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Hydrophobic and superhydrophobic coatings for corrosion protection of steel
LINA EJENSTAM
Doctoral Thesis, 2015
KTH Royal Institute of Technology
School of Chemical Science and Engineering
Department of Chemistry
Division of Surface and Corrosion Science
100 44, Stockholm, Sweden
TRITA-CHE Report 2015:54
ISSN 1654-1081
ISBN 978-91-7595-703-6
SP Chemistry, Materials and Surfaces Publication nr: A-3583
Copyright © 2015 Lina Ejenstam. All rights reserved. No part of this thesis may be
reproduced without permission from the author.
The following papers are printed with permission:
Paper I, III and IV: Copyright © Elsevier
Paper II: Copyright © Taylor & Francis
Printed at US-AB, Stockholm, Sweden 2015
Akademisk avhandling som med tillstånd av KTH i Stockholm framlägges till offentlig
granskning för avläggande av tekonologie doktorsexamen fredagen den 6 november kl.
10:00 i sal F3, KTH, Lindstedtsvägen 26, Stockholm. Avhandlingen försvaras på engelska.
iii
Abstract
Since metals in general, and steels in particular, are vital construction
materials in our modern society, the corrosion protection of said
materials is of great importance, both to ensure safety and to reduce costs
associated to corrosion. Previously, chromium (VI) and other harmful
substances were effectively used to provide corrosion protection to steel,
but since their use was heavily regulated around year 2000, no coating
has yet been developed that, in a fully satisfactory manner, replaces their
corrosion protective properties.
In this thesis, the use of hydrophobic and superhydrophobic surface
coatings as part of corrosion protective coating systems has been studied.
Since the corrosion mechanism relies on the presence of water to take
place, the use of a superhydrophobic coating to retard the penetration of
water to an underlying metal surface is intuitive. The evaluation of
corrosion protective properties of the hydrophobic and superhydrophobic
surfaces was performed using mainly contact angle measurements and
electrochemical measurements in severely corrosive 3 wt% NaCl water
solution.
First, the differences in corrosion protection achieved when employing
different hydrophobic wetting states were investigated using a model
alkyl ketene dimer wax system. It was found that superhydrophobicity in
the Lotus state is superior to the other states, when considering fairly
short immersion times of less than ten days. This is due to the continuous
air film that can form between such a superhydrophobic surface and the
electrolyte, which can retard the transport of electrolyte containing
corrosive ions to the metal surface to the point where the electrical circuit
is broken. Since corrosion cannot occur unless an electrical current is
flowing, this is a very efficient way of suppressing corrosion.
An air layer on an immersed superhydrophobic surface is, however,
not stable over long time, and to investigate long-term corrosion
protection using hydrophobic coatings a polydimethylsiloxane
formulation containing hydrophobic silica nanoparticles was developed.
This system showed enhancement in corrosion protective properties with
increasing particles loads, up until the point where the particle load
instead causes the coating to crack (at 40 wt%). The conclusion is that the
hydrophobicity of the matrix and filler, in combination with the elongated
iv
diffusion path supplied by the addition of particles, enhanced the
corrosion protection of the underlying substrate.
To further understand how hydrophobicity and particle addition affect
the corrosion protective properties of a coating a three layer composite
coating system was developed. Using this coating system, consisting of a
polyester acrylate base coating, covered by TiO2 particles (with diameter
< 100 nm) and finally coated with a thin hexamethyl disiloxane coating, it
was found that both hydrophobicity and particles are needed to reach a
great enhancement in corrosion protective properties also for this system.
Keywords
Superhydrophobic coating, hydrophobic coating, corrosion protection,
contact angles, electrochemical measurements, surface characterization
v
Sammanfattning
Eftersom metaller, och då särskilt stål, är viktigta
konstruktionsmaterial i vårt moderna samhälle är korrosionsskydd av
stor betydelse, både för att garantera säkerhet och för att minska
kostnader som uppkommer i samband med korrosion. Tidigare har
sexvärt krom och andra skadliga ämnen använts för att på ett effektivt
sätt skydda stål från korrosion, men efter att deras användning kraftigt
reglerades runt år 2000 har ännu ingen beläggning utvecklats som helt
kan ersätta krombeläggningarna med avseende på funktion.
I denna avhandling har hydrofoba och superhydrofoba ytbeläggningar
och deras möjliga applikation som en del av ett korrosionsskyddande
beläggningssystem studerats. Eftersom korrosionsmekanismen är
beroende av närvaron av vatten, är användandet av en superhydrofob
beläggning för att fördröja transporten av vatten till den underliggande
metallytan intuitiv. De korrosionsskyddande egenskaperna hos
superhydrofoba ytbeläggningar utvärderades här främst med hjälp av
kontaktvinkelmätningar och elektrokemisk utvärdering i korrosiv lösning
bestående av 3 vikts% NaCl i vatten.
Först undersöktes skillnaden i korrosionsskydd som uppnås vid
användandet av ytbeläggningar med olika hydrofoba vätningsregimer
med hjälp av ett modellsystem bestående av ett alkylketendimer vax. Det
konstaterades att superhydrofobicitet i Lotusregimen är överlägset bättre
än de andra hydrofoba vätningsregimerna, i alla fall när man ser till
relativt korta exponeringstider, typiskt mindre än tio dagar. Detta beror
på att den kontinuerliga luftfilm som kan bildas på en sådan typ av
superhydrofob yta kan minska transporten av elektrolyt (som innehåller
korrosiva joner) till metallytan till den grad att den elektriska kretsen
bryts. Eftersom korrosion inte kan ske utan en sluten elektrisk krets är
detta ett mycket effektivt sätt att förhindra korrosion från att ske.
Ett luftskikt på en superhydrofob yta nedsänkt i vatten är dock inte
stabilt under lång tid. För att undersöka möjligheten till korrosionsskydd
under längre tid med hjälp av hydrofoba beläggningar utvecklades en
hydrofob ytbeläggning bestående av polydimetylsiloxan och hydrofoba
nanopartiklar av kiseldioxid. Detta system visade en förbättring av
korrosionsskyddet vid ökat partikelinnehåll upp till den koncentration
(40 wt%) där i stället sprickbildning i ytbeläggningen observerades. Från
detta system kunde slutsatsen dras att matrisens och partiklarnas
vi
hydrofobicitet i kombination med den längre diffusionsvägen som
partiklarna orsakade förbättrade korrosionsskyddet av den underliggande
metallen.
För att ytterligare förstå hur hydrofobicitet och partikeltillsatser
påverkar en ytbeläggnings korrosionsskyddande egenskaper har
dessutom ett treskikts kompositbeläggningssystem utvecklats. Genom att
använda detta beläggningssystem, som består av en basbeläggning av
polyesterakrylat, ett lager TiO2-partiklar (med en diameter på <100 nm)
slutligen belagt med ett tunt ytskikt bestående av hexametyldisiloxan så
kunde slutsatsen dras att både en hydrofob matris och partiklar behövs
för att nå en markant förbättring av ytbeläggningens
korrosionsskyddande egenskaper.
Nyckelord
Superhydrofoba ytbeläggningar, hydrofoba ytbeläggningar,
korrosionsskydd, kontaktvinklar, elektrokemiska mätningar,
ytkaraktärisering
vii
Preface
The work presented in this thesis was performed as a joint project
between the Division of Surface and Corrosion Science at KTH, and SP
Chemistry, Materials and Surfaces. My PhD project was designed to
further promote the collaboration between KTH and SP, with me
performing my work at both sites, and was started as a part of the SSF
(Stiftelsen för strategisk forskning) funded program: Microstructure,
Corrosion and Friction Control. Additional funding was provided by
RISE Research Institutes of Sweden. Valuable supervision has been given
by professor Per Claesson and professor Jinshan Pan at KTH, and by
adjunct professor Agne Swerin at SP, throughout the project. This joint
project has been highly educational to me and I am grateful I got the
chance to work with people, and procedures, both in academia and at a
research institute.
Since the topic of corrosion protection is interesting to a broad
audience, both in academia and in industry, the technical level of this
thesis has been adapted to be, hopefully, attractive to anybody with
interest in the field, without requiring specific background in either
wetting or electrochemistry.
Stockholm, October 2015
Lina Ejenstam
viii
ix
List of papers
This doctoral thesis is based on the following papers, which are referred
to in the text by their Roman numerals.
I. The effect of superhydrophobic wetting state on
corrosion protection – The AKD example
Lina Ejenstam, Louise Ovaskainen, Irene Rodriguez-Meizoso,
Lars Wågberg, Jinshan Pan, Agne Swerin and Per M. Claesson.
Journal of Colloid and Interface Science, 2013, 412, 56-64
doi: 10.1016/j.jcis.2012.09.006
II. Towards superhydrophobic polydimethylsiloxane-silica
particle coatings
Lina Ejenstam, Agne Swerin and Per M. Claesson.
Preprint, accepted for publication in Journal of Dispersion
Science and Technology, 2015
doi: 10.1080/01932691.2015.1101610
III. Corrosion protection by hydrophobic silica particle-
polydimethylsiloxane composite coatings
Lina Ejenstam, Jinshan Pan, Agne Swerin and Per M. Claesson.
Corrosion Science, 2015, 99, 89-97
doi: 10.1016/j.corsci.2015.06.018
IV. Long-term corrosion protection by a thin nano-
composite coating
Lina Ejenstam, Mikko Tuominen, Janne Haapanen, Jyrki M.
Mäkelä, Jinshan Pan, Agne Swerin and Per M. Claesson.
Applied Surface Science, In press, available online, 2015
doi: 10.1016/j.apsusc.2015.09.238
V. Comparison between AFM-based methods for assessing
local surface mechanical properties of PDMS-silica
composite layers
Hui Huang, Lina Ejenstam, Jinshan Pan, Matthew Fielden,
David Haviland and Per M. Claesson
Manuscript
x
The author’s contribution to the included papers:
Paper I: Major part of experimental work, major part of
manuscript preparation. The surface coatings were
prepared by Dr. Louise Ovaskainen, at the division of
Fibre and Polymer technology, KTH.
Paper II: All experimental work, major part of manuscript
preparation.
Paper III: All experimental work, major part of manuscript
preparation.
Paper IV: Major part of experimental work, major part of
manuscript preparation. The polyester base coat was
prepared at Akzo Nobel in Malmö in cooperation with
Dr. Majid Sababi, and the TiO2 coating was prepared by
Dr. Mikko Tuominen at Tampere University of
Technology, Finland.
Paper V: Part of initiating measurements, part of manuscript
preparation. All measurements shown in the manuscript
were performed by Hui Huang at the division of Surface
and Corrosion Science, KTH, in cooperation with the
section of Nanostructure Physics, KTH. Hui Huang also
prepared the major part of the manuscript.
xi
Summary of papers
Paper I:
The effect on corrosion protective properties of coatings representing
different wetting states was evaluated using a model system consisting of
alkyl ketene dimer (AKD) wax coatings exhibiting different hierarchical
structures. All coatings had the same surface chemistry and the effect
seen could therefore be attributed only to the difference in surface
structure. A remarkable increase in the measured electrochemical
impedance was found for the coating wetting in the superhydrophobic
Lotus state, originating from the air layer present at that surface, which
slows down transport of corrosive ions from solution to substrate, to the
point where the electrical circuit is broken and no corrosion can proceed.
