Bruce Mayer, PE
Registered Electrical & Mechanical Engineer
BMayer@ChabotCollege.edu
Engineering-45: Materials of Engineering
1
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
List The CLASSES and TYPES of Composites
When to Use Composites Instead of
Metals, Ceramics, or Polymers
How to Estimate Composite
Stiffness & Strength
Examine some Typical Applications
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Composite
MultiPhase
Material with Significant
Proportions of Each Phase
• Phase Components
– MATRIX
– DISPERSED Phase
Matrix
• The CONTINUOUS Phase
• The Matrix Function
3
– transfer stress to other phase(s)
– Protect other phase(s) from the (corrosive) Environment
Engineering-45: Materials of Engineering
Reprinted with permission from
D. Hull and T.W. Clyne, An
Introduction to Composite
Materials, 2nd ed., Cambridge
University Press, New York, 1996,
Fig. 3.6, p. 47.
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Composite Classifications
• M MC
Metal Matrix Composite
• C MC
Ceramic Matrix Comp.
• P MC
Polymer Matrix Comp.
Dispersed Phase (DP)
• Function = To Enhance the
Matrix Properities
– MMC : increase σ y
, TS/ σ u
, creep resistance
– CMC : increase K c
(fracture toughness)
– PMC: increase E, σ y
, TS/ σ u
, creep resistance
• Classes: Particle, fiber, structural
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
PARTICLE Reinforced
LARGE
Particle
DISPERSION
Strengthened
Composites
Continous
(Aligned)
FIBER Reinforced
DIScontinous
(Short)
STRUCTURAL
Laminates
Sandwich
Panels
Aligned
Randomly Oriented
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Particle-reinforced Fiber-reinforced
Examples
-Spheroidite steel matrix: ferrite ( a )
(ductile)
Structural particles: cementite
(Fe3C)
(brittle)
Adapted from Fig.
10.10, Callister 7e.
(Fig. 10.10 is copyright United
States Steel
Corporation, 1971.)
60 m m
-WC/Co cemented carbide matrix: cobalt
(ductile)
Vm:
10-15vol%!
-Automobile tires matrix: rubber
(compliant)
Engineering-45: Materials of Engineering
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600 m m particles:
WC
(brittle, hard)
Adapted from Fig.
16.4, Callister 7e.
(Fig. 16.4 is courtesy Carboloy
Systems,
Department,
General Electric
Company.) particles:
C
(stiffer)
Adapted from Fig.
16.5, Callister 7e.
(Fig. 16.5 is courtesy Goodyear
Tire and Rubber
0.75
m m
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Concrete is a
PARTICLE
ReInforced
Composite
• Matrix = PortLand
Cement
– 3CaO-SiO
2
2CaO-SiO
2
+
• Dispersed Phases
– Sand+Gravel
Aggregate
– 60%-80% by Vol
Engineering-45: Materials of Engineering
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Steel ReInforcing
Bars (Rebar)
• A type of FIBER
Reinforcement
• Improves Tensile &
Shear Strength
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Concrete ≡ gravel + SAND + cement
• Why sand and gravel? → Sand packs into gravel VOIDS
Reinforced concrete - Reinforce with steel reBAR or reMESH
• Increases TENSILE strength - even if Concrete matrix is cracked
PreStressed concrete - reMesh under tension during setting of concrete. Tension release puts concrete under COMPRESSIVE Stress
• Concrete is much stronger under compression.
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Particle-reinforced Fiber-reinforced Structural
Composite Material Elastic Modulus, E c
• Two “Rule of Mixtures” Approximations upper limit:
E c
=
V E
+
V
“rule of mixtures” p
E p ←Springs in PARALLEL
Data:
E(GPa)
350
Cu matrix w/tungsten particles
300
250
200
150 lower limit:
1
E c
=
V m
E m
+
V p
E p
0 20 40 60 80 100
(Cu) (W) vol% tungsten
Rule-of-Mixtures Applies to Other Properties
• Electrical conductivity, σ elect
: Replace E by σ elect
• Thermal conductivity, k: Replace E by k.
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Fibers very strong
• Provide significant strength improvement compared to pure matrix-material
Example: fiber-glass
• Continuous glass filaments in a polymer matrix
• Strength due to fibers
• Polymer simply holds them in place
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Whiskers - Thin single crystals large length to diameter ratio
• graphite, SiN, SiC
• high crystal perfection – extremely strong, strongest known
• very expensive
Traditional Fibers
polycrystalline or amorphous
Generally polymers or ceramics
Ex: Al
2
O
3
, Aramid,
E-glass, Boron,
UHMWPE
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Particle-reinforced Fiber-reinforced
Fiber Materials
• Whiskers - Thin single crystals with large length to diameter ratio
– graphite, SiN, SiC
– high crystal perfection – extremely strong, strongest physical form known
– very expensive to produce
– Fibers
• polycrystalline or amorphous
• generally polymers or ceramics
• Ex: Al
2
O
3
– Wires
, Aramid, E-glass, Boron, UHMWPE
• Metal – steel, Mo, W
Structural
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Adapted from Fig.
