaterials and Nanotechnologies
Microstructure of Gold Nano-Crystals from Nanometer to Micrometer Lengthscale in Gold
Bulk Metallic Glass
N. Boonchu, A. Lawan, K. Thipayarat, S. Pintasiri, W. Kanjanakijkasem, S. Kuimalee and B.
Lohwongwatana 59
Nanotechnology and Earth Construction: The Mechanical Properties of Adobe Brick
Stabilized by Laponite Nanoparticles
F. Scalisi 63
On Optimal Planning for DNA Nanomechanical Robots
V. Popov 67
Preparation of Nano Ni2P/TiO2-Al2O3 Catalyst and Catalytic Activity for
Hydrodesulfurization
H. Song, Z.D. Wang, Z.S. Jin, F. Li, H.Y. Wang and H.L. Song 71
Study on the Nanoemulsion Formulation of Piceatannol and In Vitro Release
Y. Zhang, Y.F. Yu, Z.H. Shang, M. Du and C.F. Wang 75
The Green Preparation of Nano-Silver Particle by Reductive Polysaccharide
M.S. Yang, X.P. Wen and L.K. Li 79
Hybrid Microstructures on Si Surface Formed by Nanosecond Pulse Laser for Broadband
Antireflection
L.T. Yang 84
Computer Aided Simulation and Prototype Experiment on Nanocoated Products
J.Z. Li 90
12. b Advanced Materials and Engineering
Influence of Injection Conditions on the Mechanical Property of MWCNTs/ PC
Nanocomposites
L.J. Wang, J.H. Qiu and E. Sakai 94
Nanomechanical Properties of Core-Shell Structured Ni@NiO Nanoparticles Reinforced
Epoxy Nanocomposites
H.Y. Wang, L. Yan, Y.J. Zhu, H. Song and J.H. Zhu 99
Chapter 3: Composites and Alloys
Effect of Injection Conditions on the Electrical Conductivity of MWCNTs/PC Conductive
Composites
L.J. Wang, J.H. Qiu, E. Sakai and X.W. Wei 105
Influence of Casting Method and Heat Treatment for Corrosion Resistance of Magnesium
Alloy AZ91D
A. Dobkowska, B. Adamczyk-Cieślak, J. Zdunek, J. Mizera and K.J. Kurzydlowski 110
Low Temperature Oxidation Behaviors of CNTs/MoSi2 Composites
H. Zhang, H.J. Wu, J. Lin, S.Y. Gu and L. Yu 116
Microsegregation Behavior of Single Crystal Superalloy
Z.H. Yu and J.F. Qiang 121
Modeling the Correlation between Microstructure and Tensile Properties of Ti-17 Alloy
Using Artificial Neural Network
Z.Q. Jia and W.D. Zeng 127
One Step Fabrication of Core-Shell Structures in Immiscible Alloys for Thermal Energy
Storage
F.M. Xu, M.B. Fu, W. Dong, L. Zhao, D. Lu and Y. Tan 131
Surface Modification of Titanium Alloys Using Alumina Particles Blasting for Biomedical
Applications
S. Udomlertpreecha, P. Pavasant and B. Lohwongwatana 135
Technique Research on High Strength Low Alloy Structural Steel Used in Semi-Rigid
Guardrail
H.X. Yu, Z.W. Zhou and H.S. Zhang 141
The Effect of Co/Pd MgO Supported Catalyst Calcination Temperature on the Yield and
Morphology of CNTs via Methane Decomposition
G. Allaedini, S.M. Tasirin, J. Sahari and M.Z. Meor Talib 148
The Structure and Properties of NBR / Recycled Polytetrafluoroethylene (R-PTFE)
Composites
W.W. Chen, C.L. Cao, Y. Zhang, L.R. Xiao, Q.R. Qian and Q.H. Chen 152
Microstructure and Direct Measured Micro-Strain by TEM of Hot Iso-Static Pressed
Alumina-Titanium Carbide (Al2O3-TiC) Composite
S. Thumsoontorn, S. Kuimalee, B. Kuntalue, S. Pintasiri and B. Lohwongwatana 156
Characterization and Parametric Study of Multilayered IPMC Actuator
M.F. Shaari and Z. Samad 161
A Novel Approach for Determining Critical Fracture Strain of a near Alpha Titanium Alloy
during Hot Compression Deformation
W.W. Peng, W.D. Zeng, Q.J. Wang and Y.C. Zhu 166
Thermal Behavior of Epoxy Resins Containing Manganese Compounds
F.C. Wu, S. Tian and S. Liu 171
Thermal Degradation of Hemp Treated with Guanidine Dihydrogen Phosphate
Y.J. Sun, Y.L. Yang and M. Gao 175
Improving Mechanical Properties of Poly-β-Hydroxybutyrate-co-β-Hydroxyvalerate by
Blending with Natural Rubber and Epoxidized Natural Rubber
M. Chutamas, S. Jackapon, J.K. Hyun and S. Klanarong 179
Chapter 4: Manufacturing Processes, Materials Forming and
Machining
13. Advanced Materials Research Vol. 983 c
Application of Calculus Equation in Solving Thermal Decomposition Kinetics Parameters of
Flame Retardant Epoxy Resin
C.Y. Sun, Y.L. Yang and M. Gao 185
Application of Calculus Equation in Solving Thermal Decomposition Kinetics Parameters of
Flame Retardant Wood
C.Y. Sun, Y.L. Yang and M. Gao 190
Dynamic Analysis of Stiffness Part for a Electromagnetic High Frequency Fatigue Testing
Machine
Y. Zheng, Y. Zhang and X.W. Fan 194
New Upgrade Solution to Highway Concrete Barrier
M. Li and H.X. Yu 198
The Research of Demarcating the Laser Ranging Sensor by Least Squares Method
Y. Zheng, Y. Zhang and X.W. Fan 204
A Fundamental Investigation on Ultrasonic Assisted Fixed Abrasive CMP (UF-CMP) of
Silicon Wafer
Y.B. Wu and L.J. Wang 208
Study on Slurry of SiC Crystal Substrate (0001) C Surface in CMP Based on Silica Sol
(SiO2 Abrasive)
Z.Q. Zhang, H.F. Cheng and J.X. Su 214
Thermal Stability of Cotton Cellulose Modified with Calcium Complexes
Y.J. Sun, Y.L. Yang and M. Gao 218
UV-Radiation Curing Process of Cationic Epoxy Adhesive Materials
W.L. Zhang, J.J. Chen, M.L. Tan, B. Li, L.Q. Ye, D.J. Fu, Q. Ma, X.W. Wang and D.S. Li 222
ABAQUS Based on Machining Simulation during Metal Milling
Z. Dan and Z. Yan 226
Chapter 5: Power Systems, Energy and Environmental Engineering
Design Study of Small Gas Cooled Fast Nuclear Power Plant for Synergetic Energy System
with Renewable Energy by Employing Pump Storage
Z. Suud 233
Electrochemical Performance of LiFePO4/C Prepared from Different Carbon Source
A.F. Liu 238
Flow Field Analysis and Response Surface Research on the Rotor in Dry Powder Inhaler
Z.C. Cao, H.Y. Li, S.H. Shi and E.L. Zhou 242
Gas Permeation Properties and Characterization of Polymer Based Carbon Membrane
N. Sazali, W.N.W. Salleh, Z. Harun and A.F. Ismail 246
Measurement Principle of Glass Thermal Expansion Coefficient and Technology
Application of DIL402PC Dilatometer
Y.H. Sun, D.Q. Zhang, F. Wu and K. Sun 251
Methodology of Taguchi Optimization for Organic Rice Bran to Maximum Antioxidant
Activity
T.L. Su, S.W. Wang, H.H. Chien and C.J. Shen 257
Resolving National Energy Crisis through Energy Efficient Appliances: Use of Ground
Water Heat Pump for Air Conditioning Systems
A. Aizaz and N. Hafeez 261
Solar Hydrogen Production Research Status and Prospect
D.Z. Wang, F.Z. Zhao and C.L. Zhu 265
Stability of a Class of Power System with Interval Parameters
D. Xie, Z.H. Lu and W.J. Wang 270
The Design and Implementation of Optimal Scheduling in Hydro-Thermal-Wind System
X.F. Tian 275
The Effect of Air Cold Plasma Treatment on UHMWPE Fiber Surface Modification
X.X. Lin, X. Huang and Y.M. Wang 280
The Effects of the Total Number of Regions and Average Power Density on the Overall
Performance of Modified CANDLE Burn-Up Scheme Based Gas Cooled Fast Reactors
I. Rosidah, M. Afifah, Z. Suud, H. Sekimoto and A. Ferhat 284
14. d Advanced Materials and Engineering
The Research of Marine Nuclear Power Two Loop Simulation Software Based on the
Thermal System Analysis
G.L. Zhang, X.D. Jin, Z. Zhao and Z.J. Shi 288
Transformer Impedance Determination for Power System Studies of Distribution Network
