Transcript Materials

Materials
Composites
Introduction
Introduction
• The major problem in the application of
polymers to engineering is their low stiffness
and strength
– Moduli are 100 times lower
– Strengths are 5 times lower
Introduction
• Two methods are used to overcome these
deficiencies
– Use of shape (moment of inertia)
• Ribs
• Gussets
– The addition of reinforcing fibers to form a
composite material
Introduction
• A good reinforcing additive has the following
properties
– It is stiffer and stronger than the polymer matrix
– It has good particle size, shape, and surface
character for effective mechanical coupling to the
matrix
– It preserves the desirable qualities of the polymer
matrix
Introduction
• The best reinforcement in any application is
the one that achieves the designers objective
at the lowest cost
Mechanism of Fiber
Reinforcement
Mechanism of Fiber Reinforcement
• We have a single reinforcing fiber embedded
in a polymer matrix and perfectly bonded to
it.
• The particle is stiffer than the matrix and
deform less, causing the matrix strain to be
reduce overall
– The strain is much less at the interface
Mechanism of Fiber Reinforcement
• The reinforcing fiber achieves its restraining
effect on the matrix entirely through the fibermatrix interface
• The strength of the composite depends on the
strength of bond between fiber and matrix,
and the area of the bond.
Mechanism of Fiber Reinforcement
• A useful parameter for characterizing the
effectiveness of the reinforcement is the ratio
of surface area of the reinforcement to the
volume of reinforcement.
• We want the area to volume ratio to be as
high as possible.
• We define the aspect ratio (a) as the ratio of
length to diameter
Mechanism of Fiber Reinforcement
• The figure on the next slide show a plot of
aspect ratio(a) vs area to volume ratio.
• It show the optimum shapes for a cylindrical
reinforcement to be:
– a>>1, a fiber
– a<<1, a platelet
Mechanism of Fiber Reinforcement
Mechanism of Fiber Reinforcement
• Two main classes of reinforcement are fibers
and platelets.
• Examples of fibers:
– Glass fibers
– Carbon fibers
– Carbon nanotubes
• Examples of platelets
– Mica
– Talc
Forming Reinforced Plastics
Forming Reinforced Plastics
• Reinforced thermoplastics are usually formed
using extrusion or injection molding.
• Alignment of the fibers is caused by drag on
the particle by the flowing viscous polymer.
– Usually aligned in the direction of flow.
– But the flow field varies greatly and we end up
with random fiber alignment.
• The damage done to the fiber must also be
taken into account.
How Molecular Orientation Occurs
Forming Reinforced Plastics
• Thermoset resins can be formed by
compression molding.
• The fiber and resin are premixed before being
loaded into a heated mold which causes the
resin to crosslink.
• Many forms of premix are available, making a
variety of fiber arrangements possible.
Forming Reinforced Plastics
• Many other forming processes:
• Pultrusion
– Continuous fibers are pulled through a bath of
resin, then through a shaping die.
– The resin is then crosslinked.
– Produces a long fiber with uniaxial alignment.
Forming Reinforced Plastics
• Filament winding
– Continuous fibers are pulled through a bath of
resin, then wound onto a driven mandrel.
– Then the resin is crosslinked.
– This method is used for making pipe and other
shapes
Forming Reinforced Plastics
• Pultrusion and Filament winding
Forming Reinforced Plastics
• Hand Layup
– The fiber is laid down by hand in the required
arrangement and shape, then resin is applied with
a brush.
– The resin then crosslinks.
• Hand Spray Layup
– Fibers are fed to a spray gun which chops and
sprays the fibers at a panel where the
reinforcement is needed.
– Resin is then applied with a brush.
– The resin then crosslinks.
Physical Properties
Physical Properties
Physical Properties
• Density
• The density of the composite differs from that
of the polymer
• A mass (m) of composite occupies a volume
(V)
– mf of fibers occupies Vf
– mm of matrix (polymer) occupies Vm
– m = mf + mm
– V = Vf +Vm
Physical Properties
• The proportion of fibers and matrix in the
composite are expressed as fractions of the
total volume they occupy.
f 
vf
v
vm
m 
v
m   f  1
Physical Properties
• The density(ρ) of the composite with no voids
is:
   f   f  (1   f ) * m
Physical Properties
• In practice, composite materials contain voids.
– A void is a source of weakness
• Over 2% voids indicates poor fabrication.
• Less than 0.5% voids indicates “aircraft
quality” fabrication.
Mechanics of Fiber
Reinforcement
Mechanics of Fiber Reinforcement
• Accurately predicting the mechanical properties
of a composite material is not easy
• The differences between properties of the
reinforcing particle and the polymer matrix cause
complex distributions of stress and strain at the
microscopic level, when loads are applied.
• By using simplified assumptions about stress and
strain, reasonably accurate predictions can be
made
Mechanics of Fiber Reinforcement
• Consider the case of the fibers that are so long
that the effects of their ends can be ignored.
Mechanics of Fiber Reinforcement
• The equation for the Composite Modulus (E)
in the 1 direction is:
E1   f * E f  (1   f ) * Em
• The equation for the Composite Modulus (E)
in the 2 direction is:
E2 
E f * Em
(1   f ) * E f   f * Em
Mechanics of Fiber Reinforcement
• Poisson’s ratio (ν), the elastic constant of the
composite in the 1,2 direction is:
12   f *12  (1   f ) *12
f
m
• Poisson’s ratio (ν), the elastic constant of the
composite in the 2,1 direction is:
 21 
 12 * E2
E1
Mechanics of Fiber Reinforcement
• When a shear stress acts parallel to the fibers,
the composite deforms as if the fibers and
matrix are coupled is series.
• The shear Modulus (G12) is:
G12 
G f * Gm
(1   f ) * G f   f * Gm