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Design for Manufacturing
and Assembly
Case Study
Many well-known disasters can be traced back to design changes.
Although the root cause for the source of the fire has never been determined, there
are some lessons that still apply today.
Recap: After crossing the Atlantic, the Hindenburg attempted to land in Lakehurst,
New Jersey. During the landing procedure, a fire started on the aircraft. The
aircraft was destroyed in 30 seconds. Trivia: This flight was actually a partnership
with American Airlines.
Lesson 1: The Hindenburg design contained performance and safety improvements over the previous best-in-class airships from both Germany and the UK. Even “better” can fail catastrophically.
Lesson 2: Initial assumption was that the fire was hydrogen-burning, but the flames were yellow – indicating the side and internal containment bags were burning. The obvious root cause might not be correct.
Lesson 3: The designers originally specified Rolls-Royce gasoline engines, but the manufacturer refused to buy from a UK supplier. Instead, they installed Benz diesels with a lower power-to-weight ratio. As a result, the designers had to quickly lighten the airship. They chose to skip the flame-retardant coating on the skin. Last minute changes are risky.
Source: Pat Baird, Baxter Healthcare, 2015
Design for Assembly
Definition: DFA is a method of design of products for ease of assembly
DFA focuses on the optimization of the part/system assembly
DFA is a tool used to assist the design teams in the design of products
that will transition to production at a minimum cost, focusing on the
number of parts, handling and ease of assembly.
Concerned only with reducing product assembly cost
Minimizes number of assembly operations
Individual parts tend to be more complex in design
Copyright GCI, LLC 2015
Design for Manufacturing
Definition: DFM is a method of design for ease of manufacturing of
the collection of parts that will form the product after assembly.
DFM focuses on optimization of the manufacturing process.
DFM is a tool used to select the most cost effective material and
process to be used in production in the early stages of product design.
Concerned with reducing overall part production cost
Minimizes complexity of manufacturing operations
Uses common datum features and primary axes
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Design for Manufacturing and Assembly
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Source: Boothroyd and Dewhurst, 1989
Design for Manufacturing and Assembly
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Sequence of Analysis for DFMA
1. Concept Design
2. Design for Assembly
Optimize Design for Part Count
Optimize Design for Assembly
3. Design for Manufacturing
Optimize Design for Production Readiness
4. Detailed Design
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10 Steps of the Design for Assembly Process
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1. Gather functional requirements
2. Perform a functional analysis
3. Identify parts that can be standardized
4. Determine part count efficiencies
5. Determine the practical part count
6. Identify poka-yoke opportunities
7. Identify handling opportunities
8. Identify insertion opportunities
9. Look for ways to reduce secondary operations
10.Analyze metrics against cost and risk
Example: The CLAW
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1 of 10: Gather Functional Requirements
Understand how the product works
Review the preliminary specifications and DOE
DOE for design optimization
DOE for process optimization
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2 of 10: Functional Analysis
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There are 3 rules for functional analysis:
1. Assume the first part (the base) is always an essential part
2. Assume fasteners, spacers, washers, o-rings, connectors and
leads are always non-essential parts
3. Liquids such as glue, sealant, lube do not count as parts
Functional Analysis
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Begin by identifying each
part of The CLAW:
1. List the parts in the order of
assembly
2. Assign a part number to each
part
DFA Analysis Worksheet (courtesy of Cummins Tools)
Part
Nu
mb
er
Part Name
1 Lower Jaw Subassembly
1.1 Lower Jaw
1.2 Lower Cover
1.3 Rivet
2 Upper Jaw Subassembly
2.1 Upper Jaw
2.2 Upper Cover
2.3 Rivet
3 Spring
4 Pivot
Part
Functional Analysis
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The best way to
identify all the parts
is to take the device
apart…
Rivet
Rivet
Pivot
Upper jaw
Spring
Lower jaw
Rivet
Rivet
Upper
Cover
Lower
Cover
Functional Analysis
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Next, count the number of each
kind of part
- this value is known as Np
Then, count the number of
Interfaces between each part
- this value is known as Ni
DFA Analysis Worksheet (courtesy of Cummins Tools)
Assembly Name: ____________________________
Pa
rt N
um
be
r
Part Name Nu
mb
er
of
Pa
rts
(Np
)
Nu
mb
er
of
Inte
rfa
ces
(Ni)
(pa
rt a
to
pa
rt b
= 1
)
1 Lower Jaw Subassembly
1.1 Lower Jaw 1 6
1.2 Lower Cover 1 3
1.3 Rivet 2 4
2 Upper Jaw Subassembly
2.1 Upper Jaw 1 6
2.2 Upper Cover 1 3
2.3 Rivet 2 4
3 Spring 1 3
4 Pivot 1 3
Totals 10 32
Part DFA Complexity
Functional Analysis
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Now we’ll determine if each part is essential or non-essential, so we
can determine the theoretical minimum number of parts.