integrated with Renewable Energy Resources
J.H. Tang, M.Z. Che Wanik, A.M. Busrah and A.K.M. Hussin 292
Translational-Rotational Motion of Earth Artificial Satellite (EAS) in Hill's Gravity Field
K. Astemessova, A. Bekov, M. Shinibaev and D. Ussipbekova 300
A Proposed Method of Photovoltaic Solar Array Configuration under Different Partial
Shadow Conditions
A.M. Humada, M. Hojabri, M.B. Mohamed, M.H. Bin Sulaiman and T.H. Dakheel 307
The Development of New Steel Backing Wood Landscape Guardrail
Z.W. Zhou, C.H. Wang and M. Li 312
The Elimination of Pollution of Toxic Cadmium and Arsenic in Lead-Based Alloys of Lead-
Acid Batteries in China
X. Liu, J.C. Cai and Y.H. Shu 319
Thermal Stability and Smoke Suspension of Cotton Cellulose Modified with Magnesium
Complexes
F.C. Wu, C.Y. Chao and S. Tian 324
Phonon Interaction of Ultrasound Waves in Condensed Media
S. Omarov, T. Begimov, M. Tukibayeva, K. Maylina and G. Bedelbaeva 328
Research on Internal Flow Field of Control Valve Outlet Blockage Fault
Y.T. An, R.J. Ma and D. Zhao 338
Migration Study of Biodegradable Blends of Polylactic Acid and Epoxidized Natural
Rubber
T. Nampitch 342
Numerical Simulation of NOx Emission in Supercharged Boiler
H.Y. Zhang, J. Zhao, L.B. Yang and Y.J. Li 347
Conceptual Design Study of Small 400 MWt Pb-Bi Cooled Modified Candle Burn-Up Based
Long Life Fast Reactors
Z. Suud and H. Sekimoto 353
Chapter 6: Applied Mechanics and Engineering
Based on RFID Prefabricated Building Component Design and Monitoring System
Research
J. Wang 359
Design Optimization and Control Analysis of Mechanical Arm Equipped on Wheelchair
G.B. Luo, C.C. Zeng and L.D. Zhu 363
In 16V265H Locomotive Diesel Engine Nozzle Flow Field Simulation Analysis
S.H. Li, M.H. Li and X. Du 368
Mechanical Design to Adapt Changes to Existing Universal Test Bed Facility of Turbojet
Engine for the Turbofan Engine
F. Ahmed, A. Aizaz and Z. Mahmood 374
Simulation Analysis of Kinematics and Dynamics of 3-TPS Hybrid Robot
J.S. Shi, S. Wang, L.D. Zhu, W.S. Wang and T.B. Yu 379
The Experiment Research on Storage Characteristic of PCM Storage Device by Spheres
Piled Encapsulated for Vehicle Waste Heat
T.S. Zhang, Q.Y. Wang, G.H. Wang, C. Gao and Q. Gao 383
The Phase Shift of Reflection and Refraction of SH-Wave at an Interface of Two Media
A.L. Wang and F.P. Liu 388
The Research on Fault Diagnosis of Civil Aircraft Information Fusion Based on the
Evidence Theory
X. Peng 392
A Characteristic Seismic Study and Development of Earthquake Resistant Techniques in
Existing Structures
M. Yasuhide and H. Yashwanth 396
15. Advanced Materials Research Vol. 983 e
Shock Response Analysis of Marine Gearbox
W. Liu, T.J. Lin and Z.Y. He 400
Design on the Detection System of Stud Welding Dynamic Parameters
B. Wang, X.X. Li and W.M. Zhang 404
Influence of Lateral Shift on Normal Moveout of SH-Wave
A.L. Wang and F.P. Liu 408
Mixed Interface Stress Element-Finite Element Model with its Application
Y.H. Sun, F. Wu, K. Sun and D.D. Li 412
Modeling of Mass-Spring-Damper System by Complex Stiffness Method
S.G. Zhang and X.P. Dang 420
Study on Control Quality of Valve Outlet Blockage Fault
Y.T. An, R.J. Ma and D. Zhao 424
Development of Digital Filter Software in Auto Safety Components Test
C.J. Du, T.Q. Du and W. Liu 428
A New Type of Adjusting Coaxiality Structure Design
B.R. Sun, Y. Zheng, Y. Zhang and X.W. Fan 436
Design of a PLC-Based Engineering Training Unit
J.B. Han 440
Flexible Thermosetting Pipe
Z.B. Mustaffa and T.M.B. Albarody 444
18. tested according to GB/T 1040.2-2006 standard with a LJ-5000 tensile testing machine (Chengde
Experimental Factory).
Preparation of Flame Retardant PVC Samples
Formulation according to predetermined material (including PVC, three salts, salts of stearic
acid, DOP, hydroxide, chloride, coal) are mixed in a mixer 3 to 5 minutes at 35 - 45 °C. Then the
mixture was plastified on the two-roll mill at 165°C for 6-8 min, compressed at 180°C to form
sheets of 100mm×10mm×3mm. The test specimens were cut from the molded sheets.
Table 1 The composition of the samples
Sample
PVC
(g)
DOP
(g)
Tribasic
lead
sulfate
(g)
Dibasic
lead
phosphate
(g)
Stearic
acid
(g)
Al(OH)3
(g)
Gangue
(g)
Oxygen
index
(%)
A 500.0 150.0 7.5 7.5 5.0 0.0 0.0 24.5
B 500.0 150.0 7.5 7.5 5.0 5 0.0 0.0 26.6
C 500.0 150.0 7.5 7.5 5.0 75.0 0.0 28.4
D 500.0 150.0 7.5 7.5 5.0 100.0 0.0 29.5
E 500.0 150.0 7.5 7.5 5.0 125.0 0.0 29.4
F 500.0 150.0 7.5 7.5 5.0 125.0 5.0 29.7
G 500.0 150.0 7.5 7.5 5.0 125.0 10.0 29.8
H 500.0 150.0 7.5 7.5 5.0 125.0 15.0 29.2
I 500.0 150.0 7.5 7.5 5.0 125.0 20.0 27.9
RESULTS AND DISCUSSION
Flame retardancy of Al(OH)3 and gangue
Al(OH)3 as one halogen-free, flame-retardant additives, inorganic acid, used in plastics and
rubber industry, attracted widespread attention. From the oxygen index values in Table 1, the
flexible PVC added Al(OH)3 has good flame retardancy, whose LOI increase from 24.5% to 29.4%.
The flame-retardant effect of Al(OH)3 in soft PVC is mainly based on their dehydration
endothermic effect, thus inhibiting soft PVC temperature from rising. When addition of Al(OH)3
reaches 100g, the best effect is obtained.
To get better flame retardancy for PVC, gangue was added. The data were shown in Table 1,
LOI of samples (F,G) increase with the addition of gangue. When more gangue was added, the LOI
of samples decrease, 10g gangue is optimal. Gangue and Al (OH) 3 can be a good flame retardant
for flexible PVC.
Effect of Al(OH)3 and gangue on the Mechanical Properties
Mechanical properties such as tensile strength, breaking strain, yield stress and tensile modulus
of samples were measured, and shown in Figs.1-4.
Fig.1 shows the effect of the gangue on tensile strain of samples (TS), which shows that the TS
increase when the added gangue’s weight is less than 5g, when it is more than 5g and less than 10g,
the TS decrease. When it is more than 10g and less than 15g, the TS second increase but slowly,
while more than 15g, the TS decrease.
Fig.2 shows the effect of the gangue on breaking strain of samples (BS). We can see that the BS
increase when the added gangue’s weight is less than 7g, the BS start decreasing when the weight is
more than 7g. Obviously, the highest value of BS is obtained when the gangue’s weight is 7g.
4 Advanced Materials and Engineering
19. 0 5 10 15 20
20
22
24
26
Tensile
strength
/
MPa
Gangue / g
0 5 10 15 20
300
400
500
600
Breaking
strain
/
%
Gangue / g
Fig.1 Tensile strength of samples Fig.2 Breaking strain of samples
0 5 10 15 20
4.5
5.0
5.5
6.0
Yield
stress
/
MPa
Gangue / g
0 5 10 15 20
80
120
160
200
Tensile
modulus
/
MPa
Gangue / g
Fig.3 Yield stress of samples Fig.4 Tensile modulus of samples
Fig.3 shows the effect of the gangue on yield stress of samples (YS). When the added gangue’s
weight is less than 5g, the YS keep increasing, then the YS decreases, sometimes it also has slightly
increase, when the gangue’s weight is 5g, the YS has its highest value.
