MME131: Lecture 30 Composite Materials A. K. M. B. Rashid Professor, Department of MME BUET, Dhaka Topics to Discuss ….. What are composites? Why do we make composite material? Common terminologies Classifications of composite materials Benefits of composites Lec 30, Page 1/13 What are composite materials ? Composites are artificially materials containing of two or more physically distinct phases, separated by a distinct interface THE MATRIX (aluminium) INTERFACE (allows transfer of stress from the matrix to the dispersed phase) REINFORCEMENT (tungsten fibre) tungsten fibre reinforced aluminium composite Some examples of composite materials (a) plywood is a laminar composite of layers of wood veneer (b) fiberglass is a fiberreinforced composite containing stiff, strong glass fibers in a softer polymer matrix (175) (c) concrete is a particulate composite containing coarse sand or gravel in a cement matrix (reduced to 50%). Lec 30, Page 2/13 Natural Composites: wood and bamboo, shells, bones, muscles Natural fibres: silk, wool, cotton, jute Abalone shell: CaCO3 + 3% organic material >3000 times stronger than calcite Wood: cellulose-filaments in a matrix of lignin and hemicellulose Why do we make composites ? The combination of phases produces properties that are different from those of its constituents Offset the poor qualities of one phase with the good qualities of another The primary needs for making composites: ☐ light weight ☐ greater strength and stiffness ☐ better corrosion resistance ☐ higher operating temperatures ☐ higher impact and wear resistance ☐ higher reliability and affordability Lec 30, Page 3/13 “The best of both worlds” Metals Pros electrically, thermally conductive good strength and ductility high toughness magnetic Pros electrically, thermally insulating wear and corrosion resistant high strength and stiffness creep resistant low density Cons dense low creep resistance low/moderate corrosion resistance Composites Ceramics Cons difficult to form/machine very low toughness Pros very ductile easy to form corrosion resistant high strength-to-weight ratio Polymers Cons low stiffness & strength poor high temperature properties Common terminologies The matrix Continuous phase, or the bulk material, the property of which is generally reinforced Made from metals, polymers or ceramics Some ductility of the matrix and high bonding strength between matrix and reinforcements are desirable Functions of matrix Binds the reinforcements together Mechanically supporting the reinforcements Transfer the applied load to the reinforcements Protect the reinforcements from surface damage due to abrasion or chemical attacks Lec 30, Page 4/13 Metal matrix moderately stiff and strong moderately hard, wear and abrasion resistance moderately creep and fatigue resistance Aim – to make much stiffer, stronger and wear, creep and fatigue resistant Common matrices: Al, Cu, Ti, Ni Example: SiC reinforced Al Ceramic matrix hard and brittle Aim – to make tougher and more reliable Common matrices: glass, cement, Al2O3, ZrO2, TiO2 Example: ZrO2 toughened Al2O3, Ag toughened Al2O3 , steel reinforced concrete Polymer matrix weaker and have low melting point Aim – to make more stronger and temperature resistant Common matrices: epoxy, polyester, polyurethane, rubber Example: GFRP, CFRP The Reinforcing Material The dispersed phase in the matrix Made from metals, polymers or ceramics Can be in the form of particles, fibres or various other geometries Functions of reinforcing material: to enhance matrix properties Particle reinforcement Silver, Cobalt; Silica, Carbon black, Rocks, Alumina, Talc, SiC, Si3N4, Glass beads Fibre reinforcement Boron, Steel, Tungsten, Chromium; Carbon, Alumina, SiC, Glass, Kevlar Lec 30, Page 5/13 Classification of composites Based on Matrix Phase Metal matrix composites Matrix: Moderately strong, stiff, wear resistant and fatigue resistant Aim: To significantly improve above properties Example: SiC reinforced Al, Precipitation hardened Al, etc. Ceramic matrix composites Matrix: Hard and brittle Aim: To make tougher and more reliable Example: Ag reinforced Al2O3 , ZrO2 reinforced TiO2 , steel reinforced concrete Polymer matrix composites Matrix: Weaker and have low melting point Aim: To make stronger and more temperature resistant Example: GFRP, CFRP Lec 30, Page 6/13 Based on Dispersed Phase Fibrous composites continuous vs. discontinuous aligned vs. randomly oriented GFRP CFRP Structural composites Particulate composites Large particle vs. dispersion strengthened WC particle reinforced Co sandwich structure vs. honeycomb structure Polymer core sandwiched by Al faces Fibre materials for reinforcement Whiskers thin single crystals - large length to diameter ratio high crystal perfection – extremely strong, strongest known very expensive example: graphite, SiN, SiC Fibers polycrystalline or amorphous generally polymers or ceramics example: Al2O3 , Aramid, E-glass, Boron Wires metal – steel, Mo, W Lec 30, Page 7/13 Structural composites Properties of structural composites depends upon the geometrical design of the reinforcement. (a) Laminar composite structure – conventional (b) Sandwich structure (c) Honeycomb sandwich structure Lec 30, Page 8/13 Rule of Mixture for Fibre Reinforcement Composite stress: s c = s f Vf + s m Vm Composite strain: ec = ef = em Hook’s law: sc Ec sf sm Ef Em Composite strength: s c = s f V f + s m Vm Composite stiffness: Ec = EfVf + EmVm Problem A continuous and aligned glass fibre-reinforced composite consists of 40 vol.% glass fibres having a modulus elasticity of 69 GPa and 60 vol.% polyester resin that, when hardened, displays a modulus of 3.4 GPa. (a) Compute the modulus of elasticity of this composite in the longitudinal direction. (b) If the cross-sectional area is 250 mm2 and a stress of 50 MPa is applied in the longitudinal direction, compute the magnitude of the load carried by each of the fibre and matrix phases. (c) Determine the strain that is sustained by each phase when the stress in part b is applied. Lec 30, Page 9/13 Answer: Given data: EC = Ef Vf + Em Vm Ef = 69 GPa Em = 3.4 GPa Vf = 0.40 Vm = 0.60 = (69 GPa).(0.40) + (3.4 GPa).(0.60) = 30 GPa (a) Manipulating Hooks’ law for longitudinal directions, one may find the ratio of forces on the fibres and the matrix Ff Ef Vf = Fm Em Vm Again, forces on the composite FC = sC AC (69 GPa).(0.40) = (3.4 GPa).(0.60) Ff = 13.5 Fm [1] Given data: = (50 MPa).(250 mm2) = 12500 N FC = Ff + Fm = 12500 N Using these two equations, one may find Ff = 11640 N and Fm = 860 N For an unit length of composite Am = V m AC = (0.6).(250 mm2) = 150 mm2 and Af = 100 mm2 sC = 50 MPa AC = 250 mm2 [2] (b) sf = Ff / Af = (11640 N) / (100 mm2) = 116.40 MPa sm = Fm / Am = (860 N) / (150 mm2) = 5.73 MPa Then individual strain in each phase ef = sf / Ef = (116.40 MPa) / (69 GPa) = 1.69x10-3 (c) em = sm / Em = (5.73 MPa) / (3.4 GPa) = 1.69x10-3 (c) Thus, as they should be, strains for both fibre and matrix phases are identical Lec 30, Page 10/13 Particle materials for reinforcement Particles used can be ranging in size from microscopic (dispersionstrengthened composites) to macroscopic (large-particle composites) Dispersion strengthening Similar to precipitation hardening Strengthening occurs in atomic/molecular level by making it harder for dislocation to move Large-particle strengthening Harder and stiffer reinforcing particles tend to restrain movement of the matrix phase in the vicinity of each particle Particles may be of any shape – ranging from irregular to spherical, plate-like to needle-like. The distribution of particles in the composite matrix is random, and therefore strength and other properties of the composite material are usually isotropic Particulate strengthening is much less efficient than fibre-reinforcing SiC reinforced Al casting (compliant) (ductile) (stiffer) (brittle, hard) Large-particle composites Dispersion-strengthened composites Lec 30, Page 11/13 Example A cemented carbide cutting tool used for machining contains 75 wt% WC, 15 wt% TiC, 5 wt% TaC, and 5 wt% Co. Estimate the density of the composite. SOLUTION First, we must convert the weight percentages to volume fractions. The densities of the components of the composite are: From the rule of mixtures, the density of the composite is Lec 30, Page 12/13 Next Class Lecture 34 Materials Selection Lec 30, Page 13/13