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DFA Analysis Worksheet (courtesy of Cummins Tools)
Assembly Name: ____________________________Team Name: _______________________________
Part
Num
ber
Part Name Num
ber
of P
arts
(Np)
Num
ber
of In
terf
aces
(Ni)
(par
t a to
par
t b =
1)
Theo
retic
al M
inim
um P
art
(Fun
ctio
nal A
naly
sis
Char
t)
Part
Can
be
Stan
dard
ized
(if n
ot a
lrea
dy s
tand
ard)
Cost
(Low
/Med
ium
/Hig
h)
Prac
tical
Min
imum
Par
t
1 Lower Jaw Subassembly
1.1 Lower Jaw 1 6 Y N L Y
1.2 Lower Cover 1 3 N N L N
1.3 Rivet 2 4 N N L N
2 Upper Jaw Subassembly
2.1 Upper Jaw 1 6 N N L Y
2.2 Upper Cover 1 3 N N L N
2.3 Rivet 2 4 N N L N
3 Spring 1 3 N N L Y
4 Pivot 1 3 N N L Y
Totals 10 32 1 0 0 4
Part DFA Complexity
Functional Analysis /
Redesign Opportunity
3 of 10: Can Parts be Standardized?
• Consider if each part can be
standardized
• within the assembly station
• Within the full assembly
• Within the assembly plant
• Within the corporation
• Within the industry
• Consider if each part should be
standardized
• If you answer yes to both questions,
place “Y” in the spreadsheet cell;
otherwise, place “N” Copyright GCI, LLC 2015
4 of 10: Part Count Efficiency
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In step 4, we’ll determine part count efficiencies, beginning with the
theoretical part count efficiency.
Theoretical Part Theoretical Min. No. Parts
Count Efficiency = Total Number of Parts x 100
• In our example:
Theoretical Part 1
Count Efficiency = 10 x 100 = 10%
• Rule of thumb: part count efficiency goal is >60%
Continuing with Step 4, we’ll calculate the DFA Complexity Factor
Cummins metric for assessing complexity of a product design
Two Factors
Np – Number of Parts
Ni – Number of part-to-part interfaces
Smaller is better (goal is 0.0)
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= 17.9
Part Cost
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This is a subjective estimate
Part costs are categorized as low,
medium or high relative to other
parts in the assembly or in the
factory.
As we prepare for the next Step in the sequence, we must consider the part
cost.
5 of 10: Practical Minimum Part Count
Copyright GCI, LLC 2015
Step 5 is to determine the practical minimum part count
This is also subjective, and requires a team assessment of practical changes and
consideration of the trade offs between part cost and assembly cost.
Consider the “Part Cost” from the previous slide.
This step answers the question, “What are we prepared to do with the design
realistically and practically?”
From our example, there are 4 practical minimum parts:
spring, pivot, upper jaw, lower jaw
Practical Part Count Efficiency
Now we have enough information to calculate the Practical Part Count Efficiency:
Practical Part Practical Min. No. Parts
Count Efficiency = Total Number of Parts x 100
• In our example:
Practical Part 4
Count Efficiency = 10 x 100 = 40%
• Rule of thumb: part count efficiency goal is >60%
Copyright GCI, LLC 2015
Re-designed CLAW
Copyright GCI, LLC 2015
This simple design is the result of the
theoretical part count of 1, the
consideration of cost, and the practical
minimum part count.
