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<strong>Materials</strong> <strong>Selection</strong><br />

<strong>for</strong><br />

<strong>Mechanical</strong> <strong>Design</strong> I<br />

A Brief Overview of a Systematic Methodology<br />

Jeremy Gregory<br />

Research Associate<br />

Laboratory <strong>for</strong> Energy and Environment<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> – Slide 1


Relationship To Course<br />

�� A key concept throughout this course is<br />

how to select among technology choices<br />

�� Economic Analysis<br />

�� Cost Modeling<br />

�� Life Cycle Assessment<br />

�� Focus has been on economic assessment<br />

of alternatives<br />

�� How does this fit into larger technology<br />

choice problem?<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 2


Approach Changes as <strong>Design</strong> Evolves<br />

<strong>Design</strong> Detail<br />

Market need<br />

Concept<br />

Embodiment<br />

Detail<br />

Production etc.<br />

# of Candidates<br />

<strong>Selection</strong> Methods<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 3<br />

Economic Analysis<br />

Cost Modeling<br />

LCA<br />

Method<br />

Needed <strong>for</strong><br />

Early Stage


What parameters define material selection?<br />

Example: SUV Liftgate<br />

Image removed <strong>for</strong> copyright reasons.<br />

Schematic of components in an SUV liftgate (rear door).<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 4


Attractive Options<br />

May Be Found Outside of Expertise<br />

Unit Cost<br />

$300<br />

$250<br />

$200<br />

$150<br />

$100<br />

$50<br />

$0<br />

Steel<br />

Aluminum<br />

SMC<br />

0 25 50 75 100 125<br />

Annual Production Volume (1000s)<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 5


Need Method <strong>for</strong> Early Material <strong>Selection</strong>:<br />

Ashby Methodology*<br />

Four basic steps<br />

1. Translation: express design requirements<br />

as constraints & objectives<br />

2. Screening: eliminate materials that cannot<br />

do the job<br />

3. Ranking: find the materials that do the job<br />

best<br />

4. Supporting in<strong>for</strong>mation: explore pedigrees<br />

of top-ranked top ranked candidates<br />

M.F. Ashby, <strong>Materials</strong> <strong>Selection</strong> in <strong>Mechanical</strong> <strong>Design</strong>, 3 rd Ed., Elsevier, 2005<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 6


First Step: Translation<br />

“Express design requirements as constraints and objectives”<br />

Using design requirements, analyze four items:<br />

�� Function: What does the component do?<br />

�� Do not limit options by specifying implementation w/in<br />

function<br />

�� Objective: What essential conditions must be met?<br />

�� In what manner should implementation excel?<br />

�� Constraints: What is to be maximized or minimized?<br />

�� Differentiate between binding and soft constraints<br />

�� Free variables: Which design variables are free?<br />

�� Which can be modified?<br />

�� Which are desirable?<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 7


Identifying Desirable Characteristics<br />

Example: <strong>Materials</strong> <strong>for</strong> a Light, Strong Tie<br />

�� Function:<br />

�� Support a tension load<br />

�� Objective:<br />

�� Minimize mass<br />

�� Constraints:<br />

�� Length specified<br />

�� Carry load F, w/o failure<br />

�� Free variables:<br />

�� Cross-section Cross section area<br />

�� Material<br />

F F<br />

Area, A<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 8<br />

L<br />

�� Objective:<br />

� m = ALρ<br />

�� Constraint:<br />

� F / A < σ y


Identifying Desirable Characteristics<br />

Example: <strong>Materials</strong> <strong>for</strong> a Light, Strong Tie<br />

