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ADVANCED FABRICATION AND MULTIFUNCTIONAL PROPERTIES OF MORPHOLOGY-CONTROLLED GRAPHENE AEROGELS AND THEIR COMPOSITES FAN ZENG (B. Eng, Harbin Institute of Technology) A THESIS SUBMITTED FOR THE DEGREE OF DOCTOR OF PHILOSOPHY DEPARTMENT OF MECHANICAL ENGINEEING NATIONAL UNIVERSITY OF SINGAPORE 2015

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Page 1: FAN ZENG · and excellent multifunctional properties of graphene nanosheets, can be promising candidates for energy storage devices and light-weight nanocomposites. For this research,

ADVANCED FABRICATION AND MULTIFUNCTIONAL

PROPERTIES OF MORPHOLOGY-CONTROLLED

GRAPHENE AEROGELS AND THEIR COMPOSITES

FAN ZENG

(B. Eng, Harbin Institute of Technology)

A THESIS SUBMITTED

FOR THE DEGREE OF DOCTOR OF PHILOSOPHY

DEPARTMENT OF MECHANICAL ENGINEEING

NATIONAL UNIVERSITY OF SINGAPORE

2015

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ACKNOWLEDGEMENTS

I would like to convey my deepest and sincerest appreciation to my

supervisors, Asst. Prof. Duong Hai Minh and Assoc. Prof. Christina Lim Y. H.,

for their invaluable guidance and constant support during my whole PhD

candidature. The energy and enthusiasm that they have for research never fail to

inspire me.

I extend my sincere thanks to Assoc. Prof. Brian L. Wardle and all group

members at Massachusetts Institute of Technology (MIT) for their warm

hospitality and valuable suggestions for my research during my visit to

NECSTlab.

I am extremely grateful to my fellow group members, Dr. Nguyen Truong

Son, Mr. Gong Feng, Ms. Feng Jingduo, Mr. Cheng Hanlin, Ms. Liu Peng, Mr.

Tran Quyet Tran, Mr. Daniel Tng Z. Y., Ms. Clarisse Lim X. T., and Mr. Daryl

Lim, for their devoted help and cooperation in my research work. I am also

thankful to Asst. Prof. Chua Kian Jon, Dr. Zhao Xing, Mr. Sun Bo, and Asst.

Prof. Amy Marconnet at Purdue University for their support regarding thermal

conductivity measurements.

I also thank the technical staff in Materials Laboratory, Mr. Thomas Tan,

Mr. Ng Hongwei, Mr. Abdul Khalim Bin Abdul, and Mr. Juraimi B. Madon,

and the technical staff in the Energy Conversion Laboratory, Mr. Tan Tiong

Thiam, for their superior and professional technical support.

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Finally, I gratefully acknowledge the Start-up Grant R-265-000-361-133,

SERC 2011 Public Sector Research Funding (PSF) Grant R-265-000-424-305,

and the China Scholarship Council (CSC) for providing financial support.

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TABLE OF CONTENTS

ACKNOWLEDGEMENTS ............................................................................. i

TABLE OF CONTENTS .............................................................................. iii

SUMMARY .................................................................................................... vii

LIST OF TABLES .......................................................................................... ix

LIST OF FIGURES ......................................................................................... x

CHAPTER 1: Introduction .......................................................................... 1

1.1 Aerogels .............................................................................................. 1

1.1.1 Background ............................................................................ 1

1.1.2 Carbon-based aerogels ........................................................... 2

1.1.3 Drying techniques of aerogels ............................................... 4

1.1.4 General properties and applications of aerogels .................... 6

1.2 Carbon-based nanocomposites .............................................................. 8

1.3 Objectives of thesis ............................................................................... 9

1.4 Organization of thesis ......................................................................... 11

CHAPTER 2: Literature Review .............................................................. 13

2.1 Graphene ............................................................................................. 13

2.1.1 Introduction .......................................................................... 13

2.1.2 Structure of graphene ........................................................... 14

2.1.3 Synthesis methods of graphene ............................................ 15

2.1.4 Properties of graphene ......................................................... 24

2.1.5 Potential applications of graphene ....................................... 28

2.2 Graphene aerogels (GAs) .................................................................... 29

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2.2.1 Introduction .......................................................................... 29

2.2.2 Graphene oxide (GO) ........................................................... 31

2.2.3 Structure of GAs .................................................................. 34

2.2.4 Synthesis methods of GAs ................................................... 35

2.2.5 Properties of GAs ................................................................. 39

2.2.6 Potential applications of GAs .............................................. 42

2.3 Graphene–carbon nanotube (CNT) hybrid aerogels ........................... 44

2.3.1 Introduction .......................................................................... 44

2.3.2 Structure of graphene–CNT hybrid aerogels ....................... 44

2.3.3 Synthesis methods of graphene–CNT hybrid aerogels ........ 45

2.3.4 Properties and potential applications of graphene–CNT

hybrid aerogels ..................................................................... 46

2.4 Graphene–polymer nanocomposites ................................................... 47

2.4.1 Introduction .......................................................................... 47

2.4.2 Structure of graphene–polymer nanocomposites ................. 48

2.4.3 Synthesis methods of graphene–polymer nanocomposites .. 49

2.4.4 Properties of graphene–polymer nanocomposites ............... 50

2.4.5 Potential applications of graphene–polymer nanocomposites

.............................................................................................. 54

CHAPTER 3: Experimental Section ......................................................... 56

3.1 Materials ............................................................................................. 56

3.2 Experimental techniques ..................................................................... 57

3.2.1 Synthesis of graphene oxide (GO) ....................................... 57

3.2.2 Synthesis of graphene aerogels (GAs) ................................. 58

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3.2.3 Synthesis of graphene–CNT hybrid aerogels ...................... 59

3.2.4 Synthesis of GA–poly (methyl methacrylate) (PMMA)

nanocomposites .................................................................... 59

3.3 Characterization .................................................................................. 60

3.3.1 X-ray diffraction (XRD) ...................................................... 60

3.3.2 Scanning electron microscopy (SEM) ................................. 60

3.3.3 Physical adsorption/desorption of nitrogen (BET) .............. 61

3.3.4 Electrical conductivity measurement ................................... 63

3.3.5 Thermal conductivity measurement ..................................... 64

3.3.6 Thermogravimetric analysis (TGA) ..................................... 67

3.3.7 Vickers microhardness measurement .................................. 67

CHAPTER 4: Morphology Control of Graphene Aerogels .................... 69

4.1 Introduction ......................................................................................... 69

4.2 Nanostructured control of graphene aerogels (GAs) .......................... 70

4.2.1 Effects of chemical compositions and synthesis conditions 72

4.2.2 Effects of reducing agents .................................................... 76

4.2.3 Effects of CNTs ................................................................... 77

4.3 Conclusions ......................................................................................... 79

CHAPTER 5: Multifunctional Properties of Graphene Aerogels .......... 80

5.1 Introduction ......................................................................................... 80

5.2 Electrical property of graphene aerogels (GAs) ................................. 81

5.2.1 Effects of chemical compositions and synthesis conditions 81

5.2.2 Effects of reducing agents .................................................... 83

5.2.3 Effects of CNTs ................................................................... 85

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5.3 Thermal stability of graphene aerogels (GAs) .................................... 86

5.3.1 Effects of chemical compositions and synthesis conditions 86

5.3.2 Effects of reducing agent and CNTs .................................... 87

5.4 Thermal conductivity of graphene aerogels (GAs) ............................. 88

5.4.1 Effects of chemical compositions ........................................ 88

5.4.2 Effects of thermal annealing ................................................ 93

5.4.3 Prediction of thermal boundary resistance and thermal

conductivity of graphene nanosheets within GAs ............... 94

5.5 Conclusions ......................................................................................... 96

CHAPTER 6: Advanced Multifunctional Graphene Aerogel–Poly

(methyl methacrylate) Composites: Experiments and Modelling ............. 98

6.1 Introduction ......................................................................................... 98

6.2 Structure of GA–PMMA nanocomposites .......................................... 99

6.3 Electrical property of GA–PMMA nanocomposites ......................... 101

6.4 Thermal stability of GA–PMMA nanocomposites ........................... 103

6.5 Thermal property of GA–PMMA nanocomposites .......................... 104

6.6 Microhardness of GA–PMMA nanocomposites ............................... 106

6.7 Conclusions ....................................................................................... 109

CHAPTER 7: Conclusions and Recommendations ............................... 111

7.1 Conclusions ........................................................................................ 111

7.2 Recommendations .............................................................................. 114

REFERENCES ............................................................................................. 116

LIST OF PUBLICATIONS ........................................................................ 160

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SUMMARY

Graphene aerogels (GAs) having large surface area property of aerogels

and excellent multifunctional properties of graphene nanosheets, can be

promising candidates for energy storage devices and light-weight

nanocomposites. For this research, a cost-effective method has been developed

to synthesize self-assembled GAs from graphite at a low temperature range

(45–95 oC) through modified Hummers’ and chemical reduction methods

using various reducing agents (L-ascorbic acid, NaHSO3 and HI). The effects

of synthesis conditions, reducing agents, thermal annealing processes and

carbon nanotubes (CNTs) on the morphology, electrical and thermal properties

of the as-prepared GAs are quantified comprehensively. The GA

nanostructures are well controlled and have a large surface area of up to 577

m2/g. The CNT inclusions and annealing processes can enhance the electrical

conductivity of the as-prepared GAs by up to five times, as measured via a

two-probe method. For the first time, a comparative infrared microscopy

technique has been successfully developed to measure the thermal conductivity

of GAs, and the GAs having 0.67–2.50 vol. % graphene are measured to be

0.12–0.36 W/m·K accordingly.

For light-weight but strong material development, GA–poly (methyl

methacrylate) (PMMA) nanocomposites are further developed by backfilling

PMMA into the pores of the GAs. Due to uniform distribution of the graphene

nanosheets in the PMMA matrix, the GA–PMMA nanocomposites exhibit

significant enhancements of electrical conductivity (0.16–0.86 S/m),

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microhardness (303.6–462.5 MPa), and thermal conductivity (0.35–0.70

W/m·K) over pure PMMA and the graphene–PMMA nanocomposites prepared

by traditional powdery dispersion methods. The developed GAs and

GA–PMMA nanocomposites in this thesis can be applied in aerospace,

composite electrodes, biosensors, and energy harvest and storage devices.

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LIST OF TABLES

Table 1-1 Identification of aerogel properties and features, with their

applications [18]

. (Reproduced with permission from Ref. 18. Copyright (1998)

Elsevier.) ............................................................................................................ 7

Table 2-1 A comparison of strengths and drawbacks for the methods commonly

applied to synthesize graphene [68]

. (Reproduced with permission from Ref. 68.

Copyright (2010) Elsevier.) ............................................................................. 15

Table 4-1 Nanostructure control of the GAs. .................................................. 73

Table 4-2 Effects of reducing agent and addition of CNTs on morphology of

the GAs. ........................................................................................................... 76

Table 5-1 Morphological effects on electrical property of the GAs. .............. 82

Table 5-2 Effects of reducing agent and addition of CNTs on electrical

conductivity and thermal stability of the GAs. ................................................ 83

Table 5-3 Synthesis conditions, density, volume fraction and thermal

conductivity of the GAs. .................................................................................. 90

Table 6-1 Synthesis conditions, graphene volume fraction, and multifunctional

properties of GA–PMMA nanocomposites. .................................................. 100

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LIST OF FIGURES

Figure 1.1 Application examples of carbon-based aerogels. (a) Representation

of an electric double-layer capacitor (EDLC); (b) Three-dimensional N-doped

graphene aerogel-supported Fe3O4 nanoparticles as efficient cathode catalysts

for the redox reaction [20]

. (Reproduced with permission from Ref. 20,

Copyright (2012) American Chemical Society.) ............................................... 3

Figure 1.2 Principles of three drying methods (evaporation, freeze drying, and

CPD) to remove liquid from hydrogels in a generic phase diagram. (a) Direct

evaporation from liquid phase to gas phase causes collapse to the gel network

due to the effect of surface tension. (b) Freeze drying is a common method to

create aerogels. During this process, the samples are fast frozen and then placed

in a vacuum under raised temperature to allow the ice to sublimate. (c) In the

CPD process, the temperature and pressure of liquid carbon dioxide are raised

above its critical point to form a supercritical fluid. By slowly releasing the

pressure, the hydrogels are dried to aerogels with well-preserved networks. The

CPD process is selected as the drying method in this thesis work. Adapted from

the thesis work of Mateusz B. Bryning [33]

. ....................................................... 6

Figure 2.1 Graphene is the building block of all carbon materials, e. g. 0D

fullerenes, 1D CNTs, and 3D graphite [24]

. (Reproduced with permission from

Ref. 24. Copyright (2007) Macmillan Publisher Ltd.) ..................................... 13

Figure 2.2 Scheme of the crystal structure, Brillouin zone, and dispersion

spectrum of graphene [52]

. (Reproduced with permission from Ref. 52.

Copyright (2010) Wiley–VCH.) ...................................................................... 15

Figure 2.3 Mechanically exfoliated (a) multi-layer, (b) few-layer and

monolayer graphene. Yellow colors indicate multi-layer graphene of thickness

over 100 nm, while blue, darker, and lighter purple indicate few-layer and

monolayer graphene [68]

. (Reproduced with permission from Ref. 68. Copyright

(2010) Elsevier.) .............................................................................................. 18

Figure 2.4 (a) A SEM image of a monolayer graphene suspended on an array of

circular holes, scale bar: 3μm; (b) A scheme of nanoindentation on the

membrane of graphene [54]

. (Reproduced with permission from Ref. 54.

Copyright (2008) AAAS.) ............................................................................... 26

Figure 2.5 Two sub-models of the Lerf-Klinowski model with (top) and

without (bottom) the presence of carboxylic acid groups on the periphery of the

graphitic basal plane of GO [162, 163, 169]

. (Top: Reproduced with permission from

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Ref. 162. Copyright (1998) American Chemical Society. Bottom: Reproduced

with permission from Ref. 163. Copyright (1998) Elsevier.) .......................... 32

Figure 2.6 Schematic of hydrogen bonding formed between water (H2O) and

the oxygen-containing functional groups of GO [169]

. (Reproduced with

permission from Ref. 169. Copyright (2010) The Royal Society of Chemistry.)

.......................................................................................................................... 33

Figure 2.7 (a) A typical SEM image which shows the structure of GAs. (b)

AFM images of typical building blocks of the GAs [157]

. (Reproduced with

permission from Ref. 157. Copyright (2011) Elsevier.) .................................. 35

Figure 2.8 SEM images showing the network structures of graphene–CNT

hybrid aerogels [157]

. (Reproduced with permission from Ref. 157. Copyright

(2011) Elsevier.) .............................................................................................. 45

Figure 2.9 Relationship between d spacing of graphene nanosheet (GNS)

families and graphite [210]

. Addition of CNTs and fullerene (C60) was found to

effectively increase the interlayer spacing of graphene. (Reproduced with

permission from Ref. 210. Copyright (2008) American Chemical Society.) .. 46

Figure 3.1 A Solartron 1260+1287 electrochemical system for electrical

property testing. ............................................................................................... 63

Figure 3.2 (a) Set-up schematic of thermal conductivity measurement using the

comparative infrared thermography technique. (b) Temperature distribution and

linear best fit curves for the 3-layered stack, which consists of a GA sample

sandwiched between two amorphous quartz layers, scale: 133 μm/ pixel. (c)

Heat flux as a function of temperature gradient in the GA region at several

power levels. During the measurement, the heat flux is typically below

11.25kW/m2. .................................................................................................... 66

Figure 4.1 (a) Aqueous suspension of GO and a graphene hydrogel and (b) A

graphene aerogel. ............................................................................................. 71

Figure 4.2 XRD patterns of graphite, graphite oxide and graphene aerogel. . 72

Figure 4.3 SEM images of graphene aerogels synthesized under different

conditions: (a) 2 mg GO/ml, 70 °C, 40 h; (b) 12 mg GO/ml, 70 °C, 40 h; (c) 2

mg GO/ml, 45 °C, 40 h; (d) 2 mg GO/ml, 95 °C, 40 h; (e) 2 mg GO/ml, 70 °C, 5

h. Compared with image (a), more graphene nanosheets can be observed in

image (b). The GA sample in image (c) shows a more loose structure than those

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in image (a) and image (d). Image (e) also shows a less dense network than that

in image (a). ..................................................................................................... 73

Figure 4.4 A typical N2 adsorption/desorption isotherm of a GA. ................. 74

Figure 4.5 (a) A digital photo of a graphene–CNT hybrid aerogel; (b) and (c)

SEM images of a graphene–CNT hybrid aerogel at different magnifications. 78

Figure 5.1 I–V plot of the GA obtained from 12 mg/ml GO suspension at 70 °C

for 40 h. ............................................................................................................ 81

Figure 5.2 Effects of initial GO concentrations on electrical conductivity and

surface area of GAs. ......................................................................................... 83

Figure 5.3 Effect of reducing agents and thermal annealing on (a) electrical

conductivity and (b) thermal stability of the GAs. .......................................... 84

Figure 5.4 XRD patterns of the GAs reduced by different reducing agents with

and without thermal annealing. ........................................................................ 85

Figure 5.5 Electrical conductivity and DTA peak temperature for

graphene–CNT hybrid aerogels with various CNT concentrations. ................ 86

Figure 5.6 Thermal stability of GAs at (a) 45 °C and (b) 95 °C. .................... 87

Figure 5.7 SEM images of the GAs synthesized under different conditions:

(a)–(h) represent GA1–GA8 respectively. All images present interconnected

3D networkstructures. With annealing, images (e)–(h) show denser networks

than those in images (a)–(d) at the same GO concentration. ........................... 89

Figure 5.8 Effects of GO concentrations and thermal annealing on thermal

conductivities of the GAs................................................................................. 91

Figure 5.9 XRD patterns of the GA4–5, 7 and 8. Broad peaks indicate the

non-crystal aerogel stucture. Compared with GA7, the peak of GA8 shifts right

and indicates the smaller interspacing between graphene nanosheets. ............ 94

Figure 5.10 The thermal condictivity of the GAs as a function of graphene

volume fraction. Best fits from rule of mixtures (dashed line) and EMT (orange

dots) are shown. For the rule of mixtures, the slope of the least-squares best fits

to the experimental data is the (kG-kair). For EMT, the values calculated assume

a kG=30.2 W/m·K, a value which is obtained by manually fitting the data. .... 95

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Figure 6.1 Digital images of (a) GA and (b) GA–PMMA nanocomposite and

FE-SEM images of (c) the porous GA without PMMA infiltrated and (d) the

cross section of the GA–PMMA nanocomposite........................................... 100

Figure 6.2 (a) The electrical conductivity (black dots) of GA–PMMA

nanocomposites as a function of graphene volume fraction at room temperature.

The dashed blue line is the best fit from the power law relation 𝜎𝑐 =𝜎𝑓[(𝜑 − 𝜑𝑐)/(1 − 𝜑𝑐)]𝑡 with a nonlinear least-squares algorithm, where the

fitted values are σf=2543.8, φc=0 and t=2.18, respectively. (b) Comparative

study of electrical conductivity between this work and previously reported

graphene–PMMA nanocomposites synthesized via in situ polymerization. For

comparison purposes, the values of graphene loading reported in wt. % have

been converted to vol. %. ............................................................................... 102

Figure 6.3 Thermogravimetric curves of PMMA and GA–PMMA

nanocomposites. ............................................................................................. 104

Figure 6.4 The thermal conductivity of GA–PMMA nanocomposites as a

function of graphene volume fraction. Inset is the set-up scheme for the

comparative infrared microscopy technique, where the amorphous quartz

having thermal conductivity of 1.3 W/m·K is used as the reference material. To

extract the thermal conductivity of rGO and TBR between rGO and PMMA, the

experimental data is fitted with a modified effective medium theory

simultaneously by a nonlinear least-squares algorithm. The red dashed line

represents the best fitting with the thermal conductivity of rGO (30.0 W/ m·K)

and the rGO-PMMA TBR (3.78×10-8

Km2/W). ............................................ 105

Figure 6.5 The microhardness of GA–PMMA nanocomposites as a function of

graphene volume fractions. Inset is a typical indentation for the Vickers

microhardness test. For all GA–PMMA nanocomposites, the diagonal

dimensions range from 25 to 60 μm. A prediction of the microhardness of

GA–PMMA nanocomposites, using the modified Halpin–Tsai equation, and a

comparative study of microhardness between this work and previously reported

graphene–PMMA nanocomposites are also included. For comparison purposes,

the values of graphene loading reported in mass fraction (wt. %) are converted

to volume fraction (vol. %). ........................................................................... 108

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CHAPTER 1: Introduction

This chapter provides a background of aerogels and nanocomposites.

Among the various types of aerogels, graphene aerogels, which are a novel type

of carbon-based aerogels, are of particular interest for this study. The utilization

of graphene aerogels to prepare graphene aerogel-based nanocomposites could

effectively solve the agglomeration problem of carbon fillers in carbon-filled

nanocomposites, and further provides a promising application for graphene

aerogels.

1.1 Aerogels

1.1.1 Background

An aerogel is an open-celled, mesoporous and solid foam which comprises

a network of interconnected nanostructures, having a porosity of over 50%.

Herein, the term “mesoporous” (or “a mesoporous material”) is commonly

defined as a material containing pores in the range of 2–50 nm in diameter [1, 2]

.

In fact, aerogels are well-known for their dramatic low densities (often

varying from 0.00016 to ~0.5 g/cm3), and are even considered the lightest solid

materials (with lowest densities) that have ever been made [1, 3, 4]

. For instance,

an as-prepared silica aerogel is only three times heavier than air [5]

, and can

possibly be made even lighter by evacuating the air from its pores. However, a

typical aerogel usually opposes a density of 0.020 g/cm3 or higher,

approximately 15 times heavier than air, and has 95–99% air (or other gases) in

its volume [3]

.

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It should be noted that the term “aerogel” does not refer to a specific

substance, but rather to a network structure a substance takes on [1]

. Aerogels

can be made of various substances, including silica [5]

, most of the transition

metal oxides [6, 7]

, several main group metal oxides [6]

, organic polymers [8]

,

metals [9]

, carbon [8, 10]

, carbon nanotubes (CNTs) [11, 12]

, and graphene [13, 14]

.

From the perspective of chemistry, the aerogel of a substance is generally

analogous to the bulk of that identical substance. Nevertheless, because of their

extraordinary low densities and length-scale effects, which stem from their

nanostructures, aerogels would commonly exhibit many remarkably improved

properties superior to the non-aerogel form of the substance (e.g. dramatic

increase in surface areas and catalytic activities), while also possibly suffering

reductions in some other properties (e.g. decreased mechanical strength) [1, 2]

.

1.1.2 Carbon-based aerogels

Carbon-based aerogels possess almost similar properties to other kinds of

aerogels, but are also electrically conductive with a density-dependent

conductivity [8, 10-15]

. Due to this unique electrical property, the carbon-based

aerogels are mostly fabricated for industrial applications such as desalination

[16], solar energy collection

[17], and catalyst support

[18, 19]. Noticeably, their high

surface area and electrical conductivity can in particular meet the requirements

of the electrode materials for electrochemical devices [20]

, as shown in Figure

1.1.

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Figure 1.1 Application examples of carbon-based aerogels. (a) Representation

of an electric double-layer capacitor (EDLC); (b) Three-dimensional N-doped

graphene aerogel-supported Fe3O4 nanoparticles as efficient cathode catalysts

for the redox reaction [20]

. (Reproduced with permission from Ref. 20,

Copyright (2012) American Chemical Society.)

Carbon aerogels were first prepared from organic materials by Pekala et al.

[8, 10] in the 1980s. With this method, resorcinol (R) and formaldehyde (F) were

employed as precursors, sodium carbonate as a catalyst, and water as a solvent.

An organic gel was formed via poly-condensation of the precursors in a solvent

and then cured in an oven for 3–7 days. The as-obtained organic gels were then

supercritically dried to organic aerogels, followed by a carbonization process at

elevated temperature in an inert environment to eventually create carbon

aerogels. From this approach, a high surface area could usually be obtained

from these as-prepared carbon aerogels, which also in turn affected their

electrical conductivity. However, most of the chemicals involved in

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synthesizing these carbon aerogels are highly toxic, and a high temperature over

1000 °C is also strictly required for the carbonization process.

As a common type of carbon aerogels, CNT aerogels are developed based

on the interesting properties of CNTs [21-23]

. They are essentially CNTs

randomly accumulated in space and connected by some specific organic binder

[11, 12]. It has been indicated that CNT aerogels can offer high power density as

the electrode materials of supercapacitors. However, the high cost of CNT

fabrication and difficulty of CNT dispersion are still great challenges facing the

commercialization of CNT aerogels.

Graphene is a one-atom-thick planar sheet of sp2-bonded carbon atoms

which are densely packed in a honeycomb crystal lattice, having a high surface

area and excellent lateral mechanical, structural, thermal, and electrical

properties, similar or even superior to those of CNTs [24]

. Therefore, graphene

aerogels (GAs) have been widely studied in recent years, as an alternative to the

CNT aerogels [13, 14]

. Unlike CNT aerogels, the GAs can be synthesized from

low-cost graphite at a temperature lower than 200 °C. The extraordinary

properties of graphene and the straightforward and relatively inexpensive

approach give the GAs great potential as the next-generation conducting

aerogels for various applications [15]

, such as energy storage devices [20]

,

actuators and sensors [25]

, and nanocomposites with multifunctional properties

[26].

1.1.3 Drying techniques of aerogels

The critical point drying (CPD), also known as supercritical drying, refers

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to a special process for creating aerogels by removing the background liquid

from the hydrogel in a gentle and controlled way. It has been widely used to

preserve the porous structures of samples in the production of aerogels,

biological specimens, and microelectromechanical systems (MEMS) [27]

. The

principle of CPD is illustrated in Figure 1.2.

In contrast to the evaporation in the ambient environment, in which surface

tension of the evaporation liquid causes distortion and shrinkage to the gel

network [28, 29]

, the CPD process can allow the liquid phase to pass through a

“supercritical region” instead of crossing the liquid/gas boundary. In the

supercritical region, distinct liquid and gas phases no longer exist, and thus

there is no surface tension applied to cause the collapse of the gel structure [30]

.

However, in practice, the substances which can be used for CPD are still

very limited. This is because most liquids require rather high temperature and

pressure to reach their critical points, which are dangerous and may also destroy

many organic gels. As liquid carbon dioxide (CO2) can be supercritically

extracted at a low temperature of 31.1 °C and a modest pressure of 72.8 atm, it

has been selected as the most common solvent for CPD [31, 32]

.

It also worth mentioning that, since liquid CO2 is immiscible with water,

an intermediate solvent exchange to ethanol, which can be completely miscible

with both water and liquid CO2, is usually required before the real CPD process

to dry hydrogels. The whole process of solvent exchange is carried out by

soaking the hydrogel samples in ethanol for at least several hours and changing

the ethanol at least three times [32]

. The gel after such solvent exchange is called

“alcogel”, and is ready to be subjected to CPD to yield its aerogel form.

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Figure 1.2 Principles of three drying methods (evaporation, freeze drying, and

CPD) to remove liquid from hydrogels in a generic phase diagram. (a) Direct

evaporation from liquid phase to gas phase causes collapse to the gel network

due to the effect of surface tension. (b) Freeze drying is a common method to

create aerogels. During this process, the samples are fast frozen and then placed

in a vacuum under raised temperature to allow the ice to sublimate. (c) In the

CPD process, the temperature and pressure of liquid carbon dioxide are raised

above its critical point to form a supercritical fluid. By slowly releasing the

pressure, the hydrogels are dried to aerogels with well-preserved networks. The

CPD process is selected as the drying method in this thesis work. Adapted from

the thesis work of Mateusz B. Bryning [33]

.

According to the generic phase diagram illustrated in Figure 1.2, freeze

drying is also a commonly used method to remove the liquid from hydrogels [34]

.

However, Zhang et al. [14]

reported that the aerogels dried by CPD could exhibit

a larger surface area and superior multifunctional property over those that

underwent freeze drying. Therefore, the CPD process has been selected as the

drying method in this thesis. All the CPD processes were completed in a

Tousimis Autosamdri-815, Series B super-critical dryer, following the

procedures recommended by the manufacturer.

1.1.4 General properties and applications of aerogels

Many aerogels have a combination of impressive material properties that

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other materials may not simultaneously possess. Specific formulations of

aerogels have extreme properties, such as the lowest bulk density (down to

0.00016 g/cm3)

[4], the largest specific surface area of any non-powder material

(as high as 3200 m2/g)

[35], the lowest mean free path of diffusion and dielectric

constant of any solid material [36]

, and the slowest speed of sound through any

solid material [37]

.

Aerogels are generally fragile. Inorganic aerogels are friable and can be

destroyed by bending or a gently applied force [38]

. Organic polymer aerogels

are slightly stronger than those inorganic aerogels. However, the strength of

most types of aerogels can possibly be improved by condensing them at the

expense of their lightweight and ultralow thermal conductivity [39]

.

The real applications of aerogels depend strongly on their various

exceptional properties and features. Table 1-1 below shows some applications

of aerogels, both general and specific. These applications which have been

either demonstrated or proposed previously, arise from the specific properties

or characteristics of the aerogels. In many cases, a specific application may only

be dependent on one single property even if the aerogels have multifunctional

properties which are appropriate to the given application [18]

.

Table 1-1 Identification of aerogel properties and features, with their

applications [18]

. (Reproduced with permission from Ref. 18. Copyright (1998)

Elsevier.)

Property Features Applications

Thermal

conductivity Best insulating solid

Transparent

High temperature

Lightweight

Architectural and

appliance insulation,

portable coolers, transport

vehicles, pipes, cryogenic,

skylights

Space vehicles and

probes, casting molds

Density/ Lightest synthetic solid Catalyst, absorbents,

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porosity Homogeneous

High specific surface area

Multiple compositions

sensors, fuel storage, ion

exchange

Target for ICF, X-ray

laser

Optical Low refractive index solid

Transparent

Multiple compositions

Cherenkov detectors, light

weight optics, light guides,

special effect optics

Acoustic Lowest sound speed Impedance matchers for

transducers, range finders,

speakers

Mechanical Elastic

Light weight

Energy absorber,

hypervelocity particle trap

Electrical Lowest dielectric constant

High dielectric strength

High surface area

Dielectrics for ICs,

spacers for vacuum

electrodes, vacuum display

spacers, capacitors

The second objective of this thesis work is the utilization of graphene

aerogels to synthesize novel nanocomposites. The next section will present a

brief introduction to nanocomposites.

1.2 Carbon-based nanocomposites

A nanocomposite refers to a composite material for which at least one

dimension of its one component is less than 100 nm, or a distance in nano scale

exists and repeats constantly between its multi-components. In a specific sense,

a nanocomposite is often taken to mean the combination of a bulk matrix and

one or more nanofillers (e.g. nanoparticles, nanosheets, or nanofibers). Because

of the high aspect ratio of the nanofillers, a nanocomposite can typically exhibit

properties in one order greater than those conventional composites [40]

.

To date, carbon-based nanofillers, especially CNTs and graphene, have

been extensively investigated as the multifunctional nanofillers for fabricating

polymer nanocomposites in both industrial and academic fields [41-43]

. However,

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due to the hydrophobicity and π–π interaction, a homogeneous dispersion of

these carbon nanofillers in the polymer matrix has always been a crucial issue

during the whole fabrication process [44, 45]

. Although many strategies [46, 47]

,

such as solvent processing, in situ polymerization and melt processing, have

been developed, the properties of these nanocomposites prepared through such

powdery dispersion methods are still far less than expected.

The aerogels presented previously may pave the way to motivate the

effective fabrication of the “multifunctional nanocomposite materials”. In

general, an aerogel can first be prepared and optimized as the nanofiller material,

after which the polymer matrix in a liquid or semi-liquid phase could possibly

be backfilled into its network under capillary force [48]

. For the GAs consisting

of graphene nanosheets in particular, this approach provides a novel route for

property enhancements of the graphene-based polymer nanocomposites.

1.3 Objectives of thesis

This thesis aims to achieve an effective morphology–control of the GAs

synthesized by chemical reduction method, and investigate the effects of the

GA morphology on their multifunctional properties. In order to provide the

thermal properties of the as-prepared GAs, a proper technique for thermal

characterization needs to be established. In addition, graphene nanosheets

commonly form agglomerations in the graphene–polymer nanocomposites,

severely limiting their effectiveness. To overcome such agglomeration

problem, a new route for fabricating the graphene-based nanocomposites

should be proposed. The specific objectives of this thesis are as follows:

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(a) Apply the mild chemical reduction method to fabricate GAs and backfill

polymer into the network of GAs to prepare GA–polymer nanocomposites

by in situ polymerization;

(b) Investigate the effects of synthesis conditions on the morphology and

multifunctional properties of the GAs;

(c) Develop an improved comparative infrared microscopy technique to

characterize the thermal property of the GAs;

(d) Develop and characterize the multifunctional property of GA–polymer

nanocomposites and evaluate how it solves the agglomeration problem of

graphene–polymer nanocomposites prepared by the traditional powdery

dispersion method.

This thesis work would provide a comprehensive and systematical study of

synthesis parameters on the multifunctional properties of the GAs. In particular,

it would provide the first benchmark data of the thermal property of GAs. The

development of GA–polymer nanocomposites may also solve the

agglomeration problem of graphene in the polymer matrix, which would

significantly enhance the multifunctional properties of graphene–polymer

nanocomposites.

It should be noted that this study is based on the selected synthesis method,

while effects of various different synthesis methods on the property of GAs or

GA–polymer nanocomposites are excluded. This work also mainly focuses on

the fabrication and property optimization of materials, rather than the

development of functional applications by the as-prepared materials. In addition,

only existing theoretical models are used to fit with the experimental data in this

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thesis, and there are no new models established.

1.4 Organization of thesis

This thesis is organized into the following chapters:

Chapter 1 introduces the motivations of this thesis and provides some

background on aerogels, in particular carbon-based aerogels.

Chapter 2 presents a specific literature review of the GAs and

graphene-based nanocomposites, including their structure, synthesis methods,

and multifunctional properties.

Chapter 3 provides a description of the materials, synthesis approach, and

characterization of the developed GAs and GA–PMMA nanocomposites in this

thesis. The improved comparative infrared microscopy technique for thermal

conductivity measurement is presented in detail.

Chapter 4 comprehensively investigates the effects of synthesis conditions,

reducing agents, and CNT inclusions on the morphologies, electrical property,

and thermal stabilities of the GAs. Additionally, the impact of a thermal

annealing treatment at 450 °C for 5h in an Argon (Ar) environment is also

studied. It has been found that the post-thermal annealing treatment and the

additional CNTs can enhance the electrical conductivities of the GAs up to a

factor of 5.

Chapter 5 investigates the thermal conductivities of the GAs with various

graphene volume fractions from 0.67 to 2.50 vol. %, with and without annealing

treatment, measured using a comparative infrared microscopy technique. This

is the first systematical study of the thermal properties of GAs, and the results

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elucidate the factors limiting their thermal conductivities. The developed

thermal measurement technique can be applied to other porous material

systems.

Chapter 6 presents the fabrication of GA–PMMA nanocomposites by

backfilling PMMA into the pores of the GAs. Due to the uniform distribution of

graphene nanosheets in the PMMA matrix, as graphene loadings increase from

0.67 to 2.50 vol. %, the nanocomposites exhibit significant increases in

electrical conductivities (0.160–0.859 S/m), microhardness (303.6–462.5 MPa),

and thermal conductivities (0.35–0.70 W/m·K) compared with pure PMMA

and the graphene–PMMA nanocomposites prepared by traditional dispersion

methods.

Chapter 7 summaries the major conclusions of this thesis and gives

suggestions for future research work.

The next chapter (Chapter 2) will present a detailed literature review of the

current progress that has been made with graphene, GAs and

graphene–polymer nanocomposites.

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CHAPTER 2: Literature Review

This literature review chapter includes separate sections on graphene,

graphene aerogels (GAs) and the graphene–polymer nanocomposites: each

section includes subsections addressing the structures, synthesis methods,

multifunctional properties and potential applications of the materials in

question.

2.1 Graphene

2.1.1 Introduction

Graphene is a two-dimensional (2D) planar sheet which is composed of a

monolayer of hexagonally packed carbon atoms in a honeycomb lattice. As

illustrated in Figure 2.1, it has generally been considered as the basic unit for all

graphitic carbon allotropes, e.g. wrapped up into zero-dimensional (0D)

fullerenes, rolled into one-dimensional (1D) carbon nanotubes (CNTs), or

stacked into three-dimensional (3D) graphite [24]

.

Figure 2.1 Graphene is the building block of all carbon materials, e. g. 0D

fullerenes, 1D CNTs, and 3D graphite [24]

. (Reproduced with permission from

Ref. 24. Copyright (2007) Macmillan Publisher Ltd.)

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Graphene was first isolated from graphite in 2004, using a “Scotch tape”

(or “peel-off”) method [49]

. Since its discovery, graphene has attracted

tremendous attention from both industrial and academic research, due to its

numerous remarkable properties [49-55]

. Defect-free graphene (or “pristine

graphene”) has demonstrated an optical transmittance of 98% [50]

, a large

specific surface area of 2630 m2/g

[51, 52], high electron mobility of 250,000

cm2/Vs at room temperature

[49, 53], an outstanding Young’s modulus of 1 TPa

[54], and superior thermal conductivity of 5300±480 W/m·K

[55]. These unique

intrinsic properties provide graphene with great potential for various

applications, such as field effect devices [56-58]

, transparent conductive films [59]

,

energy storage devices [60, 61]

, and nanocomposites [43, 45, 47, 62-66]

.

2.1.2 Structure of graphene

As shown in Figure 2.2, the honeycomb lattice structure of graphene is

composed of covalently bonded carbon atoms [52, 67, 68]

, with a C–C bonding of

0.142 nm in length. In this structure, all of these carbon atoms are sp2 hybridized

and arranged in a 1s2sp

1sp

1sp

12pz

1 configuration, such that each of them forms

three σ bonds and shares one π bond with its nearest neighbors [69]

. Theory

predicts that these shared π orbitals significantly contribute to the mechanical

stability of the carbon sheet and the delocalized network of electrons [52, 68-71]

.

Although ‘graphene’ refers to a monolayer of carbon atoms in concept,

common references, especially from the experimental point of view, also exist

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for bilayer, trilayer or few-layer graphene (3–10 layers)1

[72], where several

graphene monolayers stack following the stable orders in natural graphite as an

alternating (ABAB, Bernal type) or staggered (ABCABC, rhombohedral type)

arrangement [72]

with a layer spacing of 3.35 Å [73]

.

Figure 2.2 Scheme of the crystal structure, Brillouin zone, and dispersion

spectrum of graphene [52]

. (Reproduced with permission from Ref. 52.

Copyright (2010) Wiley–VCH.)

2.1.3 Synthesis methods of graphene

There are three common approaches available to synthesize graphene and

graphene-based nanosheets. The following review provides a detailed

consideration of the experimental procedures, strengths and drawbacks of each

technique.

Table 2-1 A comparison of strengths and drawbacks for the methods commonly

applied to synthesize graphene [68]

. (Reproduced with permission from Ref. 68.

Copyright (2010) Elsevier.)

Advantages Disadvantages

Mechanical

exfoliation

Low cost and easy

No special equipment required

Better contrast

Serendipitous

Uneven films

No large-scale production

CVD Even films

Large scale area

Difficult to control

High temperature process

1 In the later sections of this thesis, ‘few-layer graphene’ refers to thin graphene films from 1 to

10 layers.

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Chemical oxidation

and reduction

Large scale fabrication

Easy suspension handling

Fragile stability

Partial reduction

2.1.3.1 Mechanical exfoliation

The inter-layer Van der Waals interaction energy within graphite is 2

eV/nm2

[74]. Therefore, only a weak force of approximately 300 nN/μm

2 is

required to exfoliate its multilayers to form graphene [74]

. In 1999, Ruoff et al.

[75, 76] first reported the exfoliation of graphite by a micromechanical exfoliation

method, in which graphite crystals were obtained by manipulating

lithographically patterned arrays of graphite micropillars and repeatedly

exfoliating them with a sharp glass tip. Since then, this work has been

considered the foundation of the micromechanical exfoliation method to

fabricate graphene, and also a milestone in outlining of the potential importance

of graphene for various fundamental studies and applications [52]

.

The micromechanical exfoliation method was subsequently modified with

the micropillars of graphite mounted on an AFM cantilever with a purposely

chosen spring constant, so that the pressure and shearing force for exfoliation

could be carefully controlled [74]

. These top–down approaches in general allow

an arbitrary deposition of graphene, yet they cannot be used for fabricating

monolayer graphene or even few-layer graphene of thickness below 10 nm.

Monolayer graphene was first obtained by Novoselov and Geim in 2004 [49, 77]

.

A piece of Scotch tape was used to repeatedly stick and peel a 1-μm-thick

graphite flake, until very smooth and thin fragments were formed. Through

optical microscopy images, the obtained graphene could be subsequently

transferred to arbitrary substrates by gently pressing the tape.

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For such exfoliation methods, one great challenge resides in the

identification of graphene sheets from the isolated fragments. As the exfoliation

occurs, a large number of fragments can be formed with various layers of

graphene, ranging from 1 to 100 [78]

. Hence the detection of the graphene

monolayer from all the fragments remains difficult. One common method for

detecting the graphene monolayer is the utilization of an optical microscopy [79,

80]. A few previous studies

[24, 49, 53, 77] have shown that when a multilayer

graphene is deposited on a 300-nm-thick silica (SiO2) substrate, its color will

change from yellow to blue under the optical microcopy as its thickness

decreases. Accordingly, when the color appears to change from darker to lighter

shades of purple, few-layer and/or monolayer graphene is indicated, as

illustrated in Figure 2.3 [68]

. The visibility of the graphene originates from the

well-known interference phenomenon [78]

, and is considered definite evidence

of the presence of graphene monolayers. However, a high-quality interface

image is very sensitive to both the thickness and purity of the SiO2 layer, e.g. a

315 nm instead of 300 nm thick SiO2 layer fails to display any apparent contrast

[81]. Therefore, this optical microscopy technique has been gradually replaced

by the Raman spectroscopy technique in recent years, as the latter can provide

more information in terms of both number of layers and structural arrangement

[82]. Another shortcoming of the mechanical exfoliation methods, like the

Scotch tape method, is the presence of glue residue on the graphene sample [83]

,

which not only contaminates the graphene, but also limits its carrier mobility

and other properties [84]

.

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Figure 2.3 Mechanically exfoliated (a) multi-layer, (b) few-layer and

monolayer graphene. Yellow colors indicate multi-layer graphene of thickness

over 100 nm, while blue, darker, and lighter purple indicate few-layer and

monolayer graphene [68]

. (Reproduced with permission from Ref. 68. Copyright

(2010) Elsevier.)

In general, these mechanical exfoliation approaches may still be the best

ways to generate graphene of the highest electrical and structural qualities

required for fundamental studies. However, due to their time-consuming

process and low yield production, mechanical exfoliation methods are not

highly desired for a scale-up fabrication in practice [68]

. To enhance the ease of

graphene separation from graphite, a liquid-phase exfoliation method has been

developed based on the mechanical exfoliation. During this process, graphite is

dispersed in organic solvents to form suspensions, and the interlayer exfoliation

of graphite is then achieved in the organic suspensions via sonication and/or

centrifugation [85]

.

In 2008, Hernandez et al. [86]

first reported the separation of graphene

layers using N–poly–methylpirrolidon (NMP), in which graphite powders

sifted through a fine sieve were used as the initial material. These graphite

powders were dispersed in NMP to form a homogeneous mixture via sonication.

The mixture exhibited a grey-colored appearance and contained a number of

particles in macroscopic sizes. These particles were subsequently removed from

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the mixture by centrifugation. A homogenous dark-colored suspension with

only monolayer and few-layer graphene was finally obtained. The properties of

such a graphene–NMP suspension could remain stable for at least five months.

