Composite Materials Engineering 45 Bruce Mayer, PE

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Engineering 45

Composite

Materials

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

Learning Goals – Composites

 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

Terms & Classifications

 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

Terms & Classifications cont.1

 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

Composite Taxonomy

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

Composite Survey – Particle-I

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

ReInforced ConCrete

 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

More ReInforced Concrete

 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

Composite Survey – Particle-II

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

Composite Survey: Fiber-I

 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

Fiber Materials

 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

Composite Survey: Fiber-II

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

Fiber Alignment

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

ISOstress & ISOstrain

 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

Composite Survey – Fiber-I

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

Composite Survey – Fiber-II

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

Composite Survey – Fiber-III

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

Fiber Lengths cont.

 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

Composite Survey – Fiber-IV

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

Composite Survey – Structural

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

Composite Benefits

 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

Composite Benefits cont.1

 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

Specific Strength

 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

Specific Strength cont.1

 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

25

Bruce Mayer, PE

BMayer@ChabotCollege.edu • ENGR-45_Lec-28_Composites.ppt

S

σ

vs S

E

Comparison

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

Summary – Composite Matls

 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

Summary – Composites cont.1

 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

Summary – Composites cont.2

 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

WhiteBoard Work

 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

Chabot Engineering

Appendix

E-glass

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

E Glass - BackGround

 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

E Glass - Composition

 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

E Glass – Key Properties

 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

E Glass – Fibre Strength

 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

E Glass – Use in Composites

 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

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