�� Objective:<br />

� m = ALρ<br />

�� Constraint:<br />

� F / A < σ y<br />

�� Rearrange to eliminate<br />

free variable<br />

≥ ( )( ) ⎜ ⎟<br />

m F L<br />

⎛ ρ ⎞<br />

⎜σ⎟ ⎝ y ⎠<br />

�� Minimize weight by<br />

minimizing<br />

⎛ ρ ⎞<br />

⎜<br />

⎟<br />

σ ⎟<br />

⎝ y ⎠<br />

F F<br />

Area, A<br />

or maximize<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 9<br />

L<br />

Material Index<br />

σ y<br />

⎛ ⎞<br />

⎜ ⎟<br />

⎝ ρ ⎠


Second Step: Screening<br />

“Eliminate materials that cannot do the job”<br />

Need effective way of<br />

evaluating large range<br />

of material classes<br />

and properties<br />

Alumina<br />

Si-carbide<br />

Ceramics<br />

Si-nitride<br />

Ziconia<br />

Soda glass<br />

Borosilicate<br />

Glasses<br />

Silica glass<br />

Glass ceramic<br />

Steels<br />

Cast irons<br />

Al-alloys<br />

Metals<br />

Cu-alloys<br />

Ti-alloys<br />

Composites<br />

Sandwiches<br />

Hybrids<br />

Lattices<br />

Segmented<br />

PE, PP, PC<br />

PS, PET, PVC<br />

PA (Nylon)<br />

Polymers<br />

Polyester<br />

Epoxy<br />

Isoprene<br />

Butyl rubber<br />

Elastomers<br />

Natural rubber<br />

Silicones<br />

EVA<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 10


Comparing Material Properties:<br />

Material Bar Charts<br />

Young’s modulus (GPa)<br />

(Log Scale)<br />

Steel<br />

Aluminum<br />

Copper<br />

Zinc<br />

Lead<br />

PEEK<br />

PP<br />

PTFE<br />

Metals Polymers Ceramics Hybrids<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 11<br />

WC<br />

Alumina<br />

Glass<br />

CFRP<br />

GFRP<br />

Fiberboard<br />

Good <strong>for</strong> elementary selection (e.g., find materials with large modulus)


Comparing Material Properties:<br />

Material Property Charts<br />

Young’s modulus (GPa)<br />

1000<br />

100<br />

10<br />

1<br />

0.1<br />

0.01<br />

Woods<br />

Foams<br />

Composites<br />

Ceramics<br />

Polymers<br />

Elastomers<br />

0.1 1 10<br />

Density (Mg/m 3 )<br />

Metals<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 12<br />

100


Screening Example:<br />

Heat Sink <strong>for</strong> Power Electronics<br />

�� Function:<br />

�� Heat Sink<br />

�� Constraints:<br />

1. Max service temp > 200 C<br />

2. Electrical insulator ��<br />

R > 10 20 µohm ohm cm<br />

3. Thermal conductor ��<br />

T-conduct. conduct. λ > 100 W/m K<br />

4. Not heavy ��<br />

Density < 3 Mg/m 3<br />

�� Free Variables:<br />

�� <strong>Materials</strong> and Processes<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 13


