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Properties of Composites Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing Methods

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Page 1: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Properties of CompositesProperties of CompositesDependent on:Constituent phases

Reinforcement Matrix

Relative amounts Interface propertiesGeometry of reinforcementProcessing Methods

Page 2: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Interface There is always an interface between

constituent phases in a composite material

Figure: Interfaces between phases in a composite material: (a) direct bonding between primary and secondary phases

Page 3: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Interphase In some cases, a third ingredient must be added

to achieve bonding of primary and secondary phases, called an interphase.

Interphase can be thought of as an adhesive

Figure : Interfaces between phases: (b) addition of a third ingredient to bond the primary phases and form an interphase

Page 4: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Figure 9.4 ‑ Interfaces and interphases between phases in a composite material: (c) formation of an interphase by solution of the primary and secondary phases at their boundary.

Another InterphaseInterphase consisting of a solution of primary and secondary phases

Page 5: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Definitions

Interface (2D interface) A surface formed by the common boundary of

reinforcing fibre and matrix in contact which constitutes the bond in-between for the transfer of loads

Interphase (3D interface region) Interphase includes the surface of the classical

fibre-matrix contact, as well as the region of finite thickness extending between the fibre and matrix

The chemical, physical and mechanical features vary continuously between the bulk fibre and matrix

Page 6: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Theories of Adhesion Adsorption and wetting

Thermodynamic work of adhesion (physical bond resulting from highly localized intermolecular forces) Wa = SV + LV - SL = LV (1+Cos ) :Young-Duprè

equation SV = SL + LV Cos

> 90: non wetting; < 90: wetting; = 0: spreading The higher the work of adhesion the stronger the

interactions between the liquid and solid phases.

Page 7: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Theories of Adhesion If the liquid does not form a droplet, i.e. ; = 0, it is

termed ‘spreading’ In this case, the equilibrium is expressed by an

inequality: SV -SL = LV

SV > LV

The surface energy of a solid (i.e. reinforcement in composites), SV, must be greater than that of a liquid (i.e. matrix resin), LV, for proper wetting to take place.

Page 8: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Examples If Surface energy of glass fibres is 63 mJ/m2 Surface energy of carbon fibers is 52 mJ/m2

Surface energy of PE fibers is 31 mJ/m2) Surface energy of epoxy is 39 mJ/m2

Surface energy of polyester is 40 mJ/m2

Then Glass fibre and carbon fibre can be readily wetted by epoxy and

polyester resins at room temperature unless the viscosity of the resin is too high.

In contrast, it is difficult to wet PE fibres with epoxy or polyester resins unless the fibers are surface treated.

Page 9: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Wetting in composite processing

Contamination: the effective surface energy is much smaller than the base solid

High viscosity: entrapped air at the solid surface

Shrinkage during curing: displacements at the solid surface.

Page 10: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Fibre Surface Treatments Sizes

Unsized fibres degrade rapidly and cannot be handled for processing.

Sizes are applied as a very thin coating (less than 1 m) to glass and carbon fibres immediately after the fibres are drawn to avoid abrasion.

Functions of Sizes To protect the fibre surface from damage To bind fibres together for ease of processing To lubricate the fibres so that they withstand abrasive tension

during subsequent processing. To impart anti-electrostatic properties. To provide a chemical link between the fibre surface and the

matrix

Page 11: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Typical components of a glass fibre size (after Dow Corning 1985) Film forming resin 1.0 to 5 % Anti-static agent 0.1 to 0.2 % Lubricant 0.1 to 0.2 % Coupling agent 1.0 to 0.5 % Solvent balance

Film former: a polymer, which binds the strand together. It must be compatible with the matrix. Fibre dispersion and wetting may be influenced by choice of film former, which dissolves or melts during downstream processing operations. Polyester, epoxy and PU resins are widely used.

Lubricant: usually a stearate. It reduces damage due to abrasion. Especially important for weaving.

Page 12: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Glass fibres and Coupling Agents Coupling agent, R-SiX3, is a di-functional chemical. One end is

designed to bond to the fibre, and the other to the resin. ( -aminopropyltriethoxysilane (APS), vinyltriethoxysilane (VS))

R=organo-functional group, to react with the resinX=siloxane group, to react with a hydroxy group of the glass surface M=Composition atom from the glass fibre

Page 13: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Two major bonding mechanisms: Chemical reaction between R-groups and functional groups in

the resin Interpenetrating network (IPN): resin is interdiffused into the

chemisorbed silane layers and the silane molecules are migrated into the matrix.

Page 14: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Carbon Fibre Surface Treatment As-manufactured surface of carbon fibre is essentially graphite

with mainly the basal planes exposed. These have low chemical reactivity.

Page 15: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Carbon Fibre Surface Treatment To improve reactivity, surface treatments are necessary, which

can be classified into the following.  1)     Oxidative Treatments

Dry Oxidation: Heating in air, oxygen, ozone or CO2 at elevated temperatures (typically 500C)

Wet Oxidation: Mild oxidation in an electrolyte (e.g. nitric acid, acidic potassium permanganate, sodium hydrochloride, etc.). Effectiveness depends on acid concentration, exposure time, temperature.

2)     Non-oxidative treatments

Whiskerisation: involves a nucleation process and the growth of very thin and high strength single crystals of the chemical compounds (e.g. SiC, TiO2, Si3N4 ) on the fibre surface in a chemical vapour deposition (CVD) process.

Plasma Treatment: etching or deposition can be performed by coupling energy into a high pressure gas (e.g. oxygen, chlorine, floride, Ar)

Page 16: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Effects of Carbon Fibre Surface Treatments To remove loose, weak material from the surface To increase the surface area by producing pits and

rugosities To produce various functional groups on the surface

(e.g. hydroxyl C-OH; carbonyl C=O; carboxyl OH-C=O groups). These groups may form primary or secondary chemical bonds with the resin matrix.

To improve the interface bond strength and thus the interlaminar shear strength (ILSS), flexural and tensile strengths of the composite.

Induces a loss in impact fracture toughness.

Page 17: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Effects of Carbon Fibre Surface Treatments

Whiskerization: SiC whiskers grown on carbon fibre surface after CVD process

Page 18: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing
Page 19: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Interdiffusion A bond between two surfaces may be formed by interdiffusion of

atoms of molecules across the interface (e.g. interpenetrating network, IPN)

Electrostatic attraction A difference in electrostatic charge between constituents at the

interface may constitute to the force of attraction bonding Chemical bonding

A bond is formed between a chemical grouping on the fibre surface and a compatible functional group in the matrix (e.g. coupling agent coated glass fibres and surface treated carbon fibres with polymer reins)

Reaction bonding Reaction occurs in MMCs and CMCs, forming new compounds

at the interface region Reaction involves transfer of atoms from one or both of the

constituent to the reaction site near the interface, and these transfer processes are diffusion controlled

Types of bonding

Page 20: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Mechanical bondMechanical bonds involves solely mechanical interlocking at the surface.

The bond strength can be significant in shear depending on the degree of roughness and residual stresses present

Other bondsHydrogen bonding,

van der Waals forces

All these mechanisms take place at the interface region either in isolation, or, most likely, in combination to produce the final bond.

Types of bonding

Page 21: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Types of bonding

Page 22: Properties of Composites Dependent on: Constituent phases Reinforcement Matrix Relative amounts Interface properties Geometry of reinforcement Processing

Interface bonding depends on Atomic arrangement, molecular

conformation and chemical constitution of the fiber and matrix

Morphological properties of the fiber Diffusivity of elements in the fibre and

matrix. Interface is specific to each fiber-matrix

system