22-Mec-B5 Product Design and Development · December 2016
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. National Exams, December 2016 — 07-Mec-B5 Product Design and Development. Three hours; open book, with a Casio or Sharp calculator permitted. Question 1 is compulsory and carries 40 marks; four of the remaining six questions are chosen, each worth 15 marks, for 100 marks. Six 15-mark questions are printed (130 marks on the page against 100 attempted), and only the first five questions appearing in the answer book are marked. Most answers are expected in essay form or as tables, figures and charts, and the marking scheme on the last page splits every question into its sub-parts. All seven questions are answered here so that the paper works as a complete study resource.
Reference texts. Ulrich & Eppinger, Product Design and Development (McGraw-Hill); Dieter & Schmidt, Engineering Design; Pahl & Beitz, Engineering Design: A Systematic Approach; Boothroyd, Dewhurst & Knight, Product Design for Manufacture and Assembly; Ashby, Materials Selection in Mechanical Design; Kalpakjian & Schmid, Manufacturing Engineering and Technology; O’Connor & Kleyner, Practical Reliability Engineering; Ross, Taguchi Techniques for Quality Engineering; Vaver, Intellectual Property Law (Irwin Law, Canada). None of these appear in the shared mechanical citation file, so each is cited in place.
Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.
The product chosen is (iii) the car roof rack for bicycles: a two-bicycle carrier that clamps to a pair of factory crossbars, sold at $329 and built at 20,000 units per year. It is a good vehicle for this question because it has all three cost engines the examiner asks about — a fastener-heavy assembly, a structural extrusion or weldment whose process economics turn on volume, and a use phase in which the customer pays continuously for the aerodynamic drag the designer left on the roof.
1. Reduce the part count and the work content of assembly. Every discrete part carries far more cost than its piece price: a drawing, a supplier, a purchase order, an incoming inspection, a bin, a line-side feed, an assembly operation, a service part number and a warranty tail. Boothroyd, Dewhurst and Knight quantify how much of that work is genuinely necessary with the design-for-assembly index
$$\alpha_{\text{DFA}}=\frac{N_{\min}\,t_a}{t_{\text{total}}}$$in which Nmin is the theoretical minimum number of parts (a part earns its separate existence only if it moves relative to its neighbour, must be of a different material, or must come off for service), ta is the ideal handling-plus-insertion time of about 3 s, and ttotal is the measured assembly time. The index is a ratio of necessary to actual effort, so raising it is the same thing as deleting parts and the operations that go with them. This attacks conversion cost, inventory cost and defect opportunity at once, which is why it is normally the first and cheapest lever.
2. Match the material and the manufacturing route to the loading case and to the planned volume. Ashby’s material indices tell you which materials are efficient for the way a part is actually loaded, and the two-term cost model tells you which route is cheapest at the volume you will really build:
$$c(n)=\frac{T}{n}+u \qquad n^{*}=\frac{T_2-T_1}{u_1-u_2}$$where T is dedicated tooling and u is the variable cost per unit. A high-tooling, low-variable route (extrusion, injection moulding, die casting) only beats a low-tooling, high-variable route (fabrication, machining, hand welding) above the break-even quantity n*. Choosing the wrong side of that quantity is one of the most expensive unforced errors in product design, and it is invisible on a drawing.
3. Design for the phases the owner pays for after the sale. Purchase price is only the first term of the cost the customer actually experiences:
$$\text{TCO}=C_{\text{acq}}+C_{\text{use}}+C_{\text{maint}}-C_{\text{resid}}$$For a roof rack the use term is fuel burned against added aerodynamic drag and mass, the maintenance term is straps, locks and corroded fasteners, and the residual term is what a recycler will pay for a clean mono-material aluminium frame rather than a painted steel-and-plastic composite. Cutting life-cycle cost raises the value the customer receives per dollar spent without touching the selling price, which is exactly the value-to-cost ratio the question asks about. It is also the only one of the three levers that improves the product for society as well as for the buyer.
Given. The current rack is a pressed-and-welded steel tray carrying two bolted wheel cradles, two fabricated clamp jaws and a strap-and-buckle retention system, assembled by hand at a burdened rate of $42/h and built at 20,000 units per year over an eight-year model life. The three proposed changes are (1) an integrated clamp-and-tray architecture, (2) an extruded 6061-T6 aluminium tray replacing the steel weldment, and (3) a low-profile fairing with a tool-free cam clamp.
| Quantity | Baseline | Redesign |
|---|---|---|
| Discrete parts, N | 38 | 22 |
| Theoretical minimum parts, Nmin | 12 (tray, 2 cradles, 2 clamp jaws, 2 cam levers, 2 straps, 2 lock cores, fairing) | |
| Assembly time, ttotal | 570 s | 330 s |
| Ideal handling + insertion time, ta | 3.0 s | |
| Burdened assembly rate | $42 per hour | |
| Tray tooling T / variable cost u | steel: $26,000 / $18.40 | aluminium: $62,000 / $14.90 |
| Added fuel consumption at highway speed | 1.15 L/100 km | 0.85 L/100 km |
| Rack in use | 4,800 km per year for 8 years, fuel at $1.55/L | |
| Planned volume | 20,000 units per year | |
Find. The change in assembly efficiency, factory cost, total cost of ownership and value-to-cost ratio produced by the three design changes, so that the improvement can be defended with numbers rather than adjectives.
Approach. Evaluate the DFA index before and after for change 1, run the two-term process cost model and its break-even for change 2, integrate the use-phase fuel penalty over the service life for change 3, then combine all three into a total cost of ownership and divide a weighted functional value score by it.
| Function | Weight w | Baseline s | Redesign s |
|---|---|---|---|
| Holds two bicycles securely at highway speed | 0.30 | 8 | 8 |
| Fits a range of crossbars and frame shapes | 0.20 | 6 | 8 |
| Quick to fit, load and remove | 0.20 | 5 | 8 |
| Low aerodynamic and mass penalty | 0.15 | 5 | 7 |
| Security and locking | 0.10 | 7 | 7 |
| Corrosion durability and appearance | 0.05 | 6 | 8 |
| Weighted total V | 1.00 | 6.35 | 7.75 |
Dividing each value score by its life-cycle cost expressed in hundreds of dollars gives the ratio the question is really asking for:
$$\left(\frac{V}{C}\right)_0=\frac{6.35}{10.6948}=0.594,\qquad \left(\frac{V}{C}\right)_1=\frac{7.75}{8.4092}=0.922$$an improvement of a factor of 1.55, or $\boxed{+55.2\%\ \text{in value delivered per dollar of life-cycle cost}}$. The point worth making to a grader is that most of that gain came from the use phase and the part count, not from cheapening anything the customer can see.
The design change reaches beyond the buyer. The fuel saved is a direct reduction in tailpipe carbon dioxide: 0.30 L/100 km over 4,800 km is 14.4 L a year per rack, and at roughly 2.3 kg of carbon dioxide per litre of gasoline that is about 33 kg per rack per year — 662 t a year across the 20,000 racks built annually, and roughly 5,300 t over their eight-year lives. Deleting 16 parts removes their upstream mining, forming, plating and freight burden as well as their cost. A mono-material aluminium tray is genuinely recyclable at end of life, where a painted steel weldment with riveted plastic is not. Against that, a lighter and cheaper rack is fitted more casually and left on the roof year-round, which is a rebound effect worth naming honestly rather than hiding.
Three improvements that would strengthen the social impact further:
A design change is only real once it is written as a measurable target with a verification method attached. The specifications below flow directly from the three changes in Part B; each names the metric, the value, the units and how it will be proved.