Don’t constrain your design to
incremental improvement unless you
have to!
Copyright GCI, LLC 2015
DFA Analysis Worksheet (courtesy of Cummins Tools)
Assembly Name: ____________________________Team Name: _______________________________
Part
Nu
mb
er
Part Name Nu
mb
er o
f Pa
rts
(Np
)
Nu
mb
er o
f In
terf
aces
(N
i)
(par
t a
to p
art
b =
1)
Theo
reti
cal M
inim
um
Par
t
(Fu
nct
ion
al A
nal
ysis
Ch
art)
Part
Can
be
Stan
dar
diz
ed
(if
no
t al
read
y st
and
ard
)
Co
st (
Low
/Med
ium
/Hig
h)
Prac
tica
l Min
imu
m P
art
1 Lower Jaw Subassembly
1.1 Lower Jaw 1 6 Y N L Y
1.2 Lower Cover 1 3 N N L N
1.3 Rivet 2 4 N N L N
2 Upper Jaw Subassembly
2.1 Upper Jaw 1 6 N N L Y
2.2 Upper Cover 1 3 N N L N
2.3 Rivet 2 4 N N L N
3 Spring 1 3 N N L Y
4 Pivot 1 3 N N L Y
Totals 10 32 1 0 0 4
DFA Metrics 10% 40%
Goals 60% 60%0.0 -
17.9 -
Part DFA Complexity
Functional Analysis /
Redesign Opportunity
General Design and Cost Considerations
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Select the least expensive fastening method that allows you to meet the
specification
General Design and Cost Considerations
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Where appropriate, choose self-fastening features
General Design and Cost Considerations
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Symmetrical parts are easier to assemble because they don’t require
reorientation
Asymmetric Symmetric
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General Design and Cost Considerations
Top-Down Assembly is preferred
General Design and Cost Considerations
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Modular Assemblies are preferred
Image courtesy hitechcontrols.com
General Design and Cost Considerations
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Received
Inspected
Rejected
Stocked
Outdated
Returned to Vendor
Unreliable
Recycled
Late from Supplier
Involved in a Customer Complaint
Eliminate parts that aren’t required. Eliminated parts are NEVER…
Designed
Detailed
Prototyped
Produced
Scrapped
Tested
Re-engineered
Purchased
Progressed
Audited by FDA
Examples
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7 of 10: Handling (Grasp and
Orientation)
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Handling time is based on: • Assembly process
• Complexity of parts
Consider: • How many hands are required?
• Is any grasping assistance needed?
• What is the effect of part symmetry on assembly?
• Is the part easy to align/position?
Handling Difficulty
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Is a function of…
Part size
Part thickness
Part weight
Part fragility
Part flexibility
Part slipperiness
Part stickiness
How many hands it takes
Is optical magnification required
Is mechanical assistance required
Picture How Difficult It Is to Handle
These Parts…
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Another Handling Challenge Is
Tangling or Nesting
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8 of 10: Insertion (Locate and Secure)
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Insertion time is based on the difficulty required
for each component’s insertion
Consider: • Is the part secured immediately upon insertion?
• Is it necessary to hold down the part to maintain
its location?
• What type of fastening process is used
(mechanical, thermal, other)?
• Is the part easy to align?