Heat Sink Screening: Bar Chart<br />

Max service temperature (K)<br />

Steel<br />

Copper<br />

Aluminum<br />

Zinc<br />

Lead<br />

Metals<br />

PEEK<br />

PP<br />

PTFE<br />

Polymers<br />

200 C<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 14<br />

WC<br />

Alumina<br />

Glass<br />

Ceramics<br />

GFRP<br />

CFRP<br />

Fiberboard<br />

Composites


Heat Sink Screening: Property Chart<br />

Thermal conductivity (W/m K)<br />

1000<br />

100<br />

10<br />

1<br />

0.1<br />

0.01<br />

Metals<br />

Composites<br />

Foams<br />

1 10 10 10 20<br />

Electrical resistivity ( µΩ cm)<br />

Ceramics<br />

Polymers &<br />

elastomers<br />

R > 10 20 µΩ cm<br />

λ > 100 W/m K<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 15<br />

10 30


Example using Granta Software:<br />

Automobile Headlight Lens<br />

�� Function:<br />

�� Protect bulb and lens; focus beam<br />

�� Objective:<br />

�� Minimize cost<br />

�� Constraints:<br />

�� Transparent w/ optical quality<br />

�� Easily molded<br />

�� Good resistance to fresh and salt water<br />

�� Good resistance to UV light<br />

�� Good abrasion resistance (high hardness)<br />

�� Free variables:<br />

�� Material choice<br />

Photo of headlight<br />

removed <strong>for</strong> copyright<br />

reasons.<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 16


<strong>Selection</strong> Criteria – Limit Stage<br />

Chart from the CES EduPack 2005, Granta <strong>Design</strong> Limited, Cambridge, UK. (c) Granta <strong>Design</strong>. Courtesy of Granta <strong>Design</strong> Limited. Used with permission.<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 17


Property Chart<br />

Hardness - Vickers (Pa)<br />

1e10<br />

1e9<br />

1e8<br />

1e7<br />

1e6<br />

100000<br />

10000<br />

Concrete<br />

Soda-lime glass<br />

Polymethyl methacrylate (Acrylic, PMMA)<br />

Borosilicate glass<br />

0.1 1<br />

Price (USD/kg)<br />

10 100<br />

•Cheapest, Cheapest, hardest<br />

material is soda-<br />

lime glass – used<br />

in car headlights<br />

•For For plastics,<br />

cheapest is PMMA<br />

– used in car tail<br />

lights<br />

Chart from the CES EduPack 2005, Granta <strong>Design</strong> Limited, Cambridge, UK. (c) Granta <strong>Design</strong>. Courtesy of Granta <strong>Design</strong> Limited. Used with permission.<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 18


Third Step: Ranking<br />

“Find Find the materials that do the job best” best<br />

What if multiple materials are selected after<br />

screening?<br />

Which one is best?<br />

What if there are multiple material parameters<br />

<strong>for</strong> evaluation?<br />

Use Material Index<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 19


Single Property Ranking Example:<br />

Overhead Transmission Cable<br />

�� Function:<br />

�� Transmit electricity<br />

�� Objective:<br />

�� Minimize electrical Resistance<br />

R = ρe<br />

�� Constraints:<br />

�� Length L and section A are specified<br />

�� Must not fail under wind or ice-load ice load ��<br />

required tensile strength > 80 MPa<br />

�� Free variables:<br />

�� Material choice<br />

Screen on strength, rank on resistivity<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 20<br />

L<br />

A<br />

L<br />

Electrical<br />

resistivity


Single Property Ranking Example:<br />

Overhead Transmission Cable<br />

•Screening Screening on<br />

strength eliminates<br />

polymers, some<br />

ceramics<br />

•Ranking Ranking on<br />

resistivity selects<br />

Al and Cu alloys<br />

Resistivity (µohm.cm) (µ-ohm cm)<br />

1e27<br />

1e24<br />

1e21<br />

1e18<br />

1e15<br />

1e12<br />

1e9<br />

1e6<br />

1000<br />

1<br />

1e-3<br />

Polystyrene (PS)<br />

Silica glass<br />

The selection<br />

Titanium alloys<br />

Low alloy steel<br />

Silicon Carbide<br />

Magnesium alloys<br />

Aluminium alloys<br />

Copper alloys<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 21<br />

Alumina<br />

PEEK<br />

Epoxies<br />

PETE<br />

Cellulose polymers<br />

Polyester<br />

Polyurethane (tpPUR)<br />

Isoprene (IR)<br />

Wood<br />

Cork<br />

Boron Carbide<br />

Chart from the CES EduPack 2005, Granta <strong>Design</strong> Limited, Cambridge, UK. (c) Granta <strong>Design</strong>. Courtesy of Granta <strong>Design</strong> Limited. Used with permission.


Advanced Ranking: The Material Index<br />

The method<br />

1. Identify function, function,<br />

constraints,<br />

constraints,<br />

objective and free variables<br />

�� List simple constraints <strong>for</strong> screening<br />

2. Write down equation <strong>for</strong> objective -- the “per<strong>for</strong>mance<br />

per<strong>for</strong>mance<br />

equation” equation<br />

�� If objective involves a free variable (other than the material):<br />

�� Identify the constraint that limits it<br />

�� Use this to eliminate the free variable in per<strong>for</strong>mance<br />

equation<br />

3. Read off the combination of material properties that<br />

maximizes per<strong>for</strong>mance -- the material index<br />

4. Use this <strong>for</strong> ranking<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 22


The Per<strong>for</strong>mance Equation, P<br />

P<br />

⎡⎛Functional ⎞ ⎛Geometric ⎞ ⎛Material ⎞⎤<br />

= ⎢⎜ ⎟, ⎜ ⎟, ⎜ ⎟⎥<br />

⎣⎝requirements, F⎠ ⎝parameters, G⎠ ⎝properties, M ⎠⎦<br />

or<br />

P= f F, G, M<br />

( )<br />

Use constraints to eliminate free variable<br />

P from previous example of a light, strong tie:<br />

≥ ( )( ) ⎜ ⎟<br />

m F L<br />

⎛ ρ ⎞<br />

⎜σ⎟ ⎝ y ⎠<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 23


The Material Index<br />

Example: <strong>Materials</strong> <strong>for</strong> a stiff, light beam<br />

�� Function:<br />

�� Support a bending load<br />

�� Objective:<br />

�� Minimize mass<br />

�� Constraints:<br />

�� Length specified<br />

�� Carry load F, without too<br />

much deflection<br />

�� Free variables:<br />

�� Cross-section Cross section area<br />

�� Material<br />

Area, A<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 24<br />

F<br />

L<br />

Deflection, δ<br />

�� Objective:<br />

� m = ALρ<br />

�� Constraint:<br />

F CEI<br />

�� S = ≥<br />

3<br />

δ L


The Material Index<br />

Example: <strong>Materials</strong> <strong>for</strong> a stiff, light beam<br />

�� Objective:<br />

� m = ALρ<br />

�� Constraint:<br />

F CEI<br />

�� S = ≥ 3<br />

δ L<br />

�� Rearrange to eliminate<br />

free variable<br />

1/2 5/2<br />

�� ⎛4Fπ⎞ ⎛ L ⎞⎛<br />

ρ ⎞<br />

m = ⎜ ⎟ ⎜ 1/2 ⎟⎜<br />

1/2 ⎟<br />

⎝ δ ⎠ ⎝C ⎠⎝<br />

E ⎠<br />

�� Minimize weight by<br />

minimizing<br />

⎛ ρ ⎞<br />

⎜ 1/2 ⎟<br />

⎝ E ⎠<br />

Area, A<br />

or maximize<br />

Material Index<br />

1/2 ⎛ ⎞<br />

E<br />

⎜ ⎟<br />

⎝ ρ ⎠<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 25<br />

F<br />

L<br />

Deflection, δ


Material Index Calculation Process Flow<br />

FUNCTION<br />

Tie<br />

Beam<br />

Shaft<br />

Column<br />

<strong>Mechanical</strong>,<br />

Thermal,<br />

Electrical...<br />

Each combination of<br />

CONSTRAINTS<br />

Stiffness<br />

specified<br />

Strength<br />

specified<br />

Fatigue limit<br />

Geometry<br />

specified<br />

OBJECTIVE<br />

Minimum cost<br />

Minimum<br />

weight<br />

Function<br />

Constraint<br />

Objective<br />

Free variable<br />

Maximum energy<br />

storage<br />

Minimum<br />

eco- impact<br />

INDEX<br />

1/2 ⎡ ⎤<br />

E<br />

= ⎢ ⎥<br />

⎣ ρ ⎦<br />

has a<br />

characterizing<br />

material index<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 26<br />

M<br />

Maximize<br />

this!