Other organic solvents, such as N, N–dimethylacetamide (DMA),

g–buthyrolactone (GBL) and 1, 3–dimethy1–2–imidasolidinon (DMEU) as the

surface active substances (SAS) for CNTs, have also been utilized in the liquid

phase exfoliation process [78]

. In addition, to improve the quality of the

as-prepared graphene, a post-treatment like thermal annealing at 1000 °C

followed by several purification steps [87]

could be performed to further bring

the graphene dispersed in the suspension to predominantly monolayer

graphene.

The utilization of liquid during exfoliation permits the penetration of

atoms or molecules into the interlayer space of graphite, thus leading to an

enhancement of its interlayer distance and a consequent decrease of the

interaction energy between its neighboring layers [78]

. Therefore, compared with

mechanical exfoliation, liquid exfoliation generally lowers the level of

difficulty in separating the graphite layers. Nevertheless, it still suffers the

disadvantages of being time-consuming and low-yielding, and the separation of

graphene from the organic solvents also remains challenging.

2.1.3.2 Chemical vapor deposition (CVD)

To date, chemical vapor deposition (CVD) is one of the most widespread

methods for the synthesis of carbon-based nanomaterials, such as carbon fibers,

CNTs and graphene. May et al. [88]

reported the observation of a ring-like

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low-energy electron diffraction pattern on a platinum substrate after thermal

annealing, yet at that time they did not ascribe it to a “monolayer of graphite”.

Later, Blakely et al. [89-92]

investigated the detailed thermodynamics of the

so-called “monolayer graphite” or “bilayer graphite” that was, however, formed

on nickel (Ni) (111) crystals, while the topic of “monolayer graphite” was

proposed as a sub-discipline of surface science for the first time.

So far, great progress has been made on the synthesis of graphene via CVD

processes [93-96]

. One successful example is the large-area growth of graphene

on silicon carbide (SiC) [94, 97, 98]

. When the SiC wafer undergoes thermal

treatment at ~1300 °C in a vacuum environment (or ambient pressure), very

thin graphene with only a few layers can consequently be formed over the

entire wafer. The formation of these graphene samples is considered a

combined result of the sublimation of Si atoms from SiC and the reorganization

and graphitization of the leftover carbon-enriched surface [99-101]

. With careful

control of the process, the graphene monolayer could even be obtained

occasionally through this thermal treatment process [97, 98]

. However, the

graphene obtained from this method exhibits only a misleading and loose

stacking of multilayer structures under Raman and scanning tunneling

microscope (STM) [102, 103]

. Therefore, in order to improve the quality of the

resultant graphene, the method of high-temperature graphitization of SiC still

needs to be modified further [100, 104-106]

.

Currently, the most effective CVD approach is based on the direct

decomposition of hydrocarbons on the metallic substrates [22]

. Land et al. [107]

reported that the decomposition of ethylene on Platinum (Pt) (111) substrates

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could result in the growth of uniformly distributed graphene islands in

nano-sizes, yet only the layers at their lower step edges appeared to be

continuous. To obtain large single-crystalline graphene, a similar CVD process

decomposing ethylene on Ruthenium (Ru) (0001) substrates was then

conducted by Stutter et al. [108]

The formation mechanism of graphene on

Ru(0001) surfaces was proposed to be analogous to that of the catalysis of

CNTs from transition metal particles [109]

. Ethylene works as the carbon source

in the CVD process and is first dissolved in Ru at 1420 K. As the temperature is

lowered to 1100 K, supersaturation of carbon atoms in Ru is then induced and

subsequently triggers the nucleation of graphene. It has been found that the

graphene formed on Ru(0001) substrates exhibits a large single-crystal with a

lateral dimension exceeding 100 μm. However, due to the strong interaction

between graphene and metal [110]

, the isolation of graphene from Ru(0001)

substrates is usually not easy. This in turn significantly restricts the size of

graphene and also limits the application of graphene for various devices.

Efforts have been made to transfer the epitaxial grown graphene onto

arbitrary substrates. Polycrystalline Ni films [111, 112]

and copper (Cu) [113]

are

applied as the catalyst materials, while centimeter-sized continuous graphene

can be obtained. The mechanism for graphene growing on Ni and Cu is similar

to the dissolution/precipitation mechanism in which Ru is applied as the

template [68]

. As for the substrate transfer, a thin layer of polymer is first coated

on the as-grown graphene, and then the entire sample is dissolved in a dilute

hydrochloric (HCl) solution to remove the Ni substrate [111, 112]

. Owing to the

good dissolubility of Ni in HCl, the metal substrate is easily released. Thereafter,

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the isolated graphene with polymer coating is attached to the target substrate by

careful pressing, and its polymer coating is eventually removed via immersion

in the organic solvents, e.g. acetone or isopropanol.

Although the CVD process has shed some light on the fabrication of

high-quality graphene over a large area, it still remains challenging to produce

graphene on an industrial scale. In addition, CVD growth of graphene requires

rather expensive templates, and this cost is intrinsically unnecessary for most

low-performance devices. As a result, chemical oxidation and reduction

methods have been developed to produce reduced graphene oxide (rGO), which

is widely considered an alternative to graphene and can be used for most

low-performance applications.

2.1.3.3 Chemical oxidation and reduction

The concept of chemical oxidation/reduction methods to synthesize

graphene basically involves the weakening of the Van der Waals force between

the interlayers of graphene upon insertion of functional groups. When graphite

is oxidized to graphite oxide, its sp2 lattices are partially degraded to sp

2–sp

3

bondings, which consequently reduce the stability of π–π stacking. Following

this, the exfoliation of graphite oxide to graphene oxide (GO) is usually carried

out in suspension under sonication, while the reduction of GO to rGO can be

completed with various reducing agents such as hydrazine and L-ascorbic acid

[114]. Therefore, chemical approaches offer a straightforward and effective route

towards the mass production of graphene [115]

.

The oxidation of graphite can be dated back to the time when Brodie

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determined the mass of a carbon atom [116]

. It was found that when potassium

chlorate was intercalated in concentrated sulphuric acid and nitric acid, graphite

flakes containing hydroxyl and carboxyl carbon sheets could be produced, with

a large amount of heat released. At that time, these carbon sheets were called

“graphitic acid”, which is basically equivalent to “graphite oxide” today. At

present, the most famous method to synthesize graphite oxide is the one

developed by Hummers et al. [117]

, in which graphite is dispersed into a mixture

of concentrated sulfuric acid (H2SO4), sodium nitrate (NaNO3) and potassium

permanganate (KMnO4), and the mixture is kept at ~45 °C for several hours.

This method has been widely applied for years to fabricate graphite

intercalation compounds, while the products have been commercialized and are

well known as the “Expandable Graphite” [85, 118]

. The volume of the

expandable graphite is over 100 times larger than that of raw graphite, and thus

it becomes a common precursor for the fabrication of GO or rGO.

The exfoliation of graphite oxide to GO could be achieved by various

approaches, such as thermal treatments, sonication or microwaves [119]

. As early

as 1962, a rapid thermal annealing at 1050 °C was applied to split graphite

oxide, and individual sheets were obtained and observed under TEM [120]

.

However, due to its facile processing, sonication has become the current most

popular method, in which the interlayer separation of graphite oxide can be

efficiently fulfilled by sonicating a 0.1–0.5 wt. % suspension for about 12

hours.

The resultant GO aqueous suspensions are usually in yellow and can

remain stable for at least one week. The stability of the GO suspensions can be

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ascribed to the effect of electrostatic repulsion. In order to further stabilize the

suspensions, some cationic polyelectrolytes such as polyaniline [121]

,

single-stranded DNA [122]

, or polystyrene sulfonate [114]

, and some surfactants

such as polystyrene [123]

, may also be employed. The GO solids can finally be

collected as thin films by deposition [50, 124]

, or as powders by freeze drying.

However, as large numbers of sp3 carbon are present in GO, it intrinsically

exhibits different properties compared with those of the graphene obtained by

mechanical exfoliation or CVD growth. To recover its electrical conductivity

and other properties, a reduction process, either via chemical [114]

or thermal [125]

approaches, is therefore required. Nevertheless, these reduction approaches can

only result in a partial recovery of sp2 configuration, and the rGO products tend

to agglomerate if the reduction is processed in liquids.

2.1.4 Properties of graphene

In recent years, there has been much interest in the development of

graphene and graphene-based materials. This is mainly due to the unique

multifunctional properties that graphene exhibits.

2.1.4.1 Electrical properties

Experimental measurements have shown that, for any graphene obtained

by micromechanical exfoliation, its electron mobility can exceed 2000 cm2/Vs

at room temperature. Similar to CNTs, the electrical conductance in graphene

can also be ascribed to a ballistic transport mode on a scale of ~16 μm [126]

.

Within this length, the electrons in graphene are able to travel without scattering,

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which leads to its exceptional high change carrier mobility. Otherwise, the

mobility shows a weak dependence when temperature ranges from 10 to 100K,

implying a scattering mechanism solely dominated by its structural defects [127]

.

As the impurities in graphene are minimized by current annealing,

mobility over 25,000 cm2/Vs can be obtained

[128], while with the improvement

of screening technique and skills of substrate removal, a further enhancement is

also possible. Bolotin et al. [84, 129]

have reported a mobility value exceeding

200,000 cm2/Vs for suspended and annealed graphene, which, however, was the

intrinsic limit caused by the scattering of acoustic photons at room temperature

[83, 130]. This remarkable high value is noted to be 10 times greater than that of

copper [131]

. When this mobility is converted to resistivity, a value on the order

of 10-6

Ω·cm is accordingly extracted, which has been considered the lowest

room temperature resistivity ever known. However, the epitaxial grown

graphene typically exhibits a slightly lower electron mobility, which is on the

order of thousands of cm2/Vs

[132], while for the chemically derived graphene

products, their electron mobility only lies on the order of several hundred

cm2/Vs

[133].

2.1.4.2 Mechanical property

As graphene and carbon nanotubes have intrinsically similar lattice

structures, their mechanical properties, such as Young’s modulus and strength,

are generally comparable. The mechanical properties of monolayer and

few-layer graphene have been extensively reported, from both experiments and

modelling.

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The current widespread values for the Young’s modulus (~1.0 TPa) and

fracture strength (~130 GPa) of the free-standing monolayer graphene were first

measured by Lee et al. [54]

in 2008. A combined technique of nanoindentation

and AFM was applied as illustrated in Figure 2.4 below. From their tests, the

measured stiffness and breaking strength of graphene were 300–400 and ~42

N/m, respectively. After being converted by division with the thickness of the

graphene monolayer, the values were found to be very close to the theoretical

values predicted for bulk graphite [54, 134]

.

Figure 2.4 (a) A SEM image of a monolayer graphene suspended on an array of

circular holes, scale bar: 3μm; (b) A scheme of nanoindentation on the

membrane of graphene [54]

. (Reproduced with permission from Ref. 54.

Copyright (2008) AAAS.)

For chemically derived graphene, i.e. rGO, which is reduced by

hydrogen plasma, the Young’s modulus can only reach one fourth that of

mechanically exfoliated graphene, ~0.25±0.15 TPa [135]

, while its breaking

strength has not been documented yet. Despite their distinctly different

electrical properties, rGO does not show significantly greater mechanical lag

(where mechanical properties are concerned) than the graphene obtained by

mechanical exfoliation. As a result, given its low cost and high mass production,

rGO can be a promising candidate for a reinforcement material [136, 137]

.

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2.1.4.3 Thermal property of graphene

Base on the estimation by the Wiedemann-Franz law, the contribution

from electrons to the thermal transport in graphene is almost negligible [138]

. The

thermal conductivity of graphene is therefore dominated by the transport of

phonons, which conduct by diffusion at high temperatures and ballistic mode at

low temperatures.

For the pristine graphene, its thermal conductivity (k) has been found to be

proportional to temperature (T) when T is beyond 100 K. Molecular dynamics

(MD) simulations predict a thermal conductivity of 6,000 W/m·K for the

suspended monolayer graphene [21]

, which is dramatically higher than that of

graphitic carbon. Besides the effect of temperatures, many other intrinsic

factors of graphene, such as its dimensions, edge roughness [139]

and edge

shapes [140]

, also significantly impact its thermal property. It has been found that

k follows a power law relationship with the length L, and the exponent lies in the

range of 0.3–0.5 at room temperature.

So far, the most widely accepted thermal conductivity of the pristine

graphene (5,300 W/m·K) is obtained based on the shift of G band from its

Raman spectrum, where the frequency of G peak is measured as a function of

excitation power and the thermal conductivity of graphene is extracted from the

slope of its trend line [141]

. Substrate attachment also plays a significant role in

the thermal conductivity of mechanically exfoliated graphene. When it is

deposited on SiO2 substrates, its thermal conductivity rapidly goes down to

~600 W/m·K, due to the severe phonons leaking and scattering at

graphene-substrate interfaces [141]

.

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For the graphene synthesized by CVD, a thermal conductivity of ~2500

W/m·K has been reported [142]

, while for chemically derived graphene, there

have been no values reported beyond 10 W/m·K [143, 144]

. In accordance with

these results, the thermal conductivity of graphene is largely determined by the

abundance of sp2 bonds. Therefore, post treatments, such as thermal annealing

[145, 146], plasma annealing

[147], or chemical purification

[87], are effective

approaches for the thermal property enhancement of graphene.

2.1.5 Potential applications of graphene

Because of its outstanding and multifunctional properties, graphene has

become an idea candidate for various applications.

Firstly, as graphene possesses a unique band structure, its electrons and

holes can be highly tunable by a gate electrical field [49]

. Several works have

reported the development of graphene-based field effect transistors (FETs) with

a single black gate [49, 53, 148]

. Levendorf et al. [149]

have proposed the scaled-up

fabrication of graphene transistors based on the epitaxial grown graphene on Cu.

In addition, Lin et al. [150]

have reported the development of high-frequency

(~26 GHz) FETs using top gate geometry. When a polymeric buffer layer was

added between the epitaxial graphene and conventional gate dielectrics, FETs

with cut-off frequencies at ~100 GHz were successfully obtained.

Secondly, due to its high electrical conductivity and extraordinary optical

transmittance in the range of visible wavelengths, graphene also shows great

potential as an important precursor material for fabricating transparent

conductive films (TCFs). Aimed at large scale fabrication, reduced graphene

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oxide is commonly applied instead of mechanically exfoliated or epitaxial

grown graphene. In addition, various techniques such as vacuum infiltration,

spray coating, spin coating, dip coating etc. have also been employed. Li et al.

[87] reported the preparation of TCFs by Langmuir–Blodgett (LB)–assembling

rGO. The resultant films exhibited a sheet resistance of 8 kΩ and 83%

transparency at 1000 nm wavelength. De et al. [59]

prepared TCFs by directly

sonicating the raw graphite in organic solvents and depositing the dispersions

by vacuum infiltration. The as-prepared films showed a sheet resistance of ~3

kΩ and ~75% transmittance at 550 nm wavelength.

Thirdly, graphene is also a promising candidate for energy storage devices,

due to its large surface area (2630 m2/g) and excellent electrical properties

[60, 61].

So far, there have been many works covering the use of graphene for energy

storage, especially as the electrode materials for electrochemical double layer

capacitors (EDLCs) [151]

. For the electrodes made of rGO reduced by

microwave irradiation or thermal treatment [119]

, high capacitances of up to 190

and 120 F/g have been achieved in aqueous and organic electrolytes

respectively.

In addition, graphene and graphene-based materials have also attracted

extensive attention as fillers in developing graphene–polymer nanocomposites,

which will be reviewed separately in Section 2.4 with more details.

2.2 Graphene aerogels (GAs)

2.2.1 Introduction

As early as 2002, a self-assembly process of three-dimensional (3D)

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carbon foams was first proposed based on the nanostructured graphite [152]

.

Later, as knowledge of graphene increased, various easier methods to expand

the interlayers of graphite were developed [85, 118]

. Therefore, the direct

preparation of 3D carbon foams using graphene or graphene-based nanosheets

has become attractive in recent years. At present, the reported methods for

fabricating GAs can in general be classified into two categories: with the use of

binders and without the use of binders. Common binders are polymers, such as

polyvinyl alcohol (PVA) [11]

, resorcinol–formaldehyde (RF) [153, 154]

,

ferrocene–grafted poly (p–phenyleneethynylene) (Fc–PPE) [12]

,

and poly

(3,4–ethylenedioxythiophene) (PEDOT) [155]

. The binderless methods can also

be further classified into several sub-categories, like hydrothermal [156]

and

chemical reduction [145, 157]

. However, regardless of which synthesis methods

are used, critical point drying (CPD) or freeze drying must be applied to

preserve the gel structures. After being dried, the resultant GAs combine the

multiple excellent properties of graphene with the high porosity of aerogels,

thus offering a number of outstanding properties, such as extremely low density,

large surface area, super hydrophobicity, and good mechanical properties. So

far, they have been successfully applied to various applications, such as

electronics [158]

, energy storage devices [159, 160]

, catalysis [161]

, and composite

materials [48]

.

Due to its ease of fabrication and dispersion capability, GO (as described

in Section 2.1.3.3) has become the most popular reactant in the graphene family

(pristine graphene, epitaxial grown graphene, etc.) for synthesizing GAs. The

next section provides a brief introduction to the GO, followed by a detailed

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literature review of work concerning GAs.

2.2.2 Graphene oxide (GO)

As described in Section 2.1.3.3, graphene oxide (GO), the intermediate

material of rGO before reduction, is considered oxidized graphene having

various reactive oxygen functional groups such as carbonyl, hydroxyl, and

epoxide groups on its surface. It is normally obtained from the oxidative

treatments of graphite and successive exfoliation. As expected, the oxygen

content of the GO, or the C: H: O compositions, exhibits slightly different

through varying procedures. However, a C: O ratio of ~2:1 has been found to be

the upper limit of the overall extent of oxidation, regardless of one-stop or

multiple oxidation approaches [85, 116-118]

.

Due to its complexity and variability (even from sample to sample), the

structural features of GO have remained debatable for many years, and even

until today. The current most well-known model was proposed by Lerf and

Klinowski [162, 163]

, and is shown in Figure 2.5 below. Two sub-models, one

incorporating the existence of carboxylic acid groups and one not, are presented.

The dominant sub-model largely depends on the operative oxidizing conditions.

Apart from the Lerf-Klinowski model, other models such as the Hofmann [117]

,

Ruess [164]

, and Nakajima-Matsuo [165, 166]

models, and modifications [167, 168]

of

the Lerf-Klinowski model, have also been proposed to explain the structure of

GO. However, the differences in raw materials and reaction pathways upon

oxidation cause substantial variance in their exact structures and properties, and

thus difficulties with the identification of a unique structural feature of the GO

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remain [169]

.

Figure 2.5 Two sub-models of the Lerf-Klinowski model with (top) and

without (bottom) the presence of carboxylic acid groups on the periphery of the

graphitic basal plane of GO [162, 163, 169]

. (Top: Reproduced with permission from

Ref. 162. Copyright (1998) American Chemical Society. Bottom: Reproduced

with permission from Ref. 163. Copyright (1998) Elsevier.)

To date, there have been many approaches proposed for the preparation of

GO. Among them, the most popular one is the modified Hummers’ method [117]

,

which applies a combination of potassium permanganate (KMnO4) and

concentrated sulfuric acid (H2SO4) to oxidize graphite. Operative procedures of

the Hummers’ method will be presented step by step in Section 3.2.1 and thus

not described here. Notably, the starting material commonly used to synthesize

GO is the graphite flake, which contains numbers of localized defects in its π

lattice serving as the seed for oxidation [170]

. Due to the abundance of

oxygen-containing functional groups, GO possesses good hydrophilicity in

water and aqueous liquids [162, 171]

. It has been deduced that the strong bonding

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between water (H2O) and the basal lattice of GO is dominated by the oxygen in

its epoxides, as illustrated in Figure 2.6.

Figure 2.6 Schematic of hydrogen bonding formed between water (H2O) and

the oxygen-containing functional groups of GO [169]

. (Reproduced with

permission from Ref. 169. Copyright (2010) The Royal Society of Chemistry.)

Although these functional groups provide GO with a good hydrophobicity,

they also disrupt the sp2 network of the graphitic lattice, consequently resulting

the GO in an electrically insulating material with a conductivity of

0.0206±0.002 S/m [125]

. As presented in Section 2.1.3.3, a reduction process,

either chemical [114]

or thermal [125]

, has been found to be conducive to the

partial recovery of the conductivity of GO . However, as the oxidation process

itself is detrimental to the graphitic lattice planar [125, 172]

, the multifunctional

properties of rGO are generally similar to, but expectedly fall behind, those of

the pristine graphene.

In terms of the synthesis of GAs, GO obtained through chemical

conversion is still the most commonly used starting material, owing to its facile

preparation, excellent hydrophobicity, and other good properties. In addition,

its chemical and thermal reduction routes also pave the way to different

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synthesis methods of the GAs, which will be presented in detail in Section 2.2.4.

Above all, the presence of functional groups on GO facilitates its multiple

chemical transformations to synthesize graphene-like materials including GAs,

thus offering great potential for various large scale applications.

2.2.3 Structure of GAs

Similar to most other aerogels such as silica aerogels, carbon aerogels and

CNT aerogels, GAs are also constructed by their substance, i.e. graphene, but in

the form of interconnected networks. As shown in Figure 2.7(a), the GAs are

intrinsically highly porous, and graphene nanosheets are randomly distributed

within their frames. So far, the graphene type used to build the blocks of GAs is

mostly rGO, rather than mechanically exfoliated graphene or epitaxial grown

graphene. This is not only due to the low cost and high production rates of rGO,

but also because rGO nanosheets themselves are able to self-assemble upon

reduction [114]

. Figure 2.7(b) shows the thickness of an rGO monolayer, close to

1nm. Although this value is nearly 3 times higher than the theoretical thickness

of the pristine graphene, such a nanosheet is still widely acceptable as the basic

unit of GAs, given the presence of functional groups, such as hydroxyl,

carboxyl and epoxide groups, on its surface [157]

.

The morphologies of the GAs are significantly affected by their synthesis

routes, including the method selected and its reaction conditions [173, 174]

. The

GAs usually have surface areas in the range of 100–1200 m2/g

[174, 175], which

are lower than that of monolayer graphene (~2630 m2/g), indicating that overlap

of varying severity occurs with the graphene nanosheets in GAs [61]

. A

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systematic study of the relation between the morphologies and reaction

conditions of the GAs has been conducted for this thesis, and will be presented

in Chapter 4.

Figure 2.7 (a) A typical SEM image which shows the structure of GAs. (b)

AFM images of typical building blocks of the GAs [157]

. (Reproduced with

permission from Ref. 157. Copyright (2011) Elsevier.)

2.2.4 Synthesis methods of GAs

2.2.4.1 Crosslinking induced method

Inspired by the synthesis of organic (resorcinol (R)–formaldehyde (F))

aerogels, Worsley et al. [153, 175]

reported the synthesis of ultralow-density GAs

using R and F as an organic binder that is to produce carbon cross-links between

graphene nanosheets. In this method, the gelation process exactly follows the

procedures to prepare R–F organic aerogels [8]

, except that GO is first dispersed

in the aqueous solutions of R and F. After the processes of solvent exchange and

supercritical drying (or freeze drying), the resultant dry gels are basically

GO–RF aerogels. A pyrolysis at 1050 °C under inert gases was subsequently

required to carbonize the GO–RF aerogels into carbon-based GAs. Besides RF,

other polymers such as PVA/poly (styrenesulfonate) (PSS) [122]

and pluronic

copolymers [176]

have also been reported as the binders to stabilize GO and

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fabricate GAs. However, as most of these binders used for linking graphene

nanosheets are toxic polymers and an extremely high temperature, over 1000

°C, is required for their carbonization, this method has been largely replaced by

several binderless methods.

Tang et al. [177]

and Jiang et al. [178]

developed an ion linkage method to

induce crosslinks between the graphene nanosheets. Under a hydrothermal

process, noble particles are present in situ and facilitate the nucleation and

assembly of the graphene nanosheets. Within the GAs, these particles also play

a role to decorate the GAs, rather than only serving as a binder. Therefore, these

embedded particles can give the resultant GAs further potential for various

functional applications, such as sensors [179]

and catalysis [180]

.

2.2.4.2 Hydrothermal method

In 2011, Xu et al. [156]

reported a one-stop hydrothermal technique to

prepare binderless GAs. A GO aqueous suspension of 2 mg/ml was sealed in a

Teflon-lined autoclave and heated at 180 °C for 12 h. After this hydrothermal

process, graphene hydrogels were formed as a result of hydrothermal reduction

and by physical links via π–π interaction. Finally, these hydrogels needed to

undergo solvent exchanges and either supercritical drying or freeze drying to

yield the GAs.

Based on this hydrothermal method, Nguyen et al. [174]

conducted a similar

synthesis process to investigate the effects of GO concentrations and

hydrothermal treatment time on the morphologies of the as-prepared GAs. It

was found that the surface areas and total pore volumes of the GAs increased

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with the increase in GO concentration, but decreased with the increase in

treatment time. However, when the GO concentration was lower than 0.5

mg/ml, GAs could not be formed during such a hydrothermal process [156]

.

Since its development, the hydrothermal method has been considered a very

effective approach to synthesize binderless GAs. However, its requirements for

high temperatures and high pressure during the operation may still strongly

limit its potential to be scaled up.

2.2.4.3 Chemical reduction method

Zhang et al. [14, 157]

reported an easy and environmental-friendly method to

synthesize GAs. The operation of this synthesis process is quite simple. GO

nanosheets were first dispersed in DI water to form aqueous suspensions, and a

reducing agent such as LAA was then added to the suspension. After being kept

still for several hours either at room temperature or low temperatures below 100

°C, graphene hydrogels were then formed via the self-assembly of graphene

nanosheets. After that, solvent exchanges and supercritical drying (or freeze

drying) were also needed to dry these hydrogels to aerogels.

As with the hydrothermal method presented above, the reaction conditions

of this chemical reduction process also significantly impact the morphologies

and properties of the GAs. Chen et al. [145]

investigated the effects of various

reducing agents on the gelation time required to form the graphene hydrogels.

They found that the gelation of L-ascorbic acid (LAA)– and sodium sulfide

(Na2S)–reduced samples took only 10 min, while the sodium hydrogen sulfite

(NaHSO3)-reduced ones took 30 min. The lowest GO concentration needed to

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form hydrogels was reported by Zhang et al. [181]

, where the gelation of rGO

nanosheets was successfully achieved via the reduction of the GO concentration

of as low as 0.1 mg/ml using oxalic acid and sodium iodide (NaI).

This chemical reduction method is considered a mild and ‘green’ way to

fabricate the GAs. However, at present, very few studies have been conducted

on the effects of synthesis parameters on the morphology and multifunctional

properties of the resultant GAs. The impact of different reducing agents on the

GA nanostructures has also yet to be investigated.

2.2.4.4 Other synthesis methods

Besides the three methods described above, there are also several other

methods to synthesize the 3D structures of GAs. When the GO concentration is

high enough (e.g. 30 mg/ml), it can self-gelate to hydrogels via partial π–π

stacking with the aid of a prolonged sonication [182]

. However, due to the

abundance of functional groups on the GO, it is usually difficult to achieve high

electrical conductivities and mechanical strengths for these aerogels after

supercritical/freeze drying.

A free-standing monolith of the graphene network can also be obtained via

a CVD process on various templates such as Ni or Cu foams [183]

, nanosilica [184]

,

and zinc oxide (ZnO) tetrapods [185]

, which basically follows the CVD of

hydrocarbons to produce graphene. After graphene is successfully formed on

these templates, acids can then be applied to remove the corresponding

framework materials, consequently leaving the 3D architectures of graphene.

Although this CVD method can yield graphene of relatively high quality,

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suitable templates for the growth of the desired graphene networks are usually

difficult to find.

Another template-direct method can be achieved by directly freeze drying

the GO suspensions [186, 187]

, which is also known as the “ice template” method.

He et al. [187]

reported a systematic study to investigate the effect of freezing

routes on the structures and properties of the aerogels. Interestingly, they even

obtained the GAs with highly ordered pores, under a unidirectional freezing

condition.

2.2.5 Properties of GAs

The multifunctional properties of GAs strongly depend on their synthesis

methods and structures. The following sections present a major review of the

electrical, mechanical and thermal properties of the GAs.

2.2.5.1 Electrical property of GAs

Due to different synthesis methods and measurement techniques, the

electrical conductivities of GAs are reported to be within a large range of

0.1–100 S/m [145, 156, 175, 188]

. For the GAs synthesized with the R-F method, a

remarkable electrical conductivity of up to 87 S/m [188]

is obtained by a

four-probe technique, while the electrical conductivity is only ~0.1 S/m [156]

for

the hydrothermally synthesized samples measured by a two-probe technique.

Such large variations may be partly due to the characterization methods, as

contact resistance may probably exist in the two-probe technique. Apart from

this reason, the different bondings formed during different synthesis approaches

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of GAs should be intrinsically responsible for their conductivities [15]

.

Efforts [145, 189]

have also been made to investigate the effects of drying

methods and reducing agents on the electrical properties of GAs. It has been

found that supercritical drying could yield a more conductive sample compared

with freeze drying [189]

, while the utilization of a more efficient reducing agent

would also ensure the GAs with a higher electrical conductivity [145]

. To further

enhance the electron transfer in GAs, post treatments such as thermal annealing

under inert gases could be performed on the as-prepared GAs. It has been

reported that the functional groups on GO could be effectively removed by

thermal treatments above 200 °C [190]

. Therefore, annealing the GAs in an inert

environment could further purify the graphene sheets and increase their

electrical conductivity. Chen et al. [145]

reported that a thermal annealing

process at 400 °C enhanced the electrical conductivity of the GAs up to nearly 5

times.

2.2.5.2 Mechanical property of the GAs

Since GAs are constructed from individual pieces of rGO, their

mechanical properties, including Young’s modulus and strength, are far less

than that of the graphene monolayer [54]

. Therefore, the GAs are usually

addressed to be fragile and brittle, and polymer binders may be needed to

reinforce their networks. Nevertheless, given the extremely low densities of the

GAs, their specific strength would become impressive. For example, the GAs

reduced by LAA and dried by supercritical CO2 have been reported to be able to

support over 14,000 times their own weights with little deformation [14]

. In this

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same work [14]

, different drying methods were also performed and compared to

study their effects on the mechanical performance of GAs. It has been found

that those GAs processed by freeze drying can only support 3,300 times their

own weight, 4 times less than those dried by supercritical CO2 [14]

.

Due to the ease of operation, most mechanical properties of the GAs are

obtained from their compressive tests. The compressive stress-strain curves of

GAs can usually be divided into 3 regions: the elastic region, yield region and

densification region [145]

. The elastic region lies at low compressive strains

where the GAs elastically behave. The region from the end of the elastic region

to ~60% compressive strains is usually considered the yield region, where the

nano-sized pores in the GAs start to collapse and the increase in stresses appears

to slowly accelerate. Finally, the densification region is defined as the region

from ~60% compressive strains onwards, where almost all the pores have

collapsed and the GAs are completely hardened by the further compression.

From the compressive tests, the measured Young’s modulus and strength of

GAs normally vary from 0.26–20 MPa and 0.042–2.2 MPa, respectively [25, 156,

191].

2.2.5.3 Thermal property of the GAs

GAs with continuous scaffolds and mesoporous structures may reduce the

internal thermal resistance and enhance the thermal efficiency of TIMs.

However, studies of the thermal transport in GAs still remain very limited.

Zhong et al. [192]

reported the thermal conductivity of a GA sample with ~11

vol. % graphene and a relatively low surface area (~43 m2/g) to be 2.18 W/m·K

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using the laser flash technique.

To characterize the thermal conductivities of nanostructured materials [193]

,

several measurement techniques have been developed, including the laser flash

technique [192, 194, 195]

, steady-state measurement techniques [196, 197]

, transient

techniques [198, 199]

, and infrared (IR) microscopy techniques [62, 200, 201]

. IR

microscopy has several advantages over the other methods as it uses the

non-contact, two-dimensional temperature mapping, eliminating the need for

intrusive temperature sensors, and is a direct measurement of thermal

conductivity (e.g. it does not require information about the specific heat and

density). IR microscopy techniques have been utilized to measure the effective

thermal conductivities of a bulk material [62]

and thermal resistances of

commercial TIMs [201]

with a reported approximated uncertainty of 10%. For

thermal conductivity measurements in particular, the heat flux can be extracted

even more accurately with the employment of reference materials based on a

comparative method similar to the ASTM E1225 standard. However, the

utilization of IR microscopy techniques to measure the thermal conductivities

of GAs has not been reported yet.

2.2.6 Potential applications of GAs

Because of their large surface areas and good electrical conductivities,

GAs have attracted great interest in the area of energy storage, especially as the

electrode materials for supercapacitors. Meng et al. [19]

prepared alkali-treated

GA electrodes in supercapacitor cells, and their specific capacitance was

measured to be 122 F/g at a discharge currency density of 50 mA/g. Sun et al.

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[202] tested the electrochemical performance of GAs in a propylene carbonate

electrolyte and obtained a specific capacitance of 140 F/g at a current density of

1 A/g. In addition, Zhang et al. [203]

assembled the supercapacitors using a GA

synthesized via hydrothermal process and reported an even higher specific

capacitance of 220 F/g at 1 A/g. These supercapacitors were also found to be

highly stable, and still retained 92% capacitance after 2000 cycles.

GAs can also be used as a thermal enhancer and container for phase change

materials. The GA–octadecanoic acid (OA) composites have been found to

effectively enhance the thermal conductivity of OA by ~14 times, and their

latent heat is close to the value of pure OA [192]

. Many other research works have

used GAs as absorbents [204]

, stain sensors [205]

, and fire-resistant materials [13]

.

Up to now, efforts are still being made to improve the multifunctional properties

of GAs, which will promisingly push the GAs forward to more practical

applications in the future.

In addition, the emergence of the GAs may also provide a new type of

reinforcement material to solve the aggregation problems in composites. A

uniform distribution of graphene fillers in the composites can probably be

achieved by backfilling polymer matrices into the pores of the GAs.

Nevertheless, the development of GA-based nanocomposites has not been

widely reported so far. A comprehensive study of the GAs and the development

and optimization of GA–PMMA nanocomposites would therefore be essential.

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2.3 Graphene–carbon nanotube (CNT) hybrid aerogels

2.3.1 Introduction

As both graphene and CNTs have similar extraordinary electrical,

mechanical, and thermal properties [206, 207]

, efforts have also been made to

combine them to achieve a synergistic effect [208, 209]

. So far, graphene–CNT

hybrid aerogels, 3D networks of graphene combined with CNTs, have been

successfully developed by many groups worldwide, showing good performance

in various applications, such as for lithium ion batteries [210]

, transparent

conductors [211]

, and capacitive deionization (CDI) electrodes [157, 212]

for water

purification.

2.3.2 Structure of graphene–CNT hybrid aerogels

The networks of GAs are formed by the self-assembly of graphene

nanosheets due to hydrophobicity and π–π interaction. Herein, for these

graphene–CNT hybrid aerogels, as shown in Figure 2.8 below, CNTs are most

physically wrapped in the GA networks, without inducing any structural change.

However, their existence may possibly prevent the stacking of graphene

nanosheets and, remarkably, enhance the surface areas of the GAs. Recently,

the formation of in situ chemical bonding between graphene and CNTs has been

reported by Yan et al. [209]

. A carefully controlled hydrothermal process has

been found to result in a removal of most functional groups and defects in both

the graphene nanosheets and functionalized CNTs. Therefore, these two carbon

allotropes can possibly be bonded after the simultaneous reduction.

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Figure 2.8 SEM images showing the network structures of graphene–CNT

hybrid aerogels [157]

. (Reproduced with permission from Ref. 157. Copyright

(2011) Elsevier.)

2.3.3 Synthesis methods of graphene–CNT hybrid aerogels

The synthesis of graphene–CNT hybrid aerogels can basically follow all

the approaches to synthesize GAs [153, 156, 157]

. Among them, the chemical

reduction method is usually selected for its facile operation and high-quality

production [157, 212]

. For a typical procedure, CNTs are first dispersed in a GO

aqueous suspension by sonication, while the mixture is then reduced by

reducing agents, such as L-ascorbic acid (LAA) or hydrazine hydrate. It has

been found that CNTs can be well dispersed in the precursors with the presence

of GO nanosheets. Therefore, the existence of a synergistic effect between

CNTs and graphene is accordingly proposed. Besides the chemical reduction

method, there some works also report the synthesis of graphene–CNT aerogels

by directly freeze drying the CNT–GO mixture [4]

, or using a hydrothermal [209]

or two-step CVD method2

[213]. Further details of these methods can be found in

Section 2.2.4.

2 In fact, the CVD approach can only lead to the formation of macroporous structures, instead

of aerogels.

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2.3.4 Properties and potential applications of graphene–CNT hybrid aerogels

It has been found that the CNTs incorporated into GAs can serve as a

bridge between the graphene nanosheets [210]

. Therefore, such hybrid materials

not only get access to the more effective electron transfer, but also minimize the

agglomeration problems of CNTs/graphene, and further increase their surface

areas. As addressed by Yoo et al. [210]

, the incorporation of CNTs with graphene

nanosheets can effectively increase the layer distance between the graphene

sheets (as shown in Figure 2.9 below), thus increasing the specific capacity of

lithium ion batteries up to ~5 times. In addition, the transparent conductive

films (TCFs) developed by combining CNTs with chemically derived graphene

can exhibit an electrical resistance of 240 Ω at 86% transmittance, which is very

impressive and almost comparable to the performance of commercial indium tin

oxide (ITO) [211].

Figure 2.9 Relationship between d spacing of graphene nanosheet (GNS)

families and graphite [210]

. Addition of CNTs and fullerene (C60) was found to

effectively increase the interlayer spacing of graphene. (Reproduced with

permission from Ref. 210. Copyright (2008) American Chemical Society.)

The most recently developed graphene–CNT hybrid aerogels show a large

surface area of 435 m2/g and high conductivity of 7.5 S/m

[212]. When used for

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water purification, they surprisingly provide a desalination capacity of 633.3

mg/g, with the concentration of sodium chloride (NaCl) reaching 35 g/L, over

15 times higher than that of most well-known CDI materials [16]

. Therefore,

these graphene–CNT hybrid aerogels hold great potential in the field of water

purification, including CDI of light metal salts, removal of organic dyes, and

enrichment of heavy metal ions in water sources [212]

.

2.4 Graphene–polymer nanocomposites

2.4.1 Introduction

As presented in Section 2.1.5, one of the promising applications of

graphene is to incorporate it with polymers to fabricate graphene–polymer

nanocomposites [43, 45, 47, 62-66]

. Compared with CNTs, graphene seems to be a

more favorable candidate due to its multiple fabrication routes and various

derived products, including GO and rGO as alternatives [43]

.

Up to now, various polymers such as PVA [214, 215]

, Poly(methyl

methacrylate) PMMA [216]

, Polystyrene (PS) [217]

, Polypropylene (PP) [218]

, and

epoxy [219]

have been used to fabricate graphene–polymer nanocomposites,

mainly through three approaches [46, 47]

: (1) solvent processing, (2) melt

processing, and (3) in situ polymerization. The multifunctional properties of

these developed nanocomposites have also been extensively investigated and

compared with the nanocomposites fabricated with CNTs. To enhance some

particular properties of the nanocomposites, efforts are still being made toward

the selection of graphene type, modification of the graphene surface, and

improvement of graphene–polymer interaction. These developed

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graphene–polymer nanocomposites show good performance in many aspects,

such as electrical, electrochemical, and thermal properties, and thus offer great

potential for many applications, including flexible electronics [220]

, energy

storage devices [221]

, and thermal interface materials (TIMs) [201]

.

2.4.2 Structure of graphene–polymer nanocomposites

The combination of the pristine graphene and polymers is normally

facilitated by the crosslinks formed by the polymers themselves. However, how

uniformly the graphene is dispersed in the polymer matrices has remarkable

effects on the structures and properties of the resultant nanocomposites, as

agglomeration of hydrophobic nanofillers in polymer matrices has been

extensively reported [222]

. Although attempts such as surface modification and

radiation treatment have been made to improve the solubility of graphene, a

uniform distribution of these nanosheets is still very difficult to achieve [223]

.

Sonication may temporarily provide a versatile way to improve the dispersion,

but often causes damage to the nanosheets and weakens their intrinsic

properties [223]

.

Currently, the rGO is regarded as a good alternative nanofiller, instead of

the pristine graphene, because the presence of various functional groups such as

epoxide and hydroxyl groups on the rGO can be very effective for its dispersion

[224]. For some cases without crucial requirements for electrical conductance,

hydrophilic GO can also be directly applied without reduction [41]

.

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2.4.3 Synthesis methods of graphene–polymer nanocomposites

2.4.3.1 Solvent processing method

In solvent processing, graphene-based fillers are usually first dispersed in

an organic solvent by sonication, after which the suspension is mixed with a

polymer solution by magnetic agitation or sonication. The graphene–polymer

nanocomposites are thereafter obtained by evaporating or distilling the organic

solvent in the mixture. Various polymers, such as PP [225]

, Polyvinylidene

fluoride (PVDF) [226]

, and PMMA [227]

, have been reported to be suitable for this

solvent processing. However, the removal of the solvent without disturbance of

graphene distribution is still critical for this method.

2.4.3.2 Melt processing method

Melt processing is a versatile method, which is believed to be

environmentally friendly and appropriate for the mass production of polymeric

materials, especially thermoplastics [224]

. Graphene-based composites using

polymers (polyurethane (PU) [228]

, polyethylene terephthalate (PET) [229]

, Poly

Carbonate (PC) [230]

etc.) have been successfully prepared with this method.

This method applies a high temperature and high shear forces to disperse

graphene nanofillers in the polymer matrix, and avoids using other toxic

solvents. Compared with solvent processing, melt mixing is inferior in

effectively dispersing graphene, as the viscosities of the molten polymers are at

times too high to intercalate the fillers [45]

. However, for the preparation of the

composites with low filler loadings, melt processing is still one of the most

practical approaches, and can be readily scaled up for industrial manufacture.

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2.4.3.3 In situ polymerization method

In situ polymerization is another efficient way to synthesize

graphene–polymer nanocomposites, as graphene fillers can be uniformly

dispersed and form strong interaction with the polymer matrix [45]

. In this

method, graphene is first mixed with monomers or pre-polymers, while the

composites are subsequently obtained by a complete polymerization [231-233]

.

Composites such as rGO–epoxy [234]

, rGO–PMMA [216]

and rGO–PU [235]

have

been successfully developed via this method, and the dispersion of graphene

nanosheets in their polymer matrices has been found to be improved. However,

the problems arising from the solvents during polymerization, similar to those

of the solvent processing method, still remain challenging. As the viscosity

increases with the processing of polymerization, the graphene loading which

can be uniformly dispersed is actually low.

2.4.4 Properties of graphene–polymer nanocomposites

2.4.4.1 Electrical properties

When applied as nanofillers in insulating polymer matrices, graphene can

significantly increase the electrical conductivity of the composites [46]

.

Considerable research [236-238]

has been conducted to develop graphene-based

nanocomposites for electrical applications. For example, the rGO–PS

nanocomposites are reported to show electrical conductivities up to 1 S/m at 2.5

vol. % rGO loading [236]

, while the rGO–epoxy composites have a conductivity

of 10 S/m with rGO concentration of 8.8 vol. % [239]

. Because of the wide

selection of polymers, fabrication methods and measurement techniques

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applied, the measured electrical conductivities of the graphene-based

nanocomposites are highly scattered. For rGO–PS composites alone, the values

are reported to vary in the range of 10-4

-72 S/m for the composites within 2.5

vol. % rGO fraction [236, 237]

. Therefore, besides the intrinsic conductivities of

the fillers, the effectiveness of the enhancement is probably also determined by

the distribution of the rGO nanosheets in the polymer composites.

To evaluate the filler distribution, the percolation threshold (φc) is always

considered an important parameter [197, 239, 240]

. It indicates the point at which a

conductive network of the fillers is formed in the composites, and thus suggests

the occurrence from insulation to conduction. For most cases, the lower the

threshold φc, the more uniform the dispersion and the more effective the

enhancement. The lowest threshold was reported by Dao et al. [241]

, which is

0.04 vol. % for rGO in PMMA microsphere.

