Introduction of Fibre-Reinforced Polymers − Polymers and Composites: Concepts, Properties and Processes
Martin Alberto Masuelli1
[1]
Instituto de Física Aplicada, CONICET. Cátedra de Química Física II,
Área de Química Física. Facultad de Química, Bioquímica y Farmacia.
Universidad Nacional de San Luis. Chacabuco 917 (CP: 5700), San Luis,
Argentina
1. Introduction
2. Manufactured process and basic concepts
2.1. Polymers
2.1.1. Polymerization
2.1.2. Polycondensation
2.1.3. Polyaddition
2.2. Composites
2.2.1. Polymer composites
2.2.2. Biocomposites
2.3. Fiberglass
2.3.1. The manufacturing process
2.3.1.1. Melting
2.3.1.2. Forming into fibers
2.3.1.3. Continuous-filament process
2.3.1.4. Staple-fiber process
2.3.1.5. Chopped fiber
2.3.1.6. Glass wool
2.3.1.7. Protective coatings
2.3.1.8. Forming into shapes
2.4. Carbon fibre
2.4.1. Classification and types
2.4.2. Manufacture
2.4.2.1. Carbon fibers from polyacrylonitrile (PAN)
2.4.2.2. Carbon fibers from rayon
2.4.2.3. Carbon fibers in meltblown nonwovens
2.4.2.4. Carbon fibers from isotropic pitch
2.4.2.5. Carbon fibers from anisotropic mesophase pitch
2.4.2.6. Structure
2.4.2.7. Properties
2.4.2.8. Applications
2.5. Aramid-definition
3. All process description
3.1. Fibre process
3.1.1. The manufacture of fibre fabric
3.1.2. The manufacture of fibre preforms
3.1.3. Molding processes
3.2. Composite molding
3.2.1. Bladder molding
3.2.2. Compression molding
3.2.3. Autoclave − Vacuum bag
3.2.4. Mandrel wrapping
3.2.5. Wet layup
3.2.6. Chopper gun
3.2.7. Filament winding
3.2.8. Pultrusion
3.3. Resin infusion
3.3.1. Advantages and limitations
3.3.2. Failure modes
3.3.3. Material requirements
3.4. Glass fibre material
3.5. Aramid fibre material process
3.6. FRP, applications
3.6.1. Carbon fibre reinforced polymers
3.6.2. Structural applications of FRP
3.6.3. Glass fibre reinforced polymers
3.6.4. Design considerations
3.6.5. Disposal and recycling concerns
4. Mechanical properties measurements
4.1. Strength
4.2. Elongation
4.3. Modulus
4.5. Mechanical properties of real polymers
4.6. Tensile properties
5. Conclusions
1. Introduction
Fibre-reinforced polymer
(FRP), also Fibre-reinforced plastic, is a composite
material made of a polymer matrix reinforced with fibres. The fibres are
usually glass, carbon, or aramid, although other fibres such as paper
or wood or asbestos have been sometimes used. The polymer is usually an
epoxy, vinylester or polyester thermosetting plastic, and phenol
formaldehyde resins are still in use. FRPs are commonly used in the
aerospace, automotive, marine, and construction industries.
Composite
materials are engineered or naturally occurring materials made from two
or more constituent materials with significantly different physical or
chemical properties which remain separate and distinct within the
finished structure. Most composites have strong, stiff fibres in a
matrix which is weaker and less stiff. The objective is usually to make a
component which is strong and stiff, often with a low density.
Commercial material commonly has glass or carbon fibres in matrices
based on thermosetting polymers, such as epoxy or polyester resins.
Sometimes, thermoplastic polymers may be preferred, since they are
moldable after initial production. There are further classes of
composite in which the matrix is a metal or a ceramic. For the most
part, these are still in a developmental stage, with problems of high
manufacturing costs yet to be overcome [1].
Furthermore, in these composites the reasons for adding the fibres (or,
in some cases, particles) are often rather complex; for example,
improvements may be sought in creep, wear, fracture toughness, thermal
stability, etc [2].
Fibre
reinforced polymer (FRP) are composites used in almost every type of
advanced engineering structure, with their usage ranging from aircraft,
helicopters and spacecraft through to boats, ships and offshore
platforms and to automobiles, sports goods, chemical processing
equipment and civil infrastructure such as bridges and buildings. The
usage of FRP composites continues to grow at an impressive rate as these
materials are used more in their existing markets and become
established in relatively new markets such as biomedical devices and
civil structures. A key factor driving the increased applications of
composites over the recent years is the development of new advanced
forms of FRP materials. This includes developments in high performance
resin systems and new styles of reinforcement, such as carbon nanotubes
and nanoparticles. This book provides an up-to-date account of the
fabrication, mechanical properties, delamination resistance, impact
tolerance and applications of 3D FRP composites [3].
The
fibre reinforced polymer composites (FRPs) are increasingly being
considered as an enhancement to and/or substitute for infrastructure
components or systems that are constructed of traditional civil
engineering materials, namely concrete and steel. FRP composites are
lightweight, no-corrosive, exhibit high specific strength and specific
stiffness, are easily constructed, and can be tailored to satisfy
performance requirements. Due to these advantageous characteristics, FRP
composites have been included in new construction and rehabilitation of
structures through its use as reinforcement in concrete, bridge decks,
modular structures, formwork, and external reinforcement for
strengthening and seismic upgrade [4].
The
applicability of Fiber Reinforced Polymer (FRP) reinforcements to
concrete structures as a substitute for steel bars or prestressing
tendons has been actively studied in numerous research laboratories and
professional organizations around the world. FRP reinforcements offer a
number of advantages such as corrosion resistance, non-magnetic
properties, high tensile strength, lightweight and ease of handling.
However, they generally have a linear elastic response in tension up to
failure (described as a brittle failure) and a relatively poor
transverse or shear resistance. They also have poor resistance to fire
and when exposed to high temperatures. They loose significant strength
upon bending, and they are sensitive to stress-rupture effects.
Moreover, their cost, whether considered per unit weight or on the basis
of force carrying capacity, is high in comparison to conventional steel
reinforcing bars or prestressing tendons. From a structural engineering
viewpoint, the most serious problems with FRP reinforcements are the
lack of plastic behavior and the very low shear strength in the
transverse direction. Such characteristics may lead to premature tendon
rupture, particularly when combined effects are present, such as at
shear-cracking planes in reinforced concrete beams where dowel action
exists. The dowel action reduces residual tensile and shear resistance
in the tendon. Solutions and limitations of use have been offered and
continuous improvements are expected in the future. The unit cost of FRP
reinforcements is expected to decrease significantly with increased
market share and demand. However, even today, there are applications
where FRP reinforcements are cost effective and justifiable. Such cases
include the use of bonded FRP sheets or plates in repair and
strengthening of concrete structures, and the use of FRP meshes or
textiles or fabrics in thin cement products. The cost of repair and
rehabilitation of a structure is always, in relative terms,
substantially higher than the cost of the initial structure. Repair
generally requires a relatively small volume of repair materials but a
relatively high commitment in labor. Moreover the cost of labor in
developed countries is so high that the cost of material becomes
secondary. Thus the highest the performance and durability of the repair
material is, the more cost-effective is the repair. This implies that
material cost is not really an issue in repair and that the fact that
FRP repair materials are costly is not a constraining drawback [5].
When
considering only energy and material resources it appears, on the
surface, the argument for FRP composites in a sustainable built
environment is questionable. However, such a conclusion needs to be
evaluated in terms of potential advantages present in use of FRP
composites related to considerations such as:
- Higher strength
- Lighter weight
- Higher performance
- Longer lasting
- Rehabilitating existing structures and extending their life
- Seismic upgrades
- Defense systems
- Space systems
- Ocean environments
In
the case of FRP composites, environmental concerns appear to be a
barrier to its feasibility as a sustainable material especially when
considering fossil fuel depletion, air pollution, smog, and
acidification associated with its production. In addition, the ability
to recycle FRP composites is limited and, unlike steel and timber,
structural components cannot be reused to perform a similar function in
another structure. However, evaluating the environmental impact of FRP
composites in infrastructure applications, specifically through life
cycle analysis, may reveal direct and indirect benefits that are more
competitive than conventional materials.
Composite
materials have developed greatly since they were first introduced.
However, before composite materials can be used as an alternative to
conventional materials as part of a sustainable environment a number of
needs remain.
- Availability of standardized durability characterization data for FRP composite materials.
- Integration of durability data and methods for service life prediction of structural members utilizing FRP composites.
- Development of methods and techniques for materials selection based on life cycle assessments of structural components and systems.
Ultimately,
in order for composites to truly be considered a viable alternative,
they must be structurally and economically feasible. Numerous studies
regarding the structural feasibility of composite materials are widely
available in literature [6].
However, limited studies are available on the economic and
environmental feasibility of these materials from the perspective of a
life cycle approach, since short term data is available or only economic
costs are considered in the comparison. Additionally, the long term
affects of using composite materials needs to be determined. The
byproducts of the production, the sustainability of the constituent
materials, and the potential to recycle composite materials needs to be
assessed in order to determine of composite materials can be part of a
sustainable environment. Therefore in this chapter describe the
physicochemical properties of polymers and composites more used in Civil
Engineering. The theme will be addressed in a simple and basic for
better understanding.
2. Manufactured process and basic concepts
The
synthetic polymers are generally manufactured by polycondensation,
polymerization or polyaddition. The polymers combined with various
agents to enhance or in any way alter the material properties of
polymers the result is referred to as a plastic. The Composite plastics
can be of homogeneous or heterogeneous mix. Composite plastics refer to
those types of plastics that result from bonding two or more homogeneous
materials with different material properties to derive a final product
with certain desired material and mechanical properties. The Fibre
reinforced plastics (or fiber reinforced polymers) are a category of
composite plastics that specifically use fibre materials (not mix with
polymer) to mechanically enhance the strength and elasticity of
plastics. The original plastic material without fibre reinforcement is
known as the matrix. The matrix is a tough but relatively weak plastic
that is reinforced by stronger stiffer reinforcing filaments or fibres.
The extent that strength and elasticity are enhanced in a fibre
reinforced plastic depends on the mechanical properties of the fibre and
matrix, their volume relative to one another, and the fibre length and
orientation within the matrix. Reinforcement of the matrix occurs by
definition when the FRP material exhibits increased strength or
elasticity relative to the strength and elasticity of the matrix alone.
Polymers
are different from other construction materials like ceramics and
metals, because of their macromolecular nature. The covalently bonded,
long chain structure makes them macromolecules and determines, via the
weight averaged molecular weight, Mw, their processability, like spin-,
blow-, deep draw-, generally melt-formability. The number averaged
molecular weight, Mn, determines the mechanical strength, and high
molecular weights are beneficial for properties like strain-to-break,
impact resistance, wear, etc. Thus, natural limits are met, since too
high molecular weights yield too high shear and elongational viscosities
that make polymers inprocessable. Prime examples are the very useful
poly-tetra-fluor-ethylenes, PTFE’s, and
ultrahigh-molecular-weight-poly-ethylenes, UHMWPE’s, and not only
garbage bags are made of polyethylene, PE, but also high-performance
fibers that are even used for bullet proof vests (alternatively made
from, also inprocessable in the melt, rigid aromatic polyamides). The
resulting mechanical properties of these high performance fibers, with
moduli of 150 GPa and strengths of up to 4 GPa, represent the optimal
use of what the potential of the molecular structure of polymers yields,
combined with their low density. Thinking about polymers, it becomes
clear why living nature used the polymeric concept to build its
structures, and not only in high strength applications like wood, silk
or spider-webs [7].
2.1. Polymers
The
linking of small molecules (monomers) to make larger molecules is a
polymer. Polymerization requires that each small molecule have at least
two reaction points or functional groups. There are two distinct major
types of polymerization processes, condensation polymerization, in which
the chain growth is accompanied by elimination of small molecules such
as H2O or CH3OH, and addition polymerization, in
which the polymer is formed without the loss of other materials. There
are many variants and subclasses of polymerization reactions.
The
polymer chains can be classified in linear polymer chain, branched
polymer chain, and cross-linked polymer chain. The structure of the
repeating unit is the difunctional monomeric unit, or “mer.” In the
presence of catalysts or initiators, the monomer yields a polymer by the
joining together of n-mers. If n is a small number, 2–10, the products
are dimers, trimers, tetramers, or oligomers, and the materials are
usually gases, liquids, oils, or brittle solids. In most solid polymers,
n has values ranging from a few score to several hundred thousand, and
the corresponding molecular weights range from a few thousand to several
million. The end groups of this example of addition polymers are shown
to be fragments of the initiator. If only one monomer is polymerized,
the product is called a homopolymer. The polymerization of a mixture of
two monomers of suitable reactivity leads to the formation of a
copolymer, a polymer in which the two types of mer units have entered
the chain in a more or less random fashion. If chains of one homopolymer
are chemically joined to chains of another, the product is called a
block or graft copolymer.
Isotactic and syndiotactic
(stereoregular) polymers are formed in the presence of complex
catalysts, or by changing polymerization conditions, for example, by
lowering the temperature. The groups attached to the chain in a
stereoregular polymer are in a spatially ordered arrangement. The
regular structures of the isotactic and syndiotactic forms make them
often capable of crystallization. The crystalline melting points of
isotactic polymers are often substantially higher than the softening
points of the atactic product.
The spatially oriented
polymers can be classified in atactic (random; dlldl or lddld, and so
on), syndiotactic (alternating; dldl, and so on), and isotactic (right-
or left-handed; dddd, or llll, and so on). For illustration, the heavily
marked bonds are assumed to project up from the paper, and the dotted
bonds down. Thus in a fully syndiotactic polymer, asymmetric carbons
alternate in their left- or right-handedness (alternating d, l
configurations), while in an isotactic polymer, successive carbons have
the same steric configuration (d or l). Among the several kinds of
polymerization catalysis, free-radical initiation has been most
thoroughly studied and is most widely employed. Atactic polymers are
readily formed by free-radical polymerization, at moderate temperatures,
of vinyl and diene monomers and some of their derivatives. Some
polymerizations can be initiated by materials, often called ionic
catalysts, which contain highly polar reactive sites or complexes. The
term heterogeneous catalyst is often applicable to these materials
because many of the catalyst systems are insoluble in monomers and other
solvents. These polymerizations are usually carried out in solution
from which the polymer can be obtained by evaporation of the solvent or
by precipitation on the addition of a nonsolvent. A distinguishing
feature of complex catalysts is the ability of some representatives of
each type to initiate stereoregular polymerization at ordinary
temperatures or to cause the formation of polymers which can be
crystallized [1, 6].
2.1.1. Polymerization
Polymerization,
emulsion polymerization any process in which relatively small
molecules, called monomers, combine chemically to produce a very large
chainlike or network molecule, called a polymer. The monomer molecules
may be all alike, or they may represent two, three, or more different
compounds. Usually at least 100 monomer molecules must be combined to
make a product that has certain unique physical properties-such as
elasticity, high tensile strength, or the ability to form fibres-that
differentiate polymers from substances composed of smaller and simpler
molecules; often, many thousands of monomer units are incorporated in a
single molecule of a polymer. The formation of stable covalent chemical
bonds between the monomers sets polymerization apart from other
processes, such as crystallization, in which large numbers of molecules
aggregate under the influence of weak intermolecular forces.
Two
classes of polymerization usually are distinguished. In condensation
polymerization, each step of the process is accompanied by formation of a
molecule of some simple compound, often water. In addition
polymerization, monomers react to form a polymer without the formation
of by-products. Addition polymerizations usually are carried out in the
presence of catalysts, which in certain cases exert control over
structural details that have important effects on the properties of the
polymer [8].
Linear
polymers, which are composed of chainlike molecules, may be viscous
liquids or solids with varying degrees of crystallinity; a number of
them can be dissolved in certain liquids, and they soften or melt upon
heating. Cross-linked polymers, in which the molecular structure is a
network, are thermosetting resins (i.e., they form under the influence
of heat but, once formed, do not melt or soften upon reheating) that do
not dissolve in solvents. Both linear and cross-linked polymers can be
made by either addition or condensation polymerization.
2.1.2. Polycondensation
The
polycondensation a process for the production of polymers from
bifunctional and polyfunctional compounds (monomers), accompanied by the
elimination of low-molecular weight by-products (for example, water,
alcohols, and hydrogen halides). A typical example of polycondensation
is the synthesis of complex polyester.
The process is
called homopolycondensation if the minimum possible number of monomer
types for a given case participates, and this number is usually two. If
at least one monomer more than the number required for the given
reaction participates in polycondensation, the process is called
copolycondensation. Polycondensation in which only bifunctional
compounds participate leads to the formation of linear macromolecules
and is called linear polycondensation. If molecules with three or more
functional groups participate in polycondensation, three-dimensional
structures are formed and the process is called three-dimensional
polycondensation. In cases where the degree of completion of
polycondensation and the mean length of the macromolecules are limited
by the equilibrium concentration of the reagents and reaction products,
the process is called equilibrium (reversible) polycondensation. If the
limiting factors are kinetic rather than thermodynamic, the process is
called nonequilibrium (irreversible) polycondensation.
Polycondensation
is often complicated by side reactions, in which both the original
monomers and the polycondensation products (oligomers and polymers) may
participate. Such reactions include the reaction of monomer or oligomer
with a mono-functional compound (which may be present as an impurity),
intramolecular cyclization (ring closure), and degradation of the
macromolecules of the resultant polymer. The rate competition of
polycondensation and the side reactions determines the molecular weight,
yield, and molecular weight distribution of the polycondensation
polymer.
Polycondensation is characterized by
disappearance of the monomer in the early stages of the process and a
sharp increase in molecular weight, in spite of a slight change in the
extent of conversion in the region of greater than 95-percent
conversion.
A necessary condition for the formation of
macro-molecular polymers in linear polycondensation is the equivalence
of the initial functional groups that react with one another.
Polycondensation is accomplished by one of three methods:
- in a melt, when a mixture of the initial compounds is heated for a long period to 10°-20°C above the melting (softening) point of the resultant polymer;
- in solution, when the monomers are present in the same phase in the solute state;
- on the phase boundary between two immiscible liquids, in which one of the initial compounds is found in each of the liquid phases (interphase polycondensation).
Polycondensation
processes play an important role in nature and technology.
Polycondensation or similar reactions are the basis for the biosynthesis
of the most important biopolymers-proteins, nucleic acids, and
cellulose. Polycondensation is widely used in industry for the
production of polyesters (polyethylene terephthalate, polycarbonates,
and alkyd resins), polyamides, phenol-formaldehyde resins,
urea-formaldehyde resins, and certain silicones [9].
In the period 1965-70, polycondensation acquired great importance in
connection with the development of industrial production of a series of
new polymers, including heat-resistant polymers (polyarylates, aromatic
polyimides, polyphe-nylene oxides, and polysulfones).
2.1.3. Polyaddition
The
polyaddition reactions are similar to polycondensation reactions
because they are also step reactions, however without splitting off low
molecular weight by-products. The reaction is exothermic rather than
endothermic and therefore cannot be stopped at will. Typical for
polyaddition reaction is that individual atoms, usually H-atoms, wander
from one monomer to another as the two monomers combine through a
covalent bond. The monomers, as in polycondensation reactions, have to
be added in stoichiometric amounts. These reactions do not start
spontaneously and they are slow.
Polyaddition does not
play a significant role in the production of thermoplastics. It is
commonly encountered with cross-linked polymers. Polyurethane, which can
be either a thermoplastic or thermosets, is synthesized by the reaction
of multi-functional isocyanates with multifunctional amines or alcohol.
Thermosetting epoxy resins are formed by polyaddition of epoxides with
curing agents, such as amines and acid anhydrides.
In
comparing chain reaction polymerization with the other two types of
polymerization the following principal differences should be noted:
Chain reaction polymerization, or simply called polymerization, is a
chain reaction as the name implies. Only individual monomer molecules
add to a reactive growing chain end, except for recombination of two
radical chain ends or reactions of a reactive chain end with an added
modifier molecule. The activation energy for chain initiation is much
grater than for the subsequent growth reaction and growth, therefore,
occurs very rapidly.
2.2. Composites
Composite
is any material made of more than one component. There are a lot of
composites around you. Concrete is a composite. It's made of cement,
gravel, and sand, and often has steel rods inside to reinforce it. Those
shiny balloons you get in the hospital when you're sick are made of a
composite, which consists of a polyester sheet and an aluminum foil
sheet, made into a sandwich. The polymer composites made from polymers,
or from polymers along with other kinds of materials [7].
But specifically the fiber-reinforced composites are materials in which
a fiber made of one material is embedded in another material.
2.2.1. Polymer composites
The
polymer composites are any of the combinations or compositions that
comprise two or more materials as separate phases, at least one of which
is a polymer. By combining a polymer with another material, such as
glass, carbon, or another polymer, it is often possible to obtain unique
combinations or levels of properties. Typical examples of synthetic
polymeric composites include glass-, carbon-, or
polymer-fiber-reinforced, thermoplastic or thermosetting resins,
carbon-reinforced rubber, polymer blends, silica- or mica-reinforced
resins, and polymer-bonded or -impregnated concrete or wood. It is also
often useful to consider as composites such materials as coatings
(pigment-binder combinations) and crystalline polymers (crystallites in a
polymer matrix). Typical naturally occurring composites include wood
(cellulosic fibers bonded with lignin) and bone (minerals bonded with
collagen). On the other hand, polymeric compositions compounded with a
plasticizer or very low proportions of pigments or processing aids are
not ordinarily considered as composites.
