22-Mec-B5 Product Design and Development · December 2019
Question 6 of 7: Design for Manufacturing and Design for Assembly Used Together
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 2019 — 16-Mec-B5
Product Design and Development. Three (3) hours; OPEN BOOK; a Casio or
Sharp approved calculator is permitted. Question 1 must be completed and is worth
40 %; four (4) of the six (6) remaining questions are chosen, each worth
15 %, for a total of 100 %. The first five questions appearing in the
answer book are the ones marked. Most questions require an essay answer or the use
of tables, figures and charts, and clarity and organisation of the answer are
explicitly marked. All seven questions are solved here.
Reference texts.
K. T. Ulrich and S. D. Eppinger, Product Design and
Development, 6th ed., McGraw-Hill — the framework text for this exam
code (concept generation and selection, product architecture, DFM, development
processes).
G. E. Dieter and L. C. Schmidt, Engineering Design,
5th ed., McGraw-Hill — design process, decision methods, cost evaluation.
G. Pahl, W. Beitz, J. Feldhusen and K.-H. Grote, Engineering Design: A
Systematic Approach, 3rd ed., Springer — requirement lists and
systematic embodiment design.
G. Boothroyd, P. Dewhurst and W. Knight, Product Design for Manufacture and
Assembly, 3rd ed., CRC Press — the DFA index and process cost models
used in Questions 1 and 6.
M. F. Ashby, Materials Selection in Mechanical Design,
5th ed., Butterworth-Heinemann — material indices and the
translate/screen/rank/document procedure.
D. P. Raymer, Aircraft Design: A Conceptual Approach,
6th ed., AIAA — the Breguet range relation and installed-propulsion
book-keeping used in Question 1.
R. G. Cooper, Winning at New Products, 5th ed., Basic Books
— stage-gate governance and the expected commercial value model in
Question 7.
Canadian instruments cited in the answers: Canadian Aviation
Regulations (SOR/96-433) Part V and Airworthiness Manual Chapter 525;
Motor Vehicle Safety Act (S.C. 1993, c. 16) and the Motor Vehicle
Safety Regulations (CMVSS series); Patent Act (R.S.C. 1985,
c. P-4) as administered by CIPO; CSA C22.1 Canadian Electrical Code,
Part I.
Question 6: Design for Manufacturing and Design for Assembly Used Together (15 marks)
Part A — How the two are used together. Design for
Assembly attacks the number of parts and the difficulty of putting them
together; Design for Manufacturing attacks the cost of each part given the
process that will make it. They are used together in a fixed order, and the order
is the whole method: DFA first, DFM second. The reason is that DFA
changes the part count, and every DFM decision is made about a specific part —
so optimising the manufacture of a part that DFA is about to eliminate is wasted
work, and worse, it creates an advocate for keeping it.
The joint procedure, as Boothroyd, Dewhurst and Knight set it out, is: analyse the
existing or proposed assembly and compute the DFA index; challenge every part against
the three retention criteria (does it move relative to its neighbours, must it be of
a different material for a fundamental reason, must it be separable for assembly or
service?); eliminate or combine every part that fails all three; re-analyse; and only
then select the process and refine the geometry of the parts that remain, using
process-specific DFM rules — draft angles, uniform wall thickness, tool access,
avoidance of secondary operations.
The combination is more than additive, and it is worth being explicit about why.
Removing a part removes not only its own piece cost but its assembly operation, its
tooling, its inspection, its part number, its purchase order, its inventory and its
opportunity to be assembled incorrectly. It also removes an interface, and interfaces
are where tolerance stacks accumulate and where field failures concentrate. Then, on
the reduced part count, DFM has more to work with: the parts that remain are larger
and carry more function, which is exactly the condition under which a high-tooling,
low-variable-cost process such as die casting or injection moulding becomes viable.
DFA thus creates the conditions in which DFM's biggest wins become available.
Quantifying the joint effect. Given. A baseline product of 47
parts with a total manual assembly time of 396 s, of which a theoretical minimum
of 12 parts is justified by the retention criteria; a standard ideal handling and
insertion time of 3 s per part; a fully burdened assembly labour rate of
CAD 42 per hour; and an annual volume of 250 000 units.
Find. The DFA index before and after a redesign that reaches 23
parts and 198 s, and the resulting annual saving.
Compute the design efficiency before and after. The Boothroyd
DFA index is
$$\alpha=\frac{N_{\min}\,t_a}{t_{\text{total}}}$$
so
$$\begin{aligned} \alpha_{\text{before}}&=\frac{12\times3}{396}=0.0909 \\ \alpha_{\text{after}}&=\frac{12\times3}{198}=\boxed{0.1818} \end{aligned}$$
The efficiency doubles, from 9.1 % to 18.2 % — still low in absolute
terms, which is normal, since the index is a comparative instrument rather than a
score to be maximised.
Convert to money. Assembly labour per unit falls from
$396/3600\times42=\text{CAD }4.62$ to $198/3600\times42=\text{CAD }2.31$, a saving of
CAD 2.31 per unit, or
$$\Delta C = 2.31\times250\,000=\boxed{\text{CAD }577\,500\ \text{per year}}$$
in direct assembly labour alone, before counting the 24 part numbers removed from
purchasing, inventory and inspection.
Show the factory-level step change. With two shifts of
7.5 hours the available time is 54 000 s per day against a demand of
1 000 units, so the takt time is
$$\begin{aligned} \tau&=\frac{54\,000}{1\,000}=54\ \text{s} \\ \text{stations}&=\left\lceil\frac{t_{\text{total}}}{\tau}\right\rceil \end{aligned}$$
giving $\lceil396/54\rceil=8$ stations before and $\lceil198/54\rceil=4$ after. The
line halves, which releases floor space, four sets of fixtures and four operators
per shift — a saving that does not appear in the per-unit labour figure at
all.