Fig.4 shows the effect of the gangue on tensile modulus of samples (TM). The TM constantly
increases. However, the TM is much greater in the range of 5-10g of gangue.
Similar to other additives, the gangue can reduce some mechanical properties. This is because
the interactions among the polymer molecules were decreased and the movement of the polymer
chains was limited when the flame-retardants reached at 15g.
Analysis of Char Yield
Fig.5, 6 present the SEM photographs of the surface of char of the samples (sample A, sample
G). From Figure 5, it can be observed that the char is very slight, loose and soft, which could not
protect the underlying material from fire. Contrarily, Figure 6 shows that the char is compact, tough
and hard though there are some holes on the surface. It is possible that the gangue could promote
the formation of effective charring layer. The structure of the intumescent charring layer may
increase the efficiency of the flame retardancy, act as heat insulation, and protect inner matrix
materials.
Advanced Materials Research Vol. 983 5
20. Fig.5 SEM photographs of sample A Fig.6 SEM photographs of sample G
Conclusions
10g gangue and 100g Al (OH) 3 were added can obtain a good flame retardant for flexible PVC,
whose LOI reached 29.8%. Gangue has little effect on the mechanical properties of the sample,
especially tensile strength, yield stress. The flame-retardant effect of Al(OH)3 in soft PVC is mainly
based on their dehydration endothermic effect, thus inhibiting soft PVC temperature from rising.
Gangue could promote the formation of effective charring layer. The structure of the intumescent
charring layer may increase the efficiency of the flame retardancy, act as heat insulation, and
protect inner matrix materials.
1
Contract grant sponsor: Fundamental research funds for the Central Universities: 3142013102.
References
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Smoke Suppression in Polymers Filled with Magnesium Hydroxide, Polymer Degradation and
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[5] Jha, N.K., Misra, A.C. and Bajaj, P. (1984). Flame-Retardant Additives for Polypropylene, J.
Macromol Sci., Rev. Macromol. Chem. Phys., C24: 1: 69.
[6] Pearce, E.M. (1986). Flame Retardants for Polymer Systems, Pure & Appl. Chem., 58: 925.
[7] Shigco, M., Takeshi, I. and Hitoshi, A. (1980). Fire-Retarding Polypropylene with Magnesium
Hydroxide, J. Appl. Polym. Sci., 25: 415.
6 Advanced Materials and Engineering
22. Experiment
Materials
Amphoteric surfactant with C18 chain length and hydrophobically modified polyacrylamide
polymer with anionic group (AP) were made by our lab. Anionic surfactant, sodium lauryl sulfate,
was received from Sinopharm Chemcial Co, China. Conventional polyacrylamide with anionic
group (CP) was obtained from Beijing Henju Co. Water was deionized.
Methods
Rheological properties were measured by a Haake Mars II Rheometer Pressured Cell. Dynamic
properties were measured by cone and plate geometry on rheometer.
Cryo-transimission electron microscopy (Cryo-TEM) observation of surfactant solution was
carried out in a controlled-environment vitrification system. Samples were prepared at 25 °C and
100% RH on a Quantifoil holey carbon grid (Electron Microscopy Sciences). The grid was
quenched rapidly in liquid ethane at -180 °C and then transferred to liquid nitrogen (-196 °C) for
storage. Imageing of the samples was performed using JEM2010 cryo-microscope with a Gatan 626
cryoholder. The acceleration voltage was 200 keV, and the working temperature was kept below -
170 °C. Digital images were recorded using a charge-coupled device camera (Gatan 832).
Results and Discussions
The surfactant studied is a mixture of amphoteric and anionic surfactant (MS) similar to system
studied previously [6]. The surfactant system showed viscoelastic behavior itself above certain
concentration which forms entangled wormlike micelle structure. The viscosity of surfactant and
polymer with variation of temperature is shown in Fig. 1. It can be seen that viscosity of fluid with
single surfactant or polymer all decreases as temperature increases. The viscosity in mixture of
conventional polymer (CP) and surfactant (MS) also decreases with increasing temperature.
However, the viscosity in mixture of hydrophobically modified polymer (AP) and surfactant (MS)
increases with increasing temperature. The overall concentration of mixed AP and MS is also
higher than their individual combined. Hence, there is positive synergism interaction between these
two materials at increasing temperature. It can be seen that viscosity starts to increase above 50 °C.
This behavior could be due to the increase of solubility of longer chain surfactant at higher
temperature. The complex fluid formed between associating polymer (AP) and surfactant (MS) is a
highly elastic gel as shown in Table 1, which the storage modulus, G’, is larger than loss modulus,
G’’ at frequency 0.1-100 rad/s.
At further higher temperature above 80 °C, formation of branches along the micelles leading to a
multionconnected rather than an entangled network. Branch junction points increase the number of
possible configurations, enabling percolation, and the formation of extended micellar networks,
which leads to a multiconnected rather than an entangled network of cylindrical micelles. Hence the
visocosity decreases for branched worm-like micelles.
The driving force for this increased viscosity in mixed polymer and surfactant system is due to
physical crosslinking of polymer and surfactant through intermolecular val der vaal interaction of
hydrophobic side chain in associating polymer and surfactant micelle. In addition, hydrogen
bonding between the polymer hydrophilic and surfactant head group could also reinforce their
interaction and crosslinking. The interpenetrating network of wormlike micelle from surfactant and
hydrophobic modified polymer is graphically shown in Fig. 2a.
8 Advanced Materials and Engineering
23. 0
20
40
60
80
100
20 30 40 50 60 70 80 90
Temperature (C)
Viscosity
(mPa.s,
100
1/s)
1% MS Surfactant
0.15% AP Polymer
1% MS+0.15%AP
0.15% CP Polymer
1% MS+0.15% CP
Figure 1. Viscosity versus temperature for polymer, surfactant and their mixture.
Table 1. Storage modulus (G’) and loss modulus (G’’) versus angular frequency for 1% mixed
surfactant (MS) and 0.15% associating polymer (AP) at 70 °C.
Augular
Frequency [rad/s]
0.10 0.40 1.58 6.31 25.10 100.00
G’ [Pa] 5.45 6.36 7.78 9.37 11.20 11.90
G’’ [Pa] 1.37 1.48 1.69 2.10 2.80 4.16
The presence of wormlike micelle structure in surfactant studied is directly confirmed by Cyro-
TEM observation as shown in Fig. 2b. It can be seen that threadlike structure with about 10nm in
diameter and >1 µm in length exists. The wormlike micelles entangle with each other as well as
polymer gives highly elastic gel.
(a) (b)
Figure 2. (a) Illustrated crosslink model of wormlike micelle and associating polymer. (b) Cryo-
TEM micrographs of wormlike micelle in mixed ampheteric and anionic surfactant (1%, wt) at 25
°C.
Advanced Materials Research Vol. 983 9
24. Conclusions
A novel smart gel based on interpenetrating network of anionic polymer and surfactants was
formed through physical crosslink. The val der vaal and hydrogen bonding interaction between
wormlike micelle and polymer network gives strong viscoelastic gel. The gel strength is stronger at
evaluated temperature. The smart gel is useful as stimulation fluids in oil and gas industry,
hydraulic fluid, household and personal care products.
Acknowledgement
The authors acknowledgement the supports from the National Hi-Tech Development (863) Plan
Project (2013AA064801) and National Natural Science Foundation of China (Grant No 51174163).
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1124-1129.
[7] Y. Zhang, Y. Han, Z. Chu, S. He, J. Zhang, Y. Feng, Thermally induced structural transitions
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(2013) 319–328.
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properties, Oilfield Chemistry, 20(2003)291-294.
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transport in hydraulic fracturing fluids, SPE International Symposium on Oilfield Chemistry, SPE-
164072, 8-10 April, The Woodlands, Texas, 2013.
10 Advanced Materials and Engineering
26. Therefore, a Nano-Hyprid-functionally graded composite (NHFG) proposed to increase the
integration between the layers and grading the structural properties across tube thickness using
magnetic nanoparticles as fillers. Furthermore, such functional composites could utilize the
magnetostrictive properties to actuate the vibration inside the composite tubes. Several models
have been found in the literature dealt with functional composite [5, 6]. Some of them could
specialize to demonstrate the vibrational behavior of multilayered and functionally graded
magnetostrictive composite. Albarody, et.al., [5] derived the exact solution for linearly constitutive
properties, simply supported, functional composite shell subjected to static and dynamic loadings.
The authors were investigated and analyzed the effects of the material properties, lay-ups of the
constituent layers, and shell parameters under the free vibration behavior.
In this paper, a STEC columns filled with magnetic nanoparticles is modeled and the vibrational
characteristic is discussed. Also, some of NHFG composite are examined.