Typically, the
goal is to improve strength, stiffness, or toughness, or dimensional
stability by embedding particles or fibers in a matrix or binding phase.
A second goal is to use inexpensive, readily available fillers to
extend a more expensive or scarce resin; this goal is increasingly
important as petroleum supplies become costlier and less reliable. Still
other applications include the use of some filler such as glass spheres
to improve processability, the incorporation of dry-lubricant particles
such as molybdenum sulfide to make a self-lubricating bearing, and the
use of fillers to reduce permeability.
The most common
fiber-reinforced polymer composites are based on glass fibers, cloth,
mat, or roving embedded in a matrix of an epoxy or polyester resin.
Reinforced thermosetting resins containing boron, polyaramids, and
especially carbon fibers confer especially high levels of strength and
stiffness. Carbon-fiber composites have a relative stiffness five times
that of steel. Because of these excellent properties, many applications
are uniquely suited for epoxy and polyester composites, such as
components in new jet aircraft, parts for automobiles, boat hulls,
rocket motor cases, and chemical reaction vessels.
Although
the most dramatic properties are found with reinforced thermosetting
resins such as epoxy and polyester resins, significant improvements can
be obtained with many reinforced thermoplastic resins as well.
Polycarbonates, polyethylene, and polyesters are among the resins
available as glass-reinforced composition. The combination of
inexpensive, one-step fabrication by injection molding, with improved
properties has made it possible for reinforced thermoplastics to replace
metals in many applications in appliances, instruments, automobiles,
and tools.
In the development of other composite systems,
various matrices are possible; for example, polyimide resins are
excellent matrices for glass fibers, and give a high- performance
composite. Different fibers are of potential interest, including
polymers [such as poly(vinyl alcohol)], single-crystal ceramic whiskers
(such as sapphire), and various metallic fibers.
Long
ago, people living in South and Central America had used natural rubber
latex, polyisoprene, to make things like gloves and boots, as well as
rubber balls which they used to play games that were a lot like modern
basketball. He took two layers of cotton fabric and embedded them in
natural rubber, also known as polyisoprene, making a three-layered
sandwich like the one you see on your right (Remember, cotton is made up
of a natural polymer called cellulose). This made for good raincoats
because, while the rubber made it waterproof, the cotton layers made it
comfortable to wear, to make a material that has the properties of both
its components. In this case, we combine the water-resistance of
polyisoprene and the comfort of cotton.
Modern
composites are usually made of two components, a fiber and matrix. The
fiber is most often glass, but sometimes Kevlar, carbon fiber, or
polyethylene. The matrix is usually a thermoset like an epoxy resin,
polydicyclopentadiene, or a polyimide. The fiber is embedded in the
matrix in order to make the matrix stronger. Fiber-reinforced composites
have two things going for them. They are strong and light. They are
often stronger than steel, but weigh much less. This means that
composites can be used to make automobiles lighter, and thus much more
fuel efficient.
A common fiber-reinforced composite is FiberglasTM.
Its matrix is made by reacting polyester with carbon-carbon double
bonds in its backbone, and styrene. We pour a mix of the styrene and
polyester over a mass of glass fibers.
The styrene and
the double bonds in the polyester react by free radical vinyl
polymerization to form a crosslinked resin. The glass fibers are trapped
inside, where they act as a reinforcement. In FiberglasTM
the fibers are not lined up in any particular direction. They are just a
tangled mass, like you see on the right. But we can make the composite
stronger by lining up all the fibers in the same direction. Oriented
fibers do some weird things to the composite. When you pull on the
composite in the direction of the fibers, the composite is very strong.
But if you pull on it at right angles to the fiber direction, it is not
very strong at all [8-9].
This is not always bad, because sometimes we only need the composite to
be strong in one direction. Sometimes the item you are making will only
be under stress in one direction. But sometimes we need strength in
more than one direction. So we simply point the fibers in more than one
direction. We often do this by using a woven fabric of the fibers to
reinforce the composite. The woven fibers give a composite good strength
in many directions.
The polymeric matrix holds the
fibers together. A loose bundle of fibers would not be of much use.
Also, though fibers are strong, they can be brittle. The matrix can
absorb energy by deforming under stress. This is to say, the matrix adds
toughness to the composite. And finally, while fibers have good tensile
strength (that is, they are strong when you pull on them), they usually
have awful compressional strength. That is, they buckle when you squash
them. The matrix gives compressional strength to the composite.
Not
all fibers are the same. Now it may seem strange that glass is used as
reinforcement, as glass is really easy to break. But for some reason,
when glass is spun into really tiny fibers, it acts very different.
Glass fibers are strong, and flexible.
Still, there are
stronger fibers out there. This is a good thing, because sometimes glass
just isn't strong and tough enough. For some things, like airplane
parts, that undergo a lot of stress, you need to break out the fancy
fibers. When cost is no object, you can use stronger, but more expensive
fibers, like KevlarTM, carbon fiber. Carbon fiber (SpectraTM) is usually stronger than KevlarTM, that is, it can withstand more force without breaking. But KevlarTM
tends to be tougher. This means it can absorb more energy without
breaking. It can stretch a little to keep from breaking, more so than
carbon fiber can. But SpectraTM, which is a kind of polyethylene, is stronger and tougher than both carbon fiber and KevlarTM.
Different
jobs call for different matrices. The unsaturated polyester/styrene
systems at are one example. They are fine for everyday applications.
Chevrolet Corvette bodies are made from composites using unsaturated
polyester matrices and glass fibers. But they have some drawbacks. They
shrink a good deal when they're cured, they can absorb water very
easily, and their impact strength is low.
2.2.2. Biocomposites
For
many decades, the residential construction field has used timber as its
main source of building material for the frames of modern American
homes. The American timber industry produced a record 49.5 billion board
feet of lumber in 1999, and another 48.0 billion board feet in 2002. At
the same time that lumber production is peaking, the home ownership
rate reached a record high of 69.2%, with over 977,000 homes being sold
in 2002. Because residential construction accounts for one-third of the
total softwood lumber use in the United States, there is an increasing
demand for alternate materials. Use of sawdust not only provides an
alternative but also increases the use of the by product efficiently.
Wood plastic composites (WPC) is a relatively new category of materials
that covers a broad range of composite materials utilizing an organic
resin binder (matrix) and fillers composed of cellulose materials. The
new and rapidly developing biocomposite materials are high technology
products, which have one unique advantage – the wood filler can include
sawdust and scrap wood products. Consequently, no additional wood
resources are needed to manufacture biocomposites. Waste products that
would traditraditionally cost money for proper disposal, now become a
beneficial resource, allowing recycling to be both profitable and
environmentally conscious. The use of biocomposites and WPC has
increased rapidly all over the world, with the end users for these
composites in the construction, motor vehicle, and furniture industries.
One of the primary problems related to the use of biocomposites is the
flammability of the two main components (binder and filler). If a flame
retardant were added, this would require the adhesion of the fiber and
the matrix not to be disturbed by the retardant. The challenge is to
develop a composite that will not burn and will maintain its level of
mechanical performance. In lieu of organic matrix compounds, inorganic
matrices can be utilized to improve the fire resistance. Inorganic-based
wood composites are those that consist of a mineral mix as the binder
system. Such inorganic binder systems include gypsum and Portland
cement, both of which are highly resistant to fire and insects. The main
disadvantage with these systems is the maximum amount of sawdust or
fibers than can be incorporated is low. One relatively new type of
inorganic matrix is potassium aluminosilicate, an environmentally
friendly compound made from naturally occurring materials. The Federal
Aviation Administration has investigated the feasibility of using this
matrix in commercial aircraft due to its ability to resist temperatures
of up to 1000 ºC without generating smoke, and its ability to enable
carbon composites to withstand temperatures of 800 ºC and maintain 63%
of its original flexural strength. Potassium aluminosilicate matrices
are compatible with many common building material including clay brick,
masonry, concrete, steel, titanium, balsa, oak, pine, and particleboard [10].
2.3. Fiberglass
Fiberglass
refers to a group of products made from individual glass fibers
combined into a variety of forms. Glass fibers can be divided into two
major groups according to their geometry: continuous fibers used in
yarns and textiles, and the discontinuous (short) fibers used as batts,
blankets, or boards for insulation and filtration. Fiberglass can be
formed into yarn much like wool or cotton, and woven into fabric which
is sometimes used for draperies. Fiberglass textiles are commonly used
as a reinforcement material for molded and laminated plastics.
Fiberglass wool, a thick, fluffy material made from discontinuous
fibers, is used for thermal insulation and sound absorption. It is
commonly found in ship and submarine bulkheads and hulls; automobile
engine compartments and body panel liners; in furnaces and air
conditioning units; acoustical wall and ceiling panels; and
architectural partitions. Fiberglass can be tailored for specific
applications such as Type E (electrical), used as electrical insulation
tape, textiles and reinforcement; Type C (chemical), which has superior
acid resistance, and Type T, for thermal insulation [11].
Though
commercial use of glass fiber is relatively recent, artisans created
glass strands for decorating goblets and vases during the Renaissance. A
French physicist, Rene-Antoine Ferchault de Reaumur, produced textiles
decorated with fine glass strands in 1713. Glass wool, a fluffy mass of
discontinuous fiber in random lengths, was first produced in Europe in
1900, using a process that involved drawing fibers from rods
horizontally to a revolving drum [12].
The
basic raw materials for fiberglass products are a variety of natural
minerals and manufactured chemicals. The major ingredients are silica
sand, limestone, and soda ash. Other ingredients may include calcined
alumina, borax, feldspar, nepheline syenite, magnesite, and kaolin clay,
among others. Silica sand is used as the glass former, and soda ash and
limestone help primarily to lower the melting temperature. Other
ingredients are used to improve certain properties, such as borax for
chemical resistance. Waste glass, also called cullet, is also used as a
raw material. The raw materials must be carefully weighed in exact
quantities and thoroughly mixed together (called batching) before being
melted into glass.
2.3.1. The manufacturing process
2.3.1.1. Melting
Once
the batch is prepared, it is fed into a furnace for melting. The
furnace may be heated by electricity, fossil fuel, or a combination of
the two. Temperature must be precisely controlled to maintain a smooth,
steady flow of glass. The molten glass must be kept at a higher
temperature (about 1371 °C) than other types of glass in order to be
formed into fiber. Once the glass becomes molten, it is transferred to
the forming equipment via a channel (forehearth) located at the end of
the furnace [13].
2.3.1.2. Forming into fibers
Several
different processes are used to form fibers, depending on the type of
fiber. Textile fibers may be formed from molten glass directly from the
furnace, or the molten glass may be fed first to a machine that forms
glass marbles of about 0.62 inch (1.6 cm) in diameter. These marbles
allow the glass to be inspected visually for impurities. In both the
direct melt and marble melt process, the glass or glass marbles are fed
through electrically heated bushings (also called spinnerets). The
bushing is made of platinum or metal alloy, with anywhere from 200 to
3,000 very fine orifices. The molten glass passes through the orifices
and comes out as fine filaments [13].
2.3.1.3. Continuous-filament process
A
long, continuous fiber can be produced through the continuous-filament
process. After the glass flows through the holes in the bushing,
multiple strands are caught up on a high-speed winder. The winder
revolves at about 3 km a minute, much faster than the rate of flow from
the bushings. The tension pulls out the filaments while still molten,
forming strands a fraction of the diameter of the openings in the
bushing. A chemical binder is applied, which helps keep the fiber from
breaking during later processing. The filament is then wound onto tubes.
It can now be twisted and plied into yarn [14].
2.3.1.4. Staple-fiber process
An
alternative method is the staplefiber process. As the molten glass
flows through the bushings, jets of air rapidly cool the filaments. The
turbulent bursts of air also break the filaments into lengths of 20-38
cm. These filaments fall through a spray of lubricant onto a revolving
drum, where they form a thin web. The web is drawn from the drum and
pulled into a continuous strand of loosely assembled fibers [15]. This strand can be processed into yarn by the same processes used for wool and cotton.
2.3.1.5. Chopped fiber
Instead
of being formed into yarn, the continuous or long-staple strand may be
chopped into short lengths. The strand is mounted on a set of bobbins,
called a creel, and pulled through a machine which chops it into short
pieces. The chopped fiber is formed into mats to which a binder is
added. After curing in an oven, the mat is rolled up. Various weights
and thicknesses give products for shingles, built-up roofing, or
decorative mats [16].
2.3.1.6. Glass wool
The
rotary or spinner process is used to make glass wool. In this process,
molten glass from the furnace flows into a cylindrical container having
small holes. As the container spins rapidly, horizontal streams of glass
flow out of the holes. The molten glass streams are converted into
fibers by a downward blast of air, hot gas, or both. The fibers fall
onto a conveyor belt, where they interlace with each other in a fleecy
mass. This can be used for insulation, or the wool can be sprayed with a
binder, compressed into the desired thickness, and cured in an oven.
The heat sets the binder, and the resulting product may be a rigid or
semi-rigid board, or a flexible bat [15-16].
2.3.1.7. Protective coatings
In
addition to binders, other coatings are required for fiberglass
products. Lubricants are used to reduce fiber abrasion and are either
directly sprayed on the fiber or added into the binder. An anti-static
composition is also sometimes sprayed onto the surface of fiberglass
insulation mats during the cooling step. Cooling air drawn through the
mat causes the anti-static agent to penetrate the entire thickness of
the mat. The anti-static agent consists of two ingredients a material
that minimizes the generation of static electricity, and a material that
serves as a corrosion inhibitor and stabilizer.
Sizing
is any coating applied to textile fibers in the forming operation, and
may contain one or more components (lubricants, binders, or coupling
agents). Coupling agents are used on strands that will be used for
reinforcing plastics, to strengthen the bond to the reinforced material.
Sometimes a finishing operation is required to remove these coatings,
or to add another coating. For plastic reinforcements, sizings may be
removed with heat or chemicals and a coupling agent applied. For
decorative applications, fabrics must be heat treated to remove sizings
and to set the weave. Dye base coatings are then applied before dying or
printing [15-16].
2.3.1.8. Forming into shapes
Fiberglass
products come in a wide variety of shapes, made using several
processes. For example, fiberglass pipe insulation is wound onto
rod-like forms called mandrels directly from the forming units, prior to
curing. The mold forms, in lengths of 91 cm or less, are then cured in
an oven. The cured lengths are then de-molded lengthwise, and sawn into
specified dimensions. Facings are applied if required, and the product
is packaged for shipment [17].
2.4. Carbon fibre
Carbon-fiber-reinforced
polymer or carbon-fiber-reinforced plastic (CFRP or CRP or often simply
carbon fiber), is a very strong and light fiber-reinforced polymer
which contains carbon fibers. Carbon fibres are created when
polyacrylonitrile fibres (PAN), Pitch resins, or Rayon are carbonized
(through oxidation and thermal pyrolysis) at high temperatures. Through
further processes of graphitizing or stretching the fibres strength or
elasticity can be enhanced respectively. Carbon fibres are manufactured
in diameters analogous to glass fibres with diameters ranging from 9 to
17 μm. These fibres wound into larger threads for transportation and
further production processes. Further production processes include
weaving or braiding into carbon fabrics, cloths and mats analogous to
those described for glass that can then be used in actual reinforcement
processes. Carbon fibers are a new breed of high-strength materials.
Carbon fiber has been described as a fiber containing at least 90%
carbon obtained by the controlled pyrolysis of appropriate fibers. The
existence of carbon fiber came into being in 1879 when Edison took out a
patent for the manufacture of carbon filaments suitable for use in
electric lamps [18].
2.4.1. Classification and types
Based
on modulus, strength, and final heat treatment temperature, carbon
fibers can be classified into the following categories:
- Ultra-high-modulus, type UHM (modulus >450Gpa)
- High-modulus, type HM (modulus between 350-450Gpa)
- Intermediate-modulus, type IM (modulus between 200-350Gpa)
- Low modulus and high-tensile, type HT (modulus < 100Gpa, tensile strength > 3.0Gpa)
- Super high-tensile, type SHT (tensile strength > 4.5Gpa)
- PAN-based carbon fibers
- Pitch-based carbon fibers
- Mesophase pitch-based carbon fibers
- Isotropic pitch-based carbon fibers
- Rayon-based carbon fibers
- Gas-phase-grown carbon fibers
- Type-I, high-heat-treatment carbon fibers (HTT), where final heat treatment temperature should be above 2000°C and can be associated with high-modulus type fiber.
- Type-II, intermediate-heat-treatment carbon fibers (IHT), where final heat treatment temperature should be around or above 1500 °C and can be associated with high-strength type fiber.
- Type-III, low-heat-treatment carbon fibers, where final heat treatment temperatures not greater than 1000 °C. These are low modulus and low strength materials [19].
2.4.2. Manufacture
In
Textile Terms and Definitions, carbon fiber has been described as a
fiber containing at least 90% carbon obtained by the controlled
pyrolysis of appropriate fibers. The term "graphite fiber" is used to
describe fibers that have carbon in excess of 99%. Large varieties of
fibers called precursors are used to produce carbon fibers of different
morphologies and different specific characteristics. The most prevalent
precursors are polyacrylonitrile (PAN), cellulosic fibers (viscose
rayon, cotton), petroleum or coal tar pitch and certain phenolic fibers.
Carbon
fibers are manufactured by the controlled pyrolysis of organic
precursors in fibrous form. It is a heat treatment of the precursor that
removes the oxygen, nitrogen and hydrogen to form carbon fibers. It is
well established in carbon fiber literature that the mechanical
properties of the carbon fibers are improved by increasing the
crystallinity and orientation, and by reducing defects in the fiber. The
best way to achieve this is to start with a highly oriented precursor
and then maintain the initial high orientation during the process of
stabilization and carbonization through tension [18-19].
2.4.2.1. Carbon fibers from polyacrylonitrile (PAN)
There
are three successive stages in the conversion of PAN precursor into
high-performance carbon fibers. Oxidative stabilization: The
polyacrylonitrile precursor is first stretched and simultaneously
oxidized in a temperature range of 200-300 °C. This treatment converts
thermoplastic PAN to a non-plastic cyclic or ladder compound.
Carbonization: After oxidation, the fibers are carbonized at about 1000
°C without tension in an inert atmosphere (normally nitrogen) for a few
hours. During this process the non-carbon elements are removed as
volatiles to give carbon fibers with a yield of about 50% of the mass of
the original PAN. Graphitization: Depending on the type of fiber
required, the fibers are treated at temperatures between 1500-3000 °C,
which improves the ordering, and orientation of the crystallites in the
direction of the fiber axis.
2.4.2.2. Carbon fibers from rayon
a- The conversion of rayon fibers into carbon fibers is three phase process
Stabilization:
Stabilization is an oxidative process that occurs through steps. In the
first step, between 25-150 °C, there is physical desorption of water.
The next step is a dehydration of the cellulosic unit between 150-240
°C. Finally, thermal cleavage of the cyclosidic linkage and scission of
ether bonds and some C-C bonds via free radical reaction (240-400 °C)
and, thereafter, aromatization takes place.
Carbonization: Between 400 and 700 °C, the carbonaceous residue is converted into a graphite-like layer.
Graphitization:
Graphitization is carried out under strain at 700-2700 °C to obtain
high modulus fiber through longitudinal orientation of the planes.
b- The carbon fiber fabrication from pitch generally consists of the following four steps:
Pitch
preparation: It is an adjustment in the molecular weight, viscosity,
and crystal orientation for spinning and further heating.
Spinning
and drawing: In this stage, pitch is converted into filaments, with
some alignment in the crystallites to achieve the directional
characteristics.
Stabilization: In this step, some kind
of thermosetting to maintain the filament shape during pyrolysis. The
stabilization temperature is between 250 and 400 °C.
Carbonization: The carbonization temperature is between 1000-1500 °C.
2.4.2.3. Carbon fibers in meltblown nonwovens
Carbon
fibers made from the spinning of molten pitches are of interest because
of the high carbon yield from the precursors and the relatively low
cost of the starting materials. Stabilization in air and carbonization
in nitrogen can follow the formation of melt-blown pitch webs. Processes
have been developed with isotropic pitches and with anisotropic
mesophase pitches. The mesophase pitch based and melt blown
discontinuous carbon fibers have a peculiar structure. These fibers are
characterized in that a large number of small domains, each domain
having an average equivalent diameter from 0.03 mm to 1mm and a nearly
unidirectional orientation of folded carbon layers, assemble to form a
mosaic structure on the cross-section of the carbon fibers. The folded
carbon layers of each domain are oriented at an angle to the direction
of the folded carbon layers of the neighboring domains on the boundary [20].
2.4.2.4. Carbon fibers from isotropic pitch
The
isotropic pitch or pitch-like material, i.e., molten polyvinyl
chloride, is melt spun at high strain rates to align the molecules
parallel to the fiber axis. The thermoplastic fiber is then rapidly
cooled and carefully oxidized at a low temperature (<100 °C). The
oxidation process is rather slow, to ensure stabilization of the fiber
by cross-linking and rendering it infusible. However, upon
carbonization, relaxation of the molecules takes place, producing fibers
with no significant preferred orientation. This process is not
industrially attractive due to the lengthy oxidation step, and only
low-quality carbon fibers with no graphitization are produced. These are
used as fillers with various plastics as thermal insulation materials [20].
2.4.2.5. Carbon fibers from anisotropic mesophase pitch
High
molecular weight aromatic pitches, mainly anisotropic in nature, are
referred to as mesophase pitches. The pitch precursor is thermally
treated above 350°C to convert it to mesophase pitch, which contains
both isotropic and anisotropic phases. Due to the shear stress occurring
during spinning, the mesophase molecules orient parallel to the fiber
axis. After spinning, the isotropic part of the pitch is made infusible
by thermosetting in air at a temperature below it's softening point. The
fiber is then carbonized at temperatures up to 1000 °C. The main
advantage of this process is that no tension is required during the
stabilization or the graphitization, unlike the case of rayon or PANs
precursors [21].
2.4.2.6. Structure
The
characterization of carbon fiber microstructure has been mainly been
performed by x-ray scattering and electron microscopy techniques. In
contrast to graphite, the structure of carbon fiber lacks any three
dimensional order. In PAN-based fibers, the linear chain structure is
transformed to a planar structure during oxidative stabilization and
subsequent carbonization. Basal planes oriented along the fiber axis are
formed during the carbonization stage. Wide-angle x-ray data suggests
an increase in stack height and orientation of basal planes with an
increase in heat treatment temperature. A difference in structure
between the sheath and the core was noticed in a fully stabilized fiber.
The skin has a high axial preferred orientation and thick crystallite
stacking. However, the core shows a lower preferred orientation and a
lower crystallite height [22].
2.4.2.7. Properties
In
general, it is seen that the higher the tensile strength of the
precursor the higher is the tenacity of the carbon fiber. Tensile
strength and modulus are significantly improved by carbonization under
strain when moderate stabilization is used. X-ray and electron
diffraction studies have shown that in high modulus type fibers, the
crystallites are arranged around the longitudinal axis of the fiber with
layer planes highly oriented parallel to the axis. Overall, the
strength of a carbon fiber depends on the type of precursor, the
processing conditions, heat treatment temperature and the presence of
flaws and defects. With PAN based carbon fibers, the strength increases
up to a maximum of 1300 ºC and then gradually decreases. The modulus has
been shown to increase with increasing temperature. PAN based fibers
typically buckle on compression and form kink bands at the innermost
surface of the fiber. However, similar high modulus type pitch-based
fibers deform by a shear mechanism with kink bands formed at 45° to the
fiber axis. Carbon fibers are very brittle. The layers in the fibers are
formed by strong covalent bonds. The sheet-like aggregations allow easy
crack propagation. On bending, the fiber fails at very low strain [23].
2.4.2.8. Applications
The
two main applications of carbon fibers are in specialized technology,
which includes aerospace and nuclear engineering, and in general
engineering and transportation, which includes engineering components
such as bearings, gears, cams, fan blades and automobile bodies.
Recently, some new applications of carbon fibers have been found. Others
include: decoration in automotive, marine, general aviation interiors,
general entertainment and musical instruments and after-market
transportation products. Conductivity in electronics technology provides
additional new application [24].
The
production of highly effective fibrous carbon adsorbents with low
diameter, excluding or minimizing external and intra-diffusion
resistance to mass transfer, and therefore, exhibiting high sorption
rates is a challenging task. These carbon adsorbents can be converted
into a wide variety of textile forms and nonwoven materials. Cheaper and
newer versions of carbon fibers are being produced from new raw
materials. Newer applications are also being developed for protective
clothing (used in various chemical industries for work in extremely
hostile environments), electromagnetic shielding and various other novel
applications. The use of carbon fibers in Nonwovens is in a new
possible application for high temperature fire-retardant insulation (eg:
furnace material) [25].
2.5. Aramid-definition
Aliphatic
polyamides are macromolecules whose structural units are
characteristically interlinked by the amide linkage -NH-CO-. The nature
of the structural unit constitutes a basis for classification. Aliphatic
polyamides with structural units derived predominantly from aliphatic
monomers are members of the generic class of nylons, whereas aromatic
polyamides in which at least 85% of the amide linkages are directly
adjacent to aromatic structures have been designated aramids. The U.S.
Federal Trade Commission defines nylon fibers as ‘‘a manufactured fiber
in which the fiber forming substance is a long chain synthetic polyamide
in which less than 85% of the amide linkages (-CO-NH-) are attached
directly to two aliphatic groups.’’ Polyamides that contain recurring
amide groups as integral parts of the polymer backbone have been
classified as condensation polymers regardless of the principal
mechanisms entailed in the polymerization process. Though many reactions
suitable for polyamide formation are known, commercially important
nylons are obtained by processes related to either of two basic
approaches: one entails the polycondensation of difunctional monomers
utilizing either amino acids or stoichiometric pairs of dicarboxylic
acids and diamines, and the other entails the ring-opening
polymerization of lactams. The polyamides formed from diacids and
diamines are generally described to be of the AABB format, whereas those
derived from either amino acids or lactams are of the AB format.
The
structure of polyamide fibers is defined by both chemical and physical
parameters. The chemical parameters are related mainly to the
constitution of the polyamide molecule and are concerned primarily with
its monomeric units, end-groups, and molecular weight. The physical
parameters are related essentially to chain conformation, orientation of
both polymer molecule segments and aggregates, and to crystallinity [26].
This characteristic for single-chain aliphatic polyamides is determined
by the structure of the monomeric units and the nature of end groups of
the polymer molecules. The most important structural parameter of the
noncrystalline (amorphous) phase is the glass transition temperature (Tg)
since it has a considerable effect on both processing and properties of
the polyamide fibers. It relates to a type of a glass–rubber transition
and is defined as the temperature, or temperature range, at which
mobility of chain segments or structural units commences. Thus it is a
function of the chemical structure; in case of the linear aliphatic
polyamides, it is a function of the number of CH2 units (mean spacing) between the amide groups. As the number of CH2 unit’s increases, Tg decreases. Although Tg
is further affected by the nature of the crystalline phase,
orientation, and molecular weight, it is associated only with what may
be considered the amorphous phase.
Any process affecting
this phase exerts a corresponding effect on the glass transition
temperature. This is particularly evident in its response to the
concentration of water absorbed in polyamides. An increase in water
content results in a steady decrease of Tg toward a limiting
value. This phenomenon may be explained by a mechanism that entails
successive replacement of intercatenary hydrogen bonds in the amorphous
phase with water. It may involve a sorption mechanism, according to
which 3 mol of water interact with two neighboring amide groups [27].
The
properties of aromatic polyamides differ significantly from those of
their aliphatic counterparts. This led the U.S. Federal Trade Commission
to adopt the term ‘‘aramid’’ to designate fibers of the aromatic
polyamide type in which at least 85% of the amide linkages are attached
directly to two aromatic rings.
The search for materials
with very good thermal properties was the original reason for research
into aromatic polyamides. Bond dissociation energies of C-C and C-N
bonds in aromatic polyamides are ~20% higher than those in aliphatic
polyamides. This is the reason why the decomposition temperature of
poly(m-phenylene isophthalamide) MPDI exceeds 450 ºC. Conjugation
between the amide group and the aromatic ring in poly(p-phenylene
terephthalamide) “PPTA” increases chain rigidity as well as the
decomposition temperature, which exceeds 550 ºC.
Obviously,
hydrogen bonding and chain rigidity of these polymers translates to
very high glass transition temperatures. Using low-molecular-weight
polymers, Aharoni [19]
measured glass transition temperatures of 272 ºC for MPDI and over 295
ºC for PPTA (which in this case had low crystallinity). Others have
reported values as high as 4928 ºC. In most cases the measurement of Tg
is difficult because PPTA is essentially 100% crystalline. As one would
expect, these values are not strongly dependent on the molecular weight
of the polymer above a DP of ~10 [22].
The
same structural characteristics that are responsible for the excellent
thermal properties of these materials are responsible for their limited
solubility as well as good chemical resistance. PPTA is soluble only in
strong acids like H2SO4, HF, and methanesulfonic
acid. Preparation of this polymer via solution polymerization in amide
solvents is accompanied by polymer precipitation. As expected, based on
its structure, MPDI is easier to solubilize then PPTA. It is soluble in
neat amide solvents like N-methyl-2-pyrrolidone (NMP) and
dimethylacetamide (DMAc), but adding salts like CaCl2 or LiCl
significantly enhances its solubility. The significant rigidity of the
PPTA chain (as discussed above) leads to the formation of anisotropic
solutions when the solvent is good enough to reach critical minimum
solids concentration. The implications of this are discussed in greater
detail later in this chapter. It is well known that chemical properties
differ significantly between crystalline and noncrystalline materials of
the same composition. In general, aramids have very good chemical
resistance. Obviously, the amide bond is subject to a hydrolytic attack
by acids and bases. Exposure to very strong oxidizing agents results in a
significant strength loss of these fibers. In addition to
crystallinity, structure consolidation affects the rate of degradation
of these materials. The hydrophilicity of the amide group leads to a
significant absorption of water by all aramids. While the chemistry is
the driving factor, fiber structure also plays a very important role;
for example, Kevlar 29 absorbs ~7% water, Kevlar 49~4%, and Kevlar 149
only 1%. Fukuda explored the relationship between fiber crystallinity
and equilibrium moisture in great detail. Because of their aromatic
character, aramids absorb UV light, which results in an oxidative color
change. Substantial exposure can lead to the loss of yarn tensile
properties. UV absorption by p-aramids is more pronounced than with
m-aramids. In this case a self-screening phenomenon is observed, which
makes thin structures more susceptible to degradation than thick ones.
Very frequently p-aramids are covered with another material in the final
application to protect them. The high degree of aromaticity of these
materials also provides significant flame resistance. All commercial
aramids have a limited oxygen index in the range of 28-32%, which
compares with ~20% for aliphatic polyamides.
Typical
properties of commercial aramid fibers are while yarns of m-aramids have
tensile properties that are no greater than those of aliphatic
polyamides, they do retain useful mechanical properties at significantly
higher temperatures. The high glass transition temperature leads to low
(less than 1%) shrinkage at temperatures below 250 ºC. In general,
mechanical properties of m-aramid fibers are developed on drawing. This
process produces fibers with a high degree of morphological homogeneity,
which leads to very good fatigue properties. The mechanical properties
of p-aramid fibers have been the subject of much study. This is because
these fibers were the first examples of organic materials with a very
high level of both strength and stiffness. These materials are practical
confirmation that nearly perfect orientation and full chain extension
are required to achieve mechanical properties approaching those
predicted for chemical bonds. In general, the mechanical properties
reflect a significant anisotropy of these fibers-covalent bonds in the
direction of the fiber axis with hydrogen bonding and van der Waals
forces in the lateral direction [26].
Aramid-based
reinforcement has been viewed as a more specialty product for
applications requiring high modulus and where the potential for
electrical conductivity would preclude the use of carbon; for example,
aramid sheet is used for all tunnel repairs. Product forms include dry
fabrics or unidirectional sheets as well as pre-cured strips or bars.