Material Index Examples<br />

�� An objective defines a per<strong>for</strong>mance metric: metric:<br />

e.g. mass or resistance<br />

�� The equation <strong>for</strong> per<strong>for</strong>mance metric contains material properties<br />

�� Sometimes a single property<br />

Either is a<br />

�� Sometimes a combination<br />

Material Index<br />

Objective:<br />

Minimize Mass<br />

Per<strong>for</strong>mance Metric:<br />

Mass<br />

Material Indices <strong>for</strong> a Beam<br />

Loading<br />

Tension<br />

Bending<br />

Torsion<br />

Stiffness<br />

Limited<br />

E/ E/ρρ<br />

E 1/2<br />

1/2 /ρρ<br />

G 1/2<br />

1/2 /ρρ<br />

Maximize!<br />

Strength<br />

Limited<br />

σσ f /ρρ<br />

σσ f 22/3 /3 /ρρ<br />

σσ f 22/3 /3 /ρρ<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 27


Optimized <strong>Selection</strong> Using<br />

Material Indices & Property Charts: Strength<br />

Example:<br />

Tension Load,<br />

strength limited<br />

�� Maximize: M = σ/ρ<br />

�� In log space:<br />

log σ = log ρ + log M<br />

�� This is a set of lines<br />

with slope=1<br />

�� <strong>Materials</strong> above line<br />

are candidates<br />

Composites<br />

Foams<br />

Woods<br />

Ceramics<br />

Metals<br />

Polymers<br />

Elastomers<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 28


Material Indices & Property Charts:<br />

Stiffness<br />

Example:<br />

Stiff beam<br />

�� Maximize: Μ = Ε1/2 /ρ<br />

�� In log space:<br />

log E =<br />

2 (log ρ + log M)<br />

�� This is a set of lines<br />

with slope=2<br />

�� Candidates change<br />

with objective<br />

Composites<br />

Woods<br />

Foams<br />

Ceramics<br />

Metals<br />

Polymers<br />

Elastomers<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 29


Material Indices & Property Charts:<br />

Toughness<br />

�� Load-limited<br />

Load limited<br />

� M = KIC �� Choose tough<br />

metals, e.g. Ti<br />

�� Energy-limited<br />

Energy limited<br />

� M = K 2<br />

IC / E<br />

�� Composites and<br />

metals compete<br />

�� Displacement-limited<br />

Displacement limited<br />

� M = KIC / E<br />

�� Polymers, foams<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 30<br />

K IC<br />

K IC 2 /E<br />

Foams<br />

K IC/E<br />

Composites<br />

Polymers Woods<br />

Metals<br />

Ceramics


Considering Multiple<br />

Objectives/Constraints<br />

�� With multiple constraints:<br />

constraints<br />

�� Solve each individually<br />

�� Select candidates based on each<br />

�� Evaluate per<strong>for</strong>mance of each<br />

�� Select per<strong>for</strong>mance based on most limiting<br />

Select per<strong>for</strong>mance based on most limiting<br />

�� May be different <strong>for</strong> each candidate<br />

�� With multiple objectives:<br />

objectives<br />

�� Requires utility function to map multiple<br />

metrics to common per<strong>for</strong>mance measures<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 31


Method <strong>for</strong> Early Technology Screening<br />

�� <strong>Design</strong> per<strong>for</strong>mance is<br />

determined by the<br />

combination of:<br />

�� Shape<br />

�� <strong>Materials</strong><br />

�� Process<br />

�� Underlying principles of<br />

selection are unchanged<br />

�� BUT, do not underestimate<br />

impact of shape or the<br />

limitation of process<br />

Process<br />

<strong>Materials</strong><br />

Shape<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 32


Ashby Method <strong>for</strong> Early Material <strong>Selection</strong>:<br />

Four basic steps<br />

1. Translation: express design requirements<br />

as constraints & objectives<br />

2. Screening: eliminate materials that cannot<br />

do the job<br />

3. Ranking: find the materials that do the job<br />

best<br />

4. Supporting in<strong>for</strong>mation: explore pedigrees<br />

of top-ranked top ranked candidates<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 33


Summary<br />

�� Material affects design based on<br />

�� Geometric specifics<br />

�� Loading requirements<br />

�� <strong>Design</strong> constraints<br />

�� Per<strong>for</strong>mance objective<br />

�� Effects can be assessed analytically<br />

�� Keep candidate set large as long as is feasible<br />

�� <strong>Materials</strong> charts give quick overview; software can<br />

be used to more accurately find options<br />

�� Remember, strategic considerations can alter best<br />

choice<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 34


Example Problem: Table Legs<br />

Figure by MIT OCW.<br />

�� Want to redesign table with thin unbraced cylindrical<br />

legs<br />

�� Want to minimize cross-section cross section and mass without<br />

buckling<br />

�� Toughness and cost are factors<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 35


Table Legs: Problem Definition<br />

�� Function:<br />

�� Support compressive loads<br />

�� Objective:<br />

�� Minimize mass<br />

�� Maximize slenderness<br />

�� Constraints:<br />

�� Length specified<br />

�� Must not buckle<br />

�� Must not fracture<br />

�� Free variables:<br />

�� Cross-section Cross section area<br />

�� Material<br />

m= π r<br />

2<br />

lρ<br />

2 3 4<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 36<br />

P<br />

crit<br />

Per<strong>for</strong>mance Equation<br />

π EI π Er<br />

= =<br />

l<br />

2<br />

4l<br />

2


Table Legs: Material Indices<br />

Use constraints to<br />

eliminate free variable, r<br />

1/2<br />

⎛4P⎞ 2 ⎡ ρ ⎤<br />

m l<br />

⎝ π ⎠ ⎣E⎦ ≥ ⎜ ⎟ () ⎢ 1/2 ⎥<br />

Functional<br />

Requirements<br />

Minimize mass by<br />

maximizing M1 M<br />

Geometric<br />

Parameters<br />

1<br />

=<br />

1/2<br />

E<br />

ρ<br />

Material<br />

Properties<br />

For slenderness,<br />

calculate r at max load<br />

1/4 1/4<br />

1/2<br />

⎛4P⎞ ⎡1⎤ r l<br />

⎝π⎠ ⎣E⎦ ≥ ⎜ ()<br />

3 ⎟ ⎢ ⎥<br />

Functional<br />

Requirements<br />

Geometric<br />

Parameters<br />

Maximize slenderness<br />

by maximizing M2 M 2 = E<br />

Material<br />

Properties<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 37


Table Legs: Material <strong>Selection</strong><br />

�� Eliminated<br />

�� Metals (too heavy)<br />

�� Polymers<br />

(not stiff enough)<br />

�� Possibilities: Ceramics,<br />

wood, composites<br />

�� Final choice: wood<br />

wood<br />

�� Ceramics too brittle<br />

�� Composites too<br />

expensive<br />

�� Note: higher constraint<br />

on modulus eliminates<br />

wood<br />

Composites<br />

Woods<br />

Foams<br />

Ceramics<br />

Metals<br />

Polymers<br />

Elastomers<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 38<br />

M 1<br />

M 2


Material Index 1<br />

Young's Modulus (GPa)<br />

100<br />

10<br />

1<br />

0.1<br />

0.01<br />

1e-3<br />

Softwood: pine, along grain<br />

Rigid Polymer Foam (LD)<br />

Silicon<br />

CFRP, epoxy matrix (isotropic)<br />

Hardwood: oak, along grain<br />

Bam boo<br />

Boron carbide<br />

Silicon carbide<br />

100 1000<br />

Density (kg/m^3)<br />

10000<br />

Chart from the CES EduPack 2005, Granta <strong>Design</strong> Limited, Cambridge, UK. (c) Granta <strong>Design</strong>. Courtesy of Granta <strong>Design</strong> Limited. Used with permission.<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 39