Note the yield benefit nobody claimed. If each station passes
99.5 % of units, rolled throughput yield is $0.995^{n}$, so halving the station
count raises end-to-end yield from $0.995^{8}=0.9607$ to $0.995^{4}=0.9802$, a gain
of 1.95 percentage points obtained purely by removing opportunities
to make a mistake. The DFA index never claimed this, and on a 250 000-unit
programme it is worth more than the labour saving.
Figure 6.1 — Unit-cost curves c(n) = T/n + u for the fabricated bracket assembly and its single die-cast replacement. Both curves decay towards their variable cost, so the decision is entirely a question of where the programme volume sits relative to the crossing.
Part B — Three improvements that satisfy both objectives.
Each of the three below reduces assembly effort and reduces the cost of
making the parts, which is the test the question sets.
Consolidate six sheet-metal brackets and fourteen fasteners into one
die-cast structural bracket. On the assembly side, twenty parts and their
twenty handling and insertion operations become one. On the manufacturing side, the
question is whether the tooling is justified. Given. The fabricated
route costs CAD 6 000 in tooling and CAD 8.40 per unit; the die-cast
route costs CAD 78 000 in tooling and CAD 3.15 per unit.
Find. The volume above which die casting is cheaper. With
$c(n)=T/n+u$, the two routes cross where
$$n^{*}=\frac{T_2-T_1}{u_1-u_2}=\frac{78\,000-6\,000}{8.40-3.15}
=\boxed{13\,714\ \text{units}}$$
At the programme volume of 250 000 units per year the die casting costs
CAD 3.46 against CAD 8.42, so the consolidation saves CAD 4.96 per
unit on the parts as well as removing nineteen assembly operations.
Figure 6.1 shows the crossing; note that the decision is unambiguous only
because the programme volume is eighteen times the break-even, and a
40 000-unit programme would need a much more careful answer.
Replace threaded fasteners with integral snap fits and self-locating
features. For assembly, a snap fit is inserted in one motion with no
separate part, no torque control, no thread-locking compound and no risk of a missing
or cross-threaded screw. For manufacture, the snap feature is formed in the same
moulding or casting operation as the wall it belongs to and costs essentially
nothing, whereas each threaded boss requires a drilled and tapped hole or an
insert. Adding a chamfered lead-in and an asymmetric locating boss at the same time
makes the part self-locating and self-aligning, which removes the fixture the station
would otherwise need — a DFM saving obtained through a DFA feature.
Make the assembly one-directional, layered and mistake-proof about a
single base part. Design so that every part is added from above onto a
stable base, so that no part can be fitted the wrong way round (asymmetric locating
features, or fully symmetric ones where orientation genuinely does not matter), and
so that no part must be held while another is fitted. On the assembly side this
removes re-orientation, holding fixtures and the entire class of orientation errors.
On the manufacturing side, one-directional assembly implies one-directional access,
which is precisely the geometry that allows single-parting-line tooling with no side
actions in the moulds and castings, and single-setup machining on the machined
parts — the single largest lever on piece cost in both processes.
Part C — A strategy for consistently achieving both in a facility
that designs and manufactures its own products. The vertically-integrated
case is the favourable one, because the firm keeps the savings it creates and can
see the consequences of its own design decisions on its own floor. The strategy has
six elements.
Make manufacturing engineering a member of the design team from the
concept phase, not a reviewer of finished drawings. The person who will own
the process must be able to influence the architecture while the architecture is
still soft. In an integrated facility this costs nothing but organisational will,
and it is the single highest-return element of the strategy.
Set numerical DFMA targets in the product specification and gate against
them. A required DFA index, a maximum part count, a maximum assembly time
and a should-cost per unit, entered in the same specification as the functional
requirements and reviewed at each gate. Targets that are not in the specification are
aspirations, and aspirations lose to schedule pressure every time.
Capture the factory's actual capability in a living design-rule set.
Minimum wall thickness, achievable tolerance by process and feature size,
standard hole sizes, available press tonnages and bed sizes, preferred fasteners and
standard tooling — published as a design manual and, better, embedded in the
CAD system as checkable rules. This is the mechanism by which one plant's hard-won
knowledge stops being one experienced engineer's memory.
Aggressively standardise parts and processes across the product
range. A managed preferred-parts library, a small approved fastener set and
common platforms across models raise the volume on each remaining part number, which
moves every part rightwards along its own $c(n)=T/n+u$ curve, and reduce the tooling
and changeover burden on the floor. This is the element that most often falls to
individual designers' preference and most needs central enforcement.
Close the feedback loop from the floor to the design office with
data. Track assembly times by station, first-pass yield, rework and scrap by
cause, and warranty returns by part, and report them back to the design team against
the design decisions that produced them. In a firm that both designs and
manufactures, this loop is a structural advantage that a firm outsourcing its
manufacture simply cannot have — and it is astonishing how often it is left
unbuilt.
Institutionalise the method, and measure whether it is working.
Train designers in DFMA analysis and give them the software; require a
documented DFMA study, with a before-and-after index, as a mandatory gate deliverable;
run structured cross-functional workshops on new assemblies; and track the portfolio
DFA index and part count over time as a management metric. Recognise and reward part
elimination explicitly, because the natural incentives run the other way —
adding a part solves an engineer's immediate problem, while removing one is somebody
else's saving.