Fabrics or sheets are applied to a concrete surface that has been
smoothed (by grinding or blasting) and wetted with a resin (usually
epoxy). The composite materials used for concrete infrastructure repair
that was initiated in the mid 1980s. After air pockets are removed using
rollers or flat, flexible squeegees, a second resin coat might be
applied. Reinforcement of concrete structures is important in earthquake
prone areas, although steel plate is the primary material used to
reinforce and repair concrete structures, higher priced fiber-based
sheet structures offer advantages for small sites where ease of handling
and corrosion resistance are important. The high strength, modulus, and
damage tolerance of aramid-reinforced sheets makes the fiber especially
suitable for protecting structures prone to seismic activity. The use
of aramid sheet also simplifies the application process. Sheets are
light in weight and can be easily handled without heavy machinery and
can be applied in confined working spaces. Sheets are also flexible, so
surface smoothing and corner rounding of columns are less critical than
for carbon fiber sheets [28].
3. All process description
FRP
involves two distinct processes, the first is the process whereby the
fibrous material is manufactured and formed, and the second is the
process whereby fibrous materials are bonded with the matrix during the
molding process.
3.1. Fibre process
3.1.1. The manufacture of fibre fabric
Reinforcing Fibre is manufactured in both two dimensional and three dimensional orientations
- Two Dimensional Fibre Reinforced Polymer are characterized by a laminated structure in which the fibres are only aligned along the plane in x-direction and y-direction of the material. This means that no fibres are aligned in the through thickness or the z-direction, this lack of alignment in the through thickness can create a disadvantage in cost and processing. Costs and labour increase because conventional processing techniques used to fabricate composites, such as wet hand lay-up, autoclave and resin transfer molding, require a high amount of skilled labour to cut, stack and consolidate into a preformed component.
- Three-dimensional Fibre Reinforced Polymer composites are materials with three dimensional fibre structures that incorporate fibres in the x-direction, y-direction and z-direction. The development of three-dimensional orientations arose from industry's need to reduce fabrication costs, to increase through-thickness mechanical properties, and to improve impact damage tolerance; all were problems associated with two dimensional fibre reinforced polymers [28].
3.1.2. The manufacture of fibre preforms
Fibre
preforms are how the fibres are manufactured before being bonded to the
matrix. Fibre preforms are often manufactured in sheets, continuous
mats, or as continuous filaments for spray applications. The four major
ways to manufacture the fibre preform is though the textile processing
techniques of Weaving, knitting, braiding and stitching.
- Weaving can be done in a conventional manner to produce two-dimensional fibres as well in a multilayer weaving that can create three-dimensional fibres. However, multilayer weaving is required to have multiple layers of warp yarns to create fibres in the z- direction creating a few disadvantages in manufacturing, namely the time to set up all the warp yarns on the loom. Therefore most multilayer weaving is currently used to produce relatively narrow width products or high value products where the cost of the preform production is acceptable. Another Fibre-reinforced plastic 3D one of the main problems facing the use of multilayer woven fabrics is the difficulty in producing a fabric that contains fibres oriented with angles other than 0º and 90º to each other respectively.
- The second major way of manufacturing fibre preforms is braiding. Braiding is suited to the manufacture of narrow width flat or tubular fabric and is not as capable as weaving in the production of large volumes of wide fabrics. Braiding is done over top of mandrels that vary in cross-sectional shape or dimension along their length. Braiding is limited to objects about a brick in size. Unlike the standard weaving process, braiding can produce fabric that contains fibres at 45 degrees angles to one another. Braiding three-dimensional fibres can be done using four steps, two-step or Multilayer Interlock Braiding. Four step or row and column braiding utilizes a flat bed containing rows and columns of yarn carriers that form the shape of the desired preform. Additional carriers are added to the outside of the array, the precise location and quantity of which depends upon the exact preform shape and structure required. There are four separate sequences of row and column motion, which act to interlock the yarns and produce the braided preform. The yarns are mechanically forced into the structure between each step to consolidate the structure in a similar process to the use of a reed in weaving.Two-step braiding is unlike the four step process because the two-step includes a large number of yarns fixed in the axial direction and a fewer number of braiding yarns. The process consists of two steps in which the braiding carriers move completely through the structure between the axial carriers. This relatively simple sequence of motions is capable of forming performs of essentially any shape, including circular and hollow shapes. Unlike the four steps process the two steps process does not require mechanical compaction the motions involved in the process allows the braid to be pulled tight by yarn tension alone. The last type of braiding is multi-layer interlocking braiding that consists of a number of standard circular braiders being joined together to form a cylindrical braiding frame. This frame has a number of parallel braiding tracks around the circumference of the cylinder but the mechanism allows the transfer of yarn carriers between adjacent tracks forming a multilayer braided fabric with yarns interlocking to adjacent layers.
The
multilayer interlock braid differs from both the four step and two-step
braids in that the interlocking yarns are primarily in the plane of the
structure and thus do not significantly reduce the in-plane properties
of the perform. The four step and two step processes produce a greater
degree of interlinking as the braiding yarns travel through the
thickness of the preform, but therefore contribute less to the in-plane
performance of the preform. A disadvantage of the multilayer interlock
equipment is that due to the conventional sinusoidal movement of the
yarn carriers to form the preform, the equipment is not able to have the
density of yarn carriers that is possible with the two step and four
step machines.
- Knitting fibre preforms can be done with the traditional methods of Warp and [Weft] Knitting, and the fabric produced is often regarded by many as two-dimensional fabric, but machines with two or more needle beds are capable of producing multilayer fabrics with yams that traverse between the layers. Developments in electronic controls for needle selection and knit loop transfer and in the sophisticated mechanisms that allow specific areas of the fabric to be held and their movement controlled. This has allowed the fabric to form itself into the required three-dimensional perform shape with a minimum of material wastage.
- Stitching is arguably the simplest of the four main textile manufacturing techniques and one that can be performed with the smallest investment in specialized machinery. Basically the stitching process consists of inserting a needle, carrying the stitch thread, through a stack of fabric layers to form a 3D structure. The advantages of stitching are that it is possible to stitch both dry and prepreg fabric, although the tackiness of prepare makes the process difficult and generally creates more damage within the prepreg material than in the dry fabric. Stitching also utilizes the standard two-dimensional fabrics that are commonly in use within the composite industry therefore there is a sense of familiarity concerning the material systems. The use of standard fabric also allows a greater degree of flexibility in the fabric lay-up of the component than is possible with the other textile processes, which have restrictions on the fibre orientations that can be produced.
3.1.3. Molding processes
There
are two distinct categories of molding processes using FRP plastics;
this includes composite molding and wet molding. Composite molding uses
Prepreg FRP, meaning the plastics are fibre reinforced before being put
through further molding processes. Sheets of Prepreg FRP are heated or
compressed in different ways to create geometric shapes. Wet molding
combines fibre reinforcement and the matrix or resist during the molding
process. The different forms of composite and wet molding, are listed
below.
3.2. Composite molding
3.2.1. Bladder molding
Individual
sheets of prepreg material are laid -up and placed in a female-style
mould along with a balloon-like bladder. The mould is closed and placed
in a heated press. Finally, the bladder is pressurized forcing the
layers of material against the mould walls. The part is cured and
removed from the hot mould. Bladder molding is a closed molding process
with a relatively short cure cycle between 15 and 60 minutes making it
ideal for making complex hollow geometric shapes at competitive costs.
3.2.2. Compression molding
A
"preform" or "charge", of SMC, BMC or sometimes prepreg fabric, is
placed into mould cavity. The mould is closed and the material is
compacted & cured inside by pressure and heat. Compression molding
offers excellent detailing for geometric shapes ranging from pattern and
relief detailing to complex curves and creative forms, to precision
engineering all within a maximum curing time of 20 minutes.
3.2.3. Autoclave − Vacuum bag
Individual
sheets of prepreg material are laid-up and placed in an open mold. The
material is covered with release film, bleeder/breather material and a
vacuum bag. A vacuum is pulled on part and the entire mould is placed
into an autoclave (heated pressure vessel). The part is cured with a
continuous vacuum to extract entrapped gasses from laminate. This is a
very common process in the aerospace industry because it affords precise
control over the molding process due to a long slow cure cycle that is
anywhere from one to two hours. This precise control creates the exact
laminate geometric forms needed to ensure strength and safety in the
aerospace industry, but it is also slow and lab our intensive, meaning
costs often confine it to the aerospace industry.
3.2.4. Mandrel wrapping
Sheets
of prepreg material are wrapped around a steel or aluminum mandrel. The
prepreg material is compacted by nylon or polypropylene cello tape.
Parts are typically batch cured by hanging in an oven. After cure the
cello and mandrel are removed leaving a hollow carbon tube. This process
creates strong and robust hollow carbon tubes.
3.2.5. Wet layup
Fibre
reinforcing fabric is placed in an open mould and then saturated with a
wet (resin) by pouring it over the fabric and working it into the
fabric and mould. The mould is then left so that the resin will cure,
usually at room temperature, though heat is sometimes used to ensure a
proper curing process. Glass fibres are most commonly used for this
process, the results are widely known as fibreglass, and are used to
make common products like skis, canoes, kayaks and surf boards.
3.2.6. Chopper gun
Continuous
strand of fibreglass are pushed through a hand-held gun that both chops
the strands and combines them with a catalyzed resin such as polyester.
The impregnated chopped glass is shot onto the mould surface in
whatever thickness the design and human operator think is appropriate.
This process is good for large production runs at economical cost, but
produces geometric shapes with less strength than other molding
processes and has poor dimensional tolerance.
3.2.7. Filament winding
Machines
pull fibre bundles through a wet bath of resin and wound over a
rotating steel mandrel in specific orientations Parts are cured either
room temperature or elevated temperatures. Mandrel is extracted, leaving
a final geometric shape but can be left in some cases.
3.2.8. Pultrusion
Fibre
bundles and slit fabrics are pulled through a wet bath of resin and
formed into the rough part shape. Saturated material is extruded from a
heated closed die curing while being continuously pulled through die.
Some of the end products of the pultrusion process are structural
shapes, i.e. beam, angle, channel and flat sheet. These materials can be
used to create all sorts of fibreglass structures such as ladders,
platforms, handrail systems tank, pipe, and pump supports.
3.3. Resin infusion
Fabrics
are placed into a mould which wet resin is then injected into. Resin is
typically pressurized and forced into a cavity which is under vacuum in
the RTM (Resin Transfer Molding) process. Resin is entirely pulled into
cavity under vacuum in the VARTM (Vacuum Assisted Resin Transfer
Molding) process. This molding process allows precise tolerances and
detailed shaping but can sometimes fail to fully saturate the fabric
leading to weak spots in the final shape.