Material Index 2<br />

Young's Modulus (Pa)<br />

1e11<br />

1e10<br />

1e9<br />

1e8<br />

1e7<br />

1e6<br />

Hardwood: oak, along grain<br />

Bamboo<br />

Softwood: pine, along grain<br />

Boron carbide<br />

CFRP, epoxy matrix (isotropic)<br />

Silicon carbide<br />

100 1000<br />

Density (kg/m^3)<br />

10000<br />

Chart from the CES EduPack 2005, Granta <strong>Design</strong> Limited, Cambridge, UK. (c) Granta <strong>Design</strong>. Courtesy of Granta <strong>Design</strong> Limited. Used with permission.<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 40


Example: Heat-Storing Heat Storing Wall<br />

�� Outer surface<br />

heated by day<br />

�� Air blown over<br />

inner surface to<br />

extract heat at<br />

night<br />

�� Inner wall must<br />

heat up ~12h after<br />

outer wall<br />

Figure by MIT OCW.<br />

Sun<br />

Air flow to<br />

extract heat<br />

from wall<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 41<br />

Heat Storing Wall<br />

W<br />

Fan


Heat-Storing Heat Storing Wall: Problem Definition<br />

�� Function:<br />

�� Heat storing medium<br />

�� Objective:<br />

�� Maximize thermal energy<br />

stored per unit cost<br />

�� Constraints:<br />

�� Heat diffusion time ~12h<br />

�� Wall thickness ≤ 0.5 m<br />

�� Working temp Tmax>100 max>100<br />

C<br />

�� Free variables:<br />

�� Wall thickness, w<br />

�� Material<br />

Heat content:<br />

Heat diffusion distance:<br />

w= 2at<br />

C = Specific Heat<br />

Thermal Conductivity<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 42<br />

p<br />

Q= wρC ∆T<br />

a = Thermal Diffusivity =<br />

λ =<br />

p<br />

λ<br />

ρC<br />

p


Heat-Storing Heat Storing Wall: Material Indices<br />

Eliminate free variable:<br />

1/2<br />

Q= 2t∆Ta<br />

ρCp<br />

Insert λ to obtain<br />

Per<strong>for</strong>mance Eqn:<br />

⎛ λ ⎞<br />

Q= 2t∆T⎜<br />

1/2 ⎟<br />

⎝a⎠ λ<br />

Maximize: M1 = 1/2<br />

a<br />

Thickness restriction:<br />

2<br />

w<br />

a ≤<br />

2t<br />

For w≤ 0.5 m and t = 12 h:<br />

M = a≤<br />

3× 10<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 43<br />

2<br />

−6<br />

2<br />

m/s


Heat-Storing Heat Storing Wall: Material <strong>Selection</strong><br />

�� Eliminated<br />

�� Foams: Too<br />

porous<br />

�� Metals: Diffusivity<br />

too high<br />

�� Possibilities:<br />

Concrete, stone,<br />

brick, glass,<br />

titanium(!)<br />

�� Final Choices<br />

�� Concrete is<br />

cheapest<br />

�� Stone is best<br />

per<strong>for</strong>mer at<br />

reasonable price<br />

Chart from the CES EduPack 2005, Granta <strong>Design</strong> Limited, Cambridge, UK. (c) Granta <strong>Design</strong>. Courtesy of Granta <strong>Design</strong> Limited. Used with permission.<br />

Massachusetts Institute of Technology<br />

Cambridge, Massachusetts <strong>Materials</strong> Systems Laboratory<br />

©Jeremy Gregory and Randolph Kirchain, 2005 <strong>Materials</strong> <strong>Selection</strong> I – Slide 44

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