Paper II:
The development of a one-pot superhydrophobic coating formulation
was addressed through systematic addition of hydrophobic silica
nanoparticles (16, 60-70, 250 and 500 nm) to a polydimethylsiloxane
(PDMS) matrix. Superhydrophobicity in the Lotus state was only reached
when particles were added at such high amount (40 wt%) it caused the
coating to crack, while the superhydrophobic rose state was achieved for
non-cracked coatings, which lead to further understanding of how the
shapes of the protrusions affect the resulting wetting state.
Paper III:
The corrosion protective properties of the most promising coating
system developed in Paper II was evaluated by coating carbon steel
substrates with formulations consisting of PDMS containing 0, 10, 20 or
40 wt% hydrophobic 16 nm particles. Due to crack formation allowing
easy passage of electrolyte through the coating, the 40 wt% coating did
not provide any corrosion protection to the underlying substrate. The 20
wt% coating performed very well, although it did not reach
superhydrophobicity but displayed hydrophobic wetting behaviour. The
protective properties were assigned to the synergistic effect of the
hydrophobicity of the matrix and particles, as well as the elongated
diffusion path arising from particle addition. Beyond this, another very
interesting effect was seen. The coatings with 0 and 10 wt% particles
exhibited a surprising increase in measured impedance during the first 24
xii
hours. This effect is so large that the most likely reason is passivation of
the underlying metal, promoted by the coating properties.
Paper IV:
To further understand the corrosion protective properties seen in
paper III, a coating system consisting of a polyester acrylate (PEA) base
coat, covered by a layer of TiO2 nanoparticles (< 100 nm) which in turn
was covered by a thin hexamethyl disiloxane (HMDSO) coating was
developed. The systematic evaluation of the protective properties of the
layers one by one, two by two, and in the three layer combination showed
that to reach a long-term stable, reproducible, protective coating a
combination of properties from all three layers is needed.
Paper V:
A comparison of coating properties on the nanoscale level using three
different operating modes of atomic force microscopy (AFM) was
conducted using the polydimethylsiloxane coating (Papers II and III)
without and with the addition of 20 wt% hydrophobic silica nanoparticles
(16 nm). The surfaces were found to be quite heterogeneous on the
nanoscale level, and different regions of softer and stiffer polymer was
encountered and attributed to variations in crosslinking degree. The 16
nm hydrophobic silica particles were found to aggregate and form
structures in the size 20 - 110 nm. In addition to the particles, spherical
shapes were also seen on the surface which were recognized as air
bubbles trapped in the matrix during curing.
xiii
Nomenclature
Scientific abbreviations
ACA Advancing contact angle
AFM Atomic force microscopy
AKD Alkyl ketene dimer
CA Contact angle
CAH Contact angle hysteresis
CE Counter electrode
CPE Constant phase element
DMT Derjaguin-Muller-Toporov
EIS Electrochemical impedance spectroscopy
HMDSO Hexamethyl disiloxane
LFS Liquid flame spray
OCP Open circuit potential
PDMS Polydimethylsiloxane
PEA Polyester acrylate
RCA Receding contact angle
RE Reference electrode
RESS Rapid expansion of supercritical solutions
WE Working electrode
Symbols
C capacitance (F)
θ contact angle (°)
γ surface energy (J/m2)
r roughness ratio
λ wavelength (nm)
xiv
xv
Table of contents
Abstract ……………………………………….……….………..…….iii
Sammanfattning………………………………………….…………...v
Preface…………………………………………………….…………..vii
List of papers…………………………………………………………ix
Summary of papers………………………………………………….xi
Nomenclature……………………………………….……………….xiii
Table of contents……………………………………………………xv
1. Introduction ............................................................................. 1 1.1. Aim of this work .................................................................................... 2
2. Background ............................................................................. 3 2.1. The corrosion mechanism ................................................................... 3 2.2. Passive corrosion protection .............................................................. 4 2.3. Hydrophobic and superhydrophobic coatings .................................. 6 2.3.1. Wetting ...................................................................................................... 6 2.3.2. Fabrication of superhydrophobic surfaces .............................................. 10
3. Experimental .......................................................................... 13 3.1. Coatings .............................................................................................. 13 3.1.1. Alkyl ketene dimer wax ........................................................................... 13 3.1.2. Polydimethylsiloxane with hydrophobic silica particles............................ 14 3.1.3. Commercial polydimethylsiloxane ........................................................... 15 3.1.4. Layered composite coating ..................................................................... 15 3.1.5. Summary of coating properties ............................................................... 16
3.2. Methods ............................................................................................... 18 3.2.1. Environmental scanning electron microscopy ......................................... 18 3.2.2. Atomic force microscopy ......................................................................... 18 3.2.3. Confocal Raman microspectroscopy....................................................... 20 3.2.4. Contact angle measurements ................................................................. 21 3.2.5. Electrochemical measurements .............................................................. 22
4. Results and discussion......................................................... 25 4.1. The AKD system ................................................................................. 25 4.2. The PDMS-hydrophobic silica nanoparticle system ....................... 27
xvi
4.3. The three layered composite system ................................................ 29 4.4. Unifying concept 1: Superhydrophobicity........................................ 30 4.4.1. Shape, size and distribution of protrusions .............................................. 30 4.4.2. Air film stability under water .................................................................... 34
4.5. Unifying concept 2: Corrosion protection ........................................ 36 4.5.1. Effect of wetting state on corrosion protection ......................................... 36 4.5.2. Barrier effect from particles ..................................................................... 39 4.5.3. Possible passivation of underlying substrate ........................................... 41
4.6. Commercial PDMS .............................................................................. 43 4.7. Mechanical properties of PDMS coating........................................... 45 4.7.1. Nanomechanical properties of PDMS coating ......................................... 45
5. Conclusions .......................................................................... 47
6. Future work ........................................................................... 49
7. Acknowledgements .............................................................. 51
8. References ............................................................................ 53
INTRODUCTION | 1
1. Introduction
Metals are important construction materials in the world today, and,
for example, steel is used in almost every bridge, building and
transportation vehicle built. Due to this, corrosion protection of metals
has become an issue of great importance, foremost to ensure the safety of
constructions and vehicles, but also to great extent out of economic
concerns. In the United States costs associated with corrosion were
concluded to be circa 3 % of the gross domestic product (GDP) in 2002
[1], and today all industrialized countries, in general, experiences costs
related to corrosion corresponding to 1 – 4 % of their country’s GDP [2].
Until recently corrosion protection could be achieved efficiently
through the use of chromium containing coatings. However, chromium
(VI) ions have been proven harmful, both to humans and to the
environment [3, 4] and around year 2000 the use of chromium (VI) was
heavily restricted. Today its use is not acceptable in any concentrations
[4]. Due to these regulations there is a need to develop efficient and
environmentally friendly, non-toxic, corrosion protection systems. One
approach is to use polymeric coatings, which gains extra interest due to
their flexibility, the possibility to make them water based or solvent free,
and their comparatively low cost [5].
From this point of view it is not surprising that the interest in the
development of environmentally friendly corrosion protective coatings
has escalated recently [6]. This is clearly visualized in Figure 1, where the
number of patents and research publications returned by a search for
“corrosi* AND protect* AND coating” are plotted versus publication year
[7]. Since the regulation of chromium (VI) use came into place, there has
been a continuous increase in reported research regarding alternative
ways to protect metal from corrosion. An increase in filed patents can also
be seen just around year 2000 when these regulations came into place.
2 | INTRODUCTION
Figure 1. Number of patents and research publications returned when searching for
“corrosi* AND protect* AND coating” versus year of publication. A continuous increase of
research articles can be seen as a reaction to the restriction of the chromium (VI) use.
1.1. Aim of this work
The overall aim of this project was initially to develop a thin top coat
layer, to be used as part of a corrosion protective coating system. The top
coat layer should retard transport of water to the underlying metallic
substrate. Subsequently an investigation of other applications for such
coating was intended, with specific focus on possible friction control and
wear. Originating from these aspirations the decision to focus the work on
superhydrophobic surface coatings was simple, especially since their
positive effect on corrosion and friction control already had been
reported. Following promising results attained at the beginning of the
corrosion protection evaluation, a need to understand the underlying
mechanism arose, and focus was put on that during the second part of
this work.
Ultimately, the two most important goals of this work became:
Develop an easy to use, one-pot, superhydrophobic surface coating,
preferably without the use of environmentally harmful compounds.
Evaluate and understand the corrosion protective properties of such
coating systems.
BACKGROUND | 3
2. Background
Corrosion protection by hydrophobic and superhydrophobic coatings
falls into an interdisciplinary field, between classical corrosion science
and wetting, and to help the reader to more easily follow the discussions
when looking at the results, the most important features of these two
fields are first briefly presented in this chapter.
2.1. The corrosion mechanism
By corrosion one commonly refers to the oxidation, and following
dissolution, of a metallic material. The oxidation is balanced by a
reduction of a non-metal, for example oxygen, to create a system of redox
reactions. The oxidation of the metal typically occurs at the
metal/environment interface and constitutes the anodic reaction, while
the reduction of oxygen, which typically occurs in solution, often
constitutes the cathodic reaction [6]. The anodic and cathodic reactions
together form an electrical circuit, which is completed by conduction of
electrons in the metal substrate and by ionic conduction through the
electrolyte. In conductive materials the anodic and cathodic reactions can
take place at widely separated locations of the surface, or just next to each
other. If there is a separation of the sites, the anodic one tends to become
acidic and the cathodic one becomes alkaline, due to the species released
by the corrosion reactions [6].
Iron is one of the most frequently used construction metals and the
corrosion mechanism of iron is therefore also one of the most well
studied, and it constitutes an important example of metallic corrosion. In
an environment including water and oxygen, corrosion products of iron
will entail a complicated mixture of hydrated iron oxides and other
related species. If these corrosion products can form a dense, insoluble,
film with good adherence to the underlying metallic surface, the corrosion
reaction may be self-limiting due to passivation [6, 8]. However, many of
the iron oxides are porous, and the more stable ones are very sensitive to
the presence of chloride ions, which will cause the oxide layer to degrade
4 | BACKGROUND
rapidly [9]. The simplest form of reactions associated with corrosion of
steel, in the presence of water and oxygen, is given below.
Fe Fe2+ + 2 e- (anodic reaction)
O2 + 4 e- + 2 H2O 4OH- (cathodic reaction)
Fe2+ + 2 OH- Fe(OH)2
4 Fe(OH)2 + O2 2 Fe2O3 + 4 H2O (formation of iron oxide)
2.2. Passive corrosion protection
Applying an organic coating to a metal surface is often an efficient way
of protecting the metal from corrosion, while still maintaining the
desirable mechanical properties [5, 6, 10], and the use of
superhydrophobic, or hydrophobic, coatings to slow down the transport
of water containing corrosive ions to the underlying substrate has been
studied before [11-18].
The corrosion process on a bare metal is complicated in itself, and the
corrosion rate and the morphology of the corrosion products depend on
several factors [19]. However, when applying an organic coating on top of
the surface, the number of parameters to take into account in an
evaluation dramatically increases. Coating thickness, size and
distribution of pores, barrier properties to water and oxygen, adhesion to
the substrate and ionic conductivity are only a few of the parameters that
greatly affect the corrosion protective properties of a coating [19].
The corrosion protective mechanism of an organic coating system can
roughly be divided into three groups: the electrochemical effect, the
physicochemical effect and the adhesion to the substrate [8]. The
adhesion is very important since the protective effect of the coating will
completely fail at areas where delamination occur, creating easy access to
areas where corrosion can proceed without restriction. The focus of this
thesis has, however, not been on coating adhesion, and therefore this
issue will not be further discussed.
By the electrochemical effect the, often high, electrical resistance of
organic coatings is referred to. This will severely slow down the corrosion
process since corrosion is dependent on electrical flow, and the possibility
to create a closed electrical circuit. No organic coating is impermeable to
BACKGROUND | 5
water [8], and will therefore not avert the reduction of water to form
hydroxide ions. However, organic coatings exhibit high electrical
resistance and low ion solubility, which will block ionic pathways between
anodic areas and cathodic areas from being formed, and effectively
suppress the formation of corrosion products and thereby also the
progress of corrosion [5, 6].
Physicochemical effects include coating properties such as wetting and
effects due to addition of fillers, pigments or inhibitors. Inhibitors are
compounds, which actively react when corrosion starts, in a way designed
to counteract the corrosion. Wetting properties and inactive fillers, such
as pigments, play a great role in the work presented here. The pigments
and fillers enhance the barrier effect of the coating by prolonging the
diffusion pathway through the coating to the substrate. Increasing the
coating thickness will also result in an increase of its barrier properties [3,
8, 9, 20, 21]. Pigments may also prevent direct ionic conduction through
the coating by blocking the formation of pathways [6]. In Figure 2, the
possible reactions associated with corrosion are visualized on a steel
substrate carrying a polymeric coating. Dotted arrows indicate how the
diffusion of iron oxides and corrosive ions from solution are slowed down
due to elongated diffusion path from fillers and selective permeability of
the polymer matrix.
Figure 2. Schematic overview of the corrosion mechanisms of a polymer coated metallic
substrate. Dotted arrows indicate partly restricted diffusion paths.
In industry, polymer coatings designed to prevent corrosion are
combined in several layers, including pigments and/or inhibitors,
reaching a final combined thickness ranging from a few micrometers up
to one millimeter [22, 23]. For coatings used for research, the thicknesses
6 | BACKGROUND
often range from a few micrometres up to several hundreds of
micrometres, and the dominating polymeric matrices used to achieve
corrosion protection are epoxy, polyester, acrylate and polyurethane [24,
25]. Since the barrier effect is directly dependent on the coating thickness
it can be difficult to compare the performance of different coatings,
especially since the coating thickness it not always reported.
2.3. Hydrophobic and superhydrophobic coatings
Since the group lead by professor Barthlott discovered the extreme
water repellency and unusual self-cleaning properties of the Lotus leaf
(Nelumbo nucifera), and coined the notion of the lotus effect,
superhydrophobic surfaces have become widely studied in the field of
surface science [26, 27]. The most robust superhydrophobic structures in
nature exhibit a hierarchical structure [28, 29], but superhydrophobic
surfaces have been created using only one level structure as well [29]. In
addition to surface roughness, low surface energy is needed to render a
surface superhydrophobic.
2.3.1. Wetting
The contact angle of a liquid droplet is a convenient way of describing
the wetting properties of a surface. The contact angle is defined as the
angle where the droplet base line and the droplet tangent meet. The
contact angle can be related to the surface energies of the three interfaces
where air, liquid and solid meet as described by Young’s equation:
cos 𝜃 =𝛾𝑆𝐺−𝛾𝑆𝐿
𝛾𝐿𝐺 (1)
where θ is the contact angle, γSG , γSL, and γLG are the surface energies of
the solid-gas, solid-liquid and liquid-gas interfaces, respectively. See
Figure 3. Surfaces exhibiting a water contact angle higher than 150° are
termed superhydrophobic. A distinction should be made between the
local microscopic contact angle and the macroscopic contact angle, which
can be different, and recently it has been suggested to term the
macroscopic one “apparent contact angle” to diminish confusion [30-32].
In this work, however, the macroscopic contact angle is the only contact
angle reported and the simpler notation “contact angle” will be kept when
BACKGROUND | 7
referring to macroscopic contact angles, in accordance with the notation
used in Papers I - IV.
Figure 3. Showing the interfacial energies experienced by a droplet resting on a surface.
On structurally rough surfaces the contact angle can be described
using one of two models. Wenzel first described the situation where the
liquid fully penetrates the surface structure [33] by the following
equation:
cos 𝜃 = 𝑟 cos 𝜃0 (2)
where θ is the contact angle, r is the roughness ratio (ratio of the true
solid surface area over the apparent area), and θ0 is the contact angle of a
corresponding flat surface of the same material. Cassie and Baxter then
described the situation when air is trapped in the surface structure
creating a composite layer for the droplet to rest on [34]. The composite
situation is described by the Cassie-Baxter equation:
cos 𝜃 = 𝑟𝑓𝑆𝐿 cos 𝜃0 − 1 + 𝑓𝑆𝐿 (3)
where fSL is the fraction of the composite consisting of solid-liquid
interface [26, 28, 35, 36]. However, the model equations proposed by
Wenzel and Cassie-Baxter are not without shortcomings, and recently
Gao and McCarthy [37-39] received significant attention when they
published several papers stating that Wenzel and Cassie were “wrong”.
However, their main concern was to encourage the equations to be used
with care. They also put emphasis on how only the situation beneath the
three phase line determines the contact angle of the sample. This was
shown by adding patches of different structures and surface energies to a
sample, which did not affect the measured contact angle as long as the
different patches were fully covered by the water droplet. Also Extrand
[40] came to similar conclusions.
8 | BACKGROUND
External stimuli such as pressure, vibration and evaporation can cause
a transition from partial wetting in the Cassie-Baxter state, to full wetting
in the Wenzel state [26, 28]. The transition is permanent, i.e. no
spontaneous restoring has been reported, however, if the wetting was
induced by wetting agents or surfactants restoring may be possible [41,
42]. Regardless, understanding of how to decrease the risk for such
transition is of importance when designing superhydrophobic surfaces. It
has been found that reducing the micro-structural scales increase the
threshold pressure of the wetting transition [26].
However, when dual roughness, i.e. a hierarchical structure, is
present, the Cassie-Baxter model is no longer sufficient to describe the
wetting properties since several intermediate states arise [35]. Here only
the two most important for this work will be discussed. Assuming that the
surface energy of the sample is low, air can be stuck in the larger
structures, in the smaller structures, or in both, giving rise to two types of
superhydrophobicity. To distinguish between these states the advancing
and receding contact angles of a surface become important. The
advancing contact angle (ACA) is defined as the contact angle measured
when the droplet front advances over the surface, while the receding
contact angle (RCA) is the contact angle measured when the droplet front
recedes. The contact angle hysteresis (CAH) is defined as the difference
between advancing and receding contact angles. The advancing and
receding contact angles are commonly measured using either the needle
in droplet method (further discussed in section 3.2.4) or by tilting the
sample and evaluating the ACA and RCA at the droplet front and rear at
the inclination where the droplet starts to slide. Figure 4 shows how ACA
and RCA are defined in these two cases.
Figure 4. In (a) definition of ACA (θAdv) and RCA (θRec) using needle in method are shown,
and in (b) the corresponding definition using the tilting method.
BACKGROUND | 9
When air is present in both structures, see Figure 5, the sample will
exhibit a very low contact angle hysteresis, and a droplet placed onto the
surface will easily roll off. The most famous example of this in nature is
the leaf of the Lotus flower, and therefore the low adhesion
superhydrophobicity is called Lotus state superhydrophobicity. When air
is stuck in only one of the structures (either the larger or the smaller
ones) another effect can be seen (Figure 5). A water droplet will still show
a very high advancing and static contact angle on such a surface, but if the
surface is turned up-side down, the droplet will adhere to the surface due
to a very large contact angle hysteresis created by a very low receding
contact angle. This effect is named the superhydrophobic rose state, since
water droplets on rose petals behave in this way [35].
Whether the adhesive effect of the rose state is caused by wetting of
the larger or the smaller structure is discussed. Traditionally, it has been
said that wetting into the larger structures causes the adhesion while air
in the smaller structure kept the contact angle high [26], but several
recent reports show the opposite, i.e. how water penetration into the
smaller structures (often promoted by surface structure shape) is
responsible for the high adhesion [43, 44]. Figure 5 shows four possible
wetting states of a surface exhibiting a hierarchical structure.
Figure 5. Schematic view of four possible wetting states on a surface exhibiting hierarchical
structure.
10 | BACKGROUND
It is clear that the wetting state depends on several surface properties
making it hard to predict. One of the properties is the pitch between the
protrusions and many attempts have been made to find the pitch size at
which the transition between different wetting states occurs. This varies,
however, from surface to surface depending on size, shape and
distribution of the asperities [29, 45, 46]. The shape of the surface
asperities has been given special attention by for example Teisala et al.
who propose that wetting of the smaller structure in a sample with
hierarchical structures is promoted by a rounded shape of said structures
[44]. It has also been shown that while vertical walls are sufficient to
create superhydrophobic structures, overhanging structures are needed
to create structures exhibiting high contact angles for non-polar liquids
[30, 45, 46].
2.3.2. Fabrication of superhydrophobic surfaces
It should be mentioned that the composite air/material layer needed
to create superhydrophobic surfaces can be achieved on surfaces not only
by protrusions but also by the presence of pores, the surfaces are then
termed positive or negative, respectively.
Superhydrophobic polymeric surfaces can be made in two steps where
one step focuses on lowering the surface energy and the other step
concerns addition of structure, alternatively in a one step process where
both these features are addressed simultaneously. Techniques to fabricate
superhydrophobic surfaces include: replication of natural surfaces
(directly or using a template) molding, roughening by introduction of
nanoparticles (often consisting of metal oxides or polymer), addition of
carbon nanotubes and surface modification by low surface energy
materials by plasma, electrospinning, and electron or laser treatment [36,
47-50].
Materials exhibiting low enough surface energy to make them
hydrophobic (CA > 90°) have been shown to reach superhydrophobicity
when roughened, regardless of the exact value of the surface energy, and
the conclusion that the roughness is the more critical property to achieve
superhydrophobicity can be drawn [29]. High contact angles, low
adhesion and good mechanical stability cannot be optimized concurrently
and the balance between them has to be optimized for each specific
application. In addition to this, due to the roughness features needed, it is
BACKGROUND | 11
even more challenging to produce superhydrophobic surfaces robust
enough to withstand a standard scratch test [32].
