Abstract
Composite
materials are continuously gaining more importance in the field of engineering.
In this paper we have focused mainly on natural fiber reinforced polymer
composite materials. This natural fiber composite are having some special
advantages such as high strength to weight ratio and stiffness. These fiber
composites are also claimed to offer environmental advantages such as lower
pollutant emission and replaces metals because of their high strength-to-weight
ratio and stiffness properties. This work concentrate on fiber extracted from
banyan tree (Natural fiber) as a reinforcement for the Polyester matrix. These
banyan fibers have some added advantage such as low cost, lesser weight and no
medical application. The most important advantage of this fiber is that the
wasted fiber can be used effectively (recycling).
Tensile
strength of the Banyan Fiber Reinforced Composite is studied. Specimens are
prepared as per ASTM Standards. Computer assisted UTM is used for testing the
Tensile Strength of the prepared composite structure. Fabrication of the pure
and hybrid composite is done by simple hand lay-up method. The Banyan short
fiber reinforced composites shown a better performance when it is hybrid with
the E-Glass fiber. The performance of
the prepared composite is also studied in moisture environment.
Introduction
Composite material is not a newly developed
field mankind knows it since several hundred years before Christ and applied
innovation to improve the quality of life. Although it is not clear has to how
man understood the fact that mud brick make sturdier houses if lined with
straw, he used them to make building that lasted. Ancient pharaohs made their
slaves use bricks with straw to enhance the structural integrity of their
buildings, some of which testify to wisdom of the dead civilization even today.
Contemporary composite results from research
and innovation from past few decades have progressed from glass fiber for
automobile bodies to particulate composites for aerospace and range other
applications. Fiberglass, developed in the late 1940s, was the first modern
composite and is still the most common. It makes up about 65 percent of all
composites produced today. More recently, fiber reinforced resin composites
that have high strength to weight and stiffness-to-weight ratios have become
important in weight sensitive application such as aircraft and space vehicles.
This kind of fiber or particle embedded in the matrix of another material would
be the best example of modern-day composite materials, which are more
structural.
Composite Theory
In its most basic form a composite material
is one, which is composed of at least two elements working together to produce
material properties that are different to the properties of those elements on
their own. In practice, most composites consist of a bulk material (the
‘matrix’), and a reinforcement of some kind, added primarily to increase the strength and
stiffness of the matrix. This reinforcement is usually in fiber form. Today,
the most common man-made composites can be divided into three main groups:
Polymer Matrix
Composites (PMC’s) – These are the most common and will be discussed here. Also
known as FRP - Fiber Reinforced Polymers (or Plastics) – these materials use a
polymer-based resin as the matrix, and a variety of fibers such as glass,
carbon and aramid as the reinforcement.
Metal Matrix Composites (MMC’s) -
Increasingly found in the automotive industry, these materials use a metal such
as aluminium as the matrix, and reinforce it with fibers such as silicon
carbide.
Ceramic
Matrix Composites (CMC’s) - Used in very high temperature environments, these
materials use a ceramic as the matrix and reinforce it with short fibers, or
whiskers such as those made from silicon carbide and boron nitride.
Composite
Material
Ironically, despite the growing familiarity
with composite material and ever-increasing range of application, the term
defines a clear definition. Loose terms like “material composed of two or more
distinctly identifiable constituents” are used to describe natural composites
like timber, organic materials, like tissue surrounding the skeletal system,
soil aggregates, mineral and rock. The properties that can be improved by
forming a composite material include strength, stiffness, less weight and
corrosion resistance.
Fiber
Reinforced Composites
Fibers are the important class of
reinforcement, as they satisfy the desired conditions and transfer strength to
the matrix constituent influencing and enhancing their properties as
desired. The orientation of the fiber in
the matrix is an indication of the strength of the composite and the strength
is greatest along the longitudinal directional of fiber. This doesn’t mean the
longitudinal fiber can take the same quantum of load irrespective of the
direction in which
it
is applied. Optimum performance from longitudinal fibers can be obtained if the
load is applied along its direction. The slightest shift in the angle of
loading may drastically reduce the strength of the composite.