Recently, it has been found that the reduction process of the GO also

impacts the percolation threshold of the rGO–polymer nanocomposites [242]

.

The chemically reduced GO has a lower threshold than the thermally reduced

GO. As it is well known that thermal reduction can remove more functional

groups of GO and lead to more restacking, the higher threshold of its resultant

composites is probably proof of the increased difficulty in filler dispersion [242]

.

So far, effective enhancement of the electrical properties of graphene-based

nanocomposites still remains a challenge.

2.4.4.2 Mechanical properties

It has been found that the inclusion of graphene or graphene-based

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nanofillers can significantly influence the strength and elastic modulus of the

composites. Nevertheless, the reported data for such improvements are

scattered. A modest strength increase of only 7 % has been reported for a 3 wt. %

GO–Polyimide (PI) composites [243]

, while a remarkable increase of 212 % has

been reported for a 2 wt. % rGO–PVA [244]

, and an increase as high as 893 % for

a 3 wt. % Octadecylamine (ODA)–GO–PI composite [243]

. Similarly, for their

elastic modulus, enhancements varying from 20 % [245]

to over 1400 % [243]

have

been reported for different composite compositions. These significant variants

are probably due to the distinguished qualities of graphene and the different

polymerization approaches involved in the processing.

The mechanical properties of the GO and rGO are inferior but still

comparable to those of the pristine graphene. The 0.7 wt. % GO–PVA

composites show an increase of 76% and 62% in strength and modulus

respectively, compared with pure PVA [238]

. Bao et al. [214]

compared the 0.8 wt. %

loading of GO and 0.8 wt. % rGO in PVA. It was found that the GO–PVA and

rGO–PVA composites exhibited an increase of 54% and 66% in strength and 52%

and 70% in modulus, respectively. As a result, the researchers reported that the

absence (or minimal presence) of functional groups on the graphene lattice may

help to restrict and order the chain arrangements in polymers, thus leading to

these minor enhancements.

2.4.4.3 Thermal properties

Thermal management is a crucial issue in the electronics industries, owing

to the continued miniaturization and rapid increase in the power of

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microelectronics, optoelectronics, and photonic devices [246, 247]

. Recently, due

to the remarkable thermal conductivity of graphene (~5300 W/m·K [55]

),

graphene–polymer nanocomposites have been considered an ideal candidate for

next-generation thermal interface materials (TIMs) [201]

.

Much effort has been made to evaluate the thermal performance of the

graphene-based nanocomposites [42, 194, 248, 249]

. Yavari et al. [248]

reported that

the thermal conductivity of graphene–1–octadecanol composites was increased

by ~140% upon ~4 wt. % graphene loading. Yu et al. [249]

applied graphene

nanoplatelets in epoxy and found that the thermal conductivity of the resultant

nanocomposites reached up to 6.44 W/m·K, at ~25 vol. % graphene loading.

However, the enhancement in thermal conductivity for graphene-based

composites is still very limited because of several factors, including local

agglomeration, defects within the graphene nanosheets, and interaction between

the graphene nanosheets and the polymer matrix [141, 183, 222]

.

The thermal boundary resistance (TBR, known as Kapitza resistance [250]

)

between the nanofillers and polymer matrix explains the large discrepancy

between the measured and theoretical thermal conductivity of polymer

composites. However, due to experimental limitations, TBRs between graphene

nanosheets and polymer matrices are generally difficult to measure. The

effective medium theory (EMT) developed by Nan et al. [251]

is one of the most

common approaches to estimate these TBR values, when given the thermal

conductivity of the composite. In Nan’s approach, the dimensions (e.g. length,

width and thickness) of graphene nanosheets are simplified and fixed to be

single input values, which is convenient for application in various composite

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systems.

2.4.5 Potential applications of graphene–polymer nanocomposites

The applications and potential of graphene–polymer nanocomposites are

strongly dependent on their properties, which have been discussed. Notably,

most applications of these graphene-based composites are similar to those for

CNT-based composites. However, the diverse approaches to obtain graphene

make it more ideal than CNTs for in-practice applications.

Based on their significantly enhanced electrical conductivities, the

development of graphene-based composite electrodes is one of the most widely

investigated applications. For instance, an rGO–PANI electrode is reported to

have a specific capacitance of over 1000 F/g [252]

. Otherwise, since conductive

polymers normally possess a specific temperature coefficient, they can also be

developed as temperature sensors, e.g. rGO–PVDF composites [26]

. In addition,

when the resistivity of a material is lower than 105 Ω/square, it can be used for

EMI shielding. It has been reported that an rGO–epoxy composite with 15 wt. %

graphene loading can reach the same competitive level as the commercial

materials [239]

.

The enhancement of the mechanical properties of polymer matrices gives

graphene-based nanocomposites great potential as advanced structure materials,

which are light-weight with high strength and modulus [243, 244]

. Additionally,

based on the improved thermal properties of graphene–polymer

nanocomposites, efforts are also being made to develop them for thermal

management applications [42, 248, 249]

. As these applications concern the aspects

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of the mechanical and thermal properties that can be directly referred to in

Section 2.4.4, the details will not be repeated here.

The next chapter will present the experimental section of this thesis.

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CHAPTER 3: Experimental Section

3.1 Materials

Graphite powder (CAS No. 7782-42-5, < 20 μm), sodium nitrate (NaNO3,

CAS No. 7631-99-4, ≥ 99.0%), potassium permanganate (KMnO4, CAS No.

7722-64-7, ≥ 99%), concentrated sulfuric acid (H2SO4, CAS No. 7664-93-9, ≥

99.999%), hydrogen peroxide (30% H2O2 in H2O, CAS No. 7722-84-1),

hydrochloric acid (HCl, ~37%, CAS No. 7647-01-0), sodium bisulfate solution

(NaHSO3, CAS No. 7631-90-5) and hydroiodic acid (HI, containing no

stabilizer, CAS No. 10034-85-2, 57 wt.%), methyl methacrylate (MMA, CAS

No. 80-62-6, 99%) monomers, and 2,2′–Azobis(2–methylpropionitrile) (AIBN,

CAS No. 78-67-1, 98%) were purchased from Sigma–Aldrich Company Ltd.

L–ascorbic acid (LAA, CAS No. 50-81-7, ≥ 99%) was supplied by Alfa Aesar.

Ethanol (CAS No. 64-17-5, ≥ 95%) was obtained from Fluka.

Multi-walled carbon nanotubes (MWNTs) and graphene oxide (GO) were

purchased from Chengdu Organic Chemicals Co. Ltd (TIMESNANO) in China.

The MWNTs (Product Code: TNIM2) have a purity of over 90 wt. %, length of

30–50 μm, outer diameter of 8–15 nm, and specific area of 250–300 m2/g. The

GO powder (Product Code: TNGO) has a purity of over 99 wt. %, layers of

1–10, diameter of 0.5–3 μm, and thickness of 0.55–1.2 nm. It should be noted

that in this work, the GO was mostly synthesized from graphite powder by a

modified Hummers’ method (as described in Section 3.2.1), while the GO

purchased from Chengdu Organic Chemicals Co. Ltd (TIMESNANO) was only

used for a comparison of the morphology and multifunctional properties of the

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as-prepared graphene aerogels (GAs).

All the chemicals were used as received without further purification.

3.2 Experimental techniques

3.2.1 Synthesis of graphene oxide (GO)

Graphene oxide (GO) was prepared from graphite powder by a modified

Hummers’ method [117, 253, 254]

. Typically, 2 g NaNO3 and 4 g graphite powder

were added to 100 ml concentrated H2SO4 in an ice bath. After stirring the

above mixture for 30 min, 14.6 g KMnO4 was then slowly added to the mixture

with stirring and cooling to keep the temperature lower than 20 °C for another 2

h. Next, the temperature of the mixture was increased to 35 °C with stirring for

12 h to convert graphite to graphite oxide. Following this, 180ml deionized (DI)

water was added to the mixture with stirring for 15 min, and 14 ml 30% H2O2

and 110 ml DI water were gradually added to the reaction mixture. Thereafter,

the color of the mixture changed from brown to yellow. The graphite oxide was

separated from the mixture by centrifugation and washed with 1 M HCl and DI

water to remove any impurities. The solid graphite oxide was finally dried at 60

°C for 3 days before collection.

To convert graphite oxide to graphene oxide (GO), the as-prepared

graphite oxide solid was first dissolved in DI water to form a 0.1–0.5 wt. %

aqueous suspension. The suspension was then sonicated (Sonics VCX-130

probe sonicator, 130 W, 100% amplitude) for 12 h to exfoliate the interlayers

of graphite oxide. GO powder was finally obtained by centrifuging the

sonicated suspension and drying the collected solid at 60° C for 3 days.

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3.2.2 Synthesis of graphene aerogels (GAs)

GO aqueous suspensions with different concentrations of 1, 2, 6, and 12

mg/ml were prepared and placed in 20 ml vials with plastic caps. L–ascorbic

acid (LAA) was added to the GO suspension, with magnetic stirring for 5

minutes until it was completely dissolved. After that, the reaction mixture was

heated for a number of hours (5, 10, 20, 40 h) at different temperatures of 45,

70, and 95 °C. The as-prepared graphene hydrogels were immersed in DI water

for 3 days to remove excessive LAA before being placed into ethanol for

solvent exchange. The ethanol was changed every 24h for 3 days. Following

this, wet gels were subsequently dried with supercritical CO2 for duration of 45

min (3 cycles) to obtain the GAs.

To investigate the effects of reducing agents on the properties of the GAs,

a 2 mg/ml GO aqueous suspension was prepared. Three common reducing

agents (L–ascorbic acid, HI, and NaHSO3) were respectively added to the GO

suspension and sonicated until completely dissolved. The reaction mixture was

then heated at 95 °C for 5 h to form graphene hydrogels. The obtained graphene

hydrogels were immersed in DI water for 3 days to remove excessive reducing

agents, and then placed into ethanol for solvent exchange for another 3 days.

Finally, the wet gels were dried with supercritical CO2 to form the GAs.

In order to investigate the impact of thermal annealing on the electrical and

thermal properties of the GAs, the as-prepared GAs were also annealed at 450

°C for 5 h in an Argon (Ar) environment.

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3.2.3 Synthesis of graphene–CNT hybrid aerogels

To develop graphene–carbon nanotube (CNT) hybrid aerogels, 10 mg

MWNTs were added to 10 ml DI water and dispersed with an ultrasonic

processor (Sonics, VCX 130). This solution was combined with 10 ml of 4

mg/ml GO suspension and sonicated for 4 h to obtain a homogenous GO–CNT

complex. Next, 160 mg LAA was added to the above suspension and sonicated

for 90 s to completely dissolve the LAA. The reaction mixture was heated at 95

°C for 5 h to form the graphene–CNT hybrid hydrogels. After solvent exchange

in DI water and ethanol, supercritical drying yielded the graphene–CNT hybrid

aerogels.

3.2.4 Synthesis of GA–poly (methyl methacrylate) (PMMA) nanocomposites

The GA–poly (methyl methacrylate) (PMMA) nanocomposites were

prepared via an in situ bulk polymerization process. Accordingly, 30 g methyl

methacrylate (MMA) and 20 mg 2,2′–Azobis (2-methylpropionitrile) (AIBN)

were first mixed in a 50 ml beaker and stirred at 75 °C for 30 min using a

magnetic stirrer. When the mixture became viscous, it was rapidly cooled

below 50 °C to cease the pre-polymerization. The GAs were then immersed into

the mixture and the mixture with the GAs immerged was kept at a low

temperature (below 10 °C) to remove air bubbles. After that, the above mixture

was maintained in a water bath at 50–55 °C for 30 h to cure the pre-polymerized

PMMA into a solid. The cured GA–PMMA nanocomposites were finally

machined and mechanically polished to remove the excessive part of PMMA

and achieve a smooth surface for subsequent characterization.

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3.3 Characterization

3.3.1 X-ray diffraction (XRD)

X-ray diffraction (XRD) is one of the common techniques for examining

detailed information about the chemical composition and crystallographic

structure of a substance [255]

. With materials having a crystalline structure, their

ordered features will coherently scatter the X-rays in the directions that meet the

criteria for constructive interference, and thus lead to signal amplification. The

conditions required for constructive interference are determined by Bragg’s

law:

𝑛𝜆 = 2𝑑𝑠𝑖𝑛𝜃 (3.1)

where n is a integer, λ corresponds to the X-ray wavelength, d refers to the

distance between the lattice planes, and θ is the angle of incidence with the

lattice plane.

In this thesis, X-ray diffraction (XRD, 6000 Shimadzu, Japan) was

conducted to investigate the structures of graphite, GO and GA, and the effects

of GO concentrations and thermal annealing processes on the structures of GAs.

A diffractometer with a Cu-Kα radiation source (λ=0.1506 nm) was used. The

continuous scan was recorded from 5 ° to 30 ° (2θ) with a scan step of 0.02 ° and

a scan rate of 0.5 °/min.

3.3.2 Scanning electron microscopy (SEM)

Scanning electron microscopy (SEM) is a type of electron microscopy that

produces images displaying information about the surface morphology and

composition of a sample [256]

. The sample is scanned by a focused beam of

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electrons, where the electrons interact with atoms in the sample and generate

various detective signals. Among them, the detection of secondary electrons

emitted by atoms is the most common mode. The secondary electrons are first

collected by inducing them towards an electrically biased grid, and then

accelerated towards a phosphor-biased one. Afterwards, the output signal of

these accelerated secondary electrons is amplified and shown as a 2D intensity

distribution, which can be eventually saved as a digital image after the

analog-to-digital conversion.

In this thesis, the nanostructures of GAs were characterized using field

emission scanning electron microscopy (FESEM, Model S-4300 Hitachi, Japan)

with a field-emission-gun operating at 10 kV for the GAs and 15 kV for the

GA–PMMA nanocomposites. Due to their good electrical conductivity, the GA

samples for FESEM were directly loaded on the holder without any pre-coating,

while the GA–PMMA nanocomposites were gold coated under 20 mA for 10s

to obtain better conductivity before surface scanning.

3.3.3 Physical adsorption/desorption of nitrogen (BET)

BET, which refers to the Brunauer–Emmett–Teller (BET) theory,

describes the physical adsorption of gas molecules on a solid surface, and is

considered the basic technique for analyzing the specific area of a material [257]

.

The concept of the BET theory originates from the Langmuir theory, but

extends adsorption of the monolayer molecular to that of the multilayer with

some specific hypotheses. These are: (i) gas molecules physically adsorb on a

solid in layers, infinitely; (ii) no interaction exists between each adsorption

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layer, and (iii) each of these layers satisfies the Langmuir theory. The BET

equation is given below:

1

𝑣[(𝑝0 𝑝⁄ )−1]=

𝑐−1

𝑣𝑚𝑐(

𝑝

𝑝0) +

1

𝑣𝑚𝑐 (3.2)

where p and p0 are the equilibrium pressure and saturation pressure of

adsorbents at the test temperature, and v and vm are the volume of gas adsorbed

at equilibrium pressure and the monolayer capacity of the adsorbent

respectively. c is the BET constant and is expressed as:

c = exp (𝐸1−𝐸𝐿

𝑅𝑇) (3.3)

where E1 is the heat of adsorption for the first layer, while EL is that for the

second and upward layers, equal to the heat of liquefaction. R and T are the gas

constant and test temperature respectively.

Through the BET theory, the total surface area and specific surface area

are expressed as:

𝑆𝑡𝑜𝑡𝑎𝑙 =(𝑣𝑚𝑁𝑠)

𝑉 (3.4)

𝑆𝐵𝐸𝑇 =𝑆𝑡𝑜𝑡𝑎𝑙

𝑎 (3.5)

where vm is in the unit of volume, N is the Avogadro’s number, s is the

adsorption cross section, V the molar volume of the adsorbate gas, and a is the

net mass of the solid sample.

In this thesis, nitrogen adsorption/desorption measurements were carried

out with a Nova 2200e (Quantachrome) to obtain the pore properties of the

resulting GAs, such as BET specific surface area, BJH pore size distribution

and total pore volume. All the samples were degassed in a vacuum at 120 °C for

2 h before measurement.

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3.3.4 Electrical conductivity measurement

Electrical conductivity measures the ability of a material to conduct

electrical current. The bulk electrical properties of the GAs or GA–PMMA

nanocomposites were measured using a two-probe method on a Solartron

1260+1287 electrochemical system, as shown in Figure 3.1 below. The samples

were sandwiched between two copper plate electrodes with silver paste applied

to eliminate the contact resistance. Except for the weight of the upper copper

electrode, no other weight was loaded on the top of the tested samples. The

dimensions of the samples were measured with a digital caliper before the

electrical conductivity measurement, which are 10–15 mm in diameter and 1–3

mm in thickness.

Figure 3.1 A Solartron 1260+1287 electrochemical system for electrical

property testing.

The electrical conductivities of the GAs and the GA–PMMA

nanocomposites were calculated from impedance values using the following

equation:

𝜎 =𝐼𝐿

𝑉𝑆 (3.6)

where V and I are the applied voltage and tested current through the samples,

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and S and L are the cross section area and thickness of the tested samples,

respectively.

The electrical conductivity measurement was conducted within a voltage

range of 0–0.6 V, and each GA and GA–PMMA nanocomposite sample was

measured at least three times for consistency. The electrical conductivities of

the GAs and GA–PMMA nanocomposites were obtained by averaging the

values from the three tests.

3.3.5 Thermal conductivity measurement

The thermal conductivity of the GAs was measured using an improved

comparative infrared microscopy technique. Prior to the measurement, a GA

sample was sandwiched between two reference layers to build a 3-layered stack

using silver paste to ensure good contact between the sample and reference

layers, which was subsequently affixed to a heat sink plate at the bottom and a

resistive heater on the top. Amorphous quartz with a thermal conductivity of

kamorphous quartz = 1.3 W/m·K [258]

was selected as the reference material for this

thesis to ensure a comparable thermal resistance between the tested sample and

reference materials, as well as good thermal conduction through the entire

sample stack. The dimensions of the reference layers were 10 mm (L) × 10 mm

(W) × 1 mm (H), and the in-plane dimensions of the GA samples were also 10

mm (L) × 10 mm (W). All the surfaces of the GAs were polished and the

thickness of the GAs was controlled to be 1.2 ± 0.2 mm. A one-dimensional

heat flux was generated through the stack by the resistive heater and a

VariCAM high resolution thermographic system captured the temperature

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distribution across the whole stack. All the surfaces facing the infrared (IR)

camera were coated with graphite to achieve a uniform and high (near unity)

emissivity. The temperature resolution of the IR camera was 0.08 K, and the

temperature through the whole stack was lower than 80 °C for all the

measurements.

The experimental set-up is illustrated in Figure 3.2(a) below. From the

measured two-dimensional temperature maps for the amorphous

quartz–GA–amorphous quartz stack, one-dimensional temperature profiles are

obtained by averaging the temperature in the direction perpendicular to the heat

flux. Figure 3.2(b) shows a typical temperature profile, where the temperature

gradients in the reference amorphous quartz region ((𝑑𝑇

𝑑𝑥)

amorphous quartz) and

sample region ((𝑑𝑇

𝑑𝑥)

GA) are calculated through fitting the temperature profile

with the least-square method [62]

.

Heat transport within the sample stack can be described by Fourier’s law.

Given the same cross section and constant heat flux in the stack, the

one-dimensional steady-state heat conduction equation is expressed as:

𝑞" = −kamorphous quartz ∙ (dT

dx)

amorphous quartz= −kGA ∙ (

dT

dx)

GA (3.7)

where 𝑞" is the heat flux through the sample stack and is calculated from the

value of kamorphous quartz and the average of the temperature gradients in the two

amorphous quartz regions. Accordingly, the thermal conductivity of the GA

(kGA) is determined from Equation (3.7) and the measured temperature gradient

in the GA.

In this thesis, to minimize the effect of the thermal boundary resistance

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(TBR), the two pixels (~133 μm/pixel) at the boundary of each layer in the stack

were eliminated from the calculation [62]

. To yield robust results, the heat flux

(𝑞" ) versus the temperature gradient in the sample region ((𝑑𝑇

𝑑𝑥)

GA) was

plotted at several power levels, and the measured thermal conductivity of the

GAs (kGA) was extracted from the slope of the least-squares best fit to this curve,

as shown in Figure 3.2(c).

Figure 3.2 (a) Set-up schematic of thermal conductivity measurement using the

comparative infrared thermography technique. (b) Temperature distribution and

linear best fit curves for the 3-layered stack, which consists of a GA sample

sandwiched between two amorphous quartz layers, scale: 133 μm/ pixel. (c)

Heat flux as a function of temperature gradient in the GA region at several

power levels. During the measurement, the heat flux is typically below

11.25kW/m2.

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3.3.6 Thermogravimetric analysis (TGA)

Thermogravimetric analysis (TGA) is a technique to determine thermal

characteristics, such as degradation temperatures, decomposition point, or the

contents of inorganic and organic components of a sample, according to its

weight changes as a function of temperature [259]

. The whole system consists of

a temperature-controlled furnace, a dual-range balance with two sample

containers, and attached thermal couples. During a typical test, approximately

10 mg powdered sample is located in one of the sample containers, while the

other acts as a reference. As the temperature of the furnace increases in a certain

gas environment, such as air, oxygen, nitrogen, or argon, the temperature of

each container and the mass of the sample are recorded accordingly.

Differential thermal analysis (DTA) is commonly performed simultaneously

with TGA, providing information about exothermic or endothermic reactions

that take place. In DTA, the temperature of the test sample is measured relative

to that of an adjacent inert material. It presents the difference in voltage

between the output of the sample thermocouple and the reference

thermocouple with temperature.

For this thesis, the TGA and DTA of both GAs and GA–PMMA

nanocomposites were conducted on a DTG60H thermogravimetric analyzer

from room temperature to 1000 °C in air with a heating rate of 5 °C/min.

3.3.7 Vickers microhardness measurement

The hardness of a material is defined as its resistance to indentation, and it

is usually determined by measuring the permanent depth of the indentation.

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Microhardness testing, also refers to as microindentation, is a common method

for measuring the hardness of a material, especially for small parts and thin

sections, on a microscopic scale [260]

.

The Vickers hardness measurement is based on an optical measurement

system and follows the procedures of ASTM E-384, which is commonly used to

determine and verify the Knoop and Vickers hardness of materials. During the

measurement, a square-based pyramid indenter is used to make an indentation

on the testing specimen under a light load. The hardness value is calculated

according to the length of the indentation, which could be precisely measured

by the optical microscopy of the testing machine. The calculation is given in the

following equation:

𝐻𝑉 =𝐹

𝐴≈

0.1891𝐹

𝑑2 (3.8)

where F is the applied force, [N], A is the surface area of the indentation, [mm2],

and d is the mean diagonal length of the indentation, [mm]. The calculated

hardness HV is in GPa.

For this thesis, the Vickers microhardness was measured with a

Shimadzu-HMV automatic digital microhardness tester using an individual

indentation force of 245.2 mN for duration of 15 seconds.

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CHAPTER 4: Morphology Control of Graphene

Aerogels

4.1 Introduction

In recent years, a large amount of research has been conducted to develop

graphene or graphene-based materials for various applications, such as energy

storage devices, sensors, and nanocomposites. It is believed that the realization

of a three-dimensional graphene nanostructure would represent a significant

step towards fulfilling the potential of graphene. However, as presented in

Section 2.2, the methods reported thus far for the fabrication of 3D graphene

nanostructures are still very limited, and a binder is usually required to achieve

the assembly. Although the chemical reduction method takes advantages of

binderless and more environmentally friendly than other approaches, very few

studies have been conducted to investigate the effects of its synthesis

parameters on the morphology and multifunctional properties of the

as-prepared GAs. The effect of different reducing agents on the GA

nanostructures has also not been reported.

In addition, a one-of-a-kind symbiotic relationship has been observed to

exist between one-dimensional CNTs and two-dimensional graphene sheets.

Therefore, integrating CNTs into the GAs could further enhance the electrical

and mechanical properties of the GAs [157, 212]

. Nevertheless, the effect of CNTs

on the morphology of GAs has also yet to be studied.

In this thesis, we report systematic research to effectively control the

morphology of GAs. The GAs were synthesized through a simple chemical

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reduction method. Since no polymeric binder was applied during the process,

the developed method is effective and environmentally friendly for mass

production of GAs. As the nanostructures of the GAs can be easily controlled

by adjusting the synthesis parameters, such as compositions (GO

concentrations), reduction temperatures, reduction times, reducing agents, and

CNT inclusions, these experimental results could serve as a guide to synthesize

the GAs with the desired nanostructures, which would be very useful for the

electrodes of energy storage devices such as supercapacitors and lithium

batteries, and nanocomposites.

4.2 Nanostructured control of graphene aerogels (GAs)

GAs are synthesized through a modified Hummers’ method and chemical

reduction method as described in Section 3.2.2. The mechanism of graphene

self-assembly by chemical reduction was first proposed by Chen et al. [145]

It is

widely known that GO can be well dispersed in DI water due to its

hydrophilicity. When the GO aqueous suspension is reduced by reducing agents

such as LAA, NaHSO3 and HI, the reduced GO (rGO) nanosheets become

hydrophobic and the π–π interaction between these hydrophobic rGO

nanosheets significantly increases, which finally leads to the formation of a 3D

structure of graphene.

Except when investigating the effects of reducing agents on the

multifunctional property of GAs, LAA is selected as the major reducing agent

for the other sections of this thesis, because it is efficient and environmentally

friendly for the reduction of GO to graphene; the excess LAA can also be easily

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removed during the solvent exchange by DI water. According to the estimated

balanced chemical reaction reported elsewhere, the required amount of LAA

should be at least 3.3 times that of the GO content by mass [157, 261]

. Thus the

amount of LAA used for this work is 4 times that of the GO content by mass, to

ensure a sufficient reduction. Figure 4.1 shows (a) the aqueous suspension of

GO and a graphene hydrogel and (b) a graphene aerogel.

Figure 4.1 (a) Aqueous suspension of GO and a graphene hydrogel and (b) A

graphene aerogel.

The oxidation of graphite into GO (or GO after exfoliation) and the

reduction of a GO into a GA are investigated by X-ray diffraction (XRD)

technique, as shown in Figure 4.2 below. From the XRD spectrum, a strong

characteristic peak of 26.4° (JCPDS card number: 75-1621) is observed for the

raw graphite powder, while a peak of 11° is found for the graphene oxide

obtained from the oxidation and exfoliation of graphite, which is consistent

with the results reported elsewhere and indicates the conversion of graphite

(Interlayer spacing: 0.34 nm) to graphite oxide (Interlayer spacing: 0.37 nm)

[14, 156, 203, 262]. For the XRD pattern of GA, a broad peak is shown at 23.5°,

indicating the effective removal of oxygen groups during the reduction process

and an amorphous structure formed between the graphene layers [145, 174]

.

Previous Raman spectra of the chemically derived graphene nanosheets

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usually exhibit a D to G band intensity ratio (ID/IG) of ~0.99–1.43 (1.07 in this

work), indicating the introduction of defects after the oxidation and reduction

of graphite [263, 264]

.

Figure 4.2 XRD patterns of graphite, graphite oxide and graphene aerogel.

4.2.1 Effects of chemical compositions and synthesis conditions

The effects of chemical compositions and synthesis conditions, such as

reduction temperatures and reduction times, on the morphologies of the GAs

are systematically investigated, as shown in Table 4-1. The GAs are synthesized

with various initial GO concentrations of 1, 2, 6, and 12 mg/ml, reduction

temperatures of 45, 70, and 95 °C, and reduction times of 5, 10, 20, and 40 h,

respectively. The nanostructures of the GAs obtained under various GO

concentrations, different reduction temperatures, and different treatment times

are compared in Figure 4.3 below. All of them present interconnected

three-dimensional network structures. It can be seen that the 3D network

formed from 12 mg/ml GO suspension is denser than that formed from the

concentration of 2 mg/ml, while the GA synthesized at 95 °C has a more

packed structure than those at 70 and 45 °C. The GA sample reduced for 40 h

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is also more overlapped than that for 5 h. This trend is also associated with

that of the surface areas of the GAs.

Table 4-1 Nanostructure control of the GAs.

No. Synthesis

conditions

Surface

area

(m2/g)

Average

pore size

(nm)

Pore

volume,

(cm3/g)

Density,

(mg/cm3)

Porosity*

(%)

GO concentrations (Temperature: 70 °C, time: 40 h)

1 1 mg/ml 284 3.6 0.51 18.24 99.13

2 2 mg/ml 302 4.1 0.63 26.53 98.74

3 6 mg/ml 365 3.9 0.72 56.44 97.31

4 12 mg/ml 473 4.0 0.95 67.97 96.76

Reduction times (GO concentration: 2 mg/ml, temperature: 70 °C)

5 5 h 560 3.9 1.09 18.47 99.12

6 10 h 438 4.0 0.88 20.81 99.01

7 20 h 381 3.9 0.74 22.84 98.91

2 40 h 302 4.1 0.63 26.53 98.74

Reduction temperatures (GO concentration: 2 mg/ml, time: 40 h)

8 45 °C 577 4.0 1.17 25.61 98.78

2 70 °C 302 4.1 0.63 26.53 98.74

9 95 °C 245 3.8 0.46 35.78 98.30

*Porosity is converted from density ratio of the GAs to graphene (2.10 g/cm3).

Figure 4.3 SEM images of graphene aerogels synthesized under different

conditions: (a) 2 mg GO/ml, 70 °C, 40 h; (b) 12 mg GO/ml, 70 °C, 40 h; (c) 2

mg GO/ml, 45 °C, 40 h; (d) 2 mg GO/ml, 95 °C, 40 h; (e) 2 mg GO/ml, 70 °C, 5

h. Compared with image (a), more graphene nanosheets can be observed in

image (b). The GA sample in image (c) shows a more loose structure than those

in image (a) and image (d). Image (e) also shows a less dense network than that

in image (a).

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The characterization of the specific surface areas and porous properties of

the GAs obtained under different conditions is conducted by nitrogen

adsorption/desorption measurements with a Nova 2200e (Quantachrome).

Before the measurements, samples are degassed at 120 °C in a vacuum for 2 h to

remove moisture, and the calculations of the specific surface area and pore size

of the GA samples are conducted by the Brunauer–Emmett–Teller (BET) and

Barrett–Joyner–Halenda (BJH) methods. A typical nitrogen

adsorption/desorption isotherm is shown in Figure 4.4. Type IV

adsorption/desorption isotherms are displayed for all the GA samples,

indicating that there are many mesopores in the GA structures. All the

morphological characteristics of the as-prepared GAs are summarized in Table

4-1 above.

Figure 4.4 A typical N2 adsorption/desorption isotherm of a GA.

For all the GAs synthesized at 70 °C for 40 h, the highest surface area of

473 m2/g is obtained with 12 mg/ml initial GO concentration, while the lowest

value of 284 m2/g is found with a GO concentration of 1 mg/ml. It can be seen

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that under the same reduction conditions, the surface area and pore volume of

the GAs increase along with the increase in the initial GO concentration, since

more graphene nanosheets are more likely to create more pores during the

reduction process. The effect of synthesis conditions on GAs is tested with 2

mg/ml GO throughout. With the same reduction time of 40 h, the GA

synthesized at 45 °C has the largest surface area of 577 m2/g and the largest pore

volume of 1.17 cm3/g, while that at 95 °C has the lowest values of 245 m

2/g and

0.46 cm3/g, respectively. When the reduction temperature is kept at 70 °C, the

surface area and pore volume values of the GA sample with 5 h reduction

treatment are much larger than those of the one treated for 40 h.

During the reduction, the formation of hydrophobic sites and π–π

interactions between graphene sheets could be the main factor determining the

porous structure of the GAs [174]

. In this case, a higher temperature or a longer

time may probably help the reduction process to be more efficient or more

complete, thus leading to the creation of more overlapping sites. Under a higher

reduction temperature, the higher pressure in the reaction vial may also favor

the assembly of graphene nanosheets. Such assembly and overlapping between

the graphene nanosheets consequently results in a reduction of the surface area

and pore volume of the as-prepared GAs. Therefore, it can be concluded that

with the same GO concentration, the surface area of the GAs is reduced with the

increase in reduction temperature or reduction time. Compared with the

previous work [174]

, the surface area and pore volume of the GAs prepared by

the mild chemical reduction method are all higher than those of the samples

prepared by the hydrothermal method, indicating the negative effect of higher

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pressure on the surface area and pore volume of the GAs.

4.2.2 Effects of reducing agents

Except for synthesis conditions, the selection of reducing agent (LAA, HI,

or NaHSO3) also impacts the morphology, electrical property, and thermal

stability of the GAs. The effect of reducing agents on the morphology of GAs is

investigated when 2 mg/ml GO suspension is reduced by LAA, HI, and

NaHSO3 under the same synthesis conditions; the amounts of three reducing

agents are enough for a sufficient reduction [145, 157]

. The GA morphologies are

characterized by nitrogen adsorption/desorption measurements to show the

specific surface area and pore size, obtained by the Brunauer–Emmett–Teller

(BET) and Barrett–Joyner–Halenda (BJH) methods, respectively. Table 4-2

summarizes the morphologies of the GAs reduced by LAA, HI, and NaHSO3,

with and without thermal annealing conditions.

Table 4-2 Effects of reducing agent and addition of CNTs on morphology of

the GAs.

Thermal

annealing

Surface area

(m2/g)

Pore size

(nm)

Density

(mg/cm3)

Porosity

(%)

Reducing agents

LAA Without 423 3.6 28.1 98.66

With 487 3.6 28.2 98.66

HI Without 385 3.6 18.4 99.12

With 281 3.6 16.4 99.22

NaHSO3 Without 679 3.6 20.2 99.04

With 582 3.6 22.3 98.94

CNTs concentration (mg/ml) (LAA as the reducing agent)

0 – 738 3.6 37.0 98.24

0.5 – 844 3.6 31.2 98.51

1 – 788 3.6 36.1 98.28

2 – 636 3.6 41.3 98.03

The surface areas of the GAs reduced by LAA, HI, and NaHSO3 are 423,

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385 and 679 m2/g respectively, due to the different reduction effectiveness of

the three reducing agents. The more efficient reducing agent (e.g. HI) removes

more functional groups (–OH, –COOH, –O–, etc.) during the reduction

processes and forms more π–π bonding and stacks between graphene

nanosheets, which decreases the surface area of the GAs.

After thermal annealing of the GAs, the surface areas of the GAs reduced

by HI and NaHSO3 decrease to 281 and 582 m2/g, respectively. The annealing

process further removes the functional groups of the GAs, causing them to

condense further. More π–π stack formation between the graphene sheets

causes decreased GA surface area. However, the surface area of the GAs

reduced by LAA increased to 487 m2/g after thermal annealing. There is no

clear explanation to explain the increase in surface area for the LAA–reduced

GAs, although it is possible that the thermal annealing process may decrease the

π–π interaction among graphene sheets and dehydroascorbic acid (the oxidized

form of LAA), in addition to removing the functional groups on graphene

sheets.

4.2.3 Effects of CNTs

As explained previously, graphene hydrogels are formed by π–π stacking

during the reduction of hydrophilic GO to hydrophobic graphene nanosheets.

The mechanism of graphene–CNT hybrid aerogel formation may be also due to

the π–π interaction between graphene nanosheets, as well as that between

graphene and CNTs. During the reduction of GO in its aqueous suspension, the

majority of the CNTs are physically wrapped inside the 3D network of

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graphene hydrogel, while a minority of the CNTs may form a π–π interaction

with the reduced graphene oxide nanosheets. Figure 4.5(a) shows an

as-prepared graphene–CNT hybrid aerogel using LAA, with 10 mm diameter

and 3 mm thickness.

Figure 4.5 (a) A digital photo of a graphene–CNT hybrid aerogel; (b) and (c)

SEM images of a graphene–CNT hybrid aerogel at different magnifications.

Different concentrations of CNTs (0, 0.5, 1 and 2 mg/ml) are added into

the GAs to form graphene–CNT hybrid aerogels. Figures 4.5(b) and (c) show

SEM images of the interconnected 3D network within the graphene–CNT

hybrid aerogel, where the CNTs are dispersed inside the graphene sheet

network. As seen in Table 4-2 previously, the surface area of the

graphene–CNT hybrid aerogels increases with CNT concentrations up to 1

mg/ml. The surface area of the graphene–CNT hybrid aerogels increases

because of: (i) the additional surface area of the dispersed CNTs, and (ii)

separation of the graphene nanosheets by the CNTs during the self-assembly

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processes. However, when the CNT concentration is further increased to 2

mg/ml, the surface area of the graphene–CNT hybrid aerogel decreases to less

than that of the pure GAs. At high CNT concentrations, local agglomeration and

bundling of the CNTs may block the pores of the GAs [265]

.

4.3 Conclusions

In summary, GAs are synthesized by a simple chemical reduction method

with various chemical compositions (initial GO concentrations), different

synthesis conditions (reduction temperatures and reduction times), and three

reducing agents (LAA, HI, and NaHSO3). A morphology control of the

as-prepared GAs can be achieved by changing these synthesis parameters

appropriately. The results show that the GAs synthesized from a higher GO

concentration possess higher surface areas, while higher reduction temperature

and reduction time make GAs a packed structure with lower surface areas.

Similarly, the GAs synthesized with a more efficient reducing agent exhibit a

lower surface area, while those synthesized with a low-efficiency reducing

agent possess a higher surface area. In addition, graphene–CNT hybrid aerogels

were successfully developed by adding CNTs during the GA synthesis. The

addition of CNTs enhances the surface area by up to 14%, compared with the

pure GAs. These results provide insight into optimizing the nanostructures of

the GAs for various applications, including the development of electrodes,

energy storage devices and nanocomposites.

The nanostructure control of GAs will be summarized again in the

Conclusion chapter.

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CHAPTER 5: Multifunctional Properties of

Graphene Aerogels

5.1 Introduction

Chapter 4 presents systematic research on the effective control of the

morphology of GAs. However, this morphological effect also has a significant

impact on the multifunctional properties of the GAs. In this chapter, the

electrical property, thermal property, and thermal stability of the GAs are

comprehensively investigated in relation to their variation in morphologies.

These experimental results are thus useful for guiding the optimization of the

surface area and multifunctional properties of the GAs at the same time.

For this thesis, the electrical property and thermal stability of the GAs were

measured by a two-probe method and TGA, respectively. In terms of the

measurement of thermal property, a comparative infrared (IR) microscopy

technique was developed based on the ASTM E1225 standard. Due to its

satisfactory accuracy and facile operation, this IR microscopy technique was

applied to determine the thermal conductivities of the GAs fabricated from

various graphene oxide (GO) aqueous suspensions. The thermal conductivity

was measured as a function of GO concentration and thermal annealing. This

thesis reports the first benchmark data of the thermal properties of the GAs, and

seeks to identify the factors limiting their thermal conductivities.

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5.2 Electrical property of graphene aerogels (GAs)

5.2.1 Effects of chemical compositions and synthesis conditions

Figure 5.1 below shows a typical current–voltage curve of the GA, which

is obtained from a 12 mg/ml GO suspension at 70 °C for 40 h. Its electrical

conductivity is calculated from this linear I–V plot based on the Ohm’s law. It

can be observed from Table 5-1 below that under the same reduction

temperature and reduction time, GA synthesized from a higher initial GO

concentration has a higher electrical conductivity, i.e. the highest electrical

conductivity of 2.1 S/m is obtained when the initial GO concentration is 12

mg/ml, which is comparable to the data reported elsewhere [266]

. A likely

explanation is that more graphene nanosheets in a higher GO concentration can

form more overlapping during the synthesis process, thus attaining better

electron mobility.

Figure 5.1 I–V plot of the GA obtained from 12 mg/ml GO suspension at 70 °C

for 40 h.

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Table 5-1 Morphological effects on electrical property of the GAs.

No. Synthesis

conditions

Surface area

(m2/g)

Pore volume,

(cm3/g)

Conductivity,

(S/m)

GO concentrations (Temperature: 70 °C, time: 40 h)

1 1 mg/ml 284 0.51 0.7

2 2 mg/ml 302 0.63 0.8

3 6 mg/ml 365 0.72 1.1

4 12 mg/ml 473 0.95 2.1

Reduction times (GO concentration: 2 mg/ml, temperature: 70 °C)

5 5 h 560 1.09 0.5

6 10 h 438 0.88 0.6

7 20 h 381 0.74 0.7

2 40 h 302 0.63 0.8

Reduction temperatures (GO concentration: 2 mg/ml, time: 40 h)

8 45 °C 577 1.17 0.5

2 70 °C 302 0.63 0.8

9 95 °C 245 0.46 1.0

Figure 5.2 shows the effect of initial GO concentrations on the electrical

conductivities and surface areas of the GAs. It may be noted that increasing the

concentration of the initial GO aqueous suspension can increase both the

electrical conductivity and surface area of the GA. However, if the GO

concentration is too high, it will be very difficult to form a uniform structure in

the as-prepared GA. For GAs synthesized from the same initial concentration of

GO, the electrical conductivities decrease with the increase in surface areas.

This is mainly because for a denser structure of GA, there would be more

stacking of graphene nanosheets and thus stronger π–π interaction existing in

its network. It has been reported that the electrical conduction of chemically

reduced graphene oxide nanosheets is dominated by an electron hopping

mechanism. Therefore, as more graphene nanosheets become intact, the

electron hopping is expected to be significantly enhanced, thus leading to a

reduction of the contact resistance and a higher electrical conductivity.

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Figure 5.2 Effects of initial GO concentrations on electrical conductivity and

surface area of GAs.

5.2.2 Effects of reducing agents

The HI–reduced GAs have the highest electrical conductivity of 3.29 S/m,

while the LAA and NaHSO3–reduced GAs have relatively lower electrical

conductivities of 2.08 and 1.67 S/m, respectively (see Table 5-2 and Figure 5.3

below). The differences in the electrical conductivities of the GAs reduced by

different reducing agents can also be explained by the morphological

differences. The GA with a lower surface area has a higher electrical

conductivity due to the more densely packed nanostructure, which enhances the

electron transport.

Table 5-2 Effects of reducing agent and addition of CNTs on electrical

conductivity and thermal stability of the GAs.

Thermal

annealing

Surface

area (m2/g)

Electrical

conductivity

(S/m)

DTA peak

temperature (°C)

Reducing agents

LAA Without 423 2.08 ± 0.20 539

With 487 4.12 ± 0.53 568

HI Without 385 3.29 ± 0.44 591

With 281 5.90 ± 0.04 598

NaHSO3 Without 679 1.67 ± 0.03 540

With 582 9.52 ± 0.38 542

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CNT concentration (mg/ml) (LAA as reducing agent)

0 – 738 0.20 ± 0.01 516

0.5 – 844 0.33 ± 0.03 495

1 – 788 0.56 ± 0.09 496

2 – 636 0.47 ± 0.06 532

Figure 5.3 Effect of reducing agents and thermal annealing on (a) electrical

conductivity and (b) thermal stability of the GAs.

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Figure 5.4 below shows the effects of the thermal annealing on the

structures and properties of the GAs. The XRD spectrum for all the GAs shows

a broad peak around 23.5–25 ° before annealing, which is consistent with

previous reports [14, 178, 203, 262]

and indicates the formation of non-crystalline

structures by the π–π stacking among the graphene nanosheets. For the annealed

GAs, the XRD spectrum shifts to the right, indicating the formation of a more

condensed nanostructure after the thermal annealing treatment. During thermal

annealing, more functional groups may be removed and stronger π–π

interactions could form among the graphene sheets. Therefore, the annealed

GAs have much higher electrical conductivities than those of the non-annealed

GAs, as shown in Figure 5.3(a) above.

Figure 5.4 XRD patterns of the GAs reduced by different reducing agents with

and without thermal annealing.

5.2.3 Effects of CNTs

The addition of CNTs into the GAs also enhances their electrical

conductivities, as shown in Table 5-2 previously and Figure 5.5 below. When

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0.5 mg/ml CNTs is added into the GA, the electrical conductivity of the

graphene–CNT hybrid aerogel is 0.33 S/m, a 65% increase over that of the pure

GA. When the concentration of CNTs is 1 mg/ml, the electrical conductivity of

the graphene–CNT hybrid aerogel reaches a maximum of 0.56 S/m, while 2

mg/ml CNTs slightly decrease the electrical conductivity of the graphene–CNT

hybrid aerogel to 0.47 S/m. Within the graphene–CNT hybrid aerogels, CNTs

could create more channels for efficient electron transfer between graphene

sheets and therefore enhance their electrical conductivities. However, when the

CNT concentration exceeds 1 mg/ml, the local agglomeration of CNTs reduces

the electrical conductivities of the GAs.

Figure 5.5 Electrical conductivity and DTA peak temperature for

graphene–CNT hybrid aerogels with various CNT concentrations.

5.3 Thermal stability of graphene aerogels (GAs)

5.3.1 Effects of chemical compositions and synthesis conditions

The thermal durability, which is an important factor for electrode materials

working at high temperatures, is studied by TGA on DTG60H using the GAs

synthesized at 45 and 95 °C for 40 h, respectively. Their TGA profiles are

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displayed in Figure 5.6 below; both exhibit similar trends, but with different

burning temperatures. The GA obtained at 95 °C shows an obvious weight loss

in the range of 450–560 °C with a DTA peak at 544 °C, while the GA obtained

at 45 °C possesses a continuous decrease in weight from 200 to 570 °C with a

DTA peak at 529 °C. It can be seen that the GA synthesized at a higher

temperature creates a denser structure and higher thermal stability, which also

indicates that more overlapping of graphene nanosheets makes the GA a more

rigid network. For comparison, the GA synthesized at a lower temperature has a

looser structure and appears to be less thermally stable due to the existence of

some unpacked part inside.

Figure 5.6 Thermal stability of GAs at (a) 45 °C and (b) 95 °C.

5.3.2 Effects of reducing agent and CNTs

As shown in Figure 5.3(b) previously, the HI–reduced GA shows a DTA

peak at 598 °C, which is higher than that of the LAA– and NaHSO3–reduced

GAs (approximately 540 °C). During TGA tests, the remaining functional

groups on the graphene nanosheets are first removed before the GA reacts with

the oxygen in an air atmosphere. Consistent with the morphological

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characteristic as discussed previously, the increased thermal stability of the

HI–reduced GA is likely due to its more condensed nanostructure and lower

surface area [145]

.

As shown in Figure 5.5 and Table 5-2 previously, the thermal stability of

GAs is affected by the CNT concentrations and the morphology of the

graphene–CNT hybrid aerogels. When the dispersed CNT concentration is

increased up to 1 mg/ml, the surface areas of GAs increase and their thermal

stabilities decrease due to the more porous structures. When the CNTs form

agglomeration/bundles, the surface area of the GAs is reduced and the thermal

stabilities are larger due to the more condensed nanostructures and the stronger

bonding between CNTs–CNTs and graphene–graphene nanosheets.

5.4 Thermal conductivity of graphene aerogels (GAs)

5.4.1 Effects of chemical compositions

During the reduction of hydrophilic GO to hydrophobic graphene, the

partial overlap of flexible graphene nanosheets due to π–π interaction results in

the formation of the 3D graphene hydrogels [14, 157]

. After supercritical drying,

the interconnected porous network is preserved in the GAs, as shown by the

FESEM images in Figure 5.7. The concentration of the GO aqueous suspension,

as well as the annealing treatment, impacts the morphologies and thermal

conductivities of the GAs. Table 5-3 summarizes the synthesis conditions,

density, volume fraction and thermal conductivities for each GA.

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Figure 5.7 SEM images of the GAs synthesized under different conditions:

(a)–(h) represent GA1–GA8 respectively. All images present interconnected

3D networkstructures. With annealing, images (e)–(h) show denser networks

than those in images (a)–(d) at the same GO concentration.

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Table 5-3 Synthesis conditions, density, volume fraction and thermal

conductivity of the GAs.

No.

GO

conc.

(mg/ml)

Thermal

annealing

Density

(mg/cm3)

Volume fraction

(vol. %)*

Thermal

conductivity kGA

(W/m·K)

GA1 1

Without

14.1 0.67 0.12 ± 0.006

GA2 2 28.1 1.34 0.18 ± 0.013

GA3 6 42.8 2.04 0.24 ± 0.007

GA4 12 52.4 2.50 0.36 ± 0.015

GA5 1

With

16.4 0.78 0.18 ± 0.006

GA6 2 28.2 1.34 0.23 ± 0.023

GA7 6 40.0 1.90 0.31 ± 0.023

GA8 12 49.0 2.33 0.28 ± 0.016 *Volume fraction is converted from density ratio of the GAs to graphene

(ρGraphene=2.10 g/cm3) using the equation: Vf= ρGA/ρGraphene×100%

[183, 208]. The

density of GA (ρGA) is determined by the mass and volume of each GA

sample.

The total thermal conductivity of the GAs consists of both electrical and

lattice contributions [183]

. However, the electronic contribution part kGA,e is

estimated to be less than 3% of the total thermal conductivity across the whole

measured temperature range, according to the Wiedemann-Franz law [267]

.

𝑘GA,e = 𝐿𝑇 𝜌GA⁄ (5.1)

where L, T, and ρ are the Lorentz number, temperature and electrical resistivity

respectively. Therefore, the lattice vibrations (phonons) are proposed to be the

dominant heat transfer mechanism in the GAs [55, 183, 194, 248, 268]

.

Our previous investigations [173, 174]

show that the GA synthesized from a

higher GO concentration exhibits higher electrical conductivity, due to the

better electron mobility through the contacts between graphene nanosheets.

Similar trends are also observed for the thermal properties of the GAs, as shown

in Figure 5.8 below. The thermal conductivity of the GA with 2.5 vol. %

graphene is 0.36 ± 0.015 W/m·K, which is significantly higher than those for

GAs with 0.67–2.04 vol. % graphene (0.12 ± 0.006, 0.18 ± 0.013 and 0.24 ±

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0.007 W/m·K). This significant increase in thermal conductivity with the initial

GO concentration could be attributed to a more connected network of graphene

sheets in the GAs synthesized from a higher GO concentration (see Figure 5.7

(a)–(d)). Specifically, the higher density of graphene nanosheets and the

increased overlap between nanosheets is expected to provide lower resistivity

pathways for phonons to transport through the GAs [248]

.

Figure 5.8 Effects of GO concentrations and thermal annealing on thermal

conductivities of the GAs.

Considering the extremely high thermal conductivity of graphene (up to

5300 W/m·K), all the measured values of the GAs are extremely low. The GAs

have extremely high porosities (≥ 97.5%), and all the pores inside are filled by

air, which has very low thermal conductivity (0.026 W/m·K [269]

). The low

density of graphene is expected to be the dominant factor which results in the

low effective thermal conductivity of the GAs in the bulk form [270]

. However,

the measured thermal conductivity was still lower than the values predicted by

the porosity and the conductivity of the individual graphene nanosheets. Thus

additional factors must contribute to and reduce the thermal conductivities of

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the GAs.

First, the quality of the graphene nanosheets significantly impacts the

thermal conductivity of the GAs [271]

. All the GAs studied for this thesis are

synthesized by the chemical reduction method, in which a number of defects are

introduced during the strong oxidation process and are not completely repaired

during the chemical or thermal reduction processes [46, 144, 272]

. Note that the

highest thermal conductivity of reduced graphene oxide (rGO) has been

measured to be only 6.8 ± 0.08 W/m·K [144]

, which falls well below the 5300

W/m·K of the defect-free graphene.

Second, the size of chemically derived graphene nanosheets is comparable

to the phonon mean free path (~775 nm at room temperature) [247]

. Given that

the individual nanosheets are reported to range in size from 0.2 to 2 μm [144, 273]

,

a large fraction of the graphene nanosheets within the GAs would be far smaller

than the mean free path (~775 nm). Therefore, their thermal conductivities

should also be significantly limited by the increased scattering at the nanosheet

boundaries [273]

.

Third, the GAs consist of numerous randomly distributed graphene

nanosheets in contact with each other. Heat must transfer between several

nanosheets as it conducts across the aerogel, and the thermal resistance between

the individual graphene nanosheets is likely quite high. This interface resistance

may limit the thermal conduction through the aerogel and increase its effective

thermal resistance. However, since the graphene nanosheets bridge the whole

GA bulk, the 3D networks still achieve more effective heat transport than

dispersed rGO in composites [183, 192]

.

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Furthermore, the measurement technique may involve errors arising from

the limited resolution of the IR camera, the convection due to high surface areas

of the GAs, and variations in the thermal conductivities of the GAs and

reference materials with temperature. All these errors should be taken into

consideration and minimized during the experiments.

5.4.2 Effects of thermal annealing

As shown in Table 5-3, after thermal annealing, the thermal conductivities

of GA5–7 are enhanced (kGA=0.18 ± 0.006, 0.23 ± 0.023 and 0.31 ± 0.023

W/m·K, respectively), compared with GA1–3 without annealing. The thermal

conductivity of GA8 (0.28 ± 0.016 W/m·K) is slightly lower than that of the

sample without annealing (GA4), and is also lower than that of GA7, which is

annealed but has a lower GO concentration.

Post growth annealing treatments of carbon nanotubes (CNTs) or graphene

remove the residual functional groups and repair some defects [145, 146]

. The

improved thermal conductivities of GA5–7 can be attributed to the significant

elimination of saturated sp3 bonds bearing functional groups (which cause

enhanced phonon scattering and hinder the thermal transport [144, 271]

) and the

formation of sp2-hybridized carbon atoms. In contrast, the decreased thermal

conductivity of the GA8 may be due to the condensation of graphene

nanosheets during thermal annealing, as is indicated by the right-shift of the

XRD spectrum for GA8 in Figure 5.9. Phonon scattering between multi-layered

graphene sheets leads to a significant decline of the instinct thermal

conductivity.

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Figure 5.9 XRD patterns of the GA4–5, 7 and 8. Broad peaks indicate the

non-crystal aerogel stucture. Compared with GA7, the peak of GA8 shifts right

and indicates the smaller interspacing between graphene nanosheets.

5.4.3 Prediction of thermal boundary resistance and thermal conductivity of

graphene nanosheets within GAs

The rule of mixtures [274]

and effective medium theory (EMT) [251]

have

been applied to predict the range of the thermal conductivity of the rGO

nanosheets, as shown in Figure 5.10 below. The GAs are considered a

two-phase system consisting of rGO and air with thermal conductivities kG and

kair, respectively (kair =0.026 W/m·K [269]

). A first estimation of the thermal

conductivity of graphene aerogels (kGA) can be calculated through the rule of

mixtures:

𝑘𝐺𝐴 = 𝑓 𝑘𝐺 + (1 − 𝑓)𝑘𝑎𝑖𝑟 (5.2)

where f is the volume fraction of graphene. This model predicts the thermal

conductivity of the rGO kG to be 12.2 W/m·K, neglecting the effects of the

thermal boundary resistance between nanosheets. Both the rule of mixtures and

the EMT approximations do not consider the details of the microstructure of the

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GAs (pore size, shape etc.) or convective heat transfer within pores, but both

provide an estimation of the thermal conductivity of the graphene fraction of the

aerogel.

Figure 5.10 The thermal condictivity of the GAs as a function of graphene

volume fraction. Best fits from rule of mixtures (dashed line) and EMT (orange

dots) are shown. For the rule of mixtures, the slope of the least-squares best fits

to the experimental data is the (kG-kair). For EMT, the values calculated assume

a kG=30.2 W/m·K, a value which is obtained by manually fitting the data.

A modified effective medium theory (EMT) based model can also be used

to estimate the thermal conductivity:

𝑘𝐺𝐴 = 𝑘𝐺 [3𝑘𝑎𝑖𝑟+2𝑓(𝑘𝐺−𝑘𝑎𝑖𝑟)

(3−𝑓)𝑘𝐺+𝑘𝑎𝑖𝑟𝑓+𝑅𝐵𝑘𝑎𝑖𝑟𝑘𝐺𝑓

𝐻

] (5.3)

where RTBR is the TBR [250]

between rGO and air (RTBR=10-5

Km2/ W

[147, 275])

and H is the total thickness of rGO, taken to be 3 nm in this calculation. The

thickness of an rGO monolayer has been reported to be 0.6 to 0.9 nm [172, 276]

,

and here the GAs are assumed to consist of 5-layer rGO nanosheets on average.

This model assumes that the graphene nanosheets are randomly dispersed and

not interconnected. It should be noted that although RTBR is incorporated in the

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EMT model, it does not take into account the TBR between nanosheets, but

rather the resistance between the nanosheets and air. The thermal conductivity

of the rGO of kG=30.2 W/m·K is determined from this EMT model [194, 277]

and

is considered an upper bound to the thermal conductivity. Thus the thermal

conductivity of the chemically derived graphene nanosheets in our work is in

the range of 12.2–30.2 W/m·K, which is a factor of 1.8–4.4 higher than the

value of the previous work [144]

.

5.5 Conclusions

In conclusion, the effects of chemical composition, synthesis conditions,

reducing agents and CNT inclusions on the multifunctional properties of the

GAs were systematically investigated in terms of the electrical property,

thermal stability and conductivity. The experimental results show that higher

GO concentrations, higher reduction temperatures and longer reduction times

increase the electrical conductivities of the GAs. The GAs synthesized with

more efficient reducing agents exhibit a higher electrical conductivity than

those with less efficient reducing agents. The addition of CNTs enhances the

electrical conductivities of pure GAs up to 2.8 times, while thermal annealing at

450 °C in Ar can lead to an increase of up to 5 times. The thermal stability of the

GAs is mainly affected by the morphological characteristics of the GAs. In

general, a more compacted structure leads to better thermal stability. The DTA

peak temperatures can possibly be optimized by adjusting the GO

concentrations, synthesis conditions, selection of reducing agents and CNT

inclusions.

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A comparative infrared technique has been developed to measure the

thermal conductivities of the GAs; it reports the first benchmark results of the

thermal conductivities of GAs as a function of GO concentrations, and also

investigates the effects of thermal annealing on their thermal properties. For this

thesis, the thermal conductivity of the GAs is measured to be 0.12–0.36 W/m·K,

much lower than that of pristine graphene. These low values are likely due to

the high porosity of the GAs, the low quality and small size of the chemically

derived graphene, and the large thermal boundary resistance at the

graphene–graphene and graphene–air contacts.

In general, the thermal conductivity of the GAs can be controlled by

optimizing the GO concentration and other synthesis conditions (i.e. synthesis

temperature and time). Post-thermal annealing increases the thermal

conductivities of the GAs synthesized with a GO suspension of low graphene

concentration. In addition, by fitting the data with the rule of mixtures and

effective medium theory, the thermal conductivity of rGO is estimated to be

12.2–30.2 W/m·K. Due to their unique mesoporous network structure, GAs

have great potential to be developed into graphene-based composites by taking

advantage of capillary forces to infiltrate the porous network.

The multifunctional properties of the GAs will be summarized again in the

Conclusion chapter.

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CHAPTER 6: Advanced Multifunctional Graphene

Aerogel–Poly (methyl methacrylate) Composites:

Experiments and Modelling

6.1 Introduction

Poly (methyl methacrylate) (PMMA) is a common type of thermoplastic.

Because of its unique advantages, such as optical clarity, low density, low cost,

and good physic-mechanical properties, PMMA has been widely used in the

medicine, optical, automobile, architectural, and construction industries.

Several articles have demonstrated the successful incorporation of graphene

nanosheets into the PMMA matrix. The results show that at only 1 wt. % of

graphene loading, the elastic modulus and ultimate tensile strength for PMMA

increase by 80% and 20% respectively [227]

, while at 2.7 vol. % loading, the

measured electrical conductivity of PMMA particles reaches 64 S/m [66]

. In

addition, at ~5 wt. % loading of graphene nanoplatelets, the glass transition

temperature Tg for PMMA is also reported to increase by 30% [278]

.

In this chapter, we develop a new approach to prepare highly conductive

and ultra-strong GA–PMMA nanocomposites by backfilling PMMA into GAs.

As presented in Section 3.2, the GAs were prepared through the modified

Hummers’ and chemical reduction method from graphite. PMMA was in situ

polymerized from the MMA monomer and infiltrated into the pores of the GAs

by capillary forces. The microhardness, electrical, and thermal properties of

these GA–PMMA nanocomposites were investigated. EMT theory was applied

to predict the thermal boundary resistance (TBR) of graphene–PMMA contact.

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6.2 Structure of GA–PMMA nanocomposites

Upon chemical reduction, robust porous GAs as shown in Figure 6.1(a)

below are self-assembled by partially overlapped graphene nanosheets due to

π–π stacking. The GA–PMMA nanocomposites are obtained after the liquid

polymer precursor (pre-polymerized PMMA) is completely infused and cured

within the framework of the GAs. Figure 6.1(b) below shows an as-prepared

GA–PMMA nanocomposite sample polished to a square shape with

dimensions of 10 mm (L) × 10 mm (W) × 1.2 mm (H). Table 6-1 below

presents a summary of the synthesis conditions, graphene volume fraction and

multiple advanced properties of the GA–PMMA nanocomposites. The GAs are

synthesized from the GO concentrations of 1, 2, 6, and 12 mg/ml respectively,

and thus their corresponding graphene volume fractions are calculated based on

the density ratio of these as-prepared GAs to pristine graphene.

To further investigate its morphological features and evaluate the infusion

efficiency of PMMA into GAs, the cross-section of the GA–PMMA

nanocomposite is subjected to FE-SEM. As the image shown in Figure 6.1(d),

the GA network (see Figure 6.1(c) below) is completely infiltrated with PMMA

and the graphene nanosheets also adhere well to the PMMA. As with the

reported interaction between graphene and other polymers [45, 192, 227, 279]

, a good

wetting behavior is also considered to exist here between the reduced graphene

oxide (rGO) and PMMA. This can be potentially attributed to the formation of

hydrogen bonds between the remaining oxygen-containing groups of rGO and

the carbonyl of PMMA, which is analogous to the crystalline interfacial region

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reported for poly (vinyl alcohol)-based composites.

Figure 6.1 Digital images of (a) GA and (b) GA–PMMA nanocomposite and

FE-SEM images of (c) the porous GA without PMMA infiltrated and (d) the

cross section of the GA–PMMA nanocomposite.

Table 6-1 Synthesis conditions, graphene volume fraction, and multifunctional

properties of GA–PMMA nanocomposites.

No.

GO

conc.

(mg/ml)

Volume

fraction

(%)*

Electrical

conductivity

(S/m)

Vickers

microhardness

(MPa)

Thermal

conductivity

(W/ (K m))

1 0 0 10-14

205.0 ± 7.8 0.20 ± 0.01

2 1 0.67 0.160 ± 0.003 303.6 ± 29.1 0.35 ± 0.01

3 2 1.34 0.215 ± 0.006 342.5 ± 28.4 0.46 ± 0.03

4 6 2.04 0.458 ± 0.009 386.8 ± 36.1 0.58 ± 0.04

5 12 2.50 0.859 ± 0.033 462.5 ± 42.5 0.70 ± 0.03

*The volume fraction is converted from the density ratio of the GAs to graphene,

as described in Table 5-3.

In addition, as there is no interfacial cracking observed in Figure 6.1(d),

the skeleton of GAs in the nanocomposite may still remain a good intact after

being backfilled with PMMA. Hence, as compared with graphene nanoplatelets,

the GAs act not only as an ideal uniformly dispersed reinforcement material, but

also as a porous molding material for the graphene-based nanocomposites.

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6.3 Electrical property of GA–PMMA nanocomposites

In order to obtain equipotential surfaces during the electrical property test,

a thin layer of silver paste (<100 μm) is applied to both the top and bottom sides

of the GA–PMMA nanocomposites (10 mm (L) × 10 mm (W) × 1mm (H)).

Figure 6.2(a) below shows the electrical conductivity of the GA–PMMA

nanocomposites with different graphene loadings. When the graphene content

increases from 0.67 to 2.50 vol. %, the electrical conductivity of the

nanocomposites increases dramatically from 0.160 to 0.859 S/m, which

represents an improvement of more than 13 orders of magnitude compared with

that of pure PMMA (10-14

S/m [224, 233, 280]

). This significant increase in electrical

conductivity is likely a result of the increasing number of current pathways

which are generated as the graphene volume fraction increases. In addition,

even at only 0.67 vol. % graphene, the electrical conductivity of 0.160 S/m can

be a sufficient level for electromagnetic interference materials [236, 281-283]

. These

results may imply that the conductive network of the GAs is well preserved

within the GA–PMMA nanocomposites even at very low graphene loadings,

which also agrees with the observations in Figure 6.1(d).

The electrical conductivity of GA–PMMA nanocomposites could be

theoretically described further by the percolation theory [41, 43, 65, 236, 240, 278, 284]

using a power law relationship:

𝜎 = 𝜎𝑓[(𝜑 − 𝜑𝑐) (1 − 𝜑𝑐)⁄ ]𝑡 (6.1)

where σf and φ are the electrical conductivity and volume fraction of graphene

respectively, φc is the percolation threshold, and t is the ‘universal critical

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exponent’.

Figure 6.2 (a) The electrical conductivity (black dots) of GA–PMMA

nanocomposites as a function of graphene volume fraction at room temperature.

The dashed blue line is the best fit from the power law relation 𝜎𝑐 =𝜎𝑓[(𝜑 − 𝜑𝑐) (1 − 𝜑𝑐)⁄ ]𝑡 with a nonlinear least-squares algorithm, where the

fitted values are σf=2543.8, φc=0 and t=2.18, respectively. (b) Comparative

study of electrical conductivity between this work and previously reported

graphene–PMMA nanocomposites synthesized via in situ polymerization. For

comparison purposes, the values of graphene loading reported in wt. % have

been converted to vol. %.