Durable and self-healing superhydrophobic surfaces
There have been a few reports on durable superhydrophobic surfaces,
and one example is the fabrication of a superhydrophobic surface by
Ebert and Bhushan. They spray coated silica particles onto an epoxy
substrate, and the resulting surface proved stable during wear
experiments using AFM, ball-on-flat tribometer and water jet apparatus
[47]. Another example is the durable superhydrophobic surface fabricated
by Deng et al. [51], using porous, raspberry-like, silica particles coated by
a fluorosilane. They tested the durability by looking at the impact of
falling sand on the superhydrophobicity and by an adhesion test using
double-sided adhesive tape. Ke et al. [52] also fabricated robust
superhydrophobic surfaces by spray coating silica particles onto the
substrate folloed by lowering of the surface energy using
polydimethylsiloxane. They then used a shear test to evaluate the
durability of the superhydrophobicity.
Lastly, there are a few reports on self-healing superhydrophobic
surfaces, for example Xue et al. [53] used an approach where particles
and low surface energy polymer are coated in a way that allows new
roughness structures to emerge if the top surface gets abraded. The same
approach was also used by Chen et al. [54], but instead facilitated by the
addition of fluorinated silica nanoparticles and photocatalytic TiO2
nanoparticles to polystyrene.
12 |
EXPERIMENTAL | 13
3. Experimental
Here follows a short description of the most important characteristics
of the four coatings featured in this thesis, and of the key techniques used
to evaluate them. A more thorough description of both coatings and
techniques can be found in Papers I-V.
3.1. Coatings
3.1.1. Alkyl ketene dimer wax
The alkyl ketene dimer (AKD) wax, used in Paper I, was spray coated
onto polished carbon steel substrates using the rapid expansion of
supercritical solutions (RESS) technique [55, 56]. Supercritical carbon
dioxide was used as solvent and different surface structures were
obtained by moving the spray nozzle at different speeds, and by varying
the number of layers applied. For reference, AKD-wax was also dissolved
in toluene and spin-coated onto a substrate. Figure 6 shows the molecular
structure for AKD where R1 and R2 are long carbon alkyl chains, in Paper
1 differential scanning calorimetry (DSC) showed a mixture of C16 and
C18 chains for the AKD used.
Figure 6. The structure of the AKD molecule where R1 and R2 represent long carbon alkyl
chains. Reprinted with permission. Copyright © Elsevier 2013.
14 | EXPERIMENTAL
3.1.2. Polydimethylsiloxane with hydrophobic silica particles
In Papers II, III and V, a model polydimethylsiloxane (PDMS) based
coating, containing varied amounts of hydrophobic silica nanoparticles,
was developed and evaluated. The formulation was based on as few
components as possible to allow fundamental understanding of the
system. PDMS was chosen as material due to its low surface energy, 20.4
mJ/m2, which renders a water contact angle of 107 ° on a flat surface
[36]. In Paper II, a range of particle sizes was evaluated, starting at
hydrophobic silica nanoparticles, with a primary particle size of 16 nm,
and continued by 60-70 nm, 250 nm and 500 nm silica particles which
were hydrophobized using dimethyl dichlorosilane before addition to the
matrix. In Papers III and V, only the 16 nm hydrophobic silica particles of
varied amounts were used. The mixtures were spin coated onto glass
slides, or polished carbon steel substrates, depending on the intended
evaluation method. A fluorosilane was used to crosslink the PDMS
coating through a condensation curing mechanism, see Figure 7. The
curing process was slow, and a steady state value for the receding contact
angle was found only after one week of curing for these surfaces. The
optimization of the PDMS-based coating is described in detail in Paper II,
in Paper III the corrosion protective properties of the coating are
evaluated and in Paper V the nanomechanical properties are studied.
Figure 7. Condensation curing of the model PDMS system, where in the first step the
fluoropolymer crosslinker is hydrated and in the second step the crosslinker binds to the
PDMS prepolymer in a condensation reaction.
EXPERIMENTAL | 15
3.1.3. Commercial polydimethylsiloxane
A commercial PDMS-formulation (PDMS 3-1953 Conformal, Dow
Corning, Ellsworth Adhesives AB) was evaluated for comparison. This
coating was chosen to match the model PDMS coating developed in Paper
II as closely as possible. It is also cures by the condensation curing
mechanism and exhibits a tack-free time of 8 min at ambient conditions.
The commercial PDMS-formulation was spin coated onto polished steel
substrates using the same settings as for the model coatings, 2000 rpm
for 30 s, and it was subsequently cured at 60 °C and 15 %RH for 1 hour.
Due to the clear color of the coating, it was concluded that it does not
contain particles with a diameter larger than 20 nm, but the coating does
contain adhesion promoters and other additives which were not present
in the experimental formulation.
3.1.4. Layered composite coating
The coating system presented in detail in Paper IV, was designed to
allow evaluation of each component with respect to the corrosion
protective properties achieved from the complete coating system. A
polyester acrylate (PEA) coating was chosen as base coat due to its
promising results regarding corrosion protection [57, 58] and its good
adhesion to the substrate. On top of that, a layer of TiO2 nanoparticles
was coated using a liquid flame spray (LFS) technique, resulting in
particles with a diameter < 100 nm [59-64]. Finally a hexametyl
disiloxane (HMDSO) coating was applied, by plasma polymerization [65],
to lower the surface energy of the coating system. These layers were then
applied one by one, two by two, and all three on top of each other, to
compile the sample matrix. A visualization of the buildup of the coatings
is provided in Figure 8, and in Figure 9 the chemical structures of PEA
and HMDSO are shown.
Figure 8. The buildup of individual samples constituting the evaluation matrix for the three
layered composite coating. Reprinted with permission. Copyright © Elsevier 2015.
16 | EXPERIMENTAL
Figure 9. Chemical structure of PEA and HMDSO, as well as the structure of HMDSO after
plasma coating.
3.1.5. Summary of coating properties
In table 1, a few important properties of the different coatings are
summarized to provide a base to the subsequent discussions. The main
coating method was spin coating because of its simplicity. The two spray
coating techniques (RESS and LFS) were very successful at creating the
coveted hierarchical structure, but the porosity of the applied coatings
posed a considerable drawback during the corrosion protection tests. The
coating thickness was approximately 11 ± 5 µm for all coatings included in
this thesis, which is considerably thinner than commercial polymeric
coatings used for corrosion protection.
Wetting states ranging from hydrophilic to superhydrophobic in the
Lotus state were realized in this work. Hydrophobicity was found to
greatly improve the corrosion protective properties of the coatings, and
focus was put on the development and evaluation of hydrophobic
coatings. The presence of particles will also enhance the corrosion
protective properties of a coating. The addition of 16 nm hydrophobic
silica to PDMS was investigated, as well as addition of a layer consisting
of TiO2 to a PEA base coat, with and without, subsequent
hydrophobization through addition of HMDSO plasma polymer.
EXPERIMENTAL | 17
Table 1. Summary of important properties for the four coating systems. Superhydrophobicity
is denoted SH.
AKD PDMS –
model
PDMS -
commercial
PEA-TiO2-
HMDSO
Application
method
Spray or
spin
coating
Spin coting Spin coating Spin coating,
LFS, plasma
Coating
thickness (µm)
6 - 8 ~13 13 - 16 ~11
Wetting states
achieved
SH Lotus,
SH rose,
Wenzel
SH Lotus,
SH rose,
Hydrophobic
Hydrophobic SH rose,
Hydrophobic,
Hydrophilic
Barrier particles None Hydrophobic
Silica
16 nm
None Hydrophilic
TiO2
<100 nm
18 | EXPERIMENTAL
3.2. Methods
3.2.1. Environmental scanning electron microscopy
The most important advantage with environmental scanning electron
microscopy (ESEM), compared to conventional scanning electron
microscopy (SEM), is that non-conductive samples can be imaged in the
presence of water vapor, or in another gaseous environment. This entails
that fragile samples can be imaged, without the need of first applying a
conductive coating onto it, which reduces the risk of misinterpretation of
the image due to coating artefacts.
The water vapor in the sample chamber fills two functions. Firstly, it
increases the pressure, up to ~10 Torr (1.33 kPa) is possible, which allows
imaging of sensitive samples. Secondly, water molecules hit by the
scattered electrons from the sample will become ionized, and the freed
electron can ionize another water molecule, creating a cascade effect
enhancing the signal from the sample on its way to the detector. This can
greatly improve the image quality when imaging non-conductive samples.
The ionized vapor molecules carry a positive charge and drift towards the
sample, which is gaining a negative charge from the electron beam, and
neutralizes the charging of the sample. This makes it possible to image
non-conductive sample without the negative effects encountered in
conventional SEM [36, 66].
3.2.2. Atomic force microscopy
Atomic force microscopy (AFM) is a powerful tool for imaging of
surface topography at the nanometer scale. AFM can be operated in
different modes, and for soft surface samples, such as polymers, the non-
contact mode is preferable since the cantilever tip of the AFM otherwise
could destroy the surface [36, 67-69]. In this work, two modes have been
of special importance, PeakForce QNM® (Quantitative Nanomechanical
Mapping) and ImAFM (intermodulation AFM) and they are therefore
shortly described here.
Using the AFM PeakForce QNM mode, nanomechanical properties of
the substrate can be mapped, see Figure 10. One force curve is captured
at each image pixel. From this force curve images showing local surface
deformation, energy dissipation and tip-surface adhesion are obtained.
By further fitting a contact mechanics model to a part of the force curve
EXPERIMENTAL | 19
(the Derjaguin-Muller-Toporov (DMT) model was used here) information
on the elastic modulus is obtained. For this model to be valid, careful
estimation of the tip end radius, and calibration of the spring constant
and the deflection sensitivity of the cantilever have to be performed
before the measurement [70-72].
Figure 10. Schematic illustration of which parts of the force curve are used to extract the
different sample properties in the PeakForce QNM mode.
ImAFM is a newly developed method to determine the local
mechanical properties of a sample through an alternative route. It works
by oscillating the cantilever with two frequencies close to the resonance
frequency of the cantilever. The nonlinear tip-surface interaction results
in interferences between these two frequencies, causing the appearance of
new frequencies, so called intermodulation products, in the response
signal. These are then analyzed to show conservative and dissipative
forces between the tip and the surface which in turn, using different
models, can be converted to represent the mechanical properties and the
viscous nature of the surface of a material. The sensitivity of this
technique allows accurate characterization of, for example, composites
with soft matrix and hard fillers [73, 74].
20 | EXPERIMENTAL
3.2.3. Confocal Raman microspectroscopy
Confocal Raman microspectroscopy is a combination of microscopy
and spectroscopy. The light source consists of a laser, and a pinhole
aperture is used to reduce the amount of scattered light which, in contrast
to conventional light microscopes, allows illumination of only a single
point on the sample. This leads to a good spatial resolution, and by using
a green laser (λ = 532 nm) and a numerical aperture (NA = 1) for the
objective, the best lateral resolution that can be obtained is ~200 nm,
while the vertical resolution is ~500 nm. The confocal Raman microscope
can be used to scan a sample both in lateral and vertical direction making
it possible to create 3D-images of the sample [69, 75].
The technique is based on the inelastic scattering of the laser beam
light which is absorbed by the sample and then re-emitted, only now
shifted in frequency compared to the incoming light. The frequency shift,
also called Raman shift, provides information about rotational and
vibrational energies of molecular bonds. The subtracted Raman spectra
usually show peaks characteristic of specific molecular bonds, and the
intensity of a given peak is proportional to concentration and can
therefore be used for quantitative analysis as well as qualitative.
Combined with the lateral and vertical scan possibilities, confocal Raman
microscopy makes a powerful tool to analyze the chemical composition of
a sample in the bulk near the surface. In Figure 11 this is illustrated by
showing how the scanning of a sample will return a full spectrum in every
individual pixel [69, 75].
Figure 11. Visualization of how a confocal Raman scan, containing local chemical
information about the sample, returns one spectrum in each individual pixel (three pixels
with corresponding spectra are highlighted).
EXPERIMENTAL | 21
3.2.4. Contact angle measurements
Measuring contact angles from sessile drops is a convenient method to
characterize surface wetting properties due to its simplicity. A droplet of
the chosen liquid is placed onto the sample surface from a syringe, and
the shape of the sessile droplet profile, during and after deposition, is
captured using a high speed camera. The contact angle is then evaluated
by measuring the angle of the droplet tangent (at the point where water,
surface and air meet) [32, 36, 76, 77]. Within some limits the contact
angle is independent of the droplet size. However, it is important to use a
droplet volume small enough to avoid shape distortion by gravity. At the
same time it is important to keep the droplet size larger than the
structural features present on the surface [29, 31]. In the work presented
here a droplet size of 4 µL was used when evaluating the static contact
angle.
To measure the advancing contact angle by the needle-in-droplet
method, the droplet volume has to be increased until the point where the
contact angle reaches a constant value, and the base line moves, resulting
in a continuous increase in the base diameter of the droplet. To measure
the receding contact angle, liquid is instead withdrawn from the droplet
and the contact angle found when the droplet base diameter continuously
decreases, is the receding contact angle. Surprisingly large droplet
volumes (i.e. >10 µL) can be needed to successfully evaluate the receding
contact angle, and for both advancing and receding contact angle it is
important to use a low rate for the addition/withdrawal of liquid to allow
the droplet to continuously find its equilibrium [77]. A volume
expansion/contraction rate of 0.1 µL/s was used throughout this work.
Even though the method is simple and robust, there are pitfalls,
especially when evaluating contact angles above 150°. The results
obtained can vary as much as 15° depending on the magnification used,
the applied contrast and the fitting model used, as well as, on if automatic
or manual fit of the drop contour was employed [32, 76, 77]. In Figure 12
the large variation of the contact angle depending on the automatic fitting
method chosen is shown. Clearly, both the Ellipse and Circle fitting
models result in poor fits when droplets exhibiting high contact angles
are evaluated, and should therefore not be used in these cases. Due to this
variation all contact angles presented in this thesis were evaluated by
hand using a protractor and the tangent method. When evaluated by
hand using a protractor, the droplet shown in Figure 12 exhibits a contact
22 | EXPERIMENTAL
angle of 163°. Thus it is of importance to report the method and
parameters used for contact angle evaluation, together with the reported
contact angles, to ensure legibility. Also, the static contact angle alone
does not provide enough information to draw unambiguous conclusions
regarding wetting, it is also important to report advancing and receding
contact angles to further describe the surface wetting characteristics [77].
Figure 12. Example of how the magnitude of the contact angle on a superhydrophobic
surface greatly depends on the choice of fitting model.
3.2.5. Electrochemical measurements
Corrosion starts and proceeds at the interface between the metal and
the coating and electrochemical measurements present a way of
investigating this process during exposure to corrosive electrolyte. The
measured results can then be fitted to models, including electric circuit,
allowing useful characteristics of the corrosion process to be extracted,
making this a suitable method for the study of corrosion protective
coatings [5, 19].
EXPERIMENTAL | 23
In this work, open circuit potential (OCP) and electrochemical
impedance spectroscopy (EIS) were employed to follow the corrosion
process of coated steel samples in real time during exposure to corrosive
electrolyte. The OCP is the potential measured if no external current is
applied to the circuit, and the EIS can be said to measure the resistance to
aqueous and ionic transport of an organic coating [5, 9, 78]. OCP was
measured versus a reference electrode of the Ag/AgCl type, and in
general, a higher measured OCP value corresponds to a more noble
material. EIS works by measuring the current response when applying a
small (10 – 20 mV) sinusoidal voltage to the system over a range of
frequencies. The applied voltage does not affect the corrosion since it is
small enough to keep the system near the steady state, which makes EIS a
reliable test method when evaluating corrosion in coated metal systems
[3, 9, 19].
Figure 13. In (a) a schematic view of the electrochemical cell and in (b) visualization of the
simplest equivalent circuit used to fit and evaluate EIS measurements from metals coated
by a one-layer coating.
To measure OCP and EIS, a coated metal sample was mounted in an
electrochemical cell, as shown in Figure 13a, where a circular area
(diameter 1 cm) of the sample constitutes the working electrode (WE),
and a platinum mesh was used as counter electrode (CE). A glass tube
was used to position the reference electrode (RE) close to the sample
surface. To evaluate the collected EIS measurements fitting to an
equivalent circuit can be done, and the simplest equivalent circuit
representing a one-layer coating on a metal is shown in Figure 13b. When
fitting the data to such a model circuit, the coating capacitance and
24 | EXPERIMENTAL
resistance can be evaluated. This does, however, require a good fit of the
data to the model, which can be hard to achieve due to the complexity of
polymer coatings. One, often used, way of addressing this problem is to
exchange the coating capacitance, Cp, in the equivalent circuit with a
constant phase element (CPE), which in a simplified manner takes into
account effects of surface heterogeneities [19]. The use of CPE, and the
coating parameters that can be extracted from such fits, is further
discussed in Paper IV. The coating capacitance can be used to calculate
water uptake in the coating, and also to predict apparent diffusion
coefficients through coatings [3, 9, 79, 80]. This is further discussed in
Paper III.
The most straightforward way to monitor the overall protective
properties of a coating is through the measured impedance at the lower
frequency limit, where the coating resistance is the dominating
contribution [9, 81]. In Figure 14, typical data achieved when measuring
OCP and EIS on a coated metal are shown. The OCP decreases when
corrosion starts and simultaneously a drop in the impedance, at the lower
frequency limit, is seen in the EIS spectrum. Commonly, the protective
properties of an organic coating are considered to be lost when the
impedance at the lower frequency limit falls below 106 Ωcm2 [6, 80].
Figure 14. Typical data collected from OCP and EIS measurements, the drop in OCP seen
at 40 days show the onset of corrosion, and simultaneously the EIS drops below 106 Ωcm
2
indicating that the barrier properties of the coating are lost.
RESULTS AND DISCUSSION | 25
4. Results and discussion
In this chapter the results obtained, and conclusions drawn, from each
coating system are first discussed. Then some interesting results from
Papers I - IV are summarized and discussed in relation to two unifying
concepts: superhydrophobicity and corrosion protection. In addition,
there are two further sections at the end of this chapter, one considering
the coatings made from a commercial PDMS (which was not included in
any of the papers) and one concerning the mechanical evaluation of the
PDMS coating, including the nanomechanical properties discussed in
Paper V.
4.1. The AKD system
In Paper I, AKD wax was used to fabricate model surface coatings
exhibiting different wetting states to allow evaluation of how said wetting
states affect the possible corrosion protection properties of the coating.
Through spin coating and spray coating, at varied speeds and number of
layers applied, samples exhibiting four different wetting states were made
and the measured water contact angles on these surfaces were used to
distinguish between their wetting states. Raman microspectroscopy was
used to ensure that the surface chemistry of the four samples was the
same, i.e. that the surface energy of the coatings was the same, and the
different wetting states achieved can hence be exclusively attributed to
differences in surface structure.
To relate the different wetting states to possible corrosion protection
of the underlying substrate, electrochemical measurements were
performed on samples immersed in 3 wt% NaCl water solution. The data
collected for the sample exhibiting the Lotus-like superhydrophobic
wetting state indicated a break in the electrical circuit, and after thorough
control of the equipment, it was concluded that the break had to be
caused within the evaluated system. The air layer present at the
superhydrophobic Lotus-state surface functions as a barrier and
26 | RESULTS AND DISCUSSION
decreases the transport of corrosive ions from solution to the metal
surface to the point where no electrical current can flow, which causes the
break in circuit. When no electrical current flows, corrosion cannot occur,
and this effect is highly desired when designing corrosion protective
coatings. The AKD wax coating showed this behavior for a period of 8
days, before the underlying substrate started corroding; indicating that
the long term stability of the air film may pose an obstacle if considering
engaging this effect in commercial coating systems.
The other wetting states evaluated, a rose-like superhydrophobic, a
mixed and a Wenzel state system, showed reduced corrosion protective
properties when compared to the Lotus-state one. The wetting Wenzel
state surface performed the worst, which was expected due to the
inherent wetting of the surface structures making it easier for the
corrosive electrolyte to reach pin holes and defects in the coating. In
Figure 15, the electrochemical data for the AKD coatings are shown, in (a)
the uncharacteristically low OCP value of circa -3 V can be seen for the
Lotus-like coating during the first 8 days. The sharp peak at 2 days was
explained by temporary contact through the air layer induced by for
example vibration. The dotted line represents the OCP for uncoated steel,
and when the samples reached this value, corrosion was occurring. In
Figure 15b the EIS for the Lotus-like coating is shown, and the break in
circuit can be seen in the very high barrier properties exhibited by this
coating, also lasting for approximately 8 days.
Figure 15. Electrochemical results achieved when investigating the different wetting states
of the AKD wax system. In (a) OCP for all four coatings, where a break in the circuit can be
clearly seen in the extremely low values measured for the Lotus-like sample. In (b) the EIS
for the Lotus-like sample is shown. Redrawn with permission. Copyright © Elsevier 2013.
RESULTS AND DISCUSSION | 27
4.2. The PDMS-hydrophobic silica nanoparticle system
In Paper II, the development of a one-pot superhydrophobic surface
coating formulation was addressed through the addition of hydrophobic
silica nanoparticles to a hydrophobic PDMS matrix. Particles of varied
sizes were used (16, 60-70, 250 and 500 nm), one at the time and in
combination two by two. Superhydrophobicity in the Lotus state was only
reached when high amounts of particles were added due to the formation
of cracks in the coating, which in turn added the extra roughness needed.
Superhydrophobicity in the rose state was reached for coatings with
slightly lower particle content, before, and at modest, crack formation.
The results correlate well with the ongoing discussion regarding how the
shape of the asperities on the surface promotes different wetting states,
sharp shapes such as the wedges of the cracks are known to promote
wetting in the superhydrophobic Lotus state, while rounded shapes, such
as those provided by the spherical particles, will promote wetting in the
superhydrophobic rose state.
Figure 16. ESEM images of PDMS coatings containing 40 wt% hydrophobic silica particles.
In (a) coating prepared using more solvent exhibiting wetting in superhydrophobic Lotus
state, and in (b) coating prepared using less solvent exhibiting wetting in the rose state. (b)
is reprinted with permission. Copyright © Elsevier 2015.
In Paper III four different PDMS coatings, with the addition of 0, 10,
20 or 40 wt% hydrophobic 16 nm silica particles, were chosen for
corrosion protection evaluation. In an attempt to minimize crack
formation, less solvent was used during fabrication of these batches of
PDMS coatings. This, however, also affected the contact angle and
superhydrophobicity in the rose state was instead achieved for the 40
28 | RESULTS AND DISCUSSION
wt% sample. In Figure 16, ESEM images of different surface structures
are shown, both containing cracks but their difference in morphology
results in different superhydrophobic wetting states for the two batches.
The 40 wt% coating (rose state) failed within two days of exposure to 3
wt% NaCl water solution, due to the formation of cracks, which allowed
the electrolyte to easily penetrate the coating and reach the underlying
metal. None of the other three coatings were subjected to particle
addition of high enough amount to change the contact angles but they all
still performed well during electrochemical corrosion protection
evaluation. The 20 wt% coating showed a long term stability of almost 80
days, which is not commonly seen for organic coatings this thin (10 – 20
µm). The synergistic effect of the hydrophobic matrix, and the enhanced
barrier properties, stemming from the addition of hydrophobic particle,
was concluded to be the reason for the promising results. The wetting
data for this system are shown in Table 2, together with the time to
failure, defined as the time until the electrochemical impedance
decreased below 106 Ωcm2 during exposure to electrolyte. Furthermore,
the coating without particles, and the one with 10 wt%, showed a large
increase in coating impedance during the first 24 hours. The increase was
so large, that passivation of the underlying metal was found to be the
most likely explanation. This effect is further discussed in section 4.6.3.
In Paper V, the nanomechanical properties of the PDMS without and
with addition of 20 wt% hydrophobic silica nanoparticles were evaluated,
the results obtained in that study are further discussed in section 4.8.1.
Table 2. Wetting data, and time to failure when immersed in electrolyte, are presented for
the four PDMS surfaces containing varied amounts of hydrophobic silica particles.
Sample SCA (°) ACA (°) RCA (°) Time to failure (days)
No added silica 121 ± 1 120 ± 1 69 ± 1 14 ± 7
10 wt% silica 120 ± 1 120 ± 1 70 ± 3 35 ± 12
20 wt% silica 122 ± 1 122 ± 1 65 ± 4 48 ± 33
40 wt% silica* 152 ± 3 161 ± 4 16 ± 3 1 ± 0.5
*The RCA depends largely on exact preparation conditions which affect the surface
structure, here data from Paper III, where less solvent was used during preparation, are
shown.
RESULTS AND DISCUSSION | 29
4.3. The three layered composite system
To better understand the results obtained in Paper III the coating
system presented in Paper IV was developed. This consisted of a base coat
of PEA, a layer of TiO2 particles (< 100 nm) and a hydrophobic HMDSO
top coat. Coating systems were fabricated exhibiting varied wetting
properties ranging from hydrophilic to supehydrophobic. The complete
three layer system showed excellent corrosion protective properties and
was stable in 3 wt% NaCl water solution for more than 100 days.
Furthermore, the three layered coating managed to quell the corrosion
that did start at some pin hole in the coating. The results obtained for the
layers combined two by two did however not give a straightforward
answer to which factor was the most important to achieve this effect. The
PEA coating, although being weakly hydrophilic with a SCA of 61 ± 1°,
showed fair corrosion protection on its own; the impedance was not as
high as for the three layer system, but the long term stability was good.
This was explained by good adhesion to the substrate. Adding particles on
top of the coating posed no significant change, which could be a result
from two opposing effects which were expected to occur, plugging of pin
holes in the PEA coating (improvement) and enhancement of coating
wetting due to the hydrophilic nature of the TiO2 particles (deterioration).
Finally, results achieved when combining the PEA with only the HMDSO
top coating showed a small improvement, but suggested that the thin
plasma coating may not reach full coverage. The conclusion is that the
excellent corrosion protective properties seen in the three layer coating
system, once more, is a combination of several factors. These factors are:
the good adhesion of the base coat, the elongated diffusion path caused by
particle addition and the lowered surface energy acquired from the
HMDSO top coat.
30 | RESULTS AND DISCUSSION
4.5. Unifying concept 1: Superhydrophobicity
4.5.1. Shape, size and distribution of protrusions
As was touched upon in the introduction, wetting of hydrophobic
structured surfaces is by no means a simple matter, but depends on the
size, shape and geometrical distribution of the protrusions and
depressions creating the surface roughness. In the research presented
here, superhydrophobicity was reached for at least one sample of each
coating system. Four of these surfaces are presented here to provide a
platform for a discussion on the effect of shape, size and distribution of
protrusions on the superhydrophobic state. From Paper I, the AKD-wax
coated through a RESS procedure that formed a flake like structure
which, when added to the inherent hydrophobicity of the wax, rendered
the surface superhydrophobic in the Lotus state was chosen. In Papers II
and III the hydrophobicity of a PDMS coating was tuned by the addition
of silica nanoparticles of different sizes and in different ratios. For
example, the addition of 40 wt% 16 nm silica particles and the addition of
40 wt% 16/500 nm silica particles with a ratio of 10:1 (both from Paper
II) resulted in superhydrophobic surfaces, and data from these two
surfaces will be discussed in this section. Lastly, the three-layered
composite coating system, described in Paper IV, consisting of PEA-TiO2-
HMDSO also exhibited superhydrophobicity, and will also be included
here.
The water contact angles measured for these surfaces are summarized
in Table 3. Looking at the receding contact angle, it is seen that
superhydrophobicity of two different states was achieved, the AKD wax
and the PDMS 40 wt% 16 nm silica samples (from Paper II) exhibit
superhydrophobicity in the Lotus state, while the PDMS 40 wt% 15/500
nm (ratio 10:1) and the PEA-TiO2-HMDSO exhibit superhydrophobicity
in the adhesive rose state.
This behavior can be explained by the shape and size of the features
making up the roughness of the surface. In Figure 17, ESEM images of the
four surfaces are shown, and parallels can be drawn between the sharper,
more flake-like, features seen in the AKD-wax, and in the 40 wt% 16 nm
silica in the PDMS coating where sharp edges are created through crack
formation. It has been proposed that widely spaced, narrow, features
promote a high receding contact angle [32]. This is consistent with the
first two coatings showing high receding contact angles while the latter
RESULTS AND DISCUSSION | 31
two results in pinned droplets on the surface. When looking at the smaller
scale structures, all surfaces except the AKD-wax exhibit a structure of the
same magnitude (≤ 1 µm) and with the same rounded shape of the
protrusions. As discussed in Paper II, and earlier by Teisala et al. [43], the
rounded shape promotes wetting in the adhesive, superhydrophobic,
rose state, which is concluded also here. To reach superhydrophobicity, in
any state, it has been stated that the smaller scale structures need to be
below 100 nm [52, 82-85]. Considering the width of the wax flakes, and
the size of nanoparticles (16 nm silica particles and < 100 nm TiO2
particles, respectively) added to the other coatings, this requirement is
met for all four surfaces exhibiting superhydrophobicity discussed in this
section.
The surface energy of these surfaces can be assumed to be comparable,
since the low surface energy is induced mainly by CH2 – groups in all
coatings, and as was stated earlier, as long as the surface energy is low
enough, the structure determines if superhydrophobicity is reached [29].
Therefore only surface roughness is discussed when comparing these
coatings.
Table 3. Water contact angles for four different surfaces, the first two exhibiting the
superhydrophobic Lotus state, and the last two exhibiting the adhesive superhydrophobic
rose state.
* Wetting data for the sample that showed Lotus-like behavior
** Sample from Paper II where more solvent was used during preparation
Sample SCA (°) ACA (°) RCA (°)
AKD wax* 152 ± 2 152 ± 2 134 ± 9
PDMS 40 wt% silica** 159 ± 3 169 ± 1 154 ± 1
PDMS 40 wt% 16/500 nm – 10:1 153 ± 3 158 ± 9 Pinned
PEA-TiO2-HMDSO 151 ± 11 162 ± 1 Pinned
32 | RESULTS AND DISCUSSION
Figure 17. ESEM images of the four different surfaces exhibiting superhydrophobicity, left
column showing the larger surface structure and the right column showing the smaller
surface structure. (c and d are images from the 40 wt% 16 nm silica system prepared using
more solvent, presented in Paper II)
RESULTS AND DISCUSSION | 33
Relating wetting to structure has been found difficult since the shape,
height and pitch of the structures all contribute to the final wetting state.
Several studies have focused on investigating this relation, and some
conclusions have been drawn. Athauda et al. [86] showed how the water
contact angle on top of two differently sized nano particles, layered on top
of each other, greatly increased when the larger particles were coated on
top of the smaller instead of the opposite. Tuteja et al. [45, 46] showed
how high re-entrant or overhang structures increase the water contact
angle of a surface significantly. However, neither of the surfaces
developed in this work can be expected to exhibit such overhang surface
structures.
Regarding width, height and spacing of the protrusions no generally
applicable relation that predicts the contact angle from such features has
yet been found, but some interesting studies have been made.
Nosonovsky and Bhushan investigated how the pitch of 30 µm high
cylindrical pillars, covered with a nanostructure similar to that seen in
Figure 17b, affected the wetting state of the sample with spacing ranging
from 23 – 210 µm. They found that a smaller spacing promotes
superhydrophobicity in the Lotus state while a larger spacing promotes
the rose state, but the boundary at which the transition occurs also
depends on the density of the nanostructure, and was in this case
approximately 100 – 110 µm [35]. Although wetting is highly dependent
on several factors, and the exact distance between features, stated above,
is valid only for cylindrical pillars of this type, the length scales discussed
agree well with the results presented in Figure 17, where the spacing
between the larger structures (left column) is below 100 µm for the two
samples displaying wetting in the superhydrophobic Lotus state and
above 100 µm for wetting in the rose state.
34 | RESULTS AND DISCUSSION
4.5.2. Air film stability under water
One important factor when considering superhydrophobic surfaces for
the application of corrosion protection, which has not been discussed in
the included papers, is the stability of the superhydrophobic effect when
the surfaces are immersed in water. By time there is an inevitable
transition from the partly wetted Cassie-Baxer state to the fully wetted
Wenzel state, and if no external factors affect the air layer the dynamic
transition will primarily be mediated by the hydrostatic pressure and gas
diffusion [87, 88].
At increasing pressure the water meniscus will advance into the valley
between protrusions, resulting in an increase of the advancing contact
angle along the side of the protrusion, and when the contact angle is large
enough the wetting front will depin and water will advance down the side
of the protrusion [32, 89]. The structure may, however, not be fully
wetted immediately since several metastable states can exist, in which the
wetting front pins at a new site of the protrusion. The metastable state
can exist since the air pressure in the void is increased when the
advancing liquid compresses it [88]. However, the air will start to diffuse
into the water bulk and the meniscus will once more advance until
depinning occurs and a new metastable state, or the bottom of the valley,
is reached. In Figure 18 (upper row), a schematic drawing of water
advancing down the protrusions of a surface is shown.
The presence of hierarchical structures can significantly prolong the
stability of submerged structures since the structured side walls enhance
the pinning of the contact line in the metastable states [88]. An example
of this is depicted in Figure 18 (lower row). Water will first wet the
microstructure and subsequently the nanostructure of a hierarchical
surface [28], and smaller features will maximize the impalement pressure
[32]. The air layer formed on a submerged surface exhibiting only one
level of structure may last for a few tens of minutes while the air layer
formed on a surface exhibiting an hierarchical structure can be stable for
several tens of hours [89]. That is, however, still a very short time
stability when commercial applications are considered.
Poetes et al. describe how the stability of the air film present at a
superhydrophobic surface depending on immersion depth varied between
0.3 and 1.4 m. They find a maximal stability of circa 16 days at the
immersion depth of 0.3 m, and an exponential decay of the stability time
with increasing immersion depth [90]. The AKD coating displaying
RESULTS AND DISCUSSION | 35
superhydrophobicity in the Lotus state, described in Paper I, was
immersed at a depth of 3 cm and the electrochemical results obtained
demonstrated the presence of an air layer for 8 days. According to the
results reported by Poetes et al. [90] much longer stability of the air layer
cannot be expected, which is a considerable limitation in any commercial
use utilizing the presence of an air layer at a submerged structure.
Figure 18. Top row shows how increased hydrostatic pressure, in combination with diffusion
of air from the pocket into the water bulk, cause the meniscus to first sag and then, when
the advancing angle is reached, to depin and either find a new metastable state or
completely wet the structure. Lower row show how hierarchical structures prolong air pocket
stability by adding more possible pinning sites.
36 | RESULTS AND DISCUSSION
4.6. Unifying concept 2: Corrosion protection
4.6.1. Effect of wetting state on corrosion protection
Paper I demonstrates how a superhydrophobic coating, in the Lotus
state, can serve as very efficient corrosion protection by breaking the
electrical circuit. This effect arises from the severely decreased transport
of ions from solution to the metallic substrate due to the insulating air
film formed on the superhydrophobic surface. Similar effects have also
been reported earlier [12, 91, 92]. Almost complete insulation of the
corrosion current by a layer of air is a very effective and also an
environmentally friendly way of achieving corrosion protection, which
should make superhydrophobic surfaces wetting in the Lotus state highly
coveted as corrosion protective coatings. However, as discussed earlier in
section 4.1 and 4.5.2, the air layer found on this type of surface is not
stable over time, and thereby not suitable for long term corrosion
protective applications of surfaces immersed in aqueous solutions [92].
In addition, the issue of wear of the surface coating has to be addressed.
Since superhydrophobicity in the Lotus state is easiest to achieve using
sharp, thin, protrusions it is difficult to make such surfaces mechanically
robust. The contact angle data and results from the electrochemical
evaluation of the AKD wax coating wetting in the Lotus state are shown in
Table 4, and Figure 19a and b, respectively.
Two other coatings that performed well during the electrochemical
evaluation of corrosion protective properties was the PEA-TiO2-HMDSO
coating presented in Paper IV, and the PDMS coating containing 20 wt%
hydrophobic silica nanoparticles presented in Paper III. Contact angles
and electrochemical results obtained from these coatings are also
included in Table 4, and in Figure 19c-f. The PEA-TiO2-HMDSO coating
exhibit wetting in the superhydrophobic rose state and the characteristic
data suggesting a break in the circuit is not seen (Figure 19c and d).
Hence, in this case there is not enough air to insulate the substrate from
the electrolyte. However, instead, this coating shows a considerably long
stability over time compared to other thin coatings. This is due to the
combined effect of a particle layer, a hydrophobic top coat and good
adhesion to the metal.
In comparison, the PDMS coating containing 20 wt% hydrophobic
silica nanoparticles did not exhibit superhydrophobicity but showed a
hydrophobic behavior (Table 4). However, this coating still performed
RESULTS AND DISCUSSION | 37
well during electrochemical testing. In Figure 19e and f, it can be seen
how the impedance reaches values at the lower frequency limit (0.01 Hz)
even higher than those seen for the PEA-TiO2-HMDSO coating, although
it also shows a slightly shorter long-term stability. From these results, the
conclusion can be drawn that the exact contact angle value is not the most
important characteristic affecting the corrosion protection. Instead it
seems that, excluding superhydrophobicity in the Lotus state that
provides an insulating air layer, superhydrophobicity is generally not
needed to receive the enhancements in coating performance which
instead could be associated with hydrophobicity combined with long
diffusion times caused by particle addition.
Table 4. Contact angles for three different coatings performing well during the immersed
corrosion protection evaluation.
* Data for the sample wetting in the Lotus state
Sample SCA (°) ACA (°) RCA (°)
AKD wax* 152 ± 2 152 ± 2 134 ± 9
PEA-TiO2-HMDSO 151 ± 11 162 ± 1 Pinned
PDMS 20 wt% hydrophobic
silica nanoparticles
122 ± 1 122 ± 1 65 ± 4
38 | RESULTS AND DISCUSSION
Figure 19. Electrochemical results for three coatings representing different wetting states, in
a and b) OCP and EIS (respectively) for the superhydrophobic Lotus-like AKD wax, in c and
d) OCP and EIS (respectively) for the PEA-TiO2-HMDSO layered coating showing
superhydrophibic rose-state, and in e and f) OCP and EIS (respectively) for the hydrophobic
PDMS coating containing 20 wt% hydrophobic silica particles. Redrawn with permission.
Copyright © Elsevier 2013 and 2015.
RESULTS AND DISCUSSION | 39
4.6.2. Barrier effect from particles
The barrier properties of a coating can be improved by the addition of
particles to a polymeric matrix [48, 93-96]. For corrosion protective
applications an important reason is the elongation of the diffusion path,
which delays the onset of corrosion by slowing down the diffusion of
corrosive species through the coating to the substrate. Another reason is
that the particle can fill cavities or act as a bridge to connect molecules in
the coating, resulting in a denser coating [97]. It has also been reported
that the addition of nanoparticles improves the barrier properties much
more than addition of micrometer sized particles due to their higher
surface to volume ratio [98, 99]. In Paper III, addition of hydrophobic
silica nanoparticles to the PDMS matrix was found to enhance and
prolong the corrosion protective properties of the coating. However, also
the PDMS coating without any particles performed well and the coating
system used in Paper IV was designed to better understand the
contributions arising from particle addition and from hydrophobicity to
the combined coating.
The three layered PEA-TiO2-HMDSO coating evaluated in Paper IV
show how the addition of particles on top of a base coat may block pores
in the coating by making it denser, but in the case of TiO2 addition, this
effect is counteracted by the hydrophilicity of the particles which instead
promote wetting of the coating. The addition of a very thin hydrophobic
coating, HMDSO, to the base coat enhanced the corrosion protective
properties, but not for all three replicates. The main conclusion in Paper
IV was that both particles and hydrophobicity are needed, and that their
properties can act synergistically, to greatly enhance the corrosion
protective properties of the coating. Also the positive effects can be
expected to be greater when the particles are distributed through the
coating as in Paper III, instead of being present in a confined layer as in
Paper IV, both due to a further elongated diffusion path and due to less
porosity when the particles are surrounded by the matrix polymer.
Another positive effect from particle addition is that not only the
diffusion paths for corrosive species are prolonged, but also the diffusion
path for corrosion products from the surface out into the electrolyte. It
has been seen in several reports how dense corrosion products can get
stuck in a coating, blocking holes and defects, and thereby enhance the
protective properties of the coating [3, 19]. In Figure 20, an example of
this effect, seen for the full PEA-TiO2-HMDSO coating system in Paper
40 | RESULTS AND DISCUSSION
IV, is shown. This coating showed an onset of corrosion already at day 20,
which proceeded for 9 days, but then stayed stable for 100 days.
Figure 20. One of the PEA-TiO2-HMDSO samples showing how corrosion is initiated after
20 days of exposure to 3 wt% NaCl water solution, proceeds for 9 days and then stops,
allowing the surface coating to stay stable for 100 days. Reprinted with permission.
Copyright © Elsevier 2015.
RESULTS AND DISCUSSION | 41
4.6.3. Possible passivation of underlying substrate
An interesting effect was noted in Paper III, where, in the beginning of
exposure to electrolyte a large increase in impedance was measured
during the first 24 hours. The effect is shown in Figure 21, and although
an improvement in the barrier properties can be seen due to corrosion
products getting stuck in the coating, and thereby blocking pores, the
increase of impedance associated with that effect is normally much
smaller than what is seen here, typically in the order of only one
magnitude [100].
Figure 21. Electrochemical data collected from the PDMS coating containing 10 wt% silica
particles showing a large increase in impedance during the first 24 hours of exposure.
Reprinted with permission. Copyright © Elsevier 2015.
The most likely explanation to this large increase in impedance is that
the coating can promote passivation of the underlying metal surface. Iron
can form conductive oxides that are stable at high pH, and the major
reaction product of the cathodic reaction is OH- through the reduction of
O2 [5]. It has also been suggested that accumulation of OH- under surface
coatings can take place since organic coatings often exhibit selective
permeability [78].
42 | RESULTS AND DISCUSSION
Iron oxides are not stable in an environment containing Cl- ions,
making the electrolyte containing 3 wt% NaCl used here, a very corrosive
environment. However, because of selective permeability the diffusion of
Cl- through a polymer coating is much slower than that of water [78], and
by combining the slow diffusion of Cl- and local increase in pH,
passivation of the substrate is possible. This may explain the large
increase in measured impedance. However, at some point, the Cl- ions
will penetrate through the coating and cause the passive oxide layer to
break.
Another factor indicating passivation is the color of the corrosion
products. For example, in Paper IV, for the PEA-TiO2-HMDSO coating
where the corrosion was seen to stop (Figure 20) the corrosion products
were black or dark grey, which is characteristic of the more stable iron
oxide Fe3O4, while corrosion causing failure of the coatings has been
noted to be red, characteristic of the porous Fe2O3 iron oxide.
Furthermore, there have been reports showing how stable Si-Fe oxides
can form and enhance the corrosion protection achieved when silica
nanoparticles are present in the coating under a mildly alkaline
environment. These Si containing oxides also resist Cl- ion penetration
allowing a Cl- free environment to be created near the metal/coating
interface which can stabilize other iron oxides [97, 99, 101, 102]. This
effect could help explain the surprisingly good corrosion protection seen
for the PDMS system with added hydrophobic silica particles, studied in
Paper III.
RESULTS AND DISCUSSION | 43
4.7. Commercial PDMS
PDMS coatings without added nano-particles were also prepared from
a commercially available PDMS formulation (results not included in
papers) for comparison. A condensation cure PDMS was chosen to match
the curing mechanism of the model PDMS described in Papers II and III.
The formulation was also coated, and subsequently evaluated, in the same
way as the model one to facilitate comparison. The water contact angles
and coating thicknesses for the two PDMS coatings are shown in Table 5.
Static and advancing contact angles match very well, while a discrepancy
can be seen for the receding contact angle. Since an increase in receding
contact angle was noted for the experimental PDMS coating in Paper II
during the first week of curing, the difference here indicates that the
coating used in Papers II and III presents a less homogenous surface
layer. When measuring coating thickness for the commercial PDMS a
difference was noted between different samples, and in Table 5, the
thicknesses for two samples are shown. This difference is most likely due
to the short tack-free time of the formulation. When preparing the last
coatings the formulation had already begun to cure and was therefore
more difficult to spin coat onto the samples.
Table 5. Water contact angles, and coating thicknesses, for the commercial and model PDMS
coatings.
* the two thicknesses for commercial PDMS are measured on two samples made from the
same batch, one made early during the coating process and one late, showing an increase
in thickness due to the short tack free time of the formulation causing the viscosity to
increase during the coating process.
The commercial PDMS coatings performed well during
electrochemical testing, showing results early after exposure that indicate
the presence of air at or in the surface and with a very good long term
stability of more than 100 days. The electrochemical data collected for the
commercial PDMS are shown in Figure 22. As for the model PDMS three
replicates were tested also for the commercial one and the best obtained
Sample SCA (°) ACA (°) RCA (°) Thickness (µm)
PDMS
commercial
120 ± 1 120 ± 0 103 ± 3 16 ± 4,
13 ± 2*
PDMS model 121 ± 1 120 ± 1 69 ± 1 13 ± 3
44 | RESULTS AND DISCUSSION
results are shown here. The OCP exhibit some turbulent behavior in the
beginning, and in correlation, the EIS at the lower frequency limit (0.01
Hz) is very high, on the border of what can be measured with the
instrument, and also somewhat scattered. Papers I and III explain this by
the presence of air at or in the coating obstructing the flow of the
electrical circuit. Both the indication of air present at the beginning of
exposure, as well as the high stable impedance modulus (at the lower
frequency limit), are different compared to the results obtained in Paper
III where the experimental PDMS coating exhibit a impedance of just
above 108 Ωcm2 at the beginning that then continuously deteriorate until
the coating fails after approximately 20 days. The mean time to failure for
the model coating was 14 ± 7 days. For the commercial PDMS one
replicate failed after 32 days, while the other two stayed stable for the
whole exposure time of 100 days.
Figure 22. Electrochemical data collected for the commercial PDMS coating during
exposure to 3 wt% NaCl water solution, in a) OCP vs. time and in b) impedance modulus
vs. frequency at different times.
The receding contact angle is the only parameter evaluated here which
is significantly different between the model and commercial PDMS
samples, but another important difference is that the commercial coating
contains adhesion promoters. Thus the model coating will have a greater
tendency to locally delaminate than the commercial PDMS samples,
which at least partly explains why the commercial coating performs better
in the corrosion protection test. However, since the content of the
RESULTS AND DISCUSSION | 45
commercial formulation is not fully known and may, most likely, contain
additives which enhance its performance, not too much weight should be
put on the differences seen here at this stage.
4.8. Mechanical properties of PDMS coating
Evaluation and improvement of the coatings regarding wear and
friction control clearly needs further development. Macroscopic wear test
of the model PDMS based coatings was performed using a minitraction
machine, and the results showed that the coating adhesion to the
underlying substrate is an issue that needs to be further addressed.
Furthermore, evaluation of the nanomechanical properties of the coating
is ongoing and some results are presented in this section.
4.8.1. Nanomechanical properties of PDMS coating
The model PDMS coating without, and with, the addition of 20 wt%
hydrophobic nanoparticles (16 nm) was evaluated using three different
AFM modes; tapping mode, PeakForce QNM and Intermodulation AFM
(ImAFM). The results show that both PeakForce QNM and ImAFM can
be used to investigate the nanomechanical surface properties of the
coatings.
Using the ImAFM mode, effective elastic modulus and adhesion were
extracted for the PDMS without added particles using the DMT model,
and the results are shown in Figure 23a. Red areas in the map showing
effective elastic modulus (left hand side) represent areas that are less
deformable. One possible explanation to why these patches occur is that
the PDMS coating has not cured in a homogenous way but instead
contains areas exhibiting higher crosslinking density, making those areas
less deformable.
The 16 nm hydrophobic silica particles were clearly visible in contrast
to the surrounding soft matrix using all three AFM modes when
evaluating the PDMS with 20 wt% particles. In topography
measurements of this sample it can be clearly seen that the particles
aggregate to form large secondary, and tertiary, structures as proposed
earlier by others [103]. The dimension of the particle aggregates observed
was estimated to measure between 20 and 110 nm.
46 | RESULTS AND DISCUSSION
Furthermore, a discussion has been raised regarding the rounded
shapes also seen in the lower right corner of Figure 23c. These rounded
shapes were seen also when using the PeakForce QNM mode and the
mechanical properties extracted for these rounded shapes are different
compared to those exhibited by particle aggregates with smaller
deformation depth, lower adhesion and lower energy dissipation. Due to
this, these rounded shapes were assigned to nanobubbles of air trapped in
the polymer matrix due to the increase in viscosity caused by the addition
of particles. This is an interesting, yet speculative, notion that could help
understand the excellent corrosion protective properties of these
coatings.
Figure 23. ImAFM mode scans of the PDMS without and with 20 wt% silica, the DMT model
was used for evaluation. In (a) effective elastic modulus and in (b) adhesion for the PDMS
coating without particles, in (c) effective elastic modulus and (d) adhesion for the PDMS
coating with addition of 20 wt% silica nanoparticles. All images are 1 x 1 µm.
CONCLUSION | 47
5. Conclusions
Three different coating systems, with focus on hydrophobicity and
superhydrophobicity, have been used to investigate which properties a
top coat layer in a corrosion protective coating system would benefit
from.
Through the use of AKD wax coatings, exhibiting the same surface
chemistry but different wetting states due to different surface structures,
it was possible to relate corrosion protective properties to the wetting
state. The superhydrophobic Lotus state can provide corrosion protection
to underlying substrates through the insulating air layer that forms on top
of such surface when it is immersed in the electrolyte, the air layer
obstructs the transport of corrosive ions to the surface to the point where
the electrical circuit is broken and corrosion cannot occur. This effect was
found to be efficient as corrosion protection during short exposure times,
in 3 wt% NaCl water solution, of less than ten days.
The aim of developing an easy-to-use, one-pot, superhydrophobic
coating was undertaken using nanoparticle containing PDMS coatings.
The conclusion is that high enough particle load to achieve
superhydrophobicity is hard to reach without causing the coating to
crack. It was also seen how the shape of the protrusions is an important
factor deciding which state of superhydrophobicity is formed; the Lotus
state is promoted by sharp, needle-like, structures, while rounded shapes
will promote the rose state.
Although not superhydrophobic, the hydrophobic PDMS coatings
containing silica nanoparticles were evaluated with respect to corrosion
protective properties and were found to perform better than expected for
coatings this thin (10 - 20 µm). The corrosion protective properties were
found to increase with increase in amount of added particles up to 20
wt%, where the coating provided corrosion protection to the underlying
substrate for almost 80 days when immersed in 3 wt% NaCl. The
properties of this coating system were concluded to be a synergistic effect
from the hydrophobic matrix and the addition of hydrophobic
nanoparticles.
48 | CONCLUSION
To further understand the corrosion protective mechanism shown by
the PDMS coating, a three layer composite coating system was developed.
Investigations of this coating system lead to the conclusion that several
factors are needed in combination to achieve the enhancement in
corrosion protection seen; good coating adhesion, blocking of pores and
an elongated diffusion path from addition of nanoparticles, and
hydrophobicity to further slow down the transport of water containing
corrosive ions. It was also noted that the hydrophobic top coat was
needed to exploit a positive effect from particle addition, if no
hydrophobic coating was applied; the hydrophilic particles instead
quicken the transport of water through the coating.
An additional conclusion, reached through comparison of the different
coating systems evaluated, is that if the insulating property of a
superhydrophobic surface in the Lotus state is not reached, the exact
wetting state is of less importance, as long as the surface is hydrophobic.
For example, the hydrophobic PDMS with 20 wt% hydrophobic
nanoparticles showed corrosion protective properties comparable to the
three layered composite coating wetting in the superhydrophobic rose
state. Therefore, when Lotus state superhydrophobicity is excluded, it was
concluded that other factors, such as elongation of diffusion path, and
blocking of pores by particles addition, were more important to the
resulting corrosion protection than the question of whether the coating
was hydrophobic or superhydrophobic.
FUTURE WORK | 49
6. Future work
There are several promising ways to continue research in this area.
One would be to start adapting either the PDMS or the PEA-TiO2-
HMDSO coating to commercial standards. To do this, coating adhesion to
the substrate, wear resistance and facilitation of the application process
have to be addressed. Another important factor of commercial corrosion
protection is the addition of active inhibitors; it would be interesting to
evaluate addition of such inhibitors to either of the coatings mentioned
above. However, care must be taken since most inhibitors are designed to
function in the presence of water, which makes them unsuitable to
combine with water repelling coatings.
When discussing commercial applications the concept of particle
volume concentration and also of critical particle volume concentration of
filler particles would be interesting to apply to facilitate understanding of
significant changes in properties in relation to filler concentration. This
calculation is, however, not entirely straight forward to perform for the
system investigated here since the fumed silica nanoparticles exhibit an
uneven surface, and it is not known whether the polymer can access all of
these structures, leading to uncertainty in the effective density of the
silica particles. One way of elucidating this is through oil absorption
measurements, and another one could be through further AFM studies of
the interphase between the polymer and the particle.
Another interesting path would be working on understanding the
corrosion protective mechanism of these coatings. One interesting
approach regarding the PDMS coating would be to look at enhancing the
wetting properties by patterning the surface, and then comparing the
corrosion protection with or without the addition of particles to evaluate
if wetting or elongated diffusion path is most important. It would also be
interesting to evaluate the diffusion of oxygen through the coatings. This
could be done using free films of the coatings, or by coating them onto
glass substrates of known porosity.
Furthermore, the addition of particles to the commercially available
PDMS formulation would be of great interest since the initial testing of
50 | FUTURE WORK
this PDMS gave promising results. This is however, not without
challenges since the formulation cures by humidity, making particle
addition in ambient conditions impossible. This could be overcome by
working in a controlled environment, such as N2 gas. Another alternative
would be to try yet another commercial PDMS formulation that does not
cure by humidity, but instead by, for example, heat.
ACKNOWLEDGEMENTS | 51
7. Acknowledgements
I would like to thank my supervisors, professor Per Claesson and
adjunct professor Agne Swerin, for giving me the opportunity to perform
this work, for countless interesting discussions, invaluable guidance and
keeping me on the right track (or at least one track). I would also like to
thank professor Jinshan Pan for sharing his expertise on electrochemistry
with us.
Thanks to all my co-authors, I enjoyed working with you and I am
proud of the publications we produced together. I am also grateful for the
funding provided by the SSF (stiftelsen för strategisk forskning) and RISE
Research Institutes of Sweden that made it possible for me to carry out
this work.
I have spent some great years at the division of Surface and Corrosion
Science, and at SP Chemistry, Materials and Surfaces, and a lot of the joy
during the work was due to truly wonderful colleges, both current and
past, thank you! Special thanks go to Petra, Josefina and Hanna who have
been there during both ups and downs to encourage me, both
educationally and privately.
Finally, I would like to thank my family. My parents who have always
believed in me and throughout the years always encouraged me to
“plugga så länge du bara orkar Lina!”, and my sister who has been there
to cheer me on whenever that has felt tough, and who always
congratulates me on every smallest progress.
Jesper, thank you for understanding how it feels to write a thesis, and
for taking care of our life while I did. Thank you for your endless support,
and for always being able to make me laugh, even at times when I do not
want to. We certainly are an effective team.
Henry, thank you for bringing perspective into all this, you will always
remain the most important thing in my life.
52 |
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