Design Self-aligning and Self-locating Parts
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…and ensure the parts do not need to be held in
position in order to secure them in place
Other Insertion Challenges…
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• Provide adequate access and visibility
• Avoid small clearances
• Avoid large insertion forces
• Avoid mating locations that cannot be seen easily
9 of 10: Secondary Operations
Eliminate Secondary Operations as much as possible
Instead of this….. Do this
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Soldering
Gluing
Welding
Measuring
Reorienting
Screwing
Crimping
Drilling
Painting
Testing
Adjusting
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DFA Analysis Worksheet (courtesy of Cummins Tools)
Assembly Name: ____________________________Team Name: _______________________________
Pa
rt
Nu
mb
er
Part Name Nu
mb
er o
f P
arts
(N
p)
Nu
mb
er o
f In
terfa
ce
s (
Ni)
(pa
rt
a t
o p
art
b =
1)
Th
eo
re
tica
l M
inim
um
Pa
rt
(F
un
cti
on
al
An
aly
sis
Ch
art)
Pa
rt
Ca
n b
e S
tan
da
rd
ize
d
(if
no
t a
lre
ad
y s
tan
da
rd
)
Co
st
(Lo
w/M
ed
ium
/H
igh
)
Pra
cti
ca
l M
inim
um
Pa
rt
Asse
mb
le w
ro
ng
pa
rt
/
Om
it p
art
Asse
mb
le w
ro
ng
wa
y a
ro
un
d
Ta
ng
le/N
est/
Sti
ck
to
ge
the
r
Fle
xib
le/F
ra
gil
e/
Sh
arp
/S
lip
pe
ry
Pli
ers/T
we
eze
rs/
Ma
gn
ify
ing
gla
ss
Dif
ficu
lt t
o a
lig
n/Lo
ca
te
Ho
ldin
g d
ow
n r
eq
uir
ed
Re
sis
tan
ce
to
in
se
rti
on
Ob
str
ucte
d a
cce
ss/v
isib
ilit
y
Re
-orie
nte
d w
ork
pie
ce
Scre
w/D
ril
l/T
wis
t/R
ive
t/
Be
nd
/C
rim
p
We
ld/S
old
er/G
lue
Pa
int/
Lu
be
/H
ea
t/
Ap
ply
liq
uid
or g
as
Te
st/
Me
asu
re
/A
dju
st
1 Lower Jaw Subassembly
1.1 Lower Jaw 1 6 Y N L Y Y N N Y N N N N N N Y N N N
1.2 Lower Cover 1 3 N N L N N N N N N N Y N N N Y N N N
1.3 Rivet 2 4 N N L N N N N Y N N Y N N N N N N N
2 Upper Jaw Subassembly
2.1 Upper Jaw 1 6 N N L Y Y N N Y N N N N N N Y N N N
2.2 Upper Cover 1 3 N N L N Y N N N N N Y N N N Y N N N
2.3 Rivet 2 4 N N L N N N N Y N N Y N N N N N N N
3 Spring 1 3 N N L Y N N Y Y N N Y Y N N Y N N N
4 Pivot 1 3 N N L Y N N N Y N N Y N N N N N N N
Totals 10 32 1 2 0 4 3 0 1 6 0 0 6 1 0 0 5 0 0 0
DFA Metrics 10% 40%
Goals 60% 60%
5.0
0.0 - 0.0 0.0 0.0 0.0
17.9 - 3.0 7.0 7.0
Secondary OperationsPart DFA Complexity
Functional Analysis /
Redesign Opportunity Poka-yoke Handling Insertion
Now Let’s Focus on
Design for Manufacturing
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6 questions to ask when selecting the manufacturing method:
Q1: Is hard tooling required?
Q2: Have we selected the best technology or process to fabricate parts?
Q3: Have we selected the best material needed for function and cost?
Q4: Have we looked at all the new technology that is available?
Q5: Are the parts shaped for the implementation of automation?
Q6: Is the supplier capable of meeting the specifications?
Image courtesy dmtcnc.com
Selection of Manufacturing Method
Material
Function
Cost
Fabrication Process
Hard Tooling
New Technology
Configure product with access for automation
Simplify and reduce the number of manufacturing operations
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…and Finally
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Understand which part features are critical to the product’s functional quality
(not every drawing call out is critical to function and quality)
Contact
Information
Roberta Goode
www.GoodeCompliance.com
(954) 399-7510
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DFMA References
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7. Introduction to Design for (Cost Effective) Assembly and
Manufacturing David Steinstra, Rose-Hulman, 2015