3.3.1. Advantages and limitations
FRP
allows the alignment of the glass fibres of thermoplastics to suit
specific design programs. Specifying the orientation of reinforcing
fibres can increase the strength and resistance to deformation of the
polymer. Glass reinforced polymers are strongest and most resistive to
deforming forces when the polymers fibres are parallel to the force
being exerted, and are weakest when the fibres are perpendicular. Thus
this ability is at once both an advantage and a limitation depending on
the context of use. Weak spots of perpendicular fibres can be used for
natural hinges and connections, but can also lead to material failure
when production processes fail to properly orient the fibres parallel to
expected forces. When forces are exerted perpendicular to the
orientation of fibres the strength and elasticity of the polymer is less
than the matrix alone. In cast resin components made of glass
reinforced polymers such as UP and EP, the orientation of fibres can be
oriented in two-dimensional and three-dimensional weaves. This means
that when forces are possibly perpendicular to one orientation, they are
parallel to another orientation; this eliminates the potential for weak
spots in the polymer.
3.3.2. Failure modes
Structural failure can occur in FRP materials when:
- Tensile forces stretch the matrix more than the fibres, causing the material to shear at the interface between matrix and fibres.
- Tensile forces near the end of the fibres exceed the tolerances of the matrix, separating the fibres from the matrix.
- Tensile forces can also exceed the tolerances of the fibres causing the fibres themselves to fracture leading to material failure [29].
3.3.3. Material requirements
The
matrix must also meet certain requirements in order to first be
suitable for the FRP process and ensure a successful reinforcement of
it. The matrix must be able to properly saturate, and bond with the
fibres within a suitable curing period. The matrix should preferably
bond chemically with the fibre reinforcement for maximum adhesion. The
matrix must also completely envelope the fibres to protect them from
cuts and notches that would reduce their strength, and to transfer
forces to the fibres. The fibres must also be kept separate from each
other so that if failure occurs it is localized as much as possible, and
if failure occurs the matrix must also debond from the fibre for
similar reasons. Finally the matrix should be of a plastic that remains
chemically and physically stable during and after reinforcement and
molding processes. To be suitable for reinforcement material fibre
additives must increase the tensile strength and modulus of elasticity
of the matrix and meet the following conditions; fibres must exceed
critical fibre content; the strength and rigidity of fibres itself must
exceed the strength and rigidity of the matrix alone; and there must be
optimum bonding between fibres and matrix.
3.4. Glass fibre material
FRPs
use textile glass fibres; textile fibres are different from other forms
of glass fibres used for insulating applications. Textile glass fibres
begin as varying combinations of SiO2, Al2O3, B2O3,
CaO, or MgO in powder form. These mixtures are then heated through a
direct melt process to temperatures around 1300 degrees Celsius, after
which dies are used to extrude filaments of glass fibre in diameter
ranging from 9 to 17 μm. These filaments are then wound into larger
threads and spun onto bobbins for transportation and further processing.
Glass fibre is by far the most popular means to reinforce plastic and
thus enjoys a wealth of production processes, some of which are
applicable to aramid and carbon fibres as well owing to their shared
fibrous qualities. Roving is a process where filaments are spun into
larger diameter threads. These threads are then commonly used for woven
reinforcing glass fabrics and mats, and in spray applications. Fibre
fabrics are web-form fabric reinforcing material that has both warped
and weft directions. Fibre mats are web-form non-woven mats of glass
fibres. Mats are manufactured in cut dimensions with chopped fibres, or
in continuous mats using continuous fibres. Chopped fibre glass is used
in processes where lengths of glass threads are cut between 3 and 26 mm,
threads are then used in plastics most commonly intended for moulding
processes. Glass fibre short strands are short 0.2–0.3 mm strands of
glass fibres that are used to reinforce thermoplastics most commonly for
injection moulding.
3.5. Aramid fibre material process
Aramid
fibres are most commonly known Kevlar, Nomex and Technora. Aramids are
generally prepared by the reaction between an amine group and a
carboxylic acid halide group (aramid); commonly this occurs when an
aromatic polyamide is spun from a liquid concentration of sulfuric acid
into a crystallized fibre. Fibres are then spun into larger threads in
order to weave into large ropes or woven fabrics (Aramid) [29].
Aramid fibres are manufactured with varying grades to base on varying
qualities for strength and rigidity, so that the material can be
somewhat tailored to specific design needs concerns, such as cutting the
tough material during manufacture.
3.6. FRP, applications
Fibre-reinforced
plastics are best suited for any design program that demands weight
savings, precision engineering, finite tolerances, and the
simplification of parts in both production and operation. A molded
polymer artifact is cheaper, faster, and easier to manufacture than cast
aluminum or steel artifact, and maintains similar and sometimes better
tolerances and material strengths. The Mitsubishi Lancer Evolution IV
also used FRP for its spoiler material [30-32].
3.6.1. Carbon fibre reinforced polymers
Rudder of commercial airplane
- Advantages over a traditional rudder made from sheet aluminum are:
- 25% reduction in weight
- 95% reduction in components by combining parts and forms into simpler molded parts.
- Overall reduction in production and operational costs, economy of parts results in lower production costs and the weight savings create fuel savings that lower the operational costs of flying the airplane.
3.6.2. Structural applications of FRP
FRP
can be applied to strengthen the beams, columns and slabs in buildings.
It is possible to increase strength of these structural members even
after these have been severely damaged due to loading conditions. For
strengthening beams, two techniques are adopted. First one is to paste
FRP plates to the bottom (generally the tension face) of a beam. This
increases the strength of beam, deflection capacity of beam and
stiffness (load required to make unit deflection). Alternatively, FRP
strips can be pasted in 'U' shape around the sides and bottom of a beam,
resulting in higher shear resistance. Columns in building can be
wrapped with FRP for achieving higher strength. This is called wrapping
of columns. The technique works by restraining the lateral expansion of
the column. Slabs may be strengthened by pasting FRP strips at their
bottom (tension face). This will result in better performance, since the
tensile resistance of slabs is supplemented by the tensile strength of
FRP. In the case of beams and slabs, the effectiveness of FRP
strengthening depends on the performance of the resin chosen for bonding
[32].
3.6.3. Glass fibre reinforced polymers
Engine intake manifolds are made from glass fibre reinforced PA 66.
- Advantages this has over cast aluminum manifolds are:
- Up to a 60% reduction in weight
- Improved surface quality and aerodynamics
- Reduction in components by combining parts and forms into simpler molded shapes. Automotive gas and clutch pedals made from glass fibre reinforced PA 66 (DWP 12-13)
- Advantages over stamped aluminum are:
- Pedals can be molded as single units combining both pedals and mechanical linkages simplifying the production and operation of the design.
- Fibres can be oriented to reinforce against specific stresses, increasing the durability and safety.
3.6.4. Design considerations
FRP
is used in designs that require a measure of strength or modulus of
elasticity those non-reinforced plastics and other material choices are
either ill suited for mechanically or economically. This means that the
primary design consideration for using FRP is to ensure that the
material is used economically and in a manner that takes advantage of
its structural enhancements specifically. This is however not always the
case, the orientation of fibres also creates a material weakness
perpendicular to the fibres. Thus the use of fibre reinforcement and
their orientation affects the strength, rigidity, and elasticity of a
final form and hence the operation of the final product itself.
Orienting the direction of fibres either, unidirectional,
2-dimensionally, or 3-dimensionally during production affects the degree
of strength, flexibility, and elasticity of the final product. Fibres
oriented in the direction of forces display greater resistance to
distortion from these forces and vice versa, thus areas of a product
that must withstand forces will be reinforced with fibres in the same
direction, and areas that require flexibility, such as natural hinges,
will use fibres in a perpendicular direction to forces. Using more
dimensions avoids this either or scenario and creates objects that seek
to avoid any specific weak points due to the unidirectional orientation
of fibres. The properties of strength, flexibility and elasticity can
also be magnified or diminished through the geometric shape and design
of the final product. These include such design consideration such as
ensuring proper wall thickness and creating multifunctional geometric
shapes that can be molding as single pieces, creating shapes that have
more material and structural integrity by reducing joints, connections,
and hardware [30].
3.6.5. Disposal and recycling concerns
As
a subset of plastic FR plastics are liable to a number of the issues
and concerns in plastic waste disposal and recycling. Plastics pose a
particular challenge in recycling processes because they are derived
from polymers and monomers that often cannot be separated and returned
to their virgin states, for this reason not all plastics can be recycled
for re-use, in fact some estimates claim only 20% to 30% of plastics
can be material recycled at all. Fibre reinforced plastics and their
matrices share these disposal and environmental concerns. In addition to
these concerns, the fact that the fibres themselves are difficult to
remove from the matrix and preserve for re-use means FRP amplify these
challenges. FRP are inherently difficult to separate into base a
material that is into fibre and matrix, and the Fibre-reinforced plastic
matrix into separate usable plastic, polymers, and monomers. These are
all concerns for environmentally informed design today, but plastics
often offer savings in energy and economic savings in comparison to
other materials, also with the advent of new more environmentally
friendly matrices such as bioplastics and UV-degradable plastics, FRP
will similarly gain environmental sensitivity [29].
4. Mechanical properties measurements
4.1. Strength
Strength
is a mechanical property that you should be able to relate to, but you
might not know exactly what we mean by the word "strong" when are
talking about polymers. First, there is more than one kind of strength.
There is tensile strength. A polymer has tensile strength if it is
strong when one pulls on it. Tensile strength is important for a
material that is going to be stretched or under tension. Fibers need
good tensile strength.
Then there is compressional
strength. A polymer sample has compressional strength if it is strong
when one tries to compress it. Concrete is an example of a material with
good compressional strength. Anything that has to support weight from
underneath has to have good compressional strength [32]. There is also flexural strength. A polymer sample has flexural strength if it is strong when one tries to bend it.
There
are other kinds of strength we could talk about. A sample torsional
strength if it is strong when one tries to twist it. Then there is
impact strength. A sample has impact strength if it is strong when one
hits it sharply and suddenly, as with a hammer.
To
measure the tensile strength of a polymer sample, we take the sample and
we try to stretch. We usually stretch it with a machine for these
studies. This machine simply has clamps on each end of the sample, then,
when you turn it on it stretches the sample. While it is stretching the
sample, it measures the amount of force (F) that it is exerting. When
we know the force being exerted on the sample, we then divide that
number by the cross-sectional area (A) of our sample. The answer is the
stress that our sample is experiencing. Then, using our machine, we
continue to increase the amount of force, and stress naturally, on the
sample until it breaks. The stress needed to break the sample is the
tensile strength of the material. Likewise, one can imagine similar
tests for compressional or flexural strength. In all cases, the strength
is the stress needed to break the sample. Since tensile stress is the
force placed on the sample divided by the cross-sectional area of the
sample, tensile stress, and tensile strength as well, are both measured
in units of force divided by units of area, usually N/cm2. Stress and
strength can also be measured in megapascals (MPa) or gigapascals (GPa).
It is easy to convert between the different units, because 1 MPa = 100
N/cm2, 1 GPa = 100,000 N/cm2, and of course 1 GPa =
1,000 MPa. Other times, stress and strength are measured in the old
English units of pounds per square inch, or psi. If you ever have to
convert psi to N/cm2, the conversion factor is 1 N/cm2 = 1.45 psi.
