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Impact Properties of Polymeric Solids

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Unlike cracks, crazes can bear a substantial load ... Craze-fibril diameters range from 0.6 nm to 30 nm for those generated far below Tg. ... – PowerPoint PPT presentation

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Title: Impact Properties of Polymeric Solids


1
Impact Properties of Polymeric Solids
  • Impact resistance is a measure of a materials
    ability to withstand a sudden applied load
    without failure.
  • Impact resistance test results are difficult to
    interpret, given its dependence on the frequency
    of the applied load, the sample geometry and its
    sensitivity to sample imperfections.
  • Designing for impact resistance is therefore a
    difficult task, requiring the engineer to
    understand the strengths and limitations of
    various test methods, the different types of
    polymer material failure (brittle, ductile, etc)
    and the mechanisms by which these materials
    dissipate
  • inputted energy.

2
High-Speed Static Tensile Testing
  • True stress-vs-true strain behavior of polymers
    (taking necking into account) measured at high
    strain rate (typically 100 s-1).
  • Note differences in yielding behaviour
  • Delrin is an acetal resin
  • Lexan a polycarbonate
  • Teflon TFE is the
  • tetrafluoroethylene
  • homopolymer
  • Teflon FEP is a copolymer
  • of tetrafluoroethylene and
  • hexafluoropropylene

3
Instrumented Falling Dart Impact Testing
  • Brittle Failure
  • Ductile Failure

4
Energy Dissipation - Molecular Relaxation
  • Storage modulus E1 and loss modulus E2 as a
    function of temperature at 138 Hz for
    poly(ethylene terephthalate) specimens of
    differing degrees of crystallinity 5 34 and
    50.

5
Energy Dissipation - Shear Yielding
  • Shear yielding is a mode of material failure
    wherein the plane of failure is 45 relative to
    the applied stress.
  • Where energy dissipation is concerned, yielding
    refers to ductile behaviour wherein the material
    deforms under the applied load.
  • Shown right are
  • instrumented dart
  • impact testing data
  • for a material at two
  • temperatures.
  • Note the differences
  • in the extent of
  • ductile behaviour.

6
Energy Dissipation - Crazing
  • Glassy sections of a polymeric material can
    respond to tension by generating crazes normal to
    the direction of the applied force (without
    lateral contraction).
  • Crazes are not cracks, but regions of low polymer
    density made of polymer microfibrils with a void
    fraction comprised of the fluid environment
    (air).
  • Unlike cracks, crazes can bear a substantial load
  • Shown here is crazing in a polycarbonate dogbone
    and an electron micrograph of a craze tip.

Crazing involves the creation of new surfaces,
and therefore is an important mode of impact
energy dissipation.
7
Energy Dissipation - Crazing
  • Craze-fibril diameters range from 0.6 nm to 30 nm
    for those generated far below Tg.
  • Strain hardening (increased resistance to
    drawing) is a key factor in stabilizing the
    microstructure, as polymer chain alignment
    increases with increased deformation.
  • Shown here is a cyclic stress-
  • strain curve for crazing
  • bisphenol-A polycarbonate
  • Note that the elastic modulus of
  • the craze is low (25 of the bulk
  • resin) due to its low volume fraction
  • of polymer, but large elongation
  • aligns microfibrils, thereby raising
  • the material strength to approach
  • its high value.

8
Failure Modes and Stress Whitening
  • Tensile rupture of polyethylene
  • (a) brittle fracture at low temperatures (T lt 95
    K)
  • (b) necking and rupture (T 100-240 K)
  • (c) non-necking ductile fracture of slowly cooled
    low molecular
  • weight material (T90-300 K)
  • (d) necking and drawing (T gt 0 C).

9
Rubber Toughening
  • Brittle plastics such as polystyrene
  • can be toughened through
  • careful blending to create
  • dispersed elastomeric domains.
  • Interfacial adhesion is required
  • to transmit forces to the
  • rubbery phase, thereby
  • generating the desired impact
  • resistance.
  • Shown above is an electron micrograph of crazed
    high-impact polystyrene (HIPS), which is a blend
    of polystyrene, polybutadiene and
    poly(styrene-graft-butadiene).
  • Recall that polymer solubility is very limited,
    creating phase-separated blends in most
    commercial applications.
  • Large-scale crazing of the material initiates at
    the stress concentrations established by the
    rubbery phase, thereby improving impact
    resistance.

10
Rubber Toughening - Crazing
  • Typical uniaxial tensile stress-strain behavior
    of polystyrene (PS), medium-impact PS (MIPS),
    high-impact PS (HIPS), and poly(acrylonitrile-co-s
    tyrene-graft-butadiene) ABS.

11
Fibre Reinforced Polymer Composites
  • The engineering definition of a composite is
    restricted to materials formed by alignment of
    strong, stiff fibres in a polymer matrix.
  • Advanced composites employ continuous fibres
  • Generic composites use chopped fibre
  • In advanced composites, the polymer serves as a
    binder
  • that aligns fibres in a manner that allows them
    to bear much of the
  • applied load.
  • This differs from chopped fibre reinforced
    plastics, where mechanical properties are
    dictated by both matrix and reinforcing fibre.

12
Reinforcing Fibres
  • E-Glass Cloth has been available since the 1940s
    and is still the most widely used and the most
    economical composite reinforcement. It is made
    from strands of continuous glass filaments plied
    and twisted into yarn. It is chrome finished
    (Volan A) and is suitable for use with all
    polyester, vinyl-ester, and epoxy resins.
  • S-2 Glass Cloth was developed by Owens Corning
    for military missile applications. Compared to
    E-Glass, S-2 Glass has much greater tensile
    strength, flexural strength, flexural modulus,
    and compressive strength. S-2 Glass laminates
    also exhibit improved impact resistance,
    toughness, a high-service temperature, and
    reduced weight. Often used for high-performance
    surf and sail boards.
  • Carbon fiber, also referred to as graphite fiber,
    is one of the strongest and stiffest
    reinforcements available. When properly
    engineered, carbon fiber advanced composites can
    achieve the strength and stiffness of metal parts
    at significant weight savings. In addition to
    the high strength-to-weight and
    stiffness-to-weight ratios, carbon fibers are
    thermally and electrically conductive, have low
    thermal expansion coefficients, and have
    excellent fatigue resistance.
  • Kevlar 49, a high modulus fabric, is an aramid
    fibre designed for plastic reinforcements. It
    displays excellent stability over a wide range of
    temperatures for prolonged periods. Even at a
    temperature as low as -320F (-196C) Kevlar
    shows essentially no brittleness or strength
    loss. Excellent dimensional stability and fatigue
    resistance. It, also, has resistance to chemicals
    and moisture.

13
Reinforcing Fibres
14
Reinforcing Fibres
15
Coupling Agents
  • Where interfacial adhesion is inadequate,
    coupling agents and/or compatabilizers are used
    to generate cross-domain bonds.
  • Examples include aminosilanes in rubber-silica
    blends and vinyl silanes in unsaturated
    polyester-glass (fibreglass) formulations.
  • Coupling agents function by bonding with both
    phases, thereby generating the adhesion needed
    for stress to be communicated between polymer and
    reinforcing agent.
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