16.8, Callister 7e .
13 aligned continuous
Engineering-45: Materials of Engineering aligned random discontinuous
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
isoSTRAIN →
Tensile strength and elastic modulus when fibers are parallel to the direction of stress
isoSTRESS →
Tensile strength and elastic modulus when fibers are perpendicular to the direction of stress
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Particle-reinforced Fiber-reinforced Structural
ALIGNED, CONTINUOUS Fibers
• Examples
Metal: g ’ (Ni
3
Al)a (Mo) by eutectic solidification.
matrix: a (Mo) (ductile)
Glass w/SiC fibers formed by glass slurry
E glass = 76GPa; E SiC = 400GPa.
15
(a)
2 m m fibers: g ’ (Ni3Al) (brittle)
From W. Funk and E. Blank, “Creep deformation of Ni
3
Al-Mo in-situ composites", Metall. Trans. A Vol. 19(4), pp. 987-998, 1988. Used with
(b)
From F.L. Matthews and R.L.
Rawlings, Composite Materials;
Engineering and Science, Reprint ed., CRC Press, Boca Raton, FL,
2000. (a) Fig. 4.22, p. 145 (photo by J. Davies); (b) Fig. 11.20, p.
349 (micrograph by H.S. Kim, P.S.
Rodgers, and R.D. Rawlings).
Used with permission of CRC
Press, Boca Raton, FL.
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Particle-reinforced Fiber-reinforced Structural
DISCONTINUOUS, RANDOM, 2D (Planer) Fibers
Example: Carbon-Carbon
• Process: fiber/pitch, then burn out at up to 2500C.
• Uses: disk brakes, gas turbine exhaust flaps, rocket nose cones.
(b) view onto plane
C fibers: very stiff very strong
C matrix: less stiff less strong fibers lie in plane
(a)
Other variations:
• Discontinuous, random 3D
• Discontinuous, 1D
– Fully Aligned
Engineering-45: Materials of Engineering
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Adapted from F.L. Matthews and R.L.
Rawlings, Composite Materials; Engineering and Science, Reprint ed., CRC Press, Boca
Raton, FL, 2000. (a) Fig. 4.24(a), p. 151; (b)
Fig. 4.24(b) p. 151. (Courtesy I.J. Davies)
Reproduced with permission of CRC Press,
Boca Raton, FL.
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Particle-reinforced Fiber-reinforced
CRITICAL fiber length for effective stiffening & strengthening:
Structural fiber strength in tension fiber length
15
f c d fiber diameter shear strength of fiber-matrix interface
The Equation Balances (want PullOut ≥ Tear)
• The Fiber Load capacity → σ f
•[A
CylXsec
] = σ f
•[πd 2 /4]
• The Fiber Pull-Out Force→ c
•[A
CylSurf
] =
c
•[πd•l]
Stronger Fibers → need LONGER fiber
Stronger Fiber-Matrix ShearBond → need SHORTER Fiber
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Example: FiberGlass
• Need Fiber Lengh > 15mm
Reason for length Criteria → examine Extreme cases
• Very Short Fiber has very little hold-in force and would PULL-OUT (Fiber PULLS OUT before Fracture)
• Very Long Fiber would take almost all the axial load
(Fiber FRACTURES before PullOut)
Shorter, thicker fiber: fiber length
15
f c d fiber length
15
f c d
Adapted from Fig.
16.7, Callister 6e.
Poorer fiber efficiency
Engineering-45: Materials of Engineering
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Better fiber efficiency
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Particle-reinforced Fiber-reinforced Structural
Estimate E c and TS
• Valid for LONG Fiber
Condition: fiber length
15
f c d
The Elastic Modulus in
Fiber Direction
E c
=
E m
V m
+
KE efficiency factor f
V f
Typical Values for K:
• Aligned 1D: K = 1 (anisotropic)
• Random 2D: K = 3/8
2D isotropy)
• Random 3D: K = 1/5
(3D isotropy)
TS in fiber direction
(1D, Aligned) by VOLUME
Weighted Average
(TS) c
=
(TS) m
V m
+
(TS) f
V f
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Particle-reinforced Fiber-reinforced Structural
Stacked and bonded fiber-reinforced sheets
• Orthogonal stacking sequence: e.g., 0°/90°
• benefit: balanced, in-plane stiffness
Sandwich panels
• low density, honeycomb core
• benefit: small weight, large bending stiffness face sheet adhesive layer honeycomb
Similar to Composite Beam
Lab Exercise
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Ceramic Matrix
Composites →
Better FRACTURE
TOUGHNESS
Metal Matrix
Composites →
Improved CREEP
RESISTANCE
Force particle-reinf fiber-reinf un-reinf
Bend displacement
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Polymer Matrix Composites →
Better E: ρ (Stiffness:Weight) ratio
103
102
10
PMCs
1 ceramics metal/ metal alloys
.1
.01
G=3E8
K=E polymers
.1 .3 1 3 10 30
Density, r [Mg/m 3]
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
The PRIMARY
Motivation for the
Use of Composites
→ Hi-Strength,
Hi-Stiffness &
Lo-Weight
Thus Two Important
Metrics
• Specific STRENGTH
S
=
Strength
Specific
Weight
Engineering-45: Materials of Engineering
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S
E
• Similarly The
Specific STIFFNESS
=
Elastic
Specific
Modulus
Weight
Now Specific Weight g = r g in N/m
3
• Where
– ρ
Density in kg/m 3
– g
Acceleration of
Gravity (9.81 m/s 2 )
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Now Determine
Units for S
σ and S
E by Way of Examples
• For 7075 Al in the
Heat treated State
– u
= 83 ksi
– g
= 0.101 lb/in 3
S
=
83000 lb
0 .