Theoretical Formulation
Based on Hamilton's variational principle linked with Gibbs free energy functions, the steel tube-
encased composite model is casted according to the first-order shear deformation shell theory. The
exact solution is derived for linearly magnetostrictive constitutive properties, simply supported, and
thick shell having rectangular plane-form. Expressed in the (meter–kilogram–second) system of
units, the generation procedure of thick composite shell model, written in curvilinear coordinates
and provides the much-needed materials in state of the smart or adaptive materials are as follows;
1. Constitutive Relations: In a system gather mechanical, magnetic, and thermal influences, the
constitutive relations are expressed formally as:
S = ς ,
ε – κ χ – λ τ , (1)
2. Kinematic Relations: According to the FOSD shell theory, the following representation of the
3D displacement and magnetic potentials is postulated:
u(α, β, ζ, t) = u (α, β, t) + ζψ (α, β, t), v(α, β, ζ, t) = v (α, β, t) + ζψ (α, β, t),
w(α, β, ζ, t) = w (α, β, t), and ϑ(α, β, ζ, t) = − ϑ (α, β, t) + ζϑ (α, β, t) , (2)
where uo, vo, and wo are referred to as the mid-surface displacement functions, and ψα and ψβ are
the midsurface rotation functions of the shell, and ϑ is the magnetic potential function. The strains at
any point in the shell can be written in terms of mid-surface strains and curvature changes as:
ε = (ε + ζε ), ε = ε + ζε , ε = ε + ζ ψ R
⁄ ,
ε = ε + ζε , ε = ε + ζε , ε = ε + ζ ψ R
⁄ .
(3)
However, the mid-surface strains as well as the curvature and twist changes are extended by
Codazzi-Gauss geometric relations, as [6]. The distributions of magnetic fields at any point in the
composite shell are assumed as:
χ = (χ + ζχ ), χ = χ + ζχ . (4)
and the magnetic field changes are
χ = − , χ = − , χ = − , χ = − . (5)
3. Kinetic Relations: The elastic, electric, and magnetic force and moment resultants are obtained
by integrating the constitutive relations (1) over the shell thickness as below:
12 Advanced Materials and Engineering
27. N , M = (1, ζ) S γ dζ + N , M , (6)
where γ = (1 + ζ R
⁄ ), the subscripts n denote either of α, β or αβ, and h is the shell thickness.
In order to gain a numerical stability and pursue a possible integration of Eq. (6) in absence of
thermal forces, the term (1 + ζ R
⁄ ) should be expanded in a geometric series as in [7, 8].
4. Variational Principle: The variational energy method via the Hamiltonian axiom has been used
by [9, 10] for coupling of the energy phenomena and to derive a consistent set of equations of
motion coupled with the free charge equation. In summary, the total energy of a shell element can
be defined as:
δ (K − P) dt = 0, (7)
where P is the total potential energy induced in the system given by:
P = ∭ ς ,
ε – κ χ – λ τ dV − ∬ t S , G , + W S , G , , (8)
where Q(S , G , T) is the thermodynamic potential. t S , G , and W(S , G ) are the tractions and
the work done by body force, and magnetic charge, respectively. The kinetic energy is given as:
K = ∬ (u + v + w ) + ζ ψ + ψ + 2ζ u ψ + v ψ
−
γ γ ABdζdA. (9)
The traction is
t(S , G ) = S δu + S δv + S δw + G δϑ + G δϑ (10)
and the external work is
W(S , G ) = F u + F v + F w + C ψ + C ψ − F ϑ + C ϑ , (11)
where F , F , and F are the distributed forces in α, β and ζ directions, respectively, while
C and C are the distributed couples about the middle surface of the shell. F and C are the
distributed forces and couples due to the magnetic charge. Hence, the temperature, τ is a known
function of position and enter the formulation only through the constitutive equations. Substituting
Eqs. (1, 10, and 11) into Eq. (8) and equating the resulting equation with Eq. (9), yields after
expanding the terms:
δ ∬
̅
(u + v + w ) +
̅
ψ + ψ
+I̅ u ψ + v ψ
ABdAdt– ∭ (ς ε − κ χ − λ τδε) dVdt
+ ∬ S δu + S δv + S δw + G δϑ + G δϑ ABdAdt
+ ∬ F u + F v + F w + C ψ + C ψ − F ϑ − C ϑ ABdAdt = 0. (12)
Replacing the constitutive terms in Eq. (12) by the kinetic relations (6), then integrating the
displacement gradients by parts to obtain only the virtual displacements, we can set the coefficients
of δuo, δvo, δwo, δψα, δψβ, δϑ0 and δϑ1 to zero, individually. The equations of motion and the
charge equilibrium equation for isothermal case are
BN + AN + N – N + Q + Q + ABF = AB I̅ + I̅ ,
Advanced Materials Research Vol. 983 13
28. AN + BN + N – N + Q + Q + ABF = AB I̅ + I̅ ,
– AB + + + BQ + AQ + ABF = AB I̅ ,
BM + AM + M – M – ABQ + P + ABC = AB I̅ + I̅
AM + BM + M – M – ABQ + P + ABC = AB I̅ + I̅ .
(13)
here I̅ , I̅ , and I̅ are the inertia terms defined as:
I̅ = I + I
R + R
R R
+
I
R R
, ,
, I , I , I , I , I
= I (1, ζ, ζ , ζ , ζ , ζ )dζ,
where Ik
is the mass density of the kth
layer of the shell per unit mid-surface area. Eqs. (13) can
be written in a matrix form as K + ∂ ∂t
⁄ M ∆ = F − F , where K and M are stiffness
and mass matrices, respectively, and F is the thermal forces. Thus, the forced method will apply
satisfying SS boundary conditions and admit specially-orthotropic rectangular laminates, to
determine the governing equations that satisfied everywhere in the domain of the shell.
Thus far, the accurate treatment of thermal, magnetic and elastic energies that are taken into
account in this smart composite shell that encased a steel tube column, expect yields rather
sophisticated equations interlink the magnetic inductions and stress resultants.
Parametric Analysis
As deepwater structures for the future developments are expected to be floating structures.
Structural systems that can adapt to the environment automatically offer new vistas for designers
and lead to novel efficient developments. An offshore structure that form from the proposed steel
tube-encased composite is defined smart due to the actuation capability of the magnetostrictive
materials that integrated into structural.
The challenging part of the offshore structural adaption is that the structure is subjected to highly
uncertain environmental forces. Thus, the effects of the material properties, and lay-ups of the
constituent layers of the encased composite and the steel tube parameters on the vibration behavior
are required to be dissected. In Fig. 1, a CoFe2O4 Nano particle material is scrutinized and the
mechanical properties of the encased shell are found to be varied in a very orderly manner across
the tube thickness. The STEC tubes that encased with shell made of composite filled with CoFe2O4
appear with higher stiffness as compared to traditional steel tube and exhibit possible actuations
when a magnetic field propagate along the tube.
14 Advanced Materials and Engineering
29. Fig 1. The transvers stresses and magnetic induction across the composite tube thickness, at unity load.
GRFE properties are (E1/ E2=15, G12/ E2=0.5, G13/ E2=0.5, υ12=0.3, a/b=1, a/h=10, and the lamination scheme
is (0/09)S), while CoFe2O4 properties and the grading material properties model can be found in [5].
Conclusions
The evolutionary process of development of adaptive steel tube-encased composite for tubular
constructions has opened up new vistas for the several interdisciplinary applications. The benefits of
these composite tubes are expected to be enormous. The concept of a structure with capability of
automatically responding to the environment by change in the self-configuration, or by changing the
interface with the environment is one which offers the potential of extremely attractive advantages
in the design, development and operation of offshore structures. The STEC columns comprising
magnetostrictive materials have been modeled and scrutinized. The present model may serve as a
reference in developing a prototype of STEC columns for further experimentations.
Acknowledgment
Authors would like to acknowledge Universiti Teknologi PETRONAS for sponsoring this work.
References
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-1.4 -1.2 -1 -0.8 -0.6 -0.4 -0.2 0
x 10
-7
-0.15
-0.1
-0.05
0
0.05
0.1
0.15
0.2
Thickness
of
Shell
in
(mm)
Magnetic Induction
-200 0 200 400 600 800 1000 1200
-0.4
-0.3
-0.2
-0.1
0
0.1
0.2
0.3
0.4
0.5
Thickness
of
Shell
in
(mm)
Transvers Stress Mpa
GRFE NHFC
Steel Tube
Advanced Materials Research Vol. 983 15
31. 2. Working principle of the smart piezoelectric materials
The working principle of the smart piezoelectric materials is based on piezoelectric effect. The
piezoelectric effect is that when there is a deformation of the materials by external forces, positive
and negative electric charges will arise in the relative two surfaces of the material due to an internal
polarization at the same time. There are direct piezoelectric effect when mechanical energy is
transformed into electrical energy and inverse piezoelectric effect electrical energy is transformed
into mechanical energy [3, 5].
3. New preparation technology of the smart piezoelectric materials
3.1 The piezoelectric coatings prepared by plasma spraying method
W Haessler et al. investigated the structure and piezoelectric properties of the PZT coatings
prepared by plasma spraying method. They found out that the heat treatment and polarization
process after spraying have a significant effect on the piezoelectric properties of the PZT coatings
[9].
Songlin Gu, Guolu Li et al. fabricated PZT coatings on the surface of 45 steel by supersonic
plasma spraying method. The research results showed that the PZT coatings with a typical layered
structure had dense microstructure, of which the surface was flat and the air hole rate was 1.6%.
The PZT coating was well bonded to the substrate, which met the requirement of application at
actual work [10].
3.2 Piezoelectric ceramic materials prepared by sol-gel method
Piezoelectric ceramic materials fabricated by sol-gel method have high purity, well-distributed
chemical constituents and low temperature of reaction compared with these prepared by the
traditional solid state reaction.
Minglei Zhao et al. prepared Na0.5Bi0.5TiO3 ceramic by sol-gel method. The piezoelectric
constant d33=173×10-12
pC/N increased by 40% compared with that fabricated by traditional method.
Meanwhile the piezoelectric ceramic in this study had small coercive field and large residual
polarization [11].
Y. D. Hou et al. investigated the fabrication of (Na0.8K0.2)0.5Bi0.5TiO3 (NKBT) prepared by
sol-gel –hydrothermal method and its densification. The analysis of the morphology and structure
showed that NKBT nanowire with pure perovskite structure could be prepared by
sol-gel-hydrothermal method with the synthetic temperature of 160 ºC, of which the diameter was
50-80nm, and the length was 1.5-2.0µm. The theoretical density of the flake made of NKBT
nanowire was more than 98% [12].
3.3 Fabrication of piezoelectric composites
Lei Dai, Shan Hu et al. prepared PZN-PZT/PVDF piezoelectric composite material by solid
phase sintering combined with solution blending method, and investigated the properties of the
materials. The results revealed that the generation of pyrochlore phase could be restrained by
appropriately excessive Pb, but too much Pb would reduce the degree of crystallization of the main
crystal phase and the piezoelectric properties of the piezoelectric composite material [13].
4. Application prospect of the smart piezoelectric materials
4.1 Application in structural health monitoring
Due to chemical corrosion, stress effect, tiny impact and influence and other factors, local
damage and micro-cracks may appear on the surface of the structure of large aircraft, nuclear
Advanced Materials Research Vol. 983 17
32. reactors, bridges, and large pipes. On the structure of local damage, especially micro - cracks on the
surface of monitoring it is a very important part of structural health monitoring system to monitor
the local damage and micro-cracks on the surface of the vital structure [14].
A damage detection method based on an innovative 2D phased sensor array made of
piezoelectric paint is proposed for in situ damage detection of a thin isotropic panel using guided
Lamb waves. In this study, a 2D phased sensor array with a spiral configuration is fabricated using
a piezoelectric composite patch and used for detecting damages in an aluminum panel. Steered
array responses are generated from the raw sensor signals using a directional filtering algorithm
based on phased array signal processing. To enhance the proposed analysis technique, empirical
mode decomposition (EMD) and a Hilbert–Huang transform (HHT) are applied. A new damage
detection algorithm including threshold setting and damage index (DI) calculation is developed and
implemented for detecting damages in the form of holes and a simulated crack. The characteristic
damage indices consistently increase as damage size grows [15].
4.2 Application in energy converter
In order to optimize the deformation and brittleness of the piezoelectric materials, the Langley
research center of the NASA fabricated a new kind of smart piezoelectric macro fiber composite
(MFC). Tungpimoluryt K, Hatti N et.al designed an energy collection device based on MFC
materials. The main structure of the device is cantilever structure with the MFC fixed on the surface
of the cantilever. When sinusoidal excitation is applied, capacitor of the energy collection device is
used to collect the electric current generated by MFC, so that the function of collecting energy is
fulfilled. The study results showed that this device can produce up to 45. 6v voltage [16].
4.3 Application in adaptive wing
Based on the inverse piezoelectric effect, Paradies et al. designed and made an active control
wing model of which the wingspan was 500mm.The key parts of the model were seven set of MFC
modules. The wings would be controlled to auto-deform while the MFC parts were applied with
voltage. The study results showed that the deformation value of the wing end was 4.3mm when the
voltage applied was 1.5kV [17].
5. Research prospect of the smart piezoelectric materials
In this paper, new fabrication methods and application of the smart piezoelectric materials are
introduced. Although the smart piezoelectric materials have been used in many fields owing to the
big driving force and fast response speed, it should be noted that the effects to decrease the
brittleness and improve the deformation degree of the smart piezoelectric materials are still needed.
The key focus of the study of smart piezoelectric materials are to compound the structures and
increase the serviceability. As the synthesis and integration of various materials and high
technology, the research of smart piezoelectric materials is bound to have a good and broad
prospects.
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Advanced Materials Research Vol. 983 19
35. added in anhydrous toluene and reacted at 75 ℃ for 14h. Then product named as the
PS-[SO3H-PMIM] was filtered off, washed with toluene and dried under vacuum. Last, dried
PS-[SO3H-PMIM] was soaked in dichloromethane at 0 ℃, and acidified with equiv concentrated
sulfuric acid or hydrochloric acid. The mixture were heated to 75 ℃ for 4h under stirring. The target
catalyst PS-[SO3H-PMIM][HSO4] or PS-[SO3H-PMIM][Cl] were collected by filtration, washed
with diethyl ether and dried under vacuum.
Scheme 1 Synthesis of PS-[SO3H-PMIM][HSO4] catalyst
Catalyst characterizations. IR spectroscopy was recorded using a Nicolet IS10 FTIR spectrometer.
TG/DSC studies were carried out using METTLER TOLEDO SDTA851e/DSC823e instrument.
Elemental analysis was determined by Vario MICRO EL. Average particle sizes and surface
morphologies were characterized by a SEM Leica S440i. GC spectra were recorded using Agilent
GC-6820 spectrometer. Acidic sites was confirmed by titration of PS-[SO3H-PMIM][HSO4] catalyst
with 2.08×10-2
M aq. NaOH, using phenolphthalein as indicator.
Catalyst for aromatics esterification reactions. PS-[SO3H-PMIM][HSO4] (0.95g), n-butyl alcohol
(96mmol), acetic acid (80mmol) and cyclohexane (8mL) were charged successively into a three-neck
flack with a water segregator, and stirred at 92℃ for length of time. The resultant mixture was cooled.
The catalyst was filtered off, washed with ethanol, and dried for the recycling experiments. The filtrate
was analyzed using GC.
Results and discussion
FT-IR. As shown in Fig.1, for PS-CH2Cl, the characteristic peaks of polystyrene exhibited the C–H
stretching vibration of aromatic ring at 3016 cm−1
, and C–H asymmetric and symmetric stretching
vibrations of methylene at 2920 cm−1
and 2855 cm−1
. The peaks at 1609 cm−1
and 1507 cm−1
were due
to the C–C skeleton vibration of aromatic ring of polystyrene. Moreover, a typical peak at 1265 cm−1
was attributed to stretching vibrations of the functional group –CH2Cl, and another peak at 672cm-1
was due to stretching vibrations of C-Cl[15]. The two typical peaks were practically omitted after
introduction of imidazole. Meanwhile, a peak assigned to the C=N stretching vibration of imidazole
ring at 1560 cm−1
appeared[16], which was indicated the imidazole anchored on the polystyrene by
covalent bond. In the IR spectrum of PS-[SO3-PMIM], several strong peaks, i.e. 1039 cm-1
, 1160 cm-1
and 1209 cm-1
, appeared which were attributed to the absorb of –SO3
-
. When PS-[SO3-PMIM] was
acidified with concentrated sulfuric acid, there were no obvious change in IR spectrum but two peaks,
1039 cm-1
and 1209 cm-1
became stronger, which were attributed to the S=O asymmetric and
symmetric stretching vibrations of –SO3– group.
Advanced Materials Research Vol. 983 21
36. Fig. 1 IR-spectra of PS-CH2Cl, PS-CH2-imidazole, PS-[SO3-PMIM] and PS-[SO3H-PMIM][HSO4].
Elements analysis of PS-CH2-imidazole and acidic sites of PS-[SO3H-PMIM][HSO4]. Table 1
showed the elemental analysis for PS-CH2-imidazole. It can be seen that the imidazole contents
increased with the increasing of VBC in feed composition of PS-CH2Cl. Acid sites of the
PS-[SO3H-PMIM][HSO4] catalyst was confirmed by acid base titration. The loading amounts of
[SO3H-PMIM][HSO4] in PS-[SO3H-PMIM][HSO4]1 and PS-[SO3H-PMIM][HSO4]2,
PS-[SO3H-PMIM][HSO4]3 were 2.22, 2.03 and 1.69mmol/g respectively.
Table 1 Elemental analysis of PS-CH2-imidazole
Sample VBC:St:DVB, vol% % C % H % N Imidazole, mmol/g
PS-CH2-imidazole1 98:0:2 73.88 6.84 12.77 4.56
PS-CH2-imidazole2 74:24:2 74.11 6.88 11.58 4.14
PS-CH2-imidazole3 49:49:2 77.50 7.09 9.24 3.30
“VBC:St:DVB, vol%”was the feed composition of PS-CH2Cl beads. “VBC, St and DVB” are the abbreviation of
“4-vinylbenzyl chloride, styrene and divinyl benzene” respectively.
SEM/TEM and TG-DSC. It can be seen that PS-CH2Cl (Fig. 2 A and C) was uniform globular in the
size of ~600 nm. After the introduction of [SO3H-PMIM][HSO4], the catalyst became big a little,
about ~700nm and the surface became smooth (Fig. 2 B and D), which is in accord with other report
[10].
Fig. 2 SEM and TEM of PS-CH2Cl (A and C)
and PS-[SO3H-PMIM][HSO4] (B and D).
Fig. 3 TG/DSC curves of PS-CH2Cl and
PS-[SO3H-PMIM][HSO4] catalyst.
TG/DSC analysis was carried out in N2 with heating rate of 10 ℃/min. As shown in Fig. 3, no
significant weight loss was observed from both PS-CH2Cl and PS-[SO3H-PMIM][HSO4] at
beginning. Above 120℃, weight loss was accelerated for both the two particles and weight loss speed
of PS-CH2Cl was quicker than that of PS-[SO3H-PMIM][HSO4]. There was a obvious weight loss
22 Advanced Materials and Engineering
37. from PS-CH2Cl nearby 150 ℃. Correspondingly, for the DSC curve of PS-CH2Cl, a small exothermic
peak appeared, however it didn’t appear in the DSC curve of PS-[SO3H-PMIM][HSO4]. The weight
loss and the exothermic peak of PS-CH2Cl were possibly ascribed to the water inside the porous
PS-CH2Cl particles. When the [SO3-PMIM] was immobilized onto PS-CH2Cl in organic solvent, the
water was droved and the holes were jammed. When the temperature further increased up to higher
than 300 ℃ for PS-CH2Cl and 410 ℃ for PS-[SO3H-PMIM][HSO4], weight loss accelerated heavily.
A possible reason is that their structures were destroyed or the chloromethyl groups and the
[SO3H-PMIM][HSO4] separated from PS. The residue weight of PS-[SO3H-PMIM][HSO4] and
PS-CH2Cl was about 56.5% and 27.2% at 450 ℃, respectively. These observations indicated that the
immobilization of [SO3H-PMIM][HSO4] onto polystyrene could improve the thermal stability of
PS-CH2Cl.
Catalytic reaction. The esterification of n-butyl alcohol with acetic acid is showed in Scheme 2.
Scheme 2 Esterification of n-butyl alcohol with acetic acid.
To evaluate the PS-[SO3H-PMIM][HSO4] catalyst described here, the catalytic activities of various
catalyst for the esterification reaction of n-butyl alcohol and acetic acid were examined under the
same reaction conditions (Table 2). Obviously, the yields of n-butyl acetate over
PS-[SO3H-PMIM][HSO4] (Table 2, entry1-3) were much higher than that over the support (Table 2,
entry 5) and no catalyst(Table 2, entry 6). This meant that the reaction hardly carried out without
catalyst and the support almost had no influence on the yield. It was worth noting that the
PS-[SO3-PMIM]1 had no influence on the reaction evidenced the scheme of the synthesis of
PS-[SO3H-PMIM][HSO4] catalyst at a certain extent. In addition, it easy to see that both the
PS-[SO3H-PMIM][HSO4] catalysts and PS-[SO3H-PMIM][Cl] (Table 2, entry 4) catalyst were
effective for the reaction of n-butyl alcohol and acetic acid although the catalytic activity of the latter
was far lower than that of the former. The reason was that both the two kinds of solid catalysts could
provide proton H+
, which could make the acetic acid protonated and then was attacked by
nucleophilic n-butyl alcohol to form n-Butyl acetate. Which analysis was based on the classical two
key steps esterfication [17-19]. Compared to PS-[SO3H-PMIM][HSO4] catalysts, there are two
groups, i.e. HSO4
-
anions and SO3
H- group, could supply proton H+
, the providing proton H+
ability
of PS-[SO3H-PMIM][Cl] is limited, which contributed lower catalytic capability.
It can be seen that all of the PS-[SO3H-PMIM][HSO4] catalysts exhibited high catalytic activity. The
yield of n-Butyl acetate increased with the increasing of [SO3H-PMIM][HSO4] content at same
reaction time, which was attributed to the gradually increasing amount of acid sites in the catalyst.
When using the PS-[SO3H-PMIM][HSO4]1 as catalyst, 98% yield was obtained at 92℃, within 1.5h,
which was better than the similar study reported by Xu[10].
Table 2 Result of n-Butyl acetate over various catalyst and reaction timea
Entry
Catalyst
Yield, %
0.75, hb
1.5, hb
3, hb
1 PS-[SO3H-PMIM][HSO4]1 94 98 98
2 PS-[SO3H-PMIM][HSO4]2 90 96 98
3 PS-[SO3H-PMIM][HSO4]3 90 93 98
4 PS-[SO3H-PMIM][Cl]1 57 68 74
5 PS-[SO3-PMIM]1 (or PS-CH2Cl1) 34 47 52
6 Blank 33 48 50
a
By quantitative GC based on crude product
b
Reaction time, h
Advanced Materials Research Vol. 983 23
38. Catalyst recycle study. The reusability of PS-[SO3H-PMIM][HSO4] catalyst was evaluated in
esterification of n-butyl alcohol with acetic acid catalyzed by PS-[SO3H-PMIM][HSO4]1. As shown
in Table 3, PS-[SO3H-PMIM][HSO4]1 still showed very high activity after third runs and the catalytic
activity decreased only 3% for 5 runs, which indicated that PS-[SO3H-PMIM][HSO4] catalyst was
efficient and reusable.
Table 3 The reusability of PS-[SO3H-PMIM][HSO4]1 for n-Butyl acetatea
Runs time 1 2 3 4 5
Yield, % 98 98 97 96 95
a
By quantitative GC based on crude product, reaction time 1.5h.
Conclusion
A series PS-[SO3H-PMIM][HSO4] catalysts were prepared by grafting [SO3H-PMIM][HSO4] onto
the highly chloromethylated polystyrene beads, and showed a better thermal stability than that of
PS-CH2Cl resins. These catalysts were efficiencies for esterification of n-butyl alcohol with acetic
acid. The yield of n-Butyl acetate generally increased with increasing of the [SO3H-PMIM][HSO4]
content. The best yield of 98% was obtained under 92℃ within 1.5h over PS-[SO3H-PMIM][HSO4]1
catalyst. The catalyst could be recovered by simple filtration, and the yield only decreased 3% after
reusing for 5 times. In conclusion, the PS-[SO3H-PMIM][HSO4] catalyst prepared in this paper was
an excellent recyclable catalyst for the synthesis of n-Butyl acetate, and it showed potential
application for carboxylic esters in industry.
This work was supported by the grant (No. 1281370046) from the Scientific Research Foundation for
the high-ranking talent of Jiangsu university.
References
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acetic acid, Ind. Eng. Chem. Res. 46 (2007) 7050–7056.
[2] X.Z. Li, W.J. Eli, A green approach for the synthesis of long chain aliphatic acid esters at room
temperature, J. Mol. Catal. A: Chem. 279 (2008) 159–164.
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Chemoselective Process for the Esterification of Carboxylic Acids, Org. Process Res. Dev. 13 (2009)
769-773.
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ionic liquids with acidic counteranion as recyclable reaction media, Catal. Commun. 3 (2002)
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[5] T. Joseph, S. Sahoo, S.B. Halligudi, Brönsted acidic ionic liquids: A green, efficient and reusable
catalyst system and reaction medium for Fischer esterification, J. Mol. Catal. A: Chem. 234 (2005)
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liquid catalyst for esterifications, J. Mol. Catal. A: Chem 332 (2010) 152-157.
24 Advanced Materials and Engineering
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3373-3377.
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acidic ionic liquids, Ind. Eng. Chem. Res. 46 (2007) 7955-7906.
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[18] S.R. Kirumakki, N. Nagaraju, S. Narayanan, A comparative esterification of benzyl alcohol with
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Advanced Materials Research Vol. 983 25
41. Fig.1 The morphology of α-Al2O3 (a:×500; b:×10000)
Preparation process. Measured 25 g α-Al2O3 and added it to 100 mL distilled water as the
reaction mother liquor. The suspending liquid was heated and stirred in certain temperature. The pH
value was adjusted by sodium hydroxide. Then injected Na2SiO3 dropwisely (about 0.75 mL/min)
into the suspending liquid and added H2SO4 (0.1 mol/L) at the same time to kept the pH value
constant (The H2SO4 was added by ProMinent Dulcometer D1Cb, a pH controller). After that, the
product was filtered and washed for several time to move the free SiO2. In the end, the precipitate
was dried at 102 o
C for 12 h.
Characterizations. The morphologies of SiO2-coated α-Al2O3 were tested by the scanning
electron microscope (JSM 7500F).
Results and discussion
Influence of concentration of sodium silicate solution. Elevated the concentration of sodium
silicate solution could accelerate the hydrolysis of sodium silicate, so the H2SiO3.nH2O would
generate massly and rapidly. The crystal particles would be small, because they didn’t have enough
time to grow up, as shown in Fig.2-b and Fig.2-c. But if the generation rate of H2SiO3.nH2O was far
faster than its deposition rate, the H2SiO3.nH2O would be more likely to formed free SiO2 or large
grain of SiO2 on the surface of α-Al2O3, as shown in Fig.2-d. Therefore the optimum concentration
is 0.10 mol/L.
Fig.2 The morphology of SiO2-coated α-Al2O3 prepared by different concentration of sodium
silicate solution (a: 0.05 mol/L ; b: 0.10 mol/L; c: 0.15 mol/L; d: 0.20 mol/L; e: 0.25 mol/L), all the
sample above were prepared in 80 o
C, with the pH 9.0
Advanced Materials Research Vol. 983 27
42. Influence of the reaction temperature. Heating properly could promote the growth of SiO2
crystal particles as well as accelerate the hydrolysis of sodium silicate. With the increase of
temperature, the crystal particles that formed in the surface of α-Al2O3 would be larger and larger, as
shown from Fig.3-a to Fig.3-d. But when the temperature was too high, the crystal might also fail to
form, as shown in Fig.3-e. Therefore the optimum reaction temperature is 80 o
C.
Fig.3 The morphology of SiO2-coated α-Al2O3 prepared in different temperature (a: 75 o
C; b: 80
o
C; c: 85 o
C; d: 90 o
C; e: 95 o
C), all the sample above were prepared by 0.10 mol/L sodium silicate
solution, with the pH 9.0
Influence of the pH value. The pH value could affect both the hydrolysis and gelling of silicate.
The sodium silicate would hydrolyze rapidly at a low pH value, which might lead to self-nucleation
of silicate. We could learn from the pre-experiment that the hydrolysis rate of sodium silicate would
be appropriate when the pH value was 8.0~10.0. The relationship of gelling time with pH was
following N curve [5]. The pH 8.0~8.5 was nearly at the bottom of the N curve, at that range, the
gelling rate would be high, and the large grain of SiO2 would be formed before it deposited on the
surface of α-Al2O3, as shown in Fig.4-a and Fig.4-b. When the pH value was 9.0, the gelling rate
was moderate and close to the deposition rate, the SiO2 on the surface of α-Al2O3 would be
well-distributed, as shown in Fig.4-c. Therefore the optimum pH is 9.0.
28 Advanced Materials and Engineering
43. Fig.4 The morphology of SiO2-coated α-Al2O3 prepared in different pH (a: 8.0; b: 8.5; c: 9.0; d:
9.5; e: 10.0), all the sample above were prepared by 0.10 mol/L sodium silicate solution, in 80 o
C
Conclusions
The SiO2-coated α-Al2O3 pearlescent pigment was prepared by liquid phase deposition (LPD).
The result of SEM showed that when the process parameters are concentration of sodium silicate
solution of 0.1 mol/L, reaction temperature of 80 o
C and pH value of 9.0, the SiO2 on the surface of
α-Al2O3 would be dense, fine and well-distributed.
Acknowledgements
This work is supported by Program for the Fujian Provincial Science and Technology and the
Provincial Financial Department (2011H6005), and the Scientific Research Foundation for the
Returned Overseas Chinese Scholars, State Education Ministry (2011-1568).
The corresponding authors are Qinghua Chen and Qingrong Qian.
References
[1] Curtis J. Zimmermann, James D. Christie, Vivian K. Doxey and Daniel Stevenson Fuller, U.S.
Patent 6,821,333. (2004)
[2] Deborah Cacace, Carolyn Lavallee, Michael T. Venturini, U.S. Patent 5,759,255. (1998)
[3] Frank J. Maile, Gerhard Pfaff, Peter Reynders, Effect pigments—past, present and future,
Progress in Organic Coatings. 54 (2005) 150-163.
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Lim, Sung Yun Jo, Kwang Choong Kang, U.S. Patent 8,287,636. (2012)
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Analysis of TiO2 surface coated with SiO2 and Al2O3, Chemical journal of Chinese universities. 19
(1998) 1727-1729.
Advanced Materials Research Vol. 983 29
45. stability within the geogrid structure to withstand the stress concentrations imposed by connection
techniques. Filtration or drainage performance of geocomposites could be also influenced by the
seam strength with different seaming methods. In this study, geotextiles - 4 woven and 4 nonwoven
types, 4 geogrids and 2 geocomposites of [nonwoven/fibers/nonwoven] structure were used as raw
materials and the different seaming methods were applied to compare the seam properties of 3
geosynthetics and transmissivities of geocomposites.
Experimental
Preparation of Samples and Seaming
8 Geotextiles(; 4 woven and 4 nonwoven types), 4 geogrids and 2 geocomposites of
[nonwoven/fibers/nonwoven] structure were used as raw materials. Geocomposites of 3-layer
structure which have the excellent drainage function under confined loading condition were
manufactured by needle punching method. Three different punching patterns were applied to
manufacture these geotextiles as , and punching pattern.
Assessments of Performance of Geosynthetics
Seaming methods that applied to geosynthetics were as following: (1) geotextiles - sewing methods :
flat seam(; SSa-1, -2), butterfly seam(; SSd-1, -2), geospacer, (2) geogrids - band and geospacer, (3)
geocomposites – flat seam(; SSa-1, -2) and geospacer. Table 1 shows the specifications and
seaming methods of these geosynthetics and Figure 1 shows the various seam types and geospacer.
Seam properties of geotextiles and geocomposites were examined by ASTM D 4884(; test method
for seam strength of sewn geotextiles) and those of geogrids were investigated through ASTM D
4884. Chemical resistance of geosynthetics were tested in the condition of pH 3 and 8, 25°C and
50°C during 360 days. These solutions were adopted to compare the chemical resistance by
considering the waste leachates. The degree of chemical resistance of geosynthetics were estimated
by comparing the tensile strength retention ratio after 360 days with ASTM D 5322. Especially for
geogrids, creep deformation tests were done to determine the reduction factor of geogrids to affect
the long-term performance by ASTM D 5262 and GRI GG 3(b). Transmissivities of geocomposites
were tested by ASTM D 4716. 2 types of geonet composites – GNC-1, -2 - having the same
thickness as smart geotextiles were used as comparison materials for drainage function and Figure 2
showed the cross sectional morphology of geocomposites and geonet composites.
Advanced Materials Research Vol. 983 31
47. (a) Smart geotextiles (b) Geonet composite
Fig 2. Photographs of cross section areas of geosynthetics
Result and Discussion
Seamed geosynthetics by geospacers
Fig. 2 shows the seamed geosynthetics, e.g., nonwoven geotextile, geogrid and geocomposite by the
geospacer. In this Figure, it was seen that this seaming method has no problem to be used in the
bonded area instead of the overlapping the geosynthetics, especially the thick geotextiles which
have the weight more than 1,000g/m2.
(a) Nonwoven geotextile (b) Geogrid
(c) Geocomposite
Fig 3. Photographs of seamed geosynthetics by geospacer
Seam Strength
Table 2 shows the seam strength of the seamed geosynthetics with the seam type. For woven
geotextiles, the butterfly seam(SSd-1 and SSd-2) shows the excellent seam strength than the flat
seam(SSa-1 and SSa-2) but the geospacer seam shows the lower seam strength than the flat and
butterfly seams. From this, it was seen that the geospacer seam is not optimum for the woven
geotrextiles. For nonwoven geotextiles, the geospacer seam shows the excellent seam strength than
the flat and butterfly seams with the increase of weight. It is thought that geospacer makes more
Advanced Materials Research Vol. 983 33
48. compact seam than the flat and butterfly seams for thicker nonwoven geotextiles. For geogrids and
geocomposites, the geospacer seam shows the excellent seam strength than the band seam without
regard to the design strength and geogrid’s composition.
Table 2. Seam strength of geosynthetics with seam type
Chemical Resistance
The degree of chemical resistance of geosynthetics in the acidic and alkaline solutions were
represented in Table 3~6. Nonwoven geotextiles showed the excellent chemical resistance than the
woven geotextiles. The tensile strength retentions of woven geotextiles was decreased with high pH
value and temperature. This is the typical phenomena of polyester fibers which were unstable
against the high pH value and temperature. However, the geospacer seam showed the excellent
chemical resistance for all geosynthetics. For geogrids, chemical resistance is not dependent on the
seam type and the design strength. Geocomposites showed the same tendency of chemical
resistance as the nonwoven geotextiles but smaller change than nonwoven geotextiles.
Table 3. Tensile strength retention of geosynthetics with seam type at pH 3, 25°C
Seam Type
Geosynthetics
SSa-1 SSa-2 SSd-1 SSd-2 Band Geospacer
WGT-1 116 120 127 134 - 86
WGT-2 118 123 134 138 - 92
WGT-3 121 127 138 143 - 101
WGT-4 124 131 141 148 - 118
NWGT-1 78 85 - - - 92
NWGT-2 80 87 - - - 98
NWGT-3 81 89 - - - 106
NWGT-4 83 92 - - - 113
GG-1 - - - - 66 76
GG-2 - - - - 68 84
GG-3 - - - - 72 78
GG-4 - - - - 76 86
GC-1 64 78 - - - 154
GC-2 81 94 - - - 158
Seam type
Geosynthetics
SSa-1 SSa-2 SSd-1 SSd-2 Band Geospacer
WGT-1 82 84 84 86 - 86
WGT-2 84 85 86 87 - 86
WGT-3 84 85 86 88 - 87
WGT-4 85 86 86 88 - 88
NWGT-1 78 80 - - - 83
NWGT-2 80 83 - - - 85
NWGT-3 82 83 - - - 87
34 Advanced Materials and Engineering
51. Long-Term Design Strength of Geogrid by Creep Reduction Factor
From GRI Standard Test Method GG4, the allowable strength of geogrid could be written in the
following equation to be taken into consideration of the ultimate strength, reduction factors for
application of geogrids. The long-term design strength of geogrid should be used in the following
equation. The reference document can be found in the GRI Standard Test Method GG4(b)
“Determination of the Long-term Design Strength of Flexible Geogrids”.
]
1
[
bd
cd
cr
id
ultimate
design
RF
RF
RF
RF
T
T
×
×
×
×
×
×
×
×
×
×
×
×
=
=
=
= (1)
where, Tdesign = long-term design strength of geogrid
Tultimate = ultimate strength of geogrid
RFid = reduction factor for installation damage
RFcr = reduction factor for creep deformation
RFcd = reduction factor for chemical degradation
RFbd = reduction factor for biological degradation
Table 7 shows the longterm design strength of geogrids by the reduction factor of the above
mentioned conditions. We used the default values of each reduction factor to be written in the
reference, [1]. In here, reduction factors of the geospacer seam are smaller than those of the band
seam and this means geospacer seam is more effective than the band seam. Therefore, the long-term
design strength values of geospacer showed higher than those of the band seam.
Table 7. Long-Term design strength by reduction factor of geogrids with seam type.
Geogrid
Reduction Factor
Long-Term
Design Strength (KN/m)
Band Geospacer Band Geospacer
GG-1 2.4 2.0 33.3 40.0
GG-2 2.4 1.9 62.5 78.9
GG-3 2.4 1.8 83.3 111.1
GG-4 2.3 1.8 108.7 138.9
Transmissivities of Geocomposite
Table 8 shows the transmissivities of geocomposites by seam type. Geospacer seam showed higher
transmissivity than the flat seam(; SSa-1 SSa-2) without regard to the kinds of filled fibers and
weight of geocomposite. For the similar specification, geocomposites showed the better
transmissivities than the typical drainage materials, geonet composites.
GG-2 - - - - 90 91
GG-3 - - - - 90 91
GG-4 - - - - 91 92
GC-1 82 83 - - - 86
GC-2 82 84 - - - 86
Advanced Materials Research Vol. 983 37
52. Table 8. Transmissivities of geocomposites and geonet composites
Seam Type
Geogrid
SSa-1 SSa-2 Geospacer
GC-1 1.581 1.224 0.983
GC-2 1.218 1.057 0.915
GNC-1 - - 0.699
GNC-2 - - 0.485
Conclusion
Woven geotextiles showed the higher seam strength in the order of butterfly seam(; SSd-1 SSd-2)
flat seam(; SSa-1 SSa-2) geospacer without regard to the design strength. For nonwoven
geotextiles of 1,000g/m2~, the order of seam strength is geospacer flat seam(; SSa-1 SSa-2).
Geogrids showed the higher seam strength in the order of band geospacer but creep deformation
were increased in the order of band geospacer without regard to the design strength and geogrid’s
compositions. Geocomposites showed the higher seam strength in the order of geospacer flat
seam(; SSa-1 SSa-2) but showed the transmissivity in the order of geospacer flat seam(; SSa-1
SSa-2) without regard to the kinds of filled fibers and weight of geocomposite.
References
[1] R. M. Koerner, 1998, Designing with Geosynthetics, 4th Ed., Prentice-Hall, New Jersey, U.S.,
Chapter 4.
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Construction Guidelines, U.S. Dept. of Transportation Federal Highway
Administration, Publication No. FHWA HI-95-038, 27-105.
[3] FHWA, 1989, Geotextile Design Construction Guidelines, U.S. Dept. of Transportation
Federal Highway Administration, Publication No. FHWA HI-90-001, 24-46.
[4] Jewell R. A., 1996, Soil Reinforcement with Geotextiles, CIRLA Special Publication, Thomas
Telford, Westminster, Chapter 5.
38 Advanced Materials and Engineering
54. diisocyanate groups, in relation to polyol amount, has increased the strength at rupture of the
obtained polymers and has decreased the polymers elongation, which has resulted into a modulus
increasing [11]. Anupama Kaushik et al., examines a series of 1,4-butane diol chain extended
polyurethane nanocomposites based on castor oil, and 4,40-diphenylmethane diisocyanate (MDI)
were synthesized with modified clay (Cloisite 30B) as filler [12].
1. Experimental
2.1 Materials
Commercial grade Castor oil was purchased from the local market. It was dehydrated at
80ºC in in a vacuum oven and characterized for hydroxyl value (148), acid value (2) and moisture
content (0.379%). Polypropylene glycol (PPG) (Mn=4000) was supplied by SIGMA- Aldrich
Company. Chain extender, 1, 4-butane diol was procured from Himedia, India. The toluene
diisocyanate (TDI), which were used as received, were supplied from SIGMA- Aldrich Company.
The catalyst used in this research is DABCO-33LV which is the mixture of triethylenediamine and
di (propylene glycol) and it was supplied by Air Products and Chemicals (United Kingdom).
2.2 Characterization Technique
Fourier transform infrared spectroscopy (FTIR) analysis of polyurethanes was done using A
Vector-22 FT-IR spectrometer (Nicolet 5DX FT-IR) with a resolution of 1 cm-1
from 4000 to 400
cm-1
. Thermal stability (TGA) of polyurethanes was carried out using a Universal V4.5A, TA
instruments under a nitrogen atmosphere. Scanning electron microscopy (SEM) was carried out on
a JEOL 6300F machine at an acceleration voltage of 5KV. Tensile testing of the nanocomposites
film was carried out on an instron model 4505 universal testing machine at 25ºC, with a load cell of
5 KN and following ASTM D 638. The crosshead speed was set to 2 mm/min. Samples were cut in
a dumbbell shape with an ASTM D 638 (type V).
3. Result and Discussion
3.1 FTIR Analysis
The micro-domain structures of the pure PU and castor oil based PU were analyzed by FTIR
as shown in Figure 1. A small broad band in the range 4000–3500 cm-1
, was observed in both
samples relating to the O-H stretching vibrations from either water or hydroxyl terminated
compounds, and N-H stretching vibrations from either urea or amine group [13-14]. The CH – CH3
peaks stretching are more prominent in castor oil based PU, then pure PU which may be due to
larger organic chain present in castor oil based PU. Peaks at 1727 cm-1
represents (C=O) non
bonded urethanes [12] which are likely to be present in larger number, in castor oil based PU
synthesis.
2.2 TGA Analysis
The result of the thermo gravimetric analysis (Figure 2) shows that thermal stability of pure
PU and castor oil PU based under identical conditions and a comparison of the weight losses
occurred. The thermal stability of these polymers is starting generally above 200 °C [15-16]. It is
40 Advanced Materials and Engineering
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