Long
fibers in various forms are inherited much stiffer and stronger than the same
material in bulk form. For example, ordinary plate glass fractures at stresses
of only few thousand pounds per square inch, yet glass fibers have strength of
400,000 to 700,000 psi in commercially available forms and about 1,000,000 psi
in laboratory prepared forms obviously then, the geometry of a fiber is somehow
crucial to the evaluation of its strength and must be considered in structural
applications.
Banyan
and Glass Fiber Composites
Our paper deals with Banyan and Glass Fiber
composites. It is one of the natural fiber polymer reinforced composites.
Banyan and Glass are used as reinforcement and the polymer-based resin is used
as a matrix. These fibers are been chosen because of their low weight, easily
available, waste can be used effectively, no medical application.
Polymer Matrix Composites
Resin systems
such as epoxies and polyesters have limited use for the manufacture of
structures on their own, since their mechanical properties are not very high
when compared to, for example, most metals. However, they have desirable
properties, most notably their ability to be easily formed into complex shapes.
Materials such as glass, aramid and boron have extremely high tensile and
compressive strength but in ‘solid form’ these properties are not readily
apparent. This is due to the fact that when stressed, random surface flaws will
cause each material to crack and fail well below its theoretical ‘breaking
point’. To overcome this problem, the material is produced in fiber form, so
that, although the same number of random flaws will occur, they will be
restricted to a small number of fibers with the remainder exhibiting the
material’s theoretical strength. Therefore a bundle of fibers will reflect more
accurately the optimum performance of the material. However, fibers alone can
only exhibit tensile properties along the fiber’s length, in the same way as
fibers in a rope.
It is when the resin systems are combined
with reinforcing fibers such as glass, carbon and aramid those exceptional
properties can be obtained. The resin matrix spreads the load applied to the
composite between each of the individual fibers and also protects the fibers
from damage caused by abrasion and impact. High strengths and stiffness, ease
of moulding complex shapes, high environmental resistance all coupled with low
densities, make the resultant composite superior to metals for many
applications. Since PMC’s combine a resin system and reinforcing fibers, the
properties of the resulting composite material will combine something of the
properties of the resin on its own with that of the fibers on their own.
Fabrication
Procedure
Fabrication of Composite Material
The
materials used to prepare the Banyan Fiber and Hybrid Glass-Banyan composite
are,
General Purpose Resin (G.P. Resin Chemically polyester).
Accelerator (Methyl Ethyl Ketone).
Catalyst (Cobalt).
Poly vinyl.
Polythene Sheets & Glass Plates.
Banyan and Glass fiber.
Overall, the properties of the composite
are determined by:
The properties of the fiber
The properties of the resin
The ratio of fiber to resin in the composite (Fiber Volume Fraction
(FVF))
The geometry and orientation of the fibers in the composite
The ratio of the fiber to resin derives
largely from the manufacturing process used to combine resin with fiber.
However, it is also influenced by the type of resin system used, and the form
in which the fibers are incorporated. In general, since the mechanical
properties of fibers are much higher than those of resins, the higher the fiber
volume fraction the higher will be the mechanical properties of the resultant
composite. In practice there are limits to this, since the fibers need to be
fully coated in resin to be effective, and there will be an optimum packing of
the generally circular cross-section fibers. In addition, the manufacturing
process used to combine fiber with resin leads to varying amounts of
imperfections and air inclusions.
Typically, with a common hand lay-up process as widely
used in the boat-building industry, a limit for FVF is approximately 30-40%.
With the higher quality, more sophisticated and precise processes used in the
aerospace industry, FVF’s approaching 70% can be successfully obtained. The
geometry of the fibers in a composite is also important since fibers have their
highest mechanical properties along their lengths, rather than across their widths.
This leads to the highly anisotropy properties of composites, where, unlike
metals, the mechanical properties of the composite are likely to be very
different when tested in different directions. This means that it is very
important when considering the use of composites to understand at the design
stage, both the magnitude and the direction of the applied loads. When
correctly accounted for, these anisotropy properties can be very advantageous
since it is only necessary to put material where loads will be applied, and
thus redundant material is avoided. It is also important to note that with
metals the material supplier largely determines the properties of the
materials, and the person who fabricates the materials into a finished
structure can do almost nothing to change those ‘in-built’ properties. However,
a composite material is formed at the same time, as the structure is itself
being fabricated. This means that the person who is making the structure is
creating the properties of the resultant composite material, and so the
manufacturing processes they use have an unusually critical part to play in
determining the performance of the resultant structure.
Fabrication Using Hand-layup method
The hand lay-up or wet lay-up method is one
of the oldest and most commonly used methods for manufacturing of composite
parts. Hand lay-up composites are a case of continuous fiber reinforced
composites. Resin is impregnated by hand in to fiber, which are in the form of
woven, knitted, stitched or bonded fabrics this is usually accomplished by
rollers or brushes.
The
fiber reinforced resin matrix composite material is fabricated as follows, Fibers
are prepared for the required size of 5 mm length. 30g of fiber is taken in a
container and it is gradually mixed with 150ml of resin in beaker. Then
accelerator about 2.5% of volume of resin is added to it and stirred well.
Then catalyst about 1.5% volume of resin is
added to it and stirred well. Then the mixture is transferred to mould setup.
Now the mould is left for 24 hours for setting. After dying we can obtain the
required composite.The various types of fibers in the fabrication process are
Banyan. Banyan and Glass.
Result and Discussion
Tensile Test
Tensile test is done by Universal Testing Machine. Tensile test is done
by applying tensile load on the specimen. We have carried out our studies on
the specimen with and without application of moisture.
Tensile Test without Moisture
Test is done on a specimen with a size of
24cm x 3cm x 0.3cm. The specimen is tested in dry condition as we are
performing the test without moisture. When the load is applied above 14.5 KN,
the specimen begins to deform. As the load increases, the deformation begins to
increase.
We have done a comparison of tensile nature
of Banyan and combination of Banyan and Glass fiber.
Load
(KN)
This chart shows the tensile strength of the Banyan and
Banyan-Glass combination For different load conditions.
Tensile Test for Specimen with Moisture
To carry out the tensile test on the
specimen with moisture, then the specimen is immersed in water for one day and
the testing is carried out. This testing is done by UTM (Universal Testing
Machine). During testing the composites begins to deform at the load of 12 KN. As
the load increases the deformation also increases.
We
have also performed the tensile test on specimen with moisture for different
combinations and a sample tensile graph is obtained as shown below.
Load
(KN)
Comparison
Between with and without Moisture
We have done a comparison of tensile nature of various
fibers and their combination in wet and dry condition. Below chart shows the
comparison of specimen for both wet and dry condition.
It is observed
from the graph that Banyan and Glass fiber reinforced resin matrix composite
material have maximum peal load in wet condition and it is about 15.95 KN. Peak
load increases in wet condition when compared with dry condition for Banyan and
Glass combination.
Due to the factors described above, there is a very
large range of mechanical properties that can be achieved with composite
materials. Even when considering one fiber type on its own, the composite properties
can vary by a factor of 10 with the range of fiber contents and orientations
that are commonly achieved. The comparisons that follow therefore show a range
of mechanical properties for the composite materials. The lowest properties for
each material are associated with simple manufacturing processes and material
forms (e.g. spray lay-up glass fiber), and the higher properties are associated
with higher technology manufacture (e.g. autoclave moulding of unidirectional glass fiber prepreg), such
as would be found in the aerospace industry.
Composites
in the aerospace industry
The aerospace industry’s unrelenting quest to enhance the performance
of its products is constantly driving the development of improved structural
materials. EADS companies have always been at the cutting edge of advanced
materials development.
Fiber-based composite materials play an ever-increasing role in the
construction of aircraft, helicopters, missiles, rocket launchers and
satellites. The most common composites used in aerospace are carbon fiber
reinforced plastics (CFRP), a mix of 60 percent carbon fiber and 40 percent
resin. Other types include sandwich and honeycomb structures, fiber/metal
laminates and glass fiber materials, while ceramic carbon fiber composites are
used in high-temperature applications such as rocket motors.