101 lb in
2 in
3
S
=
8 .
218
10
5 in
Engineering-45: Materials of Engineering
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• For Kevlar-49
(Aramid Fiber)
– E = 131 GPa
– ρ = 1444 kg/m 3
• Find g g = r g
=
1444 kg m
3
9 .
81 m s
2
=
14166
N m
3
S
Now Specific Stiffness
E
=
131
10
9
N
1 4166 N m m
3
2
S
E
=
9 .
248
10
6 m
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
σ
E
26
The High DENSITY of Metal Reduces S
σ and S
The Low STRENGTH & STIFFNESS of most
E
Polymers Reduces S
σ
Engineering-45: Materials of Engineering and S
E
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Composites Classified by:
• The Matrix Material
– Ceramic (CMC)
– Metal (MMC)
– PolyMer (PMC)
• ReInforcement Geometry
– Particles
– Fibers
– Layers
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Composites enhance matrix properties:
• MMC: enhance y
, TS, creep performance
• CMC: enhance K c
• PMC: enhance E, y
, TS, creep resistance
Particle ReInforced
• Elastic modulus can be estimated by the
Rule of Mixtures
• Properties are isotropic
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Fiber ReInforced:
• Elastic modulus and TS can be estimated along fiber direction By Rule of Mixtures
• Properties can be isotropic or anisotropic
Structural:
• Based on build-up of sandwiches in layered form
– Plys
– HoneyCombs
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Prob 16.11
• Given IsoStrain,
Longitudinal Loading for a Continuous
F
Fiber Composite: c
=
F m
+
F f
• Then Show
• Where
– F
Force
– E
Elastic Modulus
– V
Volume fraction
– Sub-f → “fiber”
– Sub-m → “matrix”
– Sub-c → “composite”
30
F
F m f =
E
E
Engineering-45: Materials of Engineering f
V m
V m f
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Bruce Mayer, PE
Licensed Electrical & Mechanical Engineer
BMayer@ChabotCollege.edu
Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Engineering-45: Materials of Engineering
31
http://www.azom.com/details.asp?Articl
eID=764
Background
• E-Glass or electrical grade glass was originally developed for stand off insulators for electrical wiring. It was later found to have excellent fibre forming capabilities and is now used almost exclusively as the reinforcing phase in the material commonly known as fibreglass.
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Composition
• E-Glass is a low alkali glass with a typical nominal composition of SiO
2
14wt%, CaO+MgO 22wt%, B
54wt%, Al
2
O
3
2
O
3
10wt% and Na
2
O+K
2
O less then 2wt%. Some other materials may also be present at impurity levels.
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Properties that have made E-glass so popular in fibreglass and other glass fibre reinforced composite include:
• Low cost
• High production rates
• High strength, (see table on next slide)
• High stiffness
• Relatively low density
• Non-flammable
• Resistant to heat
• Good chemical resistance
• Relatively insensitive to moisture
• Able to maintain strength properties over a wide range of conditions
• Good electrical insulation
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
Table 1. Comparison of typical properties for some common fibres.
Materials
E-Glass
S-Glass
Alumina (Saffil)
Carbon
Kevlar 29
Kevlar 49
Density (g/cm 3 )
2.55
2.49
3.28
2.00
1.44
1.44
Tensile Strength
(MPa)
2000
4750
1950
2900
2860
3750
Young modulus
(GPa)
80
89
297
525
64
136
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt
The use of E-Glass as the reinforcement material in polymer matrix composites is extremely common.
Optimal strength properties are gained when straight, continuous fibres are aligned parallel in a single direction. To promote strength in other directions, laminate structures can be constructed, with continuous fibres aligned in other directions. Such structures are used in storage tanks and the like.
Random direction matts and woven fabrics are also commonly used for the production of composite panels, surfboards and other similar devices.
Engineering-45: Materials of Engineering
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Bruce Mayer, PE
BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt