Materials Selection for Mechanical Design I
Materials Selection for Mechanical Design I
Materials Selection for Mechanical Design I
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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