4.2. Elongation
But
there is more to understanding a polymer's mechanical properties than
merely knowing how strong it is. All strength tells us is how much
stress is needed to break something. It doesn't tell us anything about
what happens to our sample while we're trying to break it. That's where
it pays to study the elongation behavior of a polymer sample. Elongation
is a type of deformation. Deformation is simply a change in shape that
anything undergoes under stress. When we're talking about tensile
stress, the sample deforms by stretching, becoming longer. We call this
elongation, of course. Usually we talk about percent elongation, which
is just the length the polymer sample is after it is stretched (L),
divided by the original length of the sample (L0), and then multiplied by 100.
There
are a number of things we measure related to elongation. Which is most
important depends on the type of material one is studying. Two important
things we measure are ultimate elongation and elastic elongation.
Ultimate elongation is important for any kind of material. It is nothing
more than the amount you can stretch the sample before it breaks.
Elastic elongation is the percent elongation you can reach without
permanently deforming your sample. That is, how much can you stretch it,
and still have the sample snap back to its original length once you
release the stress on it. This is important if your material is an
elastomer. Elastomers have to be able to stretch a long distance and
still bounce back. Most of them can stretch from 500 to 1000 %
elongation and return to their original lengths without any trouble [32].
4.3. Modulus
In
the elastomers are need show the high elastic elongation. But for some
other types of materials, like plastics, it usually they not stretch or
deform so easily. If we want to know how well a material resists
deformation, we measure something called modulus. To measure tensile
modulus, we do the same thing as we did to measure strength and ultimate
elongation. This time we measure the stress we're exerting on the
material, just like we did when we were measuring tensile strength.
First, is slowly increasing the amount of stress, and then we measure
the elongation the sample undergoes at each stress level. We keep doing
this until the sample breaks. This plot is called a stress-strain curve.
(Strain is any kind of deformation, including elongation. Elongation is
the word we use if we're talking specifically about tensile strain.)
The height of the curve when the sample breaks is the tensile strength,
of course, and the tensile modulus is the slope of this plot. If the
slope is steep, the sample has a high tensile modulus, which means it
resists deformation. If the slope is gentle, then the sample has a low
tensile modulus, which means it is easily deformed. There are times when
the stress-strain curve is not nice and straight, like we saw above.
The slope isn't constant as stress increases. The slope, that is the
modulus, is changing with stress. In a case like this we usually, the
initial slope change as the modulus change [32].
In
general, fibers have the highest tensile moduli, and elastomers have
the lowest, and plastics have tensile moduli somewhere in between fibers
and elastomers.
Modulus is measured by calculating
stress and dividing by elongation, and would be measured in units of
stress divided by units of elongation. But since elongation is
dimensionless, it has no units by which we can divide. So modulus is
expressed in the same units as strength, such as N/cm2.
Intrinsic
deformation is defined as the materials’ true stress-strain response
during homogeneous deformation. Since generally strain localization
phenomena occur (like necking, shear banding, crazing and cracking), the
measurement of the intrinsic materials’ response requires a special
experimental set-up, such as a video-controlled tensile or a uniaxial
compression test. Although details of the intrinsic response differ per
material, a general representation of the intrinsic deformation of
polymers can be recognized [33], see Figure 1.
4.4. Toughness
That
plot of stress versus strain can give us another very valuable piece of
information. If one measures the area underneath the stress-strain
curve (figure 2), colored red in the graph below, the number you get is something we call toughness.
Toughness
is really a measure of the energy a sample can absorb before it breaks.
Think about it, if the height of the triangle in the plot is strength,
and the base of the triangle is strain, then the area is proportional to
strength strain. Since strength is proportional to the force needed to
break the sample, and strain is measured in units of distance (the
distance the sample is stretched), then strength strain is proportional
is force times distance, and as we remember from physics, force times
distance is energy.
From a physics point of view the
strength, is that strength tells how much force is needed to break a
sample, and toughness tells how much energy is needed to break a sample.
But that does not really tell you what the practical differences are.
What is important knows that just because a material is strong, it isn't
necessarily going to be tough as well [34-35].
The gray plot is the stress-strain curve for a sample that is strong, but not tough (figure 3).
As you can see, it takes a lot of force to break this sample. Likewise,
this sample ca not stretch very much before it breaks. A material like
this which is strong, but can not deform very much before it breaks is
called brittle [36].
The
gray plot is a stress-strain curve for a sample that is both strong and
tough. This material is not as strong as the sample in the gray plot,
but the area underneath its curve is a lot larger than the area under
the gray sample's curve. So it can absorb a lot more energy than the
gray-black sample plot.
The gray-black sample elongates
a lot more before breaking than the gray sample does. You see,
deformation allows a sample to dissipate energy. If a sample can't
deform, the energy won't be dissipated, and will cause the sample to
break [37].
In
real life, we usually want materials to be tough and strong. Ideally,
it would be nice to have a material that would not bend or break, but
this is the real world. The gray-black sample has a much higher modulus
than the red sample. While it is good for materials in a lot of
applications to have high moduli and resist deformation, in the real
world it is a lot better for a material to bend than to break, and if
bending, stretching or deforming in some other way prevents the material
from breaking, all the better. So when we design new polymers, or new
composites, we often sacrifice a little bit of strength in order to make
the material tougher.
4.5. Mechanical properties of real polymers
The
rigid plastics such as polystyrene, poly(methyl methacrylate or
polycarbonate can withstand a good deal of stress, but they won't
withstand much elongation before breaking. There is not much area under
the stress-strain curve at all. So we say that materials like this are
strong, but not very tough. Also, the slope of the plot is very steep,
which means that it takes a lot of force to deform a rigid plastic. So
it is easy to see that rigid plastics have high moduli. In short, rigid
plastics tend to be strong, at resist deformation, but they tend not to
be very tough, that is, they are brittle.
Flexible
plastics like polyethylene and polypropylene are different from rigid
plastics in that they don not resist deformation as well, but they tend
not to break. The ability to deform is what keeps them from breaking.
Initial modulus is high, that is it will resist deformation for awhile,
but if enough stress is put on a flexible plastic, it will eventually
deform. If you try to stretch it a plastic bag, it will be very hard at
first, but once you have stretched it far enough it will give way and
stretch easily. The bottom line is that flexible plastics may not be as
strong as rigid ones, but they are a lot tougher.
It is
possible to alter the stress-strain behavior of a plastic with
additives called plasticizers. A plasticizer is a small molecule that
makes plastics more flexible. For example, without plasticizers,
poly(vinyl chloride), or PVC for short, is a rigid plastic. Rigid
unplasticized PVC is used for water pipes. But with plasticizers, PVC
can be made flexible enough to use to make things like hoses.
Fibers like KevlarTM,
carbon fiber and nylon tend to have stress-strain curves like the
aqua-colored plot in the graph above. Like the rigid plastics, they are
more strong than tough, and do not deform very much under tensile
stress. But when strength is what you need, fibers have plenty of it.
They are much stronger than plastics, even the rigid ones, and some
polymeric fibers, like KevlarTM, carbon fiber and ultra-high molecular weight polyethylene have better tensile strength than steel.
Elastomers
like polyisoprene, polybutadiene and polyisobutylene have completely
different mechanical behavior from the other types of materials. Take a
look at the pink plot in the graph above. Elastomers have very low
moduli. You can see this from the very gentle slope of the pink plot,
but you probably knew this already. You already knew that it is easy to
stretch or bend a piece of rubber [34]. If elastomers did not have low moduli, they would not be very good elastomers.
But
it takes more than just low modulus to make a polymer an elastomer.
Being easily stretched is not much use unless the material can bounce
back to its original size and shape once the stress is released. Rubber
bands would be useless if they just stretched and did not bounce back.
Of course, elastomers do bounce back, and that is what makes them so
amazing. They have not just high elongation, but high reversible
elongation.
4.6. Tensile properties
The
discussion of which types of polymers have which mechanical properties
has focused mostly on tensile properties. When we look at other
properties, like compressional properties or flexural properties things
can be completely different. For example, fibers have very high tensile
strength and good flexural strength as well, but they usually have
terrible compressional strength. They also only have good tensile
strength in the direction of the fibers.
Some polymers
are tough, while others are strong, and how one often has to make
trade-offs when designing new materials; the design may have to
sacrifice strength for toughness, but sometimes we can combine two
polymers with different properties to get a new material with some of
the properties of both. There are three main ways of doing this, and
they are copolymerization, blending, and making composite materials.
The
copolymer that combines the properties of two materials is spandex. It
is a copolymer containing blocks of elastomeric polyoxyethylene and
blocks of a rigid fiber-forming polyurethane. The result is a fiber that
stretches. Spandex is used to make stretchy clothing like bicycle
pants.
High-impact polystyrene, or HIPS for short, is
an immiscible blend that combines the properties of two polymers,
styrene and polybutadiene. Polystyrene is a rigid plastic. When mixed
with polybutadiene, an elastomer, it forms a phase-separated mixture
which has the strength of polystyrene along with toughness supplied by
the polybutadiene. For this reason, HIPS is far less brittle than
regular polystyrene [38].
In
the case of a composite material, we are usually using a fiber to
reinforce a thermoset. Thermosets are crosslinked materials whose
stress-strain behavior is often similar to plastics. The fiber increases
the tensile strength of the composite, while the thermoset gives it
compressional strength and toughness.
5. Conclusions
This
brief review of FRP has summarized the very broad range of unusual
functionalities that these products bring (Polymers, Aramids,
Composites, Carbon FRP, and Glass-FRP). While the chemistry plays an
important role in defining the scope of applications for which these
materials are suited, it is equally important that the final parts are
designed to maximize the value of the inherent properties of these
materials. Clearly exemplify the constant trade-off between
functionality and processability that is an ongoing challenge with these
advanced materials. The functionality that allows these materials to
perform under extreme conditions has to be balanced against
processability that allows them to be economically shaped into useful
forms. The ability of a polymer material to deform is determined by the
mobility of its molecules, characterized by specific molecular motions
and relaxation mechanisms, which are accelerated by temperature and
stress. Since these relaxation mechanisms are material specific and
depend on the molecular structure, they are used here to establish the
desired link with the intrinsic deformation behavior.
Martin Alberto Masuelli (2013). Introduction of Fibre-Reinforced Polymers − Polymers and Composites: Concepts, Properties and Processes, Fiber Reinforced Polymers - The Technology Applied for Concrete Repair, Dr. Martin Masuelli (Ed.), ISBN: 978-953-51-0938-9, InTech, DOI: 10.5772/54629. Available from: http://www.intechopen.com/books/fiber-reinforced-polymers-the-technology-applied-for-concrete-repair/introduction-of-fibre-reinforced-polymers-polymers-and-composites-concepts-properties-and-processes