The advantages of composites in aircraft design are their high strength-to-weight ratio, excellent fatigue endurance, corrosion resistance and a malleability that allows tailoring them to meet design requirements. Composites can be more easily formed into complex shapes (such as spheres) than their metallic counterparts. This not only reduces the number of parts making up a given component, but also reduces the need for fasteners and joints – often the weakest points of a structure.
Composite structures do, however, have a few drawbacks. For example, they tend to have higher manufacturing costs than metallic structures. Composites have stiffness and strength properties that may vary with temperature and moisture content and which depend on the thickness of a component. In some circumstances they may also be more sensitive to damage such as hail or bird strikes, not to mention accidental impact by servicing vehicles at airports.
Several different techniques are used in the production of CFRP aircraft parts. The most common method uses rolls of carbon fiber that have been pre-impregnated with resin, which are then cut and shaped as required and built into a series of layers. Pressure is then applied and the part is cured at high temperatures in an autoclave. In another commonly used method, the carbon fiber is shaped in a mould or by using sewing or braiding techniques. The liquid resin is added to this textile pre-form in the next step. This can be done using several processes, some of which involve placing the part in a vacuum and then curing it at room temperature.
A switch from metal to composites can make parts up to 40% lighter. The weight savings, which have a positive effect on both fuel consumption and the aircraft’s payload, are particularly important in a market environment characterized by high fuel
The advantages of composites in aircraft design are their high strength-to-weight ratio, excellent fatigue endurance, corrosion resistance and a malleability that allows tailoring them to meet design requirements. Composites can be more easily formed into complex shapes (such as spheres) than their metallic counterparts. This not only reduces the number of parts making up a given component, but also reduces the need for fasteners and joints – often the weakest points of a structure.
Composite structures do, however, have a few drawbacks. For example, they tend to have higher manufacturing costs than metallic structures. Composites have stiffness and strength properties that may vary with temperature and moisture content and which depend on the thickness of a component. In some circumstances they may also be more sensitive to damage such as hail or bird strikes, not to mention accidental impact by servicing vehicles at airports.
Several different techniques are used in the production of CFRP aircraft parts. The most common method uses rolls of carbon fiber that have been pre-impregnated with resin, which are then cut and shaped as required and built into a series of layers. Pressure is then applied and the part is cured at high temperatures in an autoclave. In another commonly used method, the carbon fiber is shaped in a mould or by using sewing or braiding techniques. The liquid resin is added to this textile pre-form in the next step. This can be done using several processes, some of which involve placing the part in a vacuum and then curing it at room temperature.
A switch from metal to composites can make parts up to 40% lighter. The weight savings, which have a positive effect on both fuel consumption and the aircraft’s payload, are particularly important in a market environment characterized by high fuel
prices and the prospect of ever more stringent aircraft emission
standards. Besides being lighter than traditional materials, composites offer
significant advantages in terms of operational reliability, leading to lower
in-service operating costs.
As already mentioned, however, composite structures have a major drawback in terms of their higher manufacturing costs compared to metallic structures. Consequently, much research continues to be directed at reducing these costs by developing methods that do not require the use of an autoclave and by increasing the automation of manufacturing processes such as automated tape lay-up, robotic fiber placement, resin transfer moulding and resin film infusion.
As already mentioned, however, composite structures have a major drawback in terms of their higher manufacturing costs compared to metallic structures. Consequently, much research continues to be directed at reducing these costs by developing methods that do not require the use of an autoclave and by increasing the automation of manufacturing processes such as automated tape lay-up, robotic fiber placement, resin transfer moulding and resin film infusion.
Conclusion
At present
there are the technical and economic prerequisites for broad use of composite
materials in large-scale machine building industries. Replacement of
traditional metallic materials by composite ones provides a reduction in
material consumption for machine parts of up to 2.5 times with an increase in
their operating life of up to 3 times and decreases the labor requirement for
production by up to 10 times with a reduction in the time for organization of
production of a new part of up to 2.5 times. The reliability of composite
materials parts is 1.5 times greater than of hose of traditional materials. The
unquestionable advantages of composite materials make it possible to
confidently predict a steady broadening of their use in advanced models of
transportation machinery in the very near future.
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