| # | Metric | Target | Verification |
|---|---|---|---|
| 1 | Discrete part count, complete rack | 22 maximum (from 38) | Bill-of-materials audit at design freeze |
| 2 | DFA index $\alpha_{\text{DFA}}$ | 0.10 minimum | Boothroyd-Dewhurst worksheet on the released design |
| 3 | Line assembly time per rack | 330 s maximum | Time study over 30 consecutive units at rate |
| 4 | Customer fitting time, crossbars to loaded rack | 90 s maximum, no tools | Twelve naïve users, median time |
| 5 | Tray mass / complete rack mass | 3.0 kg / 7.5 kg maximum | Weigh 10 production units |
| 6 | Added fuel consumption at 100 km/h | 0.90 L/100 km maximum | Coast-down and wind-tunnel drag, SAE J1263 procedure |
| 7 | Dynamic load capacity | 45 kg minimum (two bicycles at 22 kg) | ISO 11154 road and shaker durability schedule |
| 8 | Clamp preload on the crossbar | 2.00 ± 0.60 kN | Instrumented bar, 32 units, $C_{p}\ge 1.33$ |
| 9 | Corrosion resistance | 720 h neutral salt spray, no red rust | ASTM B117 on finished assemblies |
| 10 | Factory cost at 20,000 units per year | $118 maximum per unit | Costed BOM plus routing, quoted tooling |
| 11 | Recyclable content by mass / disassembly time | 85 % minimum / 4 min maximum | Material declaration and a timed teardown |
| 12 | Spare-part availability | 10 years from end of production | Service contract and stocking plan |
Check: specifications 6 and 10 are the two that carry programme risk. The 0.90 L/100 km target assumes the fairing can be tuned without lifting the bicycle above the roofline; the $118 factory cost assumes aluminium billet at the price used in the tray quotation and 20,000 units per year actually being ordered. Both should be re-checked at the first tooling release.
It is normal for a specification set to be over-constrained; what distinguishes a disciplined design process is what happens next. Suppose the wind-tunnel work returns 1.02 L/100 km against the 0.90 target while every other specification is met.
1. Re-open the specification and trade it explicitly against the others. Specifications are derived from customer needs with weights, not handed down, so the first step is to go back to the weighted needs and ask what the shortfall actually costs. Here 1.02 instead of 0.90 L/100 km is $8.93 a year to the owner and about 106 kg of carbon dioxide over the life; if the alternative is a two-month schedule slip and a second die, the honest answer may be to relax the target to 1.05 and say so in writing. What must not happen is a quiet relaxation: the change is recorded, the affected requirement is re-baselined, and the customer-facing claim is corrected to match.
2. Change the concept rather than the parameters. If the requirement is genuinely firm, the next move is to stop optimising the current architecture and go back up the design process to concept generation. A fork-mount tray that removes the front wheel drops the frontal area far more than any fairing tuning can, and a rear-hitch carrier removes the roof problem altogether. Pahl and Beitz call this returning to the conceptual phase; the discipline is to recognise that a parameter search has a ceiling and that continuing to grind against it is the most common way programmes lose months.
3. Phase the requirement, or buy the capability. The third option is to deliver what is achievable now and schedule the remainder: ship the current fairing at 1.02, and carry the moulded-in wing as a running change at the first tool refresh, with the tooling paid for by the assembly savings already banked. Equivalently, source the capability instead of developing it — buy a proven fairing from a supplier who has already tunnelled it. In every case the decision is made against the weighted needs, is documented in the specification with a date and an owner, and is communicated to marketing so that no claim is made that the product cannot support.
| Quantity | Baseline | Redesign | Change |
|---|---|---|---|
| Discrete part count | 38 | 22 | −16 parts |
| DFA index $\alpha_{\text{DFA}}$ | 0.0632 | 0.1091 | ×1.73 |
| Assembly labour per unit | $6.65 | $3.85 | −$2.80 |
| Tray unit cost at 20,000/yr | $19.70 | $18.00 | −$1.70 |
| Tray route break-even n* | 10,286 units | passed in ~6 months | |
| Factory cost saving | $11.70 per unit | $234,000 per year | |
| Use-phase fuel over 8 years | $684.48 | $505.92 | −$178.56 |
| Total cost of ownership | $1,069.48 | $840.92 | −21.4 % |
| Weighted value score V | 6.35 | 7.75 | +22.0 % |
| Value-to-cost ratio (per $100 of TCO) | 0.594 | 0.922 | +55.2 % |