When the electrical conductivities of the GA–PMMA nanocomposites are

fitted with a nonlinear least-squares algorithm, the best agreement occurs at

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φc=0 with the relation: 𝜎𝑐 = 2543.8𝜑2.18. It should be noted that the ‘zero

percolation threshold’ for the GA–PMMA nanocomposites is different from the

electrical behavior of the nanocomposites prepared from powdery graphene

fillers, but is consistent with that of other foam structures [285]

. In addition, the

electrical conductivity of rGO can be extracted to be 2543.8 S/m accordingly,

which is very close to the measured value of 2800 S/m reported by Zeng et al.

[224]

All the electrical conductivities measured in this work are approximately

one order greater than those of previously reported graphene–PMMA

composites (as shown in Figure 6.2(b) previously), indicating that the use of

GAs to develop graphene–polymer nanocomposites may be a more effective

way to solve the agglomeration problem of graphene nanosheets in the matrix.

6.4 Thermal stability of GA–PMMA nanocomposites

To investigate the thermal stability of the GA–PMMA nanocomposites, as

well as the extent of interaction between graphene nanosheets and PMMA, the

thermal degradations of pure PMMA and the GA–PMMA nanocomposite with

2.50 vol. % graphene loading are evaluated for comparison, as shown in Figure

6.3. Compare with the weight loss profile of pure PMMA, the TGA curve of the

GA–PMMA nanocomposite remarkably shifts towards a higher temperature.

The onset degradation temperature (the temperature at 5% weight loss) [286]

of

the GA–PMMA nanocomposite increases by 16 °C while the maximum

degradation temperature (the temperature at 50% weight loss) [231]

increases by

37 °C compared with pure PMMA. This significant enhancement in thermal

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stability could also be attributed to the incorporation of homogeneously

dispersed graphene nanosheets, which act as barriers to inhibit the mobility of

PMMA chains during pyrolysis [63, 231-233]

.

Figure 6.3 Thermogravimetric curves of PMMA and GA–PMMA

nanocomposites.

Additionally, while pure PMMA completely degrades above ~380 °C, ~4

wt. % residual weight could still be observed in the GA–PMMA nanocomposite

until ~550 °C, due to the presence of thermally stable graphene nanosheets [44,

286], which is consistent with the converted weight fraction of graphene in the

GA–PMMA nanocomposite.

6.5 Thermal property of GA–PMMA nanocomposites

The results, plotted in Figure 6.4 below, are similar to those of electrical

conductivity. The thermal conductivity of the GA–PMMA nanocomposites also

increases with the increase in graphene concentration. The GA with 2.50 vol. %

graphene loading yields a thermal conductivity of as high as 0.70 W/m·K,

which is 3.5 times that of the pure PMMA (0.20 W/m·K) used here [287-289]

, and

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also nearly 2 times greater than that of GO–filled PMMA nanocomposites [290]

.

Compared with the nanocomposites containing the same concentration but

non-uniformly dispersed graphene, the high thermal conductivity of the GA

network may provide much more effective channels for phonons to transfer.

Additionally, a strong interface and large contact area between the graphene and

the polymer matrix are also key factors that help increase the thermal

conductivity of the nanocomposites [248]

.

Figure 6.4 The thermal conductivity of GA–PMMA nanocomposites as a

function of graphene volume fraction. Inset is the set-up scheme for the

comparative infrared microscopy technique, where the amorphous quartz

having thermal conductivity of 1.3 W/m·K is used as the reference material. To

extract the thermal conductivity of rGO and TBR between rGO and PMMA, the

experimental data is fitted with a modified effective medium theory

simultaneously by a nonlinear least-squares algorithm. The red dashed line

represents the best fitting with the thermal conductivity of rGO (30.0 W/ m·K)

and the rGO-PMMA TBR (3.78×10-8

Km2/W).

However, considering the outstanding thermal conductivity of graphene

(5300 W/m·K [55]

), this improvement in the GA–PMMA nanocomposites seems

rather modest. This great mismatch is not only caused by the low intrinsic

thermal conductivity of rGO [143, 144]

, but also the large thermal resistance (also

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known as Kapitza [249, 250, 291]

resistance) at the graphene–graphene [291]

and

graphene–PMMA interfaces [249]

.

A modified effective medium theory (EMT) is applied to model the

thermal conductivity of the GA–PMMA nanocomposites through the

relationship:

kGA−PMMA = krGO [3kPMMA+2f(krGO−kPMMA)

(3−f)krGO+kPMMAf+RBkPMMAkrGOf

H

] (6.2)

where RB is the TBR between rGO and PMMA, and H is the total thickness of

the rGO, which is taken to be 3 nm on average in this calculation [172, 276, 292]

.

When rGO nanosheets are assumed to be uniformly dispersed in PMMA and

not interconnected, an rGO thermal conductivity of ~30.0 W/m·K and a TBR

value of 3.78×10-8

km2/W are extracted from the best fit. The results are

consistent with our previous estimation for the thermal conductivity of rGO [292]

and on the same order of other reported TBR values for graphene–polymer

systems (~10-8

km2/W)

[247], respectively. Although the direct rGO–rGO

conduction is neglected in this model, the graphene-graphene boundary

resistance [(6.5–7 .7)×10-8

km2/W]

[291] is likely to be close to the TBR between

rGO and PMMA, and thus the disparity of our estimation may not be

significant.

6.6 Microhardness of GA–PMMA nanocomposites

In order to investigate the improvement in hardness, microindentation tests

are performed on the GA–PMMA nanocomposites and compared with pure

PMMA [282, 283]

. An increasing trend of microhardness with the increase of

graphene nanosheets can be clearly observed in Figure 6.5 below. With 0.67 to

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2.50 vol. % graphene incorporated, the hardness values for the GA–PMMA

nanocomposites exhibit an increase from 48% to more than twice compared

with pure PMMA (215 MPa). In this work, the GA with 2.50 vol. % graphene

yields a maximum hardness of 462.5 MPa, which is significantly higher than

the first benchmark result (153.1 MPa at 0.6 wt. % graphene) reported by Das et

al. [293]

, and is even comparable to that of PMMA nanocomposites reinforced by

high-quality exfoliated graphite [281]

(as shown in Figure 6.5).

Besides the impact of the intrinsic high hardness and strength of graphene

[294], a strong interface between rGO and PMMA is considered an essential

reason for this great enhancement [293, 294]

. The presence of rGO nanosheets is

likely to generate numerous obstacles and interlock the motion of shear bands in

the polymer matrix, which might offer a better resistance to plastic deformation

and achieve more efficient load [227]

. Furthermore, the impact of the nucleation

of an rGO–PMMA interfacial region might also be significant, which is likely

to be much stiffer and may probably result in better stress transfer than the rest

of its amorphous bulk [295]

.

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Figure 6.5 The microhardness of GA–PMMA nanocomposites as a function of

graphene volume fractions. Inset is a typical indentation for the Vickers

microhardness test. For all GA–PMMA nanocomposites, the diagonal

dimensions range from 25 to 60 μm. A prediction of the microhardness of

GA–PMMA nanocomposites, using the modified Halpin–Tsai equation, and a

comparative study of microhardness between this work and previously reported

graphene–PMMA nanocomposites are also included. For comparison purposes,

the values of graphene loading reported in mass fraction (wt. %) are converted

to volume fraction (vol. %).

Current results in terms of the mechanical property of graphene–polymer

nanocomposites appear to be scattered. Although different polymerization

methods are applied by different groups, our fabrication method still shows a

better capability in uniformly distributing graphene in composites, which could

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potentially provide even higher microhardness levels for the GA–PMMA

nanocomposites at higher graphene loadings in the GAs.

The modified Halpin–Tsai equation [296-299]

, which has been widely used to

predict the mechanical properties of nanocomposites containing fiber or platelet

fillers, is applied to model the experimental results of the microhardness of

GA–PMMA nanocomposites in this work, as shown in Figure 6.5 above. For

randomly oriented nanoplatelets, the microhardness of GA–PMMA

nanocomposites containing φ (in vol. %) fillers can be estimated by Equation

(6.3) below:

𝐻c = 𝐻𝑚 (1+2𝛼𝜂𝜑

1−𝜂𝜑) (6.3)

where Hc and Hm are the hardness of the GA–PMMA nanocomposite and pure

PMMA respectively, α=l/d is the aspect ratio of graphene nanosheets, and η is

given by Equation (6.4) below:

𝜂 =𝐻𝑓−𝐻𝑚

𝐻𝑓+2𝛼𝐻𝑚 (6.4)

where Hf is the hardness for graphene nanosheets. When Hf and α are taken as

10.8 GPa and 400 respectively, the prediction in Figure 6.5 above shows an

excellent agreement with the experimental data. This theoretical analysis also

suggests that an effective load transfer occurs between the fillers and the matrix,

which can further confirm the good dispersion of graphene in PMMA and a

strong bond between the graphene and PMMA.

6.7 Conclusions

In summary, we have demonstrated a novel method of fabricating

GA–PMMA nanocomposites by infiltrating a PMMA precursor into the

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network of the GAs, which is followed by curing. Because of the uniform

distribution of graphene nanosheets in the PMMA matrix, when the graphene

loading increases from 0.67 to 2.50 vol. %, the GA–PMMA nanocomposites

exhibit significant enhancements in their electrical conductivities (0.160–0.859

S/m), microhardness (303.6–462.5 MPa), and thermal conductivities

(0.35–0.70 W/m·K), compared with pure PMMA and graphene–PMMA

nanocomposites prepared by traditional powdery dispersion methods. The

percolation theory, Halpin–Tsai equation, and effective medium theory are

applied to model the electrical, microhardness, and thermal properties,

respectively, of the GA–PMMA nanocomposites, and all yield good

agreements with the experimentally measured data. The thermal boundary

resistance of the graphene–PMMA is estimated to be 3.78×10-8

Km2/W in this

work. This novel fabrication method for the GA–PMMA nanocomposites may

effectively solve the dispersion issue of graphene (or CNTs) in the polymer

matrix, and also offer a facile approach for the preparation of various

filler-matrix nanocomposites with multifunctional capabilities. These

GA–PMMA are expected to find diverse applications in the fields of aerospace,

tissue scaffolds [43]

, composite electrodes [43]

, biosensors [300]

, energy generation,

and storage [301]

.

The development and multifunctional properties of the GA–PMMA

nanocomposites will be summarized again in the Conclusion chapter.

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CHAPTER 7: Conclusions and Recommendations

7.1 Conclusions

Graphene aerogels (GAs), having large surface area property of aerogels

and the excellent multifunctional properties of graphene nanosheets, can be

promising candidates for several applications, such as energy storage devices

and light-weight nanocomposites with advanced multifunctional properties.

From the findings of this thesis, the following conclusions can be drawn.

Firstly, this study has developed a cost-effective method to fabricate

self-assembled GAs from graphite at a low temperature range (45–95 oC). The

effects of chemical composition (initial GO concentration) and fabrication

conditions (such as reductions in temperature and time, reducing agents,

carbon nanotubes (CNTs), and thermal annealing processes) on the

morphology control, electrical property and thermal stability of the

as-prepared GAs have also been investigated comprehensively. It is found that

the GAs synthesized from a higher GO concentration have a higher surface area

and electrical conductivity, while higher reduction temperatures or longer

reduction times cause GAs to have a more packed structure with lower surface

area, higher electrical conductivity, and better thermal stability.

Similarly, the GAs synthesized with a more efficient reducing agent

exhibit a higher electrical conductivity and lower surface area, while those with

a low-efficiency reducing agent possess a lower electrical conductivity and

higher surface area. In addition, a thermal annealing treatment at 450 oC in

Argon is conducted on these GAs, further enhancing their electrical

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conductivities by approximately 5 times. To explore the effects of CNT

inclusions on the morphology and multifunctional properties of GAs,

graphene–CNT hybrid aerogels are successfully developed by adding CNTs

during the GA synthesis process. CNTs can increase the surface area of GAs up

to 14% and enhance their electrical conductivity by up to 2.8 times. The thermal

stability of the GAs is also affected by the choice of reducing agents and CNT

inclusions. An increased thermal stability is found in the GAs synthesized with

a high-efficiency reducing agent, while a decrease is found in those with a

dispersed CNT concentration above 1.0 mg/ml.

The experimental results of this thesis indicate that the morphology of GAs

can be effectively controlled by changing the synthesis parameters

appropriately; this also significantly impacts the multifunctional properties of

GAs in turn. This systematical study may provide insight into optimizing the

nanostructures and multifunctional properties of the GAs for various potential

applications, such as the development of electrode materials, energy storage

devices, and advanced nanocomposites in general.

Secondly, a comparative infrared technique to measure the thermal

conductivity and investigate the thermal conduction mechanisms of GAs has

been developed for the first time. This thesis reports the first benchmark results

of the thermal conductivity of GAs as a function of GO concentrations, and also

studies the effects of the thermal annealing process. The thermal conductivity of

the GAs with 0.67–2.50 vol. % graphene is measured to be 0.12–0.36 W/m·K,

which is several orders lower than that of pristine graphene. These low values

can likely be attributed to the high porosity of the GAs, the low quality and

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small size of the chemically derived graphene, and the large thermal boundary

resistance at the graphene–graphene and graphene–air contacts. The thermal

conductivity of the GAs can be controlled by optimizing the GO concentration

and other synthesis conditions (i.e. synthesis temperature and time), while a

post-thermal annealing of the as-prepared GAs is found to be able to increase

the thermal conductivity of the GAs synthesized from the GO suspension of low

graphene concentration. Based on the measured thermal conductivity of the

GAs, existing models are also applied to predict the thermal conductivity of the

reduced graphene oxide (rGO) in the GAs. By fitting the data with rule of

mixtures and effective medium theory, the thermal conductivity of rGO is

estimated to be 12.2–30.2 W/m·K. This appears to be the highest value reported

so far for the thermal conductivity of rGO. In addition, the developed

comparative infrared technique can be further applied to measure the thermal

conductivity of various other porous materials.

Owing to their unique mesoporous network structure, GAs have great

potential to be developed into graphene-based nanocomposites by taking

advantage of capillary forces to infiltrate their porous network. Finally, a novel

method to fabricate GA–PMMA nanocomposites has been demonstrated, in

which the network of the GAs is infiltrated by a PMMA precursor and cured in

situ. When graphene loading is varied from 0.67 to 2.50 vol. %, the GA–PMMA

nanocomposites exhibit significant enhancements in electrical conductivity

(0.16–0.86 S/m), microhardness (303.6–462.5 MPa) and thermal conductivity

(0.35–0.70 W/m·K), compared with pure PMMA and the graphene–PMMA

nanocomposites prepared by traditional dispersion methods. This could be

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attributed to the uniform distribution of the graphene nanosheets in the PMMA

matrix. The percolation theory, Halpin–Tsai equation, and effective medium

theory are applied to model the electrical, microhardness, and thermal

properties, respectively, of the GA–PMMA nanocomposites, and all yield good

agreements with the experimental data. The thermal boundary resistance of

graphene–PMMA is estimated to be 3.78×10-8

km2/W in this thesis. This novel

method of fabricating the GA–PMMA nanocomposites may effectively

overcome the dispersion challenge of graphene (or CNTs) in the polymer

matrix, thus offering an advanced approach for the preparation of various

filler-matrix nanocomposites with multifunctional capabilities.

7.2 Recommendations

However, it should be noted that for this thesis, only the chemical

reduction method is applied to synthesize GAs. The development of more

versatile and efficient methods of fabricating GAs and other carbon-based

aerogels with superior multifunctional properties will also be interesting to

investigate.

Moreover, the GAs are only applied to synthesize GA–PMMA

nanocomposites, while their application for energy storage devices has not been

investigated yet. Due to their high surface area and good multifunctional

properties, the morphology–controlled GAs may find promising applications in

batteries, fuel cells, and high-performance supercapacitors.

In addition, thermal boundary resistances (TBRs) at graphene–graphene

(Chapter 4) and graphene–PMMA (Chapter 5) interfaces are only estimated

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through the modified EMT theory, in which the size distribution, quantities, and

dispersions of graphene cannot be well considered, and only the linear relation

between the effective thermal conductivity and graphene volume fraction is

possibly involved. Therefore, more accurate models (or approaches) that can

take the complex geometry of graphene sheets into account to predict the

thermal conductivity of aerogels and composites are especially needed.

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LIST OF PUBLICATIONS

1. BOOK CHAPTER

(1) Hai M. Duong, Zeng Fan, Son T. Nguyen, Carbon Nanotube/Graphene

Aerogels, The Carbon Nanomaterials Sourcebook, Taylor & Francis (CRC

Press), 2015.

2. JOURNAL PAPERS

(1) Zeng Fan, Feng Gong, Son T. Nguyen, Hai M. Duong, Advanced

multifunctional graphene aerogel–poly (methyl methacrylate) composites:

Experiments and modeling, Carbon, 2015, 81, 396-404.

(2) Zeng Fan, Amy Marconnet, Son T. Nguyen, Christina Y. H. Lim, Hai M.

Duong, Effects of heat treatment on the thermal properties of highly

nanoporous graphene aerogels using the infrared microscopy technique,

International Journal of Heat and Mass Transfer, 2014, 76, 122-127.

(3) Zeng Fan, Daniel Z. Y. Tng, Clarisse X. T. Lim, Peng Liu, Son T. Nguyen,

Pengfei Xiao, Amy Marconnet, Christina Y. H. Lim, Hai M. Duong,

Thermal and electrical properties of graphene/carbon nanotube aerogels,

Colloids and Surfaces A: Physicochemical and Engineering Aspects, 2014,

445, 48-53.

(4) Zeng Fan, Daniel Z. Y. Tng, Son T. Nguyen, Chunfu Lin, Pengfei Xiao, Li

Lu, Hai M. Duong, Morphology effects on electrical and thermal properties

of binderless graphene aerogels, Chemical Physics Letters, 2013, 561–562,

92-96.

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161

(5) Son T. Nguyen, Hoa T. Nguyen, Ali Rinaldi, Nam P. V. Nguyen, Zeng Fan,

Hai M. Duong, Morphology control and thermal stability of

binderless-graphene aerogels from graphite for energy storage applications,

Colloids and Surfaces A: Physicochemical and Engineering Aspects, 2012,

414, 352-358.

(6) Jingduo Feng, Son T. Nguyen, Zeng Fan, Hai M. Duong, Advanced

fabrication and oil absorption properties of superhydrophobic recycled

cellulose aerogels, Chemical Engineering Journal, 2015, revised.

3. CONFERENCE PROCEEDINGS

(1) Zeng Fan, Peng Liu, Thang Q. Tran, Hai M. Duong, Advanced fabrication

of carbon nanotube aerogels by chemical vapor deposition. NT15, 29th

June-3rd

July 2015, Nagoya, Japan.

(2) Thang Q. Tran, Peng Liu, Zeng Fan, Nigel H.H. Ngern, Hai M. Duong,

Advanced multifunctional properties of aligned carbon nanotube–epoxy

composites from carbon nanotube aerogel method, 2015 MRS Spring

Meeting & Exhibit, 6th

-10th

April 2015, San Francisco, California, USA.

(3) Peng Liu, Thang Q. Tran, Zeng Fan, Nigel H. H. Ngern, Hai M. Duong,

Advanced multifunctional properties of aligned carbon nanotube–epoxy

composites from carbon nanotube aerogel method, APS March Meeting

2015, 2nd

-6th

March 2015, San Antonio, Texas, USA.

(4) Peng Liu, Zeng Fan, Abhik Damani, Thang Q. Tran, Hanlin Cheng, Son T.

Nguyen, Vincent Tan, Hai M. Duong, Synthesis of carbon

nanotube/graphene aerogel hybrid material by chemical vapor deposition

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162

for energy storage devices, International Meeting on the Chemistry of

Graphene and Carbon Nanotubes, 30th

March-3rd

April 2014, Riva del

Garda, Italy.

(5) Zeng Fan, Daniel Z. Y. Tng, Clarisse X. T. Lim, Son T. Nguyen, Amy

Marconnet, Christina Y. H. Lim, Hai M. Duong, Electrical and thermal

properties of morphology–controlled carbon nanotube/graphene aerogels,

International Meeting on the Chemistry of Graphene and Carbon Nanotubes,

30th

March-3rd

April 2014, Riva del Garda, Italy.

(6) Peng Liu, Zeng Fan, Thang Q. Tran, Hanlin Cheng, Son T. Nguyen, Hai M.

Duong, Vertically aligned carbon nanotubes/graphene aerogels for energy

storage devices, 22nd

International Conference on Processing and

Fabrication of Advanced Materials (PFAM XXII), 18th

-20th

December

2013, Kent Ridge Guild House, Singapore.

(7) Hanlin Cheng, Stephanie C. P. Neo, Lilian Medina, Son T. Nguyen, Zeng

Fan, Hai M. Duong, Carbon/MWNTs and PEDOT/MWNTs aerogel

composites for supercapacitor application, International Conference on

Materials for Advanced Technologies (ICMAT). 30th

June-5th

July 2013,

Singapore.

(8) Zeng Fan, Daniel Z. Y. Tng, Clarisse X. T. Lim, Chunfu Lin, Son T.

Nguyen, Amy Marconnet, Hai M. Duong, Electrical and thermal properties

of morphology–controlled graphene/carbon nanotube aerogels for energy

storage devices, NT13 : Fourteen International Conference on the Science

and Applications of Nanotubes, 24th

-28th

June 2013, Espoo, Finland.

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163

(9) Zeng Fan, Daniel Z. Y. Tng, Son T. Nguyen, Jingduo Feng, Hai M. Duong.

Morphology effects on electrical properties of advanced graphene aerogels,

2013 MRS Spring Meeting & Exhibit, 1st-5

th April 2013, San Francisco,

California, USA.

(10) Shao Kai Ng, Jia Cheng Oh, Janet P. W. Wong, Son T. Nguyen, Zeng Fan,

Hai M. Duong, Green recycled cellulose aerogels from waste paper for oil

spill cleaning, 2013 MRS Spring Meeting & Exhibit, 1st-5

th April 2013, San

Francisco, California, USA.

(11) Zeng Fan, Son T. Nguyen, Daniel Z. Y. Tng, Clarisse X. T. Lim, Jingduo

Feng, Stephanie C. P. Neo, Hai M. Duong, Simple but effective method of

morphology control of graphene aerogels for energy applications, Annual

International Conference on Chemistry, Chemical Engineering and

Chemical Process (CCECP 2013), 25th

-26